Glass compositions, fiberizable glass compositions, and glass fibers made therefrom

FIELD OF THE INVENTION

The present invention relates to glass compositions and, in particular, to glass compositions for forming fibers.

BACKGROUND OF THE INVENTION

Glass fibers have been used to reinforce various polymeric resins for many years. Some commonly used glass compositions for use in reinforcement applications include the “E-glass”, “R-glass”, and “D-glass” families of compositions. “S-glass” is another commonly used family of glass compositions that includes, for example, glass fibers commercially available from AGY (Aiken, S.C.) under the trade name “S-2 Glass.”

In reinforcement and other applications, certain mechanical properties of glass fibers or of composites reinforced with glass fibers can be important. However, in many instances, the manufacture of glass fibers having improved mechanical properties (e.g., higher strength, higher modulus, etc.) can result in higher costs due, for example, due to increased batch material costs, increased manufacturing costs, or other factors. For example, the aforementioned “S-2 Glass” has improved mechanical properties as compared to conventional E-glass but costs significantly more as well as a result of substantially higher temperature and energy demands for batch-to-glass conversion, melt fining, and fiber drawing. Fiber glass manufacturers continue to seek glass compositions that can be used to form glass fibers having desirable mechanical properties in a commercial manufacturing environment.

SUMMARY

Various embodiments of the present invention provide glass compositions, fiberizable glass compositions, and glass fibers formed from such compositions, as well as fiber glass strands, yarns, fabrics, and composites comprising such glass fibers adapted for use in various applications.

In one embodiment, a glass composition suitable for fiber forming comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. In some embodiments, MnO_xcomprises MnO₂in an amount of about 2 weight percent or greater. In some embodiments, RE₂O₃comprises at least one of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. RE₂O₃is present in an amount of at least about 1 weight percent in some embodiments. In some embodiments, the composition further comprises TiO₂in an amount greater than about 3 weight percent. In some embodiments, the composition further comprises less than about 1.5 weight percent Na₂O+K₂O+Li₂O.

In another embodiment, a glass composition suitable for fiber forming comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, BaO is present in an amount greater than about 2 weight percent. In some embodiments, SrO is present in an amount greater than about 2 weight percent. In some embodiments, ZnO is present in an amount greater than about 2 weight percent. In some embodiments, RE₂O₃comprises at least one of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. RE₂O₃is present in an amount of at least about 1 weight percent in some embodiments. In some embodiments, the composition further comprises less than about 1.5 weight percent Na₂O+K₂O+Li₂O.

In another embodiment, a glass composition suitable for fiber forming comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In some embodiments, the additional feature comprises La₂O₃in an amount of about 3 weight percent or greater. In some embodiments, MgO is present in an amount greater than about 6 weight percent, and the additional feature comprises CaO in an amount less than about 1.5 weight percent. In some embodiments, the additional feature comprises the SiO₂/Al₂O₃ratio in an amount greater than about 4.2. In some embodiments, RE₂O₃comprises at least one of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. RE₂O₃is present in an amount of at least about 1 weight percent in some embodiments. In some embodiments, the composition further comprises less than about 1.5 weight percent Na₂O+K₂O+Li₂O.

Some embodiments of the present invention relate to fiber glass strands. A number of fiberizable glass compositions are disclosed herein as part of the present invention, and it should be understand that various embodiments of the present invention can comprise glass fibers, fiber glass strands, yarns, and other products incorporating glass fibers formed from such compositions.

Some embodiments of the present invention relate to yarns formed from at least one fiber glass strand formed from a glass composition described herein. Some embodiments of the present invention relate to fabrics incorporating at least one fiber glass strand formed from a glass composition described herein. In some embodiments, a fill yarn used in the fabric can comprise the at least one fiber glass strand. A warp yarn, in some embodiments, can comprise the at least one fiber glass strand. In some embodiments, fiber glass strands can be used in both fill yarns and warp yarns used to form fabrics according to the present invention. In some embodiments, fabrics of the present invention can comprise a plain weave fabric, a twill fabric, a crowfoot fabric, a satin weave fabric, a stitch bonded fabric, or a 3D woven fabric.

Some embodiments of the present invention relate to composites comprising a polymeric resin and glass fibers formed from one of the various glass compositions described herein. The glass fibers can be from a fiber glass strand according to some embodiments of the present invention. In some embodiments, the glass fibers can be incorporated into a fabric, such as a woven fabric. For example, the glass fibers can be in a fill yarn and/or a warp yarn that are woven to form a fabric. In embodiments where the composite comprises a fabric, the fabric can comprise a plain weave fabric, a twill fabric, a crowfoot fabric, a satin weave fabric, a stitch bonded fabric, or a 3D woven fabric.

The glass fibers can be incorporated into the composite in other forms as well as discussed in more detail below.

With regard to polymeric resins, composites of the present invention can comprise one or more of a variety of polymeric resins. In some embodiments, the polymeric resin comprises at least one of polyethylene, polypropylene, polyamide, polyimide, polybutylene terephthalate, polycarbonate, thermoplastic polyurethane, phenolic, polyester, vinyl ester, polydicyclopentadiene, polyphenylene sulfide, polyether ether ketone, cyanate esters, bis-maleimides, and thermoset polyurethane resins. The polymeric resin can comprise an epoxy resin in some embodiments.

Composites of the present invention can be in a variety of forms and can be used in a variety of applications. Some examples of potential uses of composites according to some embodiments of the present invention include, without limitation, wind energy (e.g., windmill blades), automotive applications, safety/security applications (e.g., ballistics armor), aerospace or aviation applications (e.g., interior floors of planes), high pressure vessels or tanks, missile casings, electronics, and others.

These and other embodiments of the present invention are described in greater detail in the Detailed Description that follows.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a chart showing Young's modulus values relative to the amount of rare earth oxides (RE₂O₃) in various glass compositions.

FIG. 2 is a chart showing pristine fiber tensile strength values relative to the amount of rare earth oxides (RE₂O₃) in various glass compositions.

FIG. 3 is a chart showing softening and glass transition temperatures relative to the amount of rare earth oxides (RE₂O₃) in various glass compositions.

FIG. 4 is a chart showing linear coefficient of thermal expansion relative to the amount of scandium oxide (Sc₂O₃) in various glass compositions.

DETAILED DESCRIPTION

Unless indicated to the contrary, the numerical parameters set forth in the following specification are approximations that can vary depending upon the desired properties sought to be obtained by the present invention. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques.

Notwithstanding that the numerical ranges and parameters setting forth the broad scope of the invention are approximations, the numerical values set forth in the specific examples are reported as precisely as possible. Any numerical value, however, inherently contains certain errors necessarily resulting from the standard deviation found in their respective testing measurements. Moreover, all ranges disclosed herein are to be understood to encompass any and all subranges subsumed therein. For example, a stated range of “1 to 10” should be considered to include any and all subranges between (and inclusive of) the minimum value of 1 and the maximum value of 10; that is, all subranges beginning with a minimum value of 1 or more, e.g. 1 to 6.1, and ending with a maximum value of 10 or less, e.g., 5.5 to 10. Additionally, any reference referred to as being “incorporated herein” is to be understood as being incorporated in its entirety.

It is further noted that, as used in this specification, the singular forms “a,” “an,” and “the” include plural referents unless expressly and unequivocally limited to one referent.

The present invention relates generally to glass compositions. In one aspect, the present invention provides glass fibers formed from glass compositions described herein. In some embodiments, glass fibers of the present invention can have improved mechanical properties, such as, for example, Young's modulus and pristine strength, as compared to conventional E-glass fibers.

Glass compositions of the present invention comprise rare earth oxides in addition to components typically found in glass compositions such as SiO₂, Al₂O₃, CaO, MgO, and others. Such glass compositions can be fiberizable and thus can be used to make fiber glass in various embodiments. As used herein, the term “rare earth oxides” is abbreviated as “RE₂O₃” and, as understood to those of skill in the art, refers to oxides incorporating a rare earth metal and includes oxides of scandium (Sc₂O₃), yttrium (Y₂O₃), and the lanthanide elements (lanthanum (La₂O₃), cerium (Ce₂O₃and CeO₂), praseodymium (Pr₂O₃), neodymium (Nd₂O₃), promethium (Pm₂O₃), samarium (Sm₂O₃), europium (Eu₂O₃and EuO), gadolinium (Gd₂O₃), terbium (Tb₂O₃), dysprosium (Dy₂O₃), holmium (Ho₂O₃), erbium (Er₂O₃), thulium (Tm₂O₃), ytterbium (Yb₂O₃), and lutetium (Lu₂O₃)). The rare earth oxides are included in the glass compositions of the present invention in amounts that exceed those wherein the rare earth oxide is present only as a tramp material or impurity in a batch material included with a glass batch to provide another component. The glass compositions, in some embodiments, can comprise a combination of rare earth oxides (e.g., one or more of various rare earth oxides).

In some embodiments, one or more RE₂O₃can be present in a glass composition in an amount of about 0.05 weight percent or greater. The one or more RE₂O₃can be present in an amount of about 0.5 weight percent or greater in some embodiments. The one or more RE₂O₃can be present in an amount of about 1 weight percent or greater in some embodiments. The one or more RE₂O₃can be present in an amount of about 2 weight percent or greater in some embodiments. The one or more RE₂O₃can be present in an amount of about 3 weight percent or greater in some embodiments. The one or more RE₂O₃can be present in an amount of about 4 weight percent or greater in some embodiments. The one or more RE₂O₃can be present in an amount of about 5 weight percent or greater in some embodiments. In some embodiments, the one or more RE₂O₃can be present in an amount up to about 10 weight percent although greater amounts can be used in other embodiments. The one or more RE₂O₃, in some embodiments, can be present in an amount up to about 12 weight percent. The one or more RE₂O₃can be present in an amount up to about 15 weight percent in some embodiments. The one or more RE₂O₃, in some embodiments, can be present in an amount from about 0.05 to about 15 weight percent. The one or more RE₂O₃can be present in an amount from about 0.5 to about 15 weight percent in some embodiments. In some embodiments, the one or more RE₂O₃can be present in an amount from about 2.0 to about 15 weight percent. The one or more RE₂O₃, in some embodiments, can be present in an amount from about 3.0 to about 15 weight percent. In some embodiments, the one or more RE₂O₃can be present in an amount from about 4.0 to about 15 weight percent. The one or more RE₂O₃can be present in an amount from about 5.0 to about 15 weight percent in some embodiments.

The amount of RE₂O₃used in some embodiments can depend on the particular RE₂O₃used, whether other types of RE₂O₃are used in the composition, melt properties of the composition, and desired properties of the glass fibers to be formed from the composition, and others.

In some embodiments, RE₂O₃comprises at least one of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. In some embodiments, RE₂O₃is selected from the group consisting of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. In some embodiments, RE₂O₃is selected from the group consisting of La₂O₃and Y₂O₃.

In some embodiments, RE₂O₃used in glass compositions of the present invention can comprise La₂O₃in an amount of about 0.05 weight percent or greater. In some embodiments, RE₂O₃can comprise La₂O₃in an amount of about 0.5 weight percent or greater. In some embodiments, RE₂O₃can comprise La₂O₃in an amount greater than about 2 weight percent. In some embodiments, RE₂O₃can comprise La₂O₃in an amount of about 3 weight percent or greater. In some embodiments, RE₂O₃can comprise La₂O₃in an amount from greater than about 2 weight percent to about 21 weight percent. In some embodiments, RE₂O₃can comprise La₂O₃in an amount from greater than about 2 weight percent to about 10 weight percent. In some embodiments, RE₂O₃can comprise La₂O₃in an amount from greater than about 2 weight percent to about 6 weight percent. In some embodiments, RE₂O₃can comprise La₂O₃in an amount from about 3 weight percent to about 10 weight percent. In some embodiments, RE₂O₃can comprise La₂O₃in an amount from about 3 weight percent to about 6 weight percent. In some embodiments, the glass composition can be substantially free of La₂O₃. As set forth above and in the Examples below, other amounts of La₂O₃can also be included in glass compositions according to some embodiments. In some embodiments, the inclusion of La₂O₃in glass compositions is believed to have a desirable impact on glass softening temperature and glass transition temperatures as well as on tensile strength, elongation, coefficient of thermal expansion, and other properties of glass fibers formed from the compositions.

In some embodiments, the RE₂O₃used in glass compositions of the present invention can comprise Y₂O₃in an amount of about 0.05 weight percent or greater. In some embodiments, RE₂O₃can comprise Y₂O₃in an amount of about 0.5 weight percent or greater. In some embodiments, Y₂O₃can be present in an amount from about 0.05 to about 15 weight percent. In some embodiments, Y₂O₃can be present in an amount up to about 6 weight percent. In some embodiments, Y₂O₃can be present in an amount from about 3 to about 5.5 weight percent. In some embodiments, the Y₂O₃content can be about 2 weight percent or less. In some embodiments, the glass composition can be substantially free of Y₂O₃. As set forth above and in the Examples below, other amounts of Y₂O₃can also be included in glass compositions according to some embodiments. In some embodiments, the inclusion of Y₂O₃in glass compositions is believed to have a desirable impact on glass softening temperature and glass transition temperature as well as on modulus, tensile strength, elongation, coefficient of thermal expansion, and other properties of glass fibers formed from the compositions.

In some embodiments, the RE₂O₃used in glass compositions of the present invention can comprise Sc₂O₃in an amount of about 0.05 weight percent or greater. In some embodiments, RE₂O₃can comprise Sc₂O₃in an amount of about 0.5 weight percent or greater. In some embodiments, Sc₂O₃can be present in an amount from about 0.5 to about 4 weight percent. In some embodiments, the glass composition can be substantially free of Sc₂O₃. As set forth above and in the Examples below, other amounts of Sc₂O₃can also be included in glass compositions according to some embodiments. In some embodiments, while the inclusion of Sc₂O₃in glass compositions is believed to have a desirable impact on some properties of glass fibers formed from the compositions (e.g., glass softening temperature, glass transition temperature, coefficient of thermal expansion, etc.), the presence of Sc₂O₃has also been observed to raise the liquidus temperature of the compositions.

In some embodiments, the RE₂O₃used in glass compositions of the present invention can comprise Nd₂O₃in an amount of about 0.05 weight percent or greater. In some embodiments, RE₂O₃can comprise Sc₂O₃in an amount of about 0.5 weight percent or greater. In some embodiments, Nd₂O₃can be present in an amount from about 0.5 to about 15 weight percent. In some embodiments, the glass composition can be substantially free of Nd₂O₃. As set forth above and in the Examples below, other amounts of Nd₂O₃can also be included in glass compositions according to some embodiments. In some embodiments, the inclusion of Nd₂O₃in glass compositions is believed to have a desirable impact on glass softening temperature and glass transition temperature as well as on modulus, tensile strength, elongation, coefficient of thermal expansion, and other properties of glass fibers formed from the compositions.

Various combinations of RE₂O₃can be also used to achieve desirable properties (e.g., tensile strength, modulus, specific strength, specific modulus, etc.). For example, the selection of a particular RE₂O₃and its relative amount can impact the fiber density which can in turn impact specific strength (tensile strength divided by density) and specific modulus (modulus divided by density). Likewise, the selection of a particular RE₂O₃and its relative amount can impact melt properties of the glass compositions. For example, as noted above, the presence of Sc₂O₃in certain amounts can increase the liquidus temperature of a glass composition. Similarly, cerium oxide (Ce₂O₃and CeO₂) can act as an oxidizing and fining agent, such that in some embodiments, the amount of cerium oxide can be no more than 2 weight percent. In some embodiments, the glass composition can be substantially free of cerium oxide. Finally, the selection of a particular RE₂O₃and its relative amount can impact the cost of making the glass fibers due to its impact on melt properties and due its cost as a raw material as the cost of RE₂O₃varies substantially.

As noted above, glass compositions of the present invention and in particular, fiberizable glass compositions also include other components including SiO₂, Al₂O₃, CaO, MgO, and others.

In another embodiment, a glass composition suitable for fiber forming comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In some embodiments, La₂O₃is present in an amount of about 3 weight percent or greater. In some embodiments, CaO is present in an amount less than about 1.5 weight percent and MgO is present in an amount greater than about 6 weight percent. In some embodiments, the SiO₂/Al₂O₃ratio is greater than about 4.2. In some embodiments, RE₂O₃comprises at least one of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. RE₂O₃is present in an amount of at least about 1 weight percent in some embodiments. In some embodiments, the composition further comprises less than about 1.5 weight percent Na₂O+K₂O+Li₂O.

It should be understood that any component of a glass composition described as being present in amount from about 0 weight percent to another weight percent is not necessarily required in all embodiments. In other words, such components may be optional in some embodiments, depending of course on the amounts of other components included in the compositions. Likewise, in some embodiments, glass compositions can be substantially free of such components, meaning that any amount of the component present in the glass composition would result from the component being present as a trace impurity in a batch material. A component present as a trace impurity is not intentionally added to the glass composition. In other words, a trace impurity is present in a herein described glass composition by virtue of its presence as an impurity in a starting material added to the glass composition. Generally, a trace impurity is present in the glass composition in an amount no greater than about 0.1 weight percent, although some trace impurities may be present in the glass composition in an amount up to about 0.5 weight percent.

Some embodiments of the present invention can be characterized by the amount of SiO₂present in the glass compositions. SiO₂can be present in an amount from about 51 to about 70 weight percent in some embodiments. SiO₂can be present in an amount from about 51 to about 66 weight percent in some embodiments. The SiO₂content in some embodiments can be less than about 66 weight percent. SiO₂can be present in an amount from about 51 to about 65 weight percent, and from about 51 to about 63 weight percent in some embodiments. SiO₂can be present, in some embodiments, in an amount from about 54 to about 65 weight percent and from about 54 to about 63 weight percent. In some embodiments, SiO₂can be present in an amount from about 58 to about 66 weight percent. In some embodiments, SiO₂can be present in an amount from about 58 to about 64 weight percent. In some embodiments, SiO₂can be present in an amount from about 59 to about 65 weight percent. In some embodiments, SiO₂can be present in an amount from about 58 to about 70 weight percent. In some embodiments, SiO₂can be present in an amount from about 65 to about 70 weight percent. The glass compositions, in some embodiments, can comprise at least about 60 weight percent SiO₂.

Some embodiments of the present invention can be characterized by the amount of Al₂O₃present in the glass compositions. In some embodiments, glass compositions can comprise from about 12.5 to about 22 weight percent Al₂O₃. Al₂O₃can be present, in some embodiments, in an amount from about 12.5 to about 19 weight percent. Al₂O₃can be present in an amount from about 13 to about 22 weight percent in some embodiments. Al₂O₃can be present in an amount from about 14.5 to about 19 weight percent in some embodiments. In some embodiments, Al₂O₃can be present in an amount from about 15 to about 19 weight percent. In some embodiments, Al₂O₃can be present in an amount from about 15 to about 18 weight percent.

Some embodiments of the present invention can be characterized by the ratio of SiO₂content to Al₂O₃content (SiO₂/Al₂O₃). The SiO₂/Al₂O₃ratio can affect the Young's modulus of the glass compositions. In some embodiments, the SiO₂/Al₂O₃ratio is about 2 or greater. In some embodiments, the SiO₂/Al₂O₃ratio is about 3 or greater. In some embodiments, the SiO₂/Al₂O₃ratio is about 3.5 or greater. In some embodiments, the SiO₂/Al₂O₃ratio is about 3.8 or greater. In some embodiments, the SiO₂/Al₂O₃ratio is about 4 or greater. In some embodiments, the SiO₂/Al₂O₃ratio is about 4.2 or greater. In some embodiments, the SiO₂/Al₂O₃ratio is about 4.5 or greater.

Some embodiments of the present invention can be characterized by the amount of CaO present in the glass compositions. CaO can be present in an amount from about 0 to about 20 weight percent in some embodiments. CaO can be present, in some embodiments, in an amount from about 0 and to 16 weight percent. In some embodiments, the CaO content can be less than 10 weight percent. In some embodiments, the CaO content can be less than 8 weight percent. In some embodiments, the CaO content can be less than 2 weight percent. In some embodiments, the CaO content can be 1.5 weight percent or less. In some embodiments, the CaO content can be 1 weight percent or less. In some embodiments, CaO can be present in an amount from about 10 to about 20 weight percent. In some embodiments, CaO can be present in an amount from about 12 to about 20 weight percent. In some embodiments, CaO can be present in an amount from about 15 to about 20 weight percent. In some embodiments, CaO can be present in an amount from about 0.5 to about 15 weight percent. Glass compositions of the present invention, in some embodiments, can comprise from about 0.5 to about 14 weight percent. In some embodiments, CaO can be present in an amount from about 0.5 to about 10 weight percent. In some embodiments, CaO can be present in an amount from about 2 to about 8 weight percent. In some embodiments, the glass composition can be substantially free of CaO.

Some embodiments of the present invention can be characterized by the amount of MgO present in the glass compositions. MgO can be present in an amount from about 0 to about 12.5 weight percent in some embodiments. In some embodiments, glass compositions of the present invention comprise from about 0 to about 12 weight percent MgO. MgO can be present in an amount from about 0 to about 11 weight percent in some embodiments. MgO can be present in an amount from greater than about 0 to about 11 weight percent in some embodiments. MgO can be present in an amount from about 1 to about 11 weight percent in some embodiments. MgO can be present in an amount from greater than about 0 to about 9 weight percent in some embodiments. MgO can be present in an amount of about 6 weight percent or greater in some embodiments. MgO can be present in an amount of about 6.5 weight percent or greater in some embodiments. MgO can be present, in some embodiments, in an amount from about 6.5 to about 12.5 weight percent. MgO can be present, in some embodiments, in an amount from about 7 to about 12.5 weight percent. MgO can be present, in some embodiments, in an amount from about 6 to about 9 weight percent. In some embodiments, the glass composition can be substantially free of MgO.

Some embodiments of the present invention can be characterized by the ratio of MgO content to CaO content (MgO/CaO). The MgO/CaO ratio may affect the Young's modulus and the liquidus temperature of the glass composition. In some embodiments in which MgO and CaO are present, the MgO/CaO ratio may be less than about 1. In some embodiments, the MgO/CaO ratio can be less than about 0.8. In some embodiments, the MgO/CaO ratio can be less than about 0.6. In some embodiments, the MgO/CaO ratio can be greater than about 4. In some embodiments, the MgO/CaO ratio can be greater than about 4.5 In some embodiments, the MgO/CaO ratio can be greater than about 5. In some embodiments, the MgO/CaO ratio can be greater than about 10.

Some embodiments of the present invention can be characterized by the amount of BaO present in the glass compositions. In some embodiments, BaO can be present in an amount greater than 0 weight percent, 0.5 weight percent or greater, 1 weight percent or greater, 2 weight percent or greater, or 3 weight percent or greater. BaO can be present in an amount from about 0 to about 4 weight percent in some embodiments. In some embodiments, glass compositions of the present invention comprise from about 0 to about 3.5 weight percent BaO. BaO can be present in an amount from greater than about 0 to about 4 weight percent in some embodiments. BaO can be present in an amount from about 0.5 to about 4 weight percent in some embodiments. BaO can be present in an amount from about 1 to about 4 weight percent in some embodiments. BaO can be present in an amount from about 2 to about 4 weight percent in some embodiments. BaO can be present in an amount from about 2.5 to about 4 weight percent in some embodiments. BaO can be present in an amount from about 3 to about 4 weight percent in some embodiments. In some embodiments, the glass composition can be substantially free of BaO.

Some embodiments of the present invention can be characterized by the amount of SrO present in the glass compositions. In some embodiments, SrO can be present in an amount greater than 0 weight percent, 0.5 weight percent or greater, 1 weight percent or greater, 2 weight percent or greater, or 3 weight percent or greater. SrO can be present in an amount from about 0 to about 4 weight percent in some embodiments. In some embodiments, glass compositions of the present invention comprise from about 0 to about 3.5 weight percent SrO. SrO can be present in an amount from greater than about 0 to about 4 weight percent in some embodiments. SrO can be present in an amount from about 0.5 to about 4 weight percent in some embodiments. SrO can be present in an amount from about 1 to about 4 weight percent in some embodiments. SrO can be present in an amount from about 2 to about 4 weight percent in some embodiments. SrO can be present in an amount from about 2.5 to about 4 weight percent in some embodiments. In some embodiments, the glass composition can be substantially free of SrO.

Some embodiments of the present invention can be characterized by the total amount of CaO, MgO, BaO, and SrO content (CaO+MgO+BaO+SrO). The CaO+MgO+BaO+SrO content can be 23 weight percent or less in some embodiments. The CaO+MgO+BaO+SrO content can be from about 1 to about 23 weight percent. The CaO+MgO+BaO+SrO content can be from about 8 to about 23 weight percent. The CaO+MgO+BaO+SrO content can be from about 9 to about 23 weight percent. The CaO+MgO+BaO+SrO content can be from about 9 to about 20 weight percent. The CaO+MgO+BaO+SrO content can be from about 9 to about 17 weight percent. The CaO+MgO+BaO+SrO content can be from about 0 to about 8 weight percent. The CaO+MgO+BaO+SrO content can be from about 1 to about 8 weight percent. The CaO+MgO+BaO+SrO content can be from about 1 to about 6 weight percent. The CaO+MgO+BaO+SrO content can be from about 1 to about 3 weight percent.

Some embodiments of the present invention can be characterized by the amount of ZnO present in the glass compositions. In some embodiments, ZrO can be present in an amount greater than 0 weight percent, 0.5 weight percent or greater, 1 weight percent or greater, 2 weight percent or greater, or 3 weight percent or greater. ZnO can be present in an amount from about 0 to about 5.5 weight percent in some embodiments. In some embodiments, glass compositions of the present invention comprise from about 0 to about 5 weight percent ZnO. ZnO can be present in an amount from greater than about 0 to about 5.5 weight percent in some embodiments. ZnO can be present in an amount from greater than about 0 to about 5 weight percent in some embodiments. ZnO can be present in an amount from about 1 to about 5 weight percent in some embodiments. ZnO can be present in an amount from about 1.5 to about 5 weight percent in some embodiments. ZnO can be present in an amount from about 2 to about 5 weight percent in some embodiments. ZnO can be present in an amount from about 2.5 to about 5 weight percent in some embodiments. ZnO can be present in an amount from about 4 to about 5 weight percent in some embodiments. In some embodiments, the glass composition can be substantially free of ZnO.

Some embodiments of the present invention can be characterized by the total amount of BaO, SrO, and ZnO content (BaO+SrO+ZnO). The BaO+SrO+ZnO content can be greater than 1 weight percent in some embodiments. The BaO+SrO+ZnO content can be 2 weight percent or greater in some embodiments. The BaO+SrO+ZnO content can be 2.5 weight percent or greater in some embodiments. The BaO+SrO+ZnO content can be 3 weight percent or greater in some embodiments. The BaO+SrO+ZnO content can be up to 10 weight percent in some embodiments. The BaO+SrO+ZnO content can be up to 6 weight percent in some embodiments. The BaO+SrO+ZnO content can be up to 5.5 weight percent in some embodiments. The BaO+SrO+ZnO content can be up to 5 weight percent in some embodiments. The BaO+SrO+ZnO content can be from 2 to 6 weight percent in some embodiments. The BaO+SrO+ZnO content can be from 2.5 to 5 weight percent in some embodiments. In some embodiments, the glass composition can be substantially free of any one of BaO, SrO, and ZnO. In some embodiments, the glass composition can be substantially free of any combination of BaO, SrO, and ZnO, including being substantially free of all of BaO, SrO, and ZnO.

Some embodiments of the present invention can be characterized by the amount of Na₂O present in the glass compositions. In some embodiments, glass compositions of the present invention can comprise from about 0 to about 2.5 weight percent Na₂O. Na₂O can be present, in some embodiments, in an amount from about 0 to about 1.5 weight percent. Na₂O can be present, in some embodiments, in an amount from about 0 to about 1 weight percent. In some embodiments, Na₂O can be present in an amount up to about 1.5 weight percent. Na₂O can be present, in some embodiments, in an amount up to about 1.0 weight percent. Na₂O can be present, in some embodiments, in an amount up to about 0.5 weight percent. Na₂O can be present, in some embodiments, in an amount up to about 0.25 weight percent. Na₂O can be present, in some embodiments, in an amount up to about 0.1 weight percent. In some embodiments, the glass composition can be substantially free of Na₂O.

Some embodiments of the present invention can be characterized by the amount of K₂O present in the glass compositions. K₂O can be present, in some embodiments, in an amount from about 0 to about 1 weight percent. In some embodiments, K₂O can be present in an amount up to about 1 weight percent. K₂O can be present, in some embodiments, in an amount up to about 0.5 weight percent. K₂O can be present, in some embodiments, in an amount up to about 0.3 weight percent. K₂O can be present, in some embodiments, in an amount up to about 0.1 weight percent. In some embodiments, the glass composition can be substantially free of K₂O.

Some embodiments of the present invention can be characterized by the amount of Li₂O present in the glass compositions. In some embodiments, glass compositions of the present invention can comprise from about 0 to about 2 weight percent Li₂O. Li₂O can be present, in some embodiments, in an amount from about 0 to about 1 weight percent. In some embodiments, Li₂O can be present from greater than about 0 to about 1 weight percent. Li₂O can be present, in some embodiments, in an amount from about 0.4 to about 2 weight percent. Li₂O can be present, in some embodiments, in an amount from about 0.4 to about 1 weight percent. Li₂O can be present, in some embodiments, in an amount from about 0.5 to about 1 weight percent. In some embodiments, the glass composition can be substantially free of Li₂O. Some embodiments of the present invention can be characterized by the total amount of Na₂O, K₂O, and Li₂O content (Na₂O+K₂O+Li₂O). In some embodiments, the Na₂O+K₂O+Li₂O content in glass compositions of the present invention is greater than about 1 weight percent. The Na₂O+K₂O+Li₂O content, in some embodiments, is up to about 2.5 weight percent. In some embodiments, the Na₂O+K₂O+Li₂O content is present in an amount greater than about 1 weight percent and up to about 2.5 weight percent. In some embodiments, the Na₂O+K₂O+Li₂O content in glass compositions of the present invention is from about 0 to about 1.5 weight percent. In some embodiments, the Na₂O+K₂O+Li₂O content in glass compositions of the present invention is from about 0 to about 1.0 weight percent. In some embodiments, the Na₂O+K₂O+Li₂O content in glass compositions of the present invention is from about 0 to about 0.8 weight percent. In some embodiments, the Na₂O+K₂O+Li₂O content in glass compositions of the present invention is from about 0 to about 0.6 weight percent.

Some embodiments of the present invention can be characterized by the amount of Cu₂O present in the glass compositions. Cu₂O can be present, in some embodiments, in an amount from about 0 to about 2.5 weight percent. Cu₂O can be present, in some embodiments, in an amount from about 0 to about 2 weight percent. Cu₂O can be present, in some embodiments, in an amount from about 0 to about 1.7 weight percent. Cu₂O can be present, in some embodiments, in an amount from greater than about 0 to about 2.5 weight percent. Cu₂O can be present, in some embodiments, in an amount from greater than about 0 to about 2 weight percent. Cu₂O can be present, in some embodiments, in an amount from greater than about 0 to about 1.7 weight percent. Cu₂O can be present, in some embodiments, in an amount of 0.5 weight percent or greater. Cu₂O can be present, in some embodiments, in an amount from about 0.5 to about 2.5 weight percent. Cu₂O can be present, in some embodiments, in an amount from about 0.5 to about 2 weight percent. Cu₂O can be present, in some embodiments, in an amount from about 0.5 to about 1.7 weight percent. In some embodiments, the glass composition can be substantially free of Cu₂O.

Some embodiments of the present invention can be characterized by the amount of B₂O₃present in the glass compositions. B₂O₃can be present in an amount from about 0 to about 3 weight percent in some embodiments. In some embodiments, B₂O₃can be present in an amount from about 0 to about 2 weight percent or from about 0 to less than about 2 weight percent. B₂O₃can be present, in some embodiments, in an amount from about 0 to about 1.5 weight percent. In some embodiments, the B₂O₃content can be about 1 weight percent or less. In some embodiments, the B₂O₃content can be about 0.5 weight percent or less. In some embodiments, glass compositions of the present invention can be substantially free of B₂O₃. In other embodiments, glass compositions of the present invention can comprise greater than about 1 weigh percent B₂O₃. In some embodiments, B₂O₃can be present in an amount from greater than about 0 to about 10 weight percent.

Some embodiments of the present invention can be characterized by the amount of Fe₂O₃present in the glass compositions. In some embodiments, Fe₂O₃can be present in an amount from about 0 to about 1.0 weight percent. In some embodiments, Fe₂O₃can be about 0.5 weight percent or less. In some embodiments, Fe₂O₃can be present in an amount from greater than about 0 to about 1.0 weight percent. Fe₂O₃can be present, in some embodiments, in an amount from greater than about 0 to about 0.5 weight percent. In some embodiments, Fe₂O₃can be present in an amount from greater than about 0 to about 0.4 weight percent. Fe₂O₃can be present, in some embodiments, from about 0.1 to about 1.0 weight percent. Fe₂O₃can be present, in some embodiments, from about 0.2 to about 1.0 weight percent. Fe₂O₃can be present, in some embodiments, from about 0.25 to about 1.0 weight percent. Fe₂O₃can be present, in some embodiments, from about 0.3 to about 1.0 weight percent. Fe₂O₃can be present, in some embodiments, from about 0.2 to about 0.8 weight percent, or from about 0.2 to about 0.5 weight percent. Fe₂O₃can be present, in some embodiments, from about 0.25 to about 0.8 weight percent, or from about 0.25 to about 0.5 weight percent. Fe₂O₃can be present, in some embodiments, from about 0.3 to about 0.8 weight percent, or from about 0.3 to about 0.5 weight percent.

Some embodiments of the present invention can be characterized by the amount of TiO₂present in the glass compositions. TiO₂can be present, in some embodiments, in an amount greater than 0 weight percent, 1.5 weight percent or greater, 3 weight percent or greater, 4 weight percent or greater, or 5 weight percent or greater. TiO₂can be present, in some embodiments, in an amount from about 0 to about 9 weight percent. TiO₂can be present, in some embodiments, in an amount from greater than about 1.5 to about 9 weight percent. TiO₂can be present, in some embodiments, in an amount from greater than about 3 to about 9 weight percent. TiO₂can be present, in some embodiments, in an amount from greater than about 4 to about 9 weight percent. TiO₂can be present, in some embodiments, in an amount from about 5 to about 9 weight percent. TiO₂can be present, in some embodiments, in an amount from about 0 to about 3 weight percent. TiO₂can be present, in some embodiments, in an amount from about 0 to about 2 weight percent. TiO₂can be present, in some embodiments, in an amount from about 0 to about 1 weight percent. In some embodiments, TiO₂can be present in an amount from greater than 0 to about 3 weight percent. In some embodiments, the glass composition can be substantially free of TiO₂.

Some embodiments of the present invention can be characterized by the amount of ZrO₂present in the glass compositions. ZrO₂can be present, in some embodiments, in an amount from about 0 to about 3 weight percent. In some embodiments, ZrO₂can be present in an amount up to about 2 weight percent. In some embodiments, glass compositions of the present invention can be substantially free of ZrO₂.

Some embodiments of the present invention can be characterized by the amount of MnO present in the glass compositions. As used herein, the term MnO_xrefers to the genus consisting of MnO and MnO₂. As used throughout, a range of MnO_xcan include any amount of MnO and MnO₂which, in sum, are within the range of MnO_x. By way of example, a range from about 0 to about 9.5 MnO_xcan include (i) about 0 weight percent MnO and about 9.5 weight percent MnO₂, (ii) about 9.5 weight percent MnO and about 0 weight percent MnO₂, or (iii) any weight percent combination of MnO and MnO_xwithin the range from about 0 to about 9.5 weight percent. MnO_xcan be present, in some embodiments, in an amount of about 1 weight percent or greater, about 1.5 weight percent or greater, about 2 weight percent or greater, about 3 weight percent or greater, or about 4 weight percent or greater. MnO_xcan be present, in some embodiments, in an amount from about 0 to about 9.5 weight percent. MnO_xcan be present, in some embodiments, in an amount from greater than about 0 to about 9.5 weight percent. MnO_xcan be present, in some embodiments, in an amount from about 1 to about 9.5 weight percent. MnO_xcan be present, in some embodiments, in an amount from about 1.5 to about 9.5 weight percent. MnO can be present, in some embodiments, in an amount from about 2 to about 9.5 weight percent. MnO_xcan be present, in some embodiments, in an amount from about 4 to about 9.5 weight percent. In some embodiments in which MnO is present, MnO can be present in an amount greater than about 2 weight percent. Thus, the MnO_xcontent can be greater than about 1 weight percent, wherein if MnO is present, then MnO is present an amount of about 2 weight percent or greater. In some embodiments, MnO_xconsists essentially of MnO in an amount from about 0 to about 8.5 weight percent. In some embodiments, MnO_xconsists essentially of MnO in an amount from about 1.5 to about 8.5 weight percent. In some embodiments, MnO_xconsists essentially of MnO in an amount from about 2 to about 8 weight percent. In some embodiments, MnO_xconsists essentially of MnO₂in an amount from about 0 to about 9.5 weight percent. In some embodiments, MnO_xconsists essentially of MnO₂in an amount from about 1.5 to about 9.5 weight percent. In some embodiments, MnO_xconsists essentially of MnO₂in an amount from about 4 to about 9.5 weight percent. In some embodiments, glass compositions of the present invention can be substantially free of MnO, MnO₂, or MnO_x.

Some embodiments of the present invention can be characterized by the amount of P₂O₅present in the glass compositions. P₂O₅can be present, in some embodiments, in an amount from about 0 to about 3 weight percent. In some embodiments, P₂O₅can be present in an amount up to about 2.5 weight percent. In some embodiments, glass compositions of the present invention can be substantially free of P₂O₅.

Sulfate (expressed as SO₃) may also be present as a refining agent. Small amounts of impurities may also be present from raw materials or from contamination during the melting processes, such as Cl₂, Cr₂O₃, or NiO (not limited to these particular chemical forms). Other refining agents and/or processing aids may also be present such as As₂O₃, Sb₂O₃, SnO₂or CeO₂(not limited to these particular chemical forms). These impurities and refining agents, when present, are each typically present in amounts less than about 0.5% by weight of the total glass composition. In some embodiments, the glass composition can be substantially free of any one of these refining agents, or can be substantially free of any combination of these refining agents. Some embodiments of the present invention can be characterized by the presence of an additional feature in the glass compositions. The additional feature is not particularly limited. The additional feature can comprise any one or more compound(s), component(s), and/or ratio(s) in any amount(s) or range(s) disclosed herein. In some embodiments, the additional feature can comprise La₂O₃in an amount greater than about 2 weight percent. In some embodiments, the additional feature can comprise CaO in an amount less than about 2 weight percent. In some embodiments, the additional feature can comprise a MgO/CaO ratio less than about 1. In some embodiments, the additional feature can comprise a SiO₂/Al₂O₃ratio greater than about 4.

As noted above, glass compositions, according to some embodiments of the present invention are fiberizable. In some embodiments, glass compositions of the present invention have forming temperatures (T_F) desirable for use in commercial fiber glass manufacturing operations. As used herein, the term “forming temperature” or T_F, means the temperature at which the glass composition has a viscosity of 1000 poise (or “log 3 temperature”). Glass compositions of the present invention, in some embodiments, have a forming temperature (T_F) ranging from about 1250° C. to about 1550° C. In another embodiment, glass compositions of the present invention have a forming temperature ranging from about 1250° C. to about 1415° C. In another embodiment, glass compositions of the present invention have a forming temperature ranging from about 1250° C. to about 1350° C. In some embodiments, glass compositions have a forming temperature ranging from about 1250° C. to about 1310° C.

Glass compositions of the present invention, in some embodiments, have a liquidus temperature ranging from about 1150° C. to about 1515° C. In another embodiment, glass compositions of the present invention have a liquidus temperature ranging from about 1190° C. to about 1515° C. In another embodiment, glass compositions of the present invention have a liquidus temperature ranging from about 1190° C. to about 1300° C. In some embodiments, glass compositions of the present invention have a liquidus temperature ranging from about 1190° C. to about 1260° C.

In some embodiments, the difference between the forming temperature and the liquidus temperature of a glass composition of the present invention is desirable for commercial fiber glass manufacturing operations. For example, for some embodiments of glass compositions, the difference between the forming temperature and the liquidus temperature ranges from about 25° C. to greater than 60° C. In some embodiments, the difference between the forming temperature and the liquidus temperature of a glass composition of the present invention ranges from about 35° C. to greater than 60° C. In some embodiments, the difference between the forming temperature and the liquidus temperature of a glass composition of the present invention is at least 50° C. In some embodiments, the difference between the forming temperature and the liquidus temperature of a glass composition of the present invention is up to 200° C.

As provided herein, glass fibers can be formed from some embodiments of the glass compositions of the present invention. Thus, embodiments of the present invention can comprise glass fibers formed from any of the glass compositions described herein. In some embodiments, the glass fibers may be arranged into a fabric. In some embodiments, glass fibers of the present invention can be provided in other forms including, for example and without limitation, as continuous strands, chopped strands (dry or wet), yarns, rovings, prepregs, etc. In short, various embodiments of the glass compositions (and any fibers formed therefrom) can be used in a variety of applications.

Some embodiments of the present invention relate to fiber glass strands. Some embodiments of the present invention relate to yarns comprising fiber glass strands. Some embodiments of yarns of the present invention are particularly suitable for weaving applications. In addition, some embodiments of the present invention relate to glass fiber fabrics. Some embodiments of fiber glass fabrics of the present invention are particularly suitable for use in reinforcement applications, especially reinforcement applications in which high modulus, high strength, and/or high elongation are important. Further, some embodiments of the present invention relate to composites that incorporate fiber glass strands, fiber glass yarns, and fiber glass fabrics, such as fiber reinforced polymer composites. Some composites of the present invention are particularly suitable for use in reinforcement applications, especially reinforcement applications in which high modulus, high strength, and/or high elongation are important, such as wind energy (e.g., windmill blades), automotive applications, safety/security applications (e.g., ballistics armor or armor panels), aerospace or aviation applications (e.g., interior floors of planes), high pressure vessels or tanks, missile casings, and others. Some embodiments of the present invention relate to automotive composites. Some embodiments of the present invention relate to aerospace composites. Other embodiments of the present application relate to aviation composites. Still other embodiments of the present invention relate to composites suitable for use in wind energy applications. Some embodiments of the present invention relate to prepregs. Some embodiments of the present invention relate to composites for safety/security applications such as armor panels. Other embodiments of the present invention relate to composites for high pressure vessels or storage tanks. Some embodiments of the present invention relate to composites for missile casings. Other embodiments of the present invention relate to composites for use in high temperature thermal insulation applications. Some embodiments of the present invention relate to printed circuit boards where lower coefficients of thermal expansion are particularly desirable such as substrates for chip packaging.

Some embodiments of the present invention relate to fiber glass strands. In some embodiments, a fiber glass strand of the present invention comprises a plurality of glass fibers comprising a glass composition that comprises the following components:

SiO₂
from about 51 to about 70 weight percent;

Al₂O₃
from about 12.5 to about 22 weight percent;

CaO
from about 0 to about 20 weight percent;

MgO
from about 0 to about 11 weight percent;

Fe₂O₃
from about 0.2 to about 1 weight percent;

RE₂O₃
about 0.05 or greater weight percent; and

MnO_x
greater than about 1 weight percent.

In some embodiments, MnO_xcomprises MnO₂in an amount of about 2 weight percent or greater. In some embodiments, RE₂O₃comprises at least one of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. RE₂O₃is present in an amount of at least about 1 weight percent in some embodiments. In some embodiments, the composition further comprises TiO₂in an amount greater than about 3 weight percent. In some embodiments, the composition further comprises less than about 1.5 weight percent Na₂O+K₂O+Li₂O.

In some embodiments, a fiber glass strand of the present invention comprises a plurality of glass fibers comprising a glass composition that comprises the following components:

wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent.

In some embodiments, BaO is present in an amount greater than about 2 weight percent. In some embodiments, SrO is present in an amount greater than about 2 weight percent. In some embodiments, ZnO is present in an amount greater than about 2 weight percent. In some embodiments, RE₂O₃comprises at least one of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. RE₂O₃is present in an amount of at least about 1 weight percent in some embodiments. In some embodiments, the composition further comprises less than about 1.5 weight percent Na₂O+K₂O+Li₂O.

In some embodiments, a fiber glass strand of the present invention comprises a plurality of glass fibers comprising a glass composition that comprises the following components:

In some embodiments, the composition comprises 0.5 weight percent or greater Cu₂O. In some embodiments, RE₂O₃comprises at least one of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. RE₂O₃is present in an amount of at least about 1 weight percent in some embodiments. In some embodiments, the composition further comprises less than about 1.5 weight percent Na₂O+K₂O+Li₂O.

In some embodiments, a fiber glass strand of the present invention comprises a plurality of glass fibers comprising a glass composition that comprises the following components:

SiO₂
from about 51 to about 70 weight percent;

Al₂O₃
from about 12.5 to about 22 weight percent;

CaO
from about 0 to about 20 weight percent;

MgO
from about 0 to about 12.5 weight percent;

Fe₂O₃
from about 0.2 to about 1 weight percent;

RE₂O₃
about 0.05 or greater weight percent; and

at least one additional feature selected from the group consisting of:

La₂O₃is present in an amount greater than about 2 weight percent;

CaO is present in an amount less than about 2 weight percent;

a MgO/CaO ratio less than about 1; and

a SiO₂/Al₂O₃ratio greater than about 4.

In some embodiments, the additional feature comprises La₂O₃in an amount of about 3 weight percent or greater. In some embodiments, MgO is present in an amount greater than about 6 weight percent, and the additional feature comprises CaO in an amount less than about 1.5 weight percent. In some embodiments, the additional feature comprises the SiO₂/Al₂O₃ratio in an amount greater than about 4.2. In some embodiments, RE₂O₃comprises at least one of La₂O₃, Y₂O₃, Sc₂O₃, and Nd₂O₃. RE₂O₃is present in an amount of at least about 1 weight percent in some embodiments. In some embodiments, the composition further comprises less than about 1.5 weight percent Na₂O+K₂O+Li₂O.

A number of other glass compositions are disclosed herein as part of the present invention, and other embodiments of the present invention relate to fiber glass strands formed from such compositions.

In some embodiments, glass fibers of the present invention can exhibit desirable mechanical and other properties. Glass fibers of the present invention, in some embodiments, can exhibit one or more improved mechanical properties relative to glass fibers formed from E-glass. In some embodiments, glass fibers of the present invention can provide one or more improved properties relative to glass fibers formed from R-glass and/or S-glass. Examples of desirable properties exhibited by some embodiments of glass fibers of the present invention include, without limitation, tensile strength, Young's modulus, coefficient of thermal expansion, softening point, elongation, and dielectric constant.

Glass fibers of the present invention can have desirable Young's modulus (E) values in some embodiments. In some embodiments, fibers formed from glass compositions of the present invention can have a Young's modulus greater than about 87 GPa. In some embodiments, glass fibers of the present invention can have a Young's modulus greater than about 90 GPa. Fibers formed from glass compositions of the present invention can have a Young's modulus greater than about 92 GPa in some embodiments. In some embodiments, glass fibers of the present invention can have a Young's modulus greater than about 93 GPa. Glass fibers of the present invention can have a Young's modulus greater than about 95 GPa in some embodiments. Unless otherwise stated herein, Young's modulus values discussed herein are determined using the procedure set forth in the Examples section below.

Glass fibers of the present invention, in some embodiments, can have desirable tensile strengths. In some embodiments, glass fibers of the present invention can have a tensile strength greater than 4000 MPa. Glass fibers of the present invention, in some embodiments, can have a tensile strength greater than 4,500 MPa. In some embodiments, glass fibers of the present invention can have a tensile strength greater than about 5000 MPa. Glass fibers of the present invention, in some embodiments, can have a tensile strength greater than about 5500 MPa. Unless otherwise stated herein, tensile strength values are determined using the procedure set forth in the Examples section.

Glass fibers of the present invention, in some embodiments, can have desirable elongation values. In some embodiments, glass fibers of the present invention can have an elongation of at least 5.0%. Glass fibers of the present invention can have an elongation of at least 5.5% in some embodiments. Unless otherwise stated herein, elongation values are determined using the procedure set forth in the Examples section.

Glass fibers of the present invention, in some embodiments, can have desirable coefficients of thermal expansion. In some embodiments, glass fibers of the present invention can have a coefficient of thermal expansion less than about 4.5 ppm/° C. Glass fibers of the present invention, in some embodiments, can have a coefficient of thermal expansion less than about 3.1 ppm/° C. Unless otherwise stated, coefficients of thermal expansion are determined using the procedure set forth in the Examples section.

Glass fibers of the present invention, in some embodiments, can have desirable softening points. In some embodiments, glass fibers of the present invention can have a softening point of at least about 900° C. Glass fibers of the present invention, in some embodiments, can have a softening point of at least about 950° C. Unless otherwise stated, softening point values are determined using the procedure set forth in the Examples section.

Glass fibers of the present invention, in some embodiments, can have dielectric constant values (D_k) desirable for use in electronics applications. In some embodiments, glass fibers of the present invention can have a dielectric constant value (D_k) of less than about 6.0 at 1 MHz frequency. Unless otherwise stated herein, dielectric constant (D_k) is determined from 1 MHz to 1 GHz by ASTM Test Method D150—“Standard Test Methods for A-C Loss Characteristics and Permittivity (Dielectric Constant) of Solid Electrical Insulating Materials.”

Fiber glass strands can comprise glass fibers of various diameters, depending on the desired application. In some embodiments, a fiber glass strand of the present invention comprises at least one glass fiber having a diameter between about 5 and about 18 μm. In other embodiments, the at least one glass fiber has a diameter between about 5 and about 10 μm.

In some embodiments, fiber glass strands of the present invention can be formed into rovings. Rovings can comprise assembled, multi-end, or single-end direct draw rovings. Rovings comprising fiber glass strands of the present invention can comprise direct draw single-end rovings having various diameters and densities, depending on the desired application. In some embodiments, a roving comprising fiber glass strands of the present invention exhibits a density up to about 112 yards/pound.

Some embodiments of the present invention relate to yarns comprising at least one fiber glass strand as disclosed herein. In some embodiments, a yarn of the present invention comprises at least one fiber glass strand comprising a glass composition that comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. A yarn, in some embodiments, comprises at least one fiber glass strand comprising a glass composition that comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, a yarn of the present invention comprises at least one fiber glass strand comprising a glass composition that comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments, a yarn of the present invention comprises at least one fiber glass strand comprising a glass composition that comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In other embodiments, a yarn of the present invention can comprise at least one fiber glass strand comprising one of the other glass compositions disclosed herein as part of the present invention.

In some embodiments, a yarn of the present invention comprises at least one fiber glass strand as disclosed herein, wherein the at least one fiber glass strand is at least partially coated with a sizing composition. In some embodiments, the sizing composition is compatible with a thermosetting polymeric resin. In other embodiments, the sizing composition can comprise a starch-oil sizing composition.

Yarns can have various linear mass densities, depending on the desired application. In some embodiments, a yarn of the present invention has a linear mass density from about 5,000 yards/pound to about 10,000 yards/pound.

Yarns can have various twist levels and directions, depending on the desired application. In some embodiments, a yarn of the present invention has a twist in the z direction of about 0.5 to about 2 turns per inch. In other embodiments, a yarn of the present invention has a twist in the z direction of about 0.7 turns per inch.

Yarns can be made from one or more strands that are twisted together and/or plied, depending on the desired application. Yarns can be made from one or more strands that are twisted together but not plied; such yarns are known as “singles.” Yarns of the present invention can be made from one or more strands that are twisted together but not plied. In some embodiments, yarns of the present invention comprise 1-4 strands twisted together. In other embodiments, yarns of the present invention comprise 1 twisted strand.

Some embodiments of the present invention relate to fabrics comprising at least one fiber glass strand as disclosed herein. In some embodiments, a fabric of the present invention comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. A fabric, in some embodiments, comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, a fabric of the present invention comprises at least one fiber glass strand comprising a glass composition that comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments, a fabric of the present invention comprises at least one fiber glass strand comprising a glass composition that comprises from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In other embodiments, a fabric of the present invention can comprise at least one fiber glass strand comprising one of the other glass compositions disclosed herein as part of the present invention.

In some embodiments of the present invention comprising a fabric, the glass fiber fabric is a fabric woven in accordance with industrial fabric style no. 7781. In other embodiments, the fabric comprises a plain weave fabric, a twill fabric, a crowfoot fabric, a satin weave fabric, a stitch bonded fabric (also known as a non-crimp fabric), or a “three-dimensional” woven fabric. Some embodiments of the present invention relate to composites. In some embodiments, a composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. A composite of the present invention, in some embodiments, comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, a composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments, a composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4.

In other embodiments, a composite of the present invention can comprise a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers was formed from one of the other glass compositions disclosed herein as part of the present invention. In some embodiments, a composite of the present invention comprises a polymeric resin and at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In some embodiments, a composite of the present invention comprises a polymeric resin and at least a portion of a roving comprising at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In other embodiments, a composite of the present invention comprises a polymeric resin and at least one yarn as disclosed herein disposed in the polymeric resin. In still other embodiments, a composite of the present invention comprises a polymeric resin and at least one fabric as disclosed herein disposed in the polymeric resin. In some embodiments, a composite of the present invention comprises at least one fill yarn comprising at least one fiber glass strand as disclosed herein and at least one warp yarn comprising at least one fiber glass strand as disclosed herein.

Composites of the present invention can comprise various polymeric resins, depending on the desired properties and applications. In some embodiments of the present invention comprising a composite, the polymeric resin comprises an epoxy resin. In other embodiments of the present invention comprising a composite, the polymeric resin can comprise polyethylene, polypropylene, polyamide, polyimide, polybutylene terephthalate, polycarbonate, thermoplastic polyurethane, phenolic, polyester, vinyl ester, polydicyclopentadiene, polyphenylene sulfide, polyether ether ketone, cyanate esters, bis-maleimides, and thermoset polyurethane resins.

Some embodiments of the present invention relate to aerospace composites. In some embodiments, an aerospace composite of the present invention exhibits properties desirable for use in aerospace applications, such as high strength, high elongation, high modulus, and/or low density.

In some embodiments, an aerospace composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. An aerospace composite of the present invention, in some embodiments, comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, an aerospace composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments, an aerospace composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In other embodiments, an aerospace composite of the present invention can comprise a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers was formed from one of the other glass compositions disclosed herein as part of the present invention.

In some embodiments, an aerospace composite of the present invention comprises a polymeric resin and at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In some embodiments, an aerospace composite of the present invention comprises a polymeric resin and at least a portion of a roving comprising at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In other embodiments, an aerospace composite of the present invention comprises a polymeric resin and at least one yarn as disclosed herein disposed in the polymeric resin. In still other embodiments, an aerospace composite of the present invention comprises a polymeric resin and at least one fabric as disclosed herein disposed in the polymeric resin. In some embodiments, an aerospace composite of the present invention comprises at least one fill yarn comprising at least one fiber glass strand as disclosed herein and at least one warp yarn comprising at least one fiber glass strand as disclosed herein.

Aerospace composites of the present invention can comprise various polymeric resins, depending on the desired properties and applications. In some embodiments of the present invention comprising an aerospace composite, the polymeric resin comprises an epoxy resin. In other embodiments of the present invention comprising an aerospace composite, the polymeric resin can comprise polyethylene, polypropylene, polyamide, polyimide, polybutylene terephthalate, polycarbonate, thermoplastic polyurethane, phenolic, polyester, vinyl ester, polydicyclopentadiene, polyphenylene sulfide, polyether ether ketone, cyanate esters, bis-maleimides, and thermoset polyurethane resins. Examples of parts in which aerospace composites of the present invention might be used can include, but are not limited to floor panels, overhead bins, galleys, seat back, and other internal compartments that are potentially prone to impact, as well as external components such as helicopter rotor blades.

Some embodiments of the present invention relate to aviation composites. In some embodiments, an aviation composite of the present invention exhibits properties desirable for use in aviation applications, such as high strength, high elongation, high modulus, lower density, high specific strength, and/or high specific modulus. The high elongation of some aviation composites of the present invention can make such composites especially desirable for use in aviation applications in which high impact resistance is important, such as aircraft interior applications. In some embodiments, aviation composites of the present invention can demonstrate increased impact performance as compared to composites formed from E-glass fabrics. Aviation composites of the present invention can be suitable for use in aircraft interiors (including, among other things, luggage storage bins, seats, and floors).

In some embodiments, an aviation composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. An aviation composite of the present invention, in some embodiments, comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, an aviation composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments, an aviation composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In other embodiments, an aviation composite of the present invention can comprise a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers was formed from one of the other glass compositions disclosed herein as part of the present invention.

In some embodiments, an aviation composite of the present invention comprises a polymeric resin and at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In some embodiments, an aviation composite of the present invention comprises a polymeric resin and at least a portion of a roving comprising at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In other embodiments, an aviation composite of the present invention comprises a polymeric resin and at least one yarn as disclosed herein disposed in the polymeric resin. In still other embodiments, an aviation composite of the present invention comprises a polymeric resin and at least one fabric as disclosed herein disposed in the polymeric resin. In some embodiments, an aviation composite of the present invention comprises at least one fill yarn comprising at least one fiber glass strand as disclosed herein and at least one warp yarn comprising at least one fiber glass strand as disclosed herein.

Aviation composites of the present invention can comprise various polymeric resins, depending on the desired properties and applications. In some embodiments of the present invention comprising an aviation composite, the polymeric resin comprises a phenolic resin. In other embodiments of the present invention comprising an aviation composite, the polymeric resin can comprise epoxy, polyethylene, polypropylene, polyamide, polyimide, polybutylene terephthalate, polycarbonate, thermoplastic polyurethane, phenolic, polyester, vinyl ester, polydicyclopentadiene, polyphenylene sulfide, polyether ether ketone, cyanate esters, bis-maleimides, and thermoset polyurethane resins. Examples of parts in which aviation composites of the present invention might be used can include, but are not limited to, floor panels, overhead bins, galleys, seat back, and other internal compartments that are potentially prone to impact, as well as external components such as helicopter rotor blades.

Some embodiments of the present invention relate to automotive composites. In some embodiments, an automotive composite of the present invention exhibits properties desirable for use in automotive applications, such as high strength, high elongation and low fiber density. The combination of high strength and high elongation (or failure-to-strain) of some composites of the present invention can make such composites especially desirable for use in automotive applications in which high impact resistance is important, such as automobile structural components, bodies, and bumpers. In some embodiments, automotive composites of the present invention can demonstrate increased impact performance as compared to composites formed from E-glass fabrics, R-glass fabrics, and/or S-glass fabrics.

In some embodiments, an automotive composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. An automotive composite of the present invention, in some embodiments, comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, an automotive composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments, an automotive composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In other embodiments, an automotive composite of the present invention can comprise a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers was formed from one of the other glass compositions disclosed herein as part of the present invention.

In some embodiments, an automotive composite of the present invention comprises a polymeric resin and at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In some embodiments, an automotive composite of the present invention comprises a polymeric resin and at least a portion of a roving comprising at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In other embodiments, an automotive composite of the present invention comprises a polymeric resin and at least one yarn as disclosed herein disposed in the polymeric resin. In still other embodiments, an automotive composite of the present invention comprises a polymeric resin and at least one fabric as disclosed herein disposed in the polymeric resin. In some embodiments, an automotive composite of the present invention comprises at least one fill yarn comprising at least one fiber glass strand as disclosed herein and at least one warp yarn comprising at least one fiber glass strand as disclosed herein.

Automotive composites of the present invention can comprise various polymeric resins, depending on the desired properties and applications. In some embodiments of the present invention comprising an automotive composite, the polymeric resin can comprise a thermoplastic resin or a thermosetting resin. Examples of common thermoplastic resins used in automotive composites include, without limitation, polypropylene, polyamide, high temperature polyamide, polyester, and other thermoplastic resins known to those of skill in the art. Examples of common thermosetting resins used in automotive composites include, without limitation, epoxy, phenolic, polyester, and other thermosetting resins known to those of skill in the art. Examples of parts in which automotive composites of the present invention might be used can include, but are not limited to, automobile structural components, bodies, and bumpers.

Some embodiments of the present invention relate to composites that can be used in wind energy applications. In some embodiments, a composite of the present invention suitable for use in wind energy applications exhibits properties desirable for use in wind energy applications, such as high modulus, high elongation, low fiber density, and/or high specific modulus. Composites of the present invention can be suitable for use in wind turbine blades, particularly long wind turbine blades that are lighter weight but still strong compared to other long wind turbine blades.

In some embodiments, a composite of the present invention suitable for use in wind energy applications comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. A composite of the present invention suitable for use in wind energy applications, in some embodiments, comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, a composite of the present invention suitable for use in wind energy applications comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments, a composite of the present invention suitable for use in wind energy applications comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In other embodiments, a composite suitable for use in wind energy applications of the present invention can comprise a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers was formed from one of the other glass compositions disclosed herein as part of the present invention.

In some embodiments, a composite of the present invention suitable for use in wind energy applications comprises a polymeric resin and at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In some embodiments, a composite of the present invention suitable for use in wind energy applications comprises a polymeric resin and at least a portion of a roving comprising at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In other embodiments, a composite of the present invention suitable for use in wind energy applications comprises a polymeric resin and at least one yarn as disclosed herein disposed in the polymeric resin. In still other embodiments, a composite of the present invention suitable for use in wind energy applications comprises a polymeric resin and at least one fabric as disclosed herein disposed in the polymeric resin. In some embodiments, a composite of the present invention suitable for use in wind energy applications comprises at least one fill yarn comprising at least one fiber glass strand as disclosed herein and at least one warp yarn comprising at least one fiber glass strand as disclosed herein.

Composites of the present invention suitable for use in wind energy applications can comprise various polymeric resins, depending on the desired properties and applications. In some embodiments of the present invention comprising a composite suitable for use in wind energy applications, the polymeric resin comprises an epoxy resin. In other embodiments of the present invention comprising a composite suitable for use in wind energy applications, the polymeric resin can comprise polyester resins, vinyl esters, thermoset polyurethanes, or polydicyclopentadiene resins.

Some embodiments of the present invention relate to composites for use in high pressure vessels and/or tanks. In some embodiments, a composite for use in high pressure vessels and/or tanks of the present invention exhibits properties desirable for use in such applications, such as high strength, high elongation, low density, and/or high specific strength.

In some embodiments, a composite for use in high pressure vessels and/or tanks of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. A composite for use in high pressure vessels and/or tanks of the present invention, in some embodiments, comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, a composite for use in high pressure vessels and/or tanks of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments, a composite for use in high pressure vessels and/or tanks of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In other embodiments, a composite for use in high pressure vessels and/or tanks of the present invention can comprise a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers was formed from one of the other glass compositions disclosed herein as part of the present invention.

In some embodiments, a composite for use in high pressure vessels and/or tanks of the present invention comprises a polymeric resin and at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In some embodiments, a composite for use in high pressure vessels and/or tanks of the present invention comprises a polymeric resin and at least a portion of a roving comprising at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In other embodiments, a composite for use in high pressure vessels and/or tanks of the present invention comprises a polymeric resin and at least one yarn as disclosed herein disposed in the polymeric resin. In still other embodiments, a composite for use in high pressure vessels and/or tanks of the present invention comprises a polymeric resin and at least one fabric as disclosed herein disposed in the polymeric resin. In some embodiments, a composite for use in high pressure vessels and/or tanks of the present invention comprises at least one fill yarn comprising at least one fiber glass strand as disclosed herein and at least one warp yarn comprising at least one fiber glass strand as disclosed herein.

Composites for use in high pressure vessels and/or tanks of the present invention can comprise various polymeric resins, depending on the desired properties and applications. In some embodiments of the present invention comprising a composite for use in high pressure vessels and/or tanks, the polymeric resin can comprise a thermosetting resin. Examples of common thermosetting resins used in high pressure vessels and/or tanks include, without limitation, epoxy, phenolic, polyester, vinyl ester and other thermosetting resins known to those of skill in the art.

In some embodiments, composites of the present invention can be useful in safety and/or security applications. For example, composites of the present invention, in some embodiments, are suitable for use in high mechanical stress applications, including, but not limited to, high energy impact applications. Glass fibers useful in some embodiments of the present invention can exhibit properties especially desirable for high energy impact applications such as ballistic or blast resistance applications. Compared to glass fibers comprising E-glass, glass fibers useful in some embodiments of the present invention can exhibit low dielectric constant, low dielectric loss, high glass transition temperature and/or low thermal expansion.

In some embodiments, composites of the present invention can be suitable for use in armor applications. For example, some embodiments of composites can be used in the production of armor panels. In some embodiments, a composite of the present invention can be formed into a panel, wherein the panel are expected to exhibit desirable 0.30 cal FSP (“fragment simulating projectile”) V50 values (e.g., at least about 900 feet per second (fps) at a panel areal density of about 2 lb/ft²and a panel thickness of about 5-6 mm) when measured by the U.S. Department of Defense Test Method Standard for V50 Ballistic Test for Armor, MIL-STD-662F, December 1997 (hereinafter “MIL-STD-662F”), the entirety of which is incorporated herein by reference. In this context, the term “composite” refers generically to a material comprising a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, whereas the term “panel” refers to a composite having sheet-like physical dimensions or shape. In other embodiments, a composite of the present invention can be formed into a panel, wherein the panel is expected to exhibit desirable 0.50 cal FSP V50 values (e.g., at least about 1200 fps at a panel areal density of about 4.8-4.9 lb/ft²and a panel thickness of about 13-13.5 mm) when measured by MIL-STD-662F. As V50 values can depend on the panel areal density and the panel thickness, composites of the present invention can have different V50 values depending on how the panel is constructed. One advantage of some embodiments of the present invention is the provision of composites having higher V50 values than similarly constructed composites assembled using E-glass fibers.

In some embodiments, a composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x, wherein the composite is adapted for use in ballistics or blast resistance applications. A composite of the present invention, in some embodiments, comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent, and wherein the composite is adapted for use in ballistics or blast resistance applications. In some embodiments, a composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O, wherein the composite is adapted for use in ballistics or blast resistance applications. In some embodiments, a composite of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4, wherein the composite is adapted for use in ballistics or blast resistance applications. In other embodiments, a composite of the present invention adapted for use in ballistics or blast resistance applications can comprise a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers was formed from one of the other glass compositions disclosed herein as part of the present invention.

Some embodiments of the present invention relate to panels, such as armor panels, comprising composites of the present invention. In some embodiments, a composite of the present invention can be formed into a panel, wherein the panel is expected to exhibit desirable 0.30 cal FSP V50 values (e.g., at least about 900 fps at a panel areal density of about 2 lb/ft²and a panel thickness of about 5-6 mm) when measured by MIL-STD-662F. In other embodiments, a composite of the present invention can be formed into a panel, wherein the panel is expected to exhibit desirable 0.30 cal FSP V50 values (e.g., at least about 1000 fps at a panel areal density of about 2 lb/ft²and a panel thickness of about 5-6 mm) when measured by MIL-STD-662F. In still other embodiments of the present invention, a composite can be formed into a panel, wherein the panel is expected to exhibit desirable 0.30 cal FSP V50 values (e.g., at least about 1100 fps at a panel areal density of about 2 lb/ft²and a panel thickness of about 5-6 mm) when measured MIL-STD-662F. In some embodiments of the present invention, a composite can be formed into a panel, wherein the panel is expected to exhibit desirable 0.30 cal FSP V50 values (e.g., about 900 fps to about 1140 fps at a panel areal density of about 2 lb/ft²and a panel thickness of about 5-6 mm) when measured by MIL-STD-662F.

In some embodiments, a composite of the present invention can be formed into a panel, wherein the panel is expected to exhibit desirable 0.50 cal FSP V50 values (e.g., at least about 1200 fps at a panel areal density of about 4.8-4.9 lb/ft²and a panel thickness of about 13-13.5 mm) when measured by MIL-STD-662F. In other embodiments of the present invention, a composite can be formed into a panel, wherein the panel is expected to exhibit desirable 0.50 cal FSP V50 values (at least about 1300 fps at a panel areal density of about 4.8-4.9 lb/ft²and a panel thickness of about 13-13.5 mm) when measured by MIL-STD-662F. In still other embodiments of the present invention, a composite can be formed into a panel, wherein the panel is expected to exhibit desirable 0.50 cal FSP V50 values (at least about 1400 fps at a panel areal density of about 4.8-4.9 lb/ft²and a panel thickness of about 13-13.5 mm) when measured by MIL-STD-662F. In some embodiments of the present invention, a composite can be formed into a panel, wherein the panel is expected to exhibit desirable 0.50 cal FSP V50 values (e.g., about 1200 fps to about 1440 fps at a panel areal density of about 4.8-4.9 lb/ft²and a panel thickness of about 13-13.5 mm) when measured by MIL-STD-662F.

Composites of the present invention adapted for use in ballistics or blast resistance can comprise various polymeric resins. In some embodiments of the present invention, a composite comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition as disclosed herein, the composite can be formed into a panel, such as an armor panel for ballistic or blast resistance, and the polymeric resin comprises an epoxy resin. A composite of the present invention, in some embodiments, comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition as disclosed herein, the composite can be formed into a panel, such as an armor panel for ballistic or blast resistance, and the polymeric resin comprises a polydicyclopentadiene resin. In some embodiments of the present invention, the polymeric resin can comprise polyethylene, polypropylene, polyamides (including Nylon), polybutylene terephthalate, polycarbonate, thermoplastic polyurethane, phenolic, polyester, vinyl ester, thermoset polyurethane, cyanate esters, or bis-maleimide resins.

Some embodiments of the present invention relate to composites for use in casings for missiles and other explosive delivery devices. In some embodiments, a composite for use in casings for missiles and other explosive delivery devices of the present invention exhibits properties desirable for use in such applications, such as high modulus, high strength, high elongation, low coefficient of thermal expansion, high glass softening temperature, and/or high glass transition temperature.

In some embodiments, a composite for use in casings for missiles and other explosive delivery devices of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. A composite for use in casings for missiles and other explosive delivery devices of the present invention, in some embodiments, comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments a composite for use in casings for missiles and other explosive delivery devices of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments a composite for use in casings for missiles and other explosive delivery devices of the present invention comprises a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In other embodiments, a composite for use in casings for missiles and other explosive delivery devices of the present invention can comprise a polymeric resin and a plurality of glass fibers disposed in the polymeric resin, wherein at least one of the plurality of glass fibers was formed from one of the other glass compositions disclosed herein as part of the present invention.

In some embodiments, a composite for use in casings for missiles and other explosive delivery devices of the present invention comprises a polymeric resin and at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In some embodiments, a composite for use in casings for missiles and other explosive delivery devices of the present invention comprises a polymeric resin and at least a portion of a roving comprising at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In other embodiments, a composite for use in casings for missiles and other explosive delivery devices of the present invention comprises a polymeric resin and at least one yarn as disclosed herein disposed in the polymeric resin. In still other embodiments, a composite for use in casings for missiles and other explosive delivery devices of the present invention comprises a polymeric resin and at least one fabric as disclosed herein disposed in the polymeric resin. In some embodiments, a composite for use in casings for missiles and other explosive delivery devices of the present invention comprises at least one fill yarn comprising at least one fiber glass strand as disclosed herein and at least one warp yarn comprising at least one fiber glass strand as disclosed herein.

Composites for use in casings for missiles and other explosive delivery devices of the present invention can comprise various polymeric resins, depending on the desired properties and applications. In some embodiments of the present invention comprising a composite for use in casings for missiles and other explosive delivery devices, the polymeric resin can comprise a thermosetting resin. Examples of common thermosetting resins that can be used in such applications include, without limitation, epoxy, phenolic, polyester, and other thermosetting resins known to those of skill in the art.

While a number of exemplary uses and applications for composites of the present invention are described herein, persons of skill in the art can identify other potential uses for such composites including, for example, other applications in the oil and gas industry, other applications related to transportation and infrastructure, other applications in alternative energy, other high temperature thermal insulation (i.e., thermal shielding) applications (due to higher strength, higher modulus, higher softening temperature and higher glass transition temperature), etc.

Some embodiments of the present invention relate to prepregs. Prepregs of the present invention can comprise a polymeric resin and at least one fiber glass strand as disclosed herein. In some embodiments, a prepreg of the present invention comprises a polymeric resin and a plurality of glass fibers in contact with the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and greater than about 1 weight percent MnO_x. A prepreg of the present invention, in some embodiments, comprises a polymeric resin and a plurality of glass fibers in contact with the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, from about 0 to about 4 weight percent BaO, from about 0 to about 4 weight percent SrO, and from about 0 to about 5.5 weight percent ZrO, wherein the sum of BaO+SrO+ZnO is greater than about 2 weight percent. In some embodiments, a prepreg of the present invention comprises a polymeric resin and a plurality of glass fibers in contact with the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 11 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and from greater than about 0 to about 2.5 weight percent Cu₂O. In some embodiments, a prepreg of the present invention comprises a polymeric resin and a plurality of glass fibers in contact with the polymeric resin, wherein at least one of the plurality of glass fibers comprises a glass composition that comprises the following components: from about 51 to about 70 weight percent SiO₂, from about 12.5 to about 22 weight percent Al₂O₃, from about 0 to about 20 weight percent CaO, from about 0 to about 12.5 weight percent MgO, from about 0.2 to about 1 weight percent Fe₂O₃, about 0.05 or greater weight percent RE₂O₃, and at least one additional feature selected from the group consisting of La₂O₃is present in an amount greater than about 2 weight percent, CaO is present in an amount less than about 2 weight percent, a MgO/CaO ratio less than about 1, and a SiO₂/Al₂O₃ratio greater than about 4. In other embodiments, a prepreg of the present invention can comprise a polymeric resin and a plurality of glass fibers in contact with the polymeric resin, wherein at least one of the plurality of glass fibers was formed from one of the other glass compositions disclosed herein as part of the present invention.

In some embodiments, a prepreg of the present invention comprises a polymeric resin and at least one fiber glass strand as disclosed herein in contact with the polymeric resin. In some embodiments, a prepreg of the present invention comprises a polymeric resin and at least a portion of a roving comprising at least one fiber glass strand as disclosed herein disposed in the polymeric resin. In other embodiments, a prepreg of the present invention comprises a polymeric resin and at least one yarn as disclosed herein in contact with the polymeric resin. In still other embodiments, a prepreg of the present invention comprises a polymeric resin and at least one fabric as disclosed herein in contact with the polymeric resin. In some embodiments, a prepreg of the present invention comprises at least one fill yarn comprising at least one fiber glass strand as disclosed herein and at least one warp yarn comprising at least one fiber glass strand as disclosed herein.

Prepregs of the present invention can comprise various polymeric resins, depending on the desired properties and applications. In some embodiments of the present invention comprising a prepreg, the polymeric resin comprises an epoxy resin. In other embodiments of the present invention comprising a prepreg, the polymeric resin can comprise polyethylene, polypropylene, polyamide, polyimide, polybutylene terephthalate, polycarbonate, thermoplastic polyurethane, phenolic, polyester, vinyl ester, polydicyclopentadiene, polyphenylene sulfide, polyether ether ketone, cyanate esters, bis-maleimides, and thermoset polyurethane resins.

While many of the applications for the glass fibers described herein are reinforcement applications, some embodiments of glass fibers of the present invention can be utilized in electronics applications such as printed circuit boards (“PCB”). More particularly, some embodiments of the present invention relate to glass fiber reinforcements that have electrical properties that permit enhancing performance of a PCB. For example, some embodiments of glass fibers of the present invention can have a dielectric constant (D_k) desirable for electronics applications. The dielectric constant of a material (D_k), also known as “permittivity,” is a measure of the ability of a material to store electric energy. A material to be used as a capacitor desirably has a relatively high D_k, whereas a material to be used as part of a PCB substrate desirably has a low D_k, particularly for high speed circuits. D_kis the ratio of the charge that would be stored (i.e., the capacitance) of a given material between two metal plates to the amount of charge that would be stored by a void (air or vacuum) between the same two metal plates. As another example, some embodiments of glass fibers of the present invention can have a coefficient for thermal expansion desirable for electronics applications. Accordingly, some embodiments of the present invention can be used in a variety of electrical applications including, without limitation, printed circuit boards, precursors to printed circuit boards (e.g., fabrics, laminates, prepregs, etc.). In such embodiments, the printed circuit board or other composite to be used in electrical applications can comprise a polymeric resin and a plurality of glass fibers in contact with the polymeric resin, wherein at least one of the plurality of glass fibers was formed from any of the glass compositions disclosed herein as part of the present invention. The polymeric resin can include any of those known to those of skill in the art for use in printed circuit boards or other electrical applications.

Turning now to methods of manufacturing glass fibers of the present invention and related products, glass fibers of the present invention can be prepared in the conventional manner well known in the art, by blending the raw materials used to supply the specific oxides that form the composition of the fibers. Glass fibers according to the various embodiments of the present invention can be formed using any process known in the art for forming glass fibers, and more desirably, any process known in the art for forming essentially continuous glass fibers. For example, although not limiting herein, the glass fibers according to non-limiting embodiments of the present invention can be formed using direct-melt or indirect-melt fiber forming methods. These methods are well known in the art and further discussion thereof is not believed to be necessary in view of the present disclosure. See, e.g., K. L. Loewenstein, The Manufacturing Technology of Continuous Glass Fibers, 3rd Ed., Elsevier, N.Y., 1993 at pages 47-48 and 117-234.

Following formation of the glass fibers, a primary sizing composition can be applied to the glass fibers using any suitable method known to one of ordinary skill in the art. In some embodiments, the sizing composition can be applied immediately after forming the glass fibers. In general, glass fibers used to form fiber glass strands, fabrics, composites, laminates, and prepregs of the present invention will be at least partially coated with a sizing composition. One skilled in the art may choose one of many commercially available sizing compositions for the glass fibers based upon a number of factors including, for example, performance properties of the sizing compositions, desired flexibility of the resulting fabric, cost, and other factors. In some embodiments, the sizing composition does not comprise a starch-oil sizing composition. In some embodiments of the present invention comprising a sizing composition that does not comprise a starch-oil sizing composition, a sized glass fiber or glass fiber strand need not be further treated with a slashing composition prior to using the fiber or strand in weaving applications. In other embodiments comprising a sizing composition that does not comprise a starch-oil sizing composition, a sized glass fiber or glass fiber strand may optionally be further treated with a slashing composition prior to using the fiber or strand in weaving applications. In some embodiments of the present invention comprising a primary sizing composition, the sizing composition can comprise a starch-oil sizing composition. In some embodiments of the present invention comprising a starch-oil sizing composition, the starch-oil sizing composition may later be removed from a fabric formed from at least one sized glass fiber or fiber glass strand. In some embodiments, the starch-oil sizing may be removed from a fabric using any suitable method known to one of ordinary skill in the art, such as but not limited to heat cleaning. In embodiments of the present invention comprising fabrics from which a starch-oil sizing composition has been removed, a fabric of the present invention may further be treated with a finish coating.

Non-limiting examples of commercially available sizing compositions that can be used in some embodiments of the present invention include sizing compositions often used on single-end rovings, such as Hybon 2026, Hybon 2002, Hybon 1383, Hybon 2006, Hybon 2022, Hybon 2032, Hybon 2016, and Hybon 1062, as well as sizing compositions often used on yarns, such as 1383, 611, 900, 610, 695, and 690, each of which refer to sizing compositions for products commercially available from PPG Industries, Inc.

Fiber glass strands of the present invention can be prepared by any suitable method known to one of ordinary skill in the art. Glass fiber fabrics of the present invention can generally be made by any suitable method known to one of ordinary skill in the art, such as but not limited to interweaving weft yarns (also referred to as “fill yarns”) into a plurality of warp yarns. Such interweaving can be accomplished by positioning the warp yarns in a generally parallel, planar array on a loom, and thereafter weaving the weft yarns into the warp yarns by passing the weft yarns over and under the warp yarns in a predetermined repetitive pattern. The pattern used depends upon the desired fabric style.

Warp yarns can generally be prepared using techniques known to those of skill in the art. Warp yarns can be formed by attenuating a plurality of molten glass streams from a bushing or spinner. Thereafter, a sizing composition can be applied to the individual glass fibers and the fibers can be gathered together to form a strand. The strands can be subsequently processed into yarns by transferring the strands to a bobbin via a twist frame. During this transfer, the strands can be given a twist to aid in holding the bundle of fibers together. These twisted strands can then be wound about the bobbin, and the bobbins can be used in the weaving processes.

Positioning of the warp yarns on the loom can generally be done using techniques known to those of ordinary skill in the art. Positioning of the warp yarns on the loom can be done by way of a loom beam. A loom beam comprises a specified number of warp yarns (also referred to as “ends”) wound in an essentially parallel arrangement (also referred to as “warp sheet”) about a cylindrical core. Loom beam preparation can comprise combining multiple yarn packages, each package comprising a fraction of the number of ends required for the loom beam, into a single package or loom beam. For example and although not limiting herein, a 50 inch (127 cm) wide, 7781 style fabric which utilizes a DE75 yarn input typically requires 2868 ends. However, conventional equipment for forming a loom beam does not allow for all of these ends to be transferred from bobbins to a single beam in one operation. Therefore, multiple beams comprising a fraction of the number of required ends, typically referred to as “section beams,” can be produced and thereafter combined to form the loom beam. In a manner similar to a loom beam, a section beam can include a cylindrical core comprising a plurality of essentially parallel warp yarns wound thereabout. While it will be recognized by one skilled in the art that the section beam can comprise any number of warp yarns required to form the final loom beam, generally the number of ends contained on a section beam is limited by the capacity of the warping creel. For a 7781 style fabric, four section beams of 717 ends each of DE75 yarn are typically provided and when combined offer the required 2868 ends for the warp sheet, as discussed above.

Composites of the present invention can be prepared by any suitable method known to one of ordinary skill in the art, such as but not limited to vacuum assisted resin infusion molding, extrusion compounding, compression molding, resin transfer molding, filament winding, prepreg/autoclave curing, and pultrusion. Composites of the present invention can be prepared using such molding techniques as known to those of ordinary skill in the art. In particular, embodiments of composites of the present invention that incorporate woven fiber glass fabrics can be prepared using techniques known to those of skill in the art for preparation of such composites.

As an example, some composites of the present invention can be made using vacuum assisted compression molding, which technique is well-known to those of skill in the art and described briefly below. As known to those of skill in the art, with vacuum assisted compression molding, a stack of pre-impregnated glass fabrics is placed within a press platen. In some embodiments of the present invention, the stack of pre-impregnated glass fabrics can include one or more fabrics of the present invention as described herein that have been cut to a desired size and shape. Upon completion of the stacking operation for the corresponding number of layers, the press is closed and the platens are connected to a vacuum pump so that the upper platen compresses on the stack of fabrics until the desired pressure is achieved. The vacuum aids in the evacuation of entrapped air within the stack and provides for a reduced void content in the molded laminate. Following connection of the platens to a vacuum pump, the temperature of the platens is then increased to accelerate the conversion rate of the resin (e.g., a thermosetting resin) to a predetermined temperature setting particular to the resin utilized, and kept at that temperature and pressure setting until the laminate reaches full cure. At this point, the heat is turned off and the platens are cooled by water circulation until they reach room temperature. The platens can then be opened, and the molded laminate can be removed from the press.

As another example, some composites of the present invention can be made using vacuum assisted resin infusion technology, as further described herein. A stack of glass fiber fabrics of the present invention may be cut to a desired size and placed on a silicone release treated glass table. The stack may then be covered with a peel ply, fitted with a flow enhancing media, and vacuum bagged using nylon bagging film. Next, the so-called “lay up” may be subjected to a vacuum pressure of about 27 inches Hg. Separately, the polymeric resin that is to be reinforced with the fiber glass fabrics can be prepared using techniques known to those of skill in the art for that particular resin. For example, for some polymeric resins, an appropriate resin (e.g., an amine-curable epoxy resin) may be mixed with an appropriate curing agent (e.g., an amine for an amine-curable epoxy resin) in the proportions recommended by the resin manufacturer or otherwise known to a person of ordinary skill in the art. The combined resin may then be degassed in a vacuum chamber for 30 minutes and infused through the fabric preform until substantially complete wet out of the fabric stack is achieved. At this point, the table may be covered with heated blankets (set to a temperature of about 45-50° C.) for 24 hours. The resulting rigid composites may then be de-molded and post cured at about 250° F. for 4 hours in a programmable convection oven. As is known to persons of ordinary skill in the art, however, various parameters such as degassing time, heating time, and post curing conditions may vary based on the specific resin system used, and persons of ordinary skill in the art understand how to select such parameters based on a particular resin system.

Prepregs of the present invention can be prepared by any suitable means known to one of ordinary skill in the art, such as but not limited to passing fiber glass strands, rovings, or fabrics through a resin bath; using a solvent-based resin; or using a resin film.

As noted above, composites of the present invention can comprise a polymeric resin, in some embodiments. A variety of polymeric resins can be used. Polymeric resins that are known to be useful in reinforcement applications can be particularly useful in some embodiments. In some embodiments, the polymeric resin can comprise a thermoset resin. Thermoset resin systems useful in some embodiments of the present invention can include but are not limited to epoxy resin systems, phenolic based resins, polyesters, vinyl esters, thermoset polyurethanes, polydicyclopentadiene (pDCPD) resins, cyanate esters, and bis-maleimides. In some embodiments, the polymeric resin can comprise an epoxy resin. In other embodiments, the polymeric resin can comprise a thermoplastic resin. Thermoplastic polymers useful in some embodiments of the present invention include but are not limited to polyethylene, polypropylene, polyamides (including Nylon), polybutylene terephthalate, polycarbonate, thermoplastic polyurethanes (TPU), polyphenylene sulfides, and polyether ether keteone (PEEK). Non-limiting examples of commercially available polymeric resins useful in some embodiments of the present invention include EPIKOTE Resin MGS® RIMR 135 epoxy with Epikure MGS RIMH 1366 curing agent (available from Momentive Specialty Chemicals Inc. of Columbus, Ohio), Applied Poleramic MMFCS2 epoxy (available from Applied Poleramic, Inc., Benicia, Calif.), and EP255 modified epoxy (available from Barrday Composite Solutions, Millbury, Mass.).

The invention will be illustrated through the following series of specific embodiments. However, it will be understood by one of skill in the art that many other embodiments are contemplated by the principles of the invention.

EXAMPLES

Table 1 provides a plurality of fiberizable glass compositions according to various embodiments of the present invention as well as data relating to various properties of such compositions. Examples 1, 20, 21, 25, 62, and 77 are comparative examples, while the remaining examples represent various embodiments of the present invention.

The glasses in these examples were made by melting mixtures of commercial and reagent grade chemicals (reagent grade chemicals were used only for the rare earth oxides) in powder form in 10% Rh/Pt crucibles at the temperatures between 1500° C. and 1550° C. (2732° F.-2822° F.) for four hours. Each batch was about 1000 grams. After the 4 hour melting period, the molten glass was poured onto a steel plate for quenching. Volatile species, such as fluoride and alkali oxides, were not adjusted in the batches for their emission loss because of their low concentrations in the glasses. The compositions in the Examples represent as-batched compositions. Commercial ingredients were used in preparing the glasses. In the batch calculation, special raw material retention factors were considered to calculate the oxides in each glass. The retention factors are based on years of glass batch melting and oxides yield in the glass as measured. Hence, the as-batched compositions illustrated in the examples are considered to be close to the measured compositions.

Melt Properties

Melt viscosity as a function of temperature and liquidus temperature was determined by using ASTM Test Method C965 “Standard Practice for Measuring Viscosity of Glass Above the Softening Point,” and C829 “Standard Practices for Measurement of Liquidus Temperature of Glass by the Gradient Furnace Method,” respectively.

Table 1 includes measured liquidus temperature (T_L), reference temperature of forming (T_F) defined by melt viscosity of 1000 Poise, and reference temperature of melting (T_m) defined by viscosity of 100 Poise, for the glass compositions. The difference between the forming temperature and the liquidus temperature (ΔT) is also shown. Table 1 also provides softening temperatures (T_soft), glass transition temperatures (T_g), and coefficients of thermal expansion (CTE) for some of the compositions. Softening temperature (T_soft) values were measured in accordance with ASTM Test Method C338-93 “Standard Test Method for Softening Point of Glass” (2008). Glass transition temperature (T_g) values were measured in accordance with ASTM Test Method C336-71 “Annealing Point and Strain Point by Fiber Elongation.” Coefficient of thermal expansion (CTE) values were determined in accordance with ASTM E228-11 “Standard Test Method for Linear Thermal Expansion of Solid Materials with a Push-Rod Dilatometer.”

Mechanical Properties

For the fiber tensile strength test, fiber samples from the glass compositions were produced from a 10Rh/90Pt single tip fiber drawing unit. Approximately, 85 grams of cullet of a given composition was fed into the bushing melting unit and conditioned at a temperature close or equal to the 100 Poise melt viscosity for two hours. The melt was subsequently lowered to a temperature close or equal to the 1000 Poise melt viscosity and stabilized for one hour prior to fiber drawing. Fiber diameter was controlled to produce an approximately 10 μm diameter fiber by controlling the speed of the fiber drawing winder. All fiber samples were captured in air without any contact with foreign objects. The fiber drawing was completed in a room with a controlled humidity of between 40 and 45% RH.

Fiber tensile strength was measured using a Kawabata KES-G1 (Kato Tech Co. Ltd., Japan) tensile strength analyzer equipped with a Kawabata type C load cell. Fiber samples were mounted on paper framing strips using a resin adhesive. A tensile force was applied to the fiber until failure, from which the fiber strength was determined based on the fiber diameter and breaking stress. The test was done at room temperature under the controlled humidity between 40-45% RH. The average values were computed based on a sample size of 65-72 fibers for each composition. Table 1 reports the average tensile strengths for fibers formed from some of the compositions. Specific strengths were calculated by dividing the tensile strength values (in N/m²) by the corresponding densities (in g/m³).

Young's modulus was also measured for certain glass compositions in Table 1 using the following technique. Approximately 50 grams of glass cullet having a composition corresponding to the appropriate example Table 1 was re-melted in a 90Pt/10Rh crucible for two hours at a melting temperature defined by 100 Poise. The crucible was subsequently transferred into a vertical tube, electrically heated furnace. The furnace temperature was preset at a fiber pulling temperature close or equal to a 1000 Poise melt viscosity. The glass was equilibrated at the temperature for one hour before fiber drawing. The top of the fiber drawing furnace had a cover with a center hole, above which a water-cooled copper coil was mounted to regulate the fiber cooling. A silica rod was then manually dipped into the melt through the cooling coil, and a fiber about 1-1.5 m long was drawn out and collected. The diameter of the fiber ranged from 100μ at one end to 1000 μm at the other end.

Elastic moduli were determined using an ultrasonic acoustic pulse technique (Panatherm 5010 unit from Panametrics, Inc. of Waltham, Mass.) for the fibers drawn from the glass melts. Extensional wave reflection time was obtained using twenty micro-second duration, 200 kHz pulses. The sample length was measured and the respective extensional wave velocity (V_E) was calculated. Fiber density (p) was measured using a Micromeritics AccuPyc 1330 pycnometer. About 20 measurements were made for each composition and the average Young's modulus (E) was calculated from the following formula:

E=V_E²×ρ

The modulus tester uses a wave guide with a diameter of 1 mm, which sets the fiber diameter at the contact side with the wave guide to be about the same as the wave guide diameter. In other words, the end of the fiber having a diameter of 1000 μm was connected at the contact side of the wave guide. Fibers with various diameters were tested for Young's modulus and the results show that a fiber diameter from 100 to 1000 μm does not affect fiber modulus. Specific modulus values were calculated by dividing the Young's modulus values by the corresponding densities.

The values of “Fiber Failure strain (%)” (i.e., fiber elongation) in Table 1 were determined based on Hooke's law by dividing the tensile strength values by the corresponding Young's modulus values (in the same units (e.g., all in MPa)), and multiplying by 100.

TABLE 1

1
2
3
4
5
6

SiO₂
61.49
61.46
61.37
61.46
61.37
61.46

Al₂O₃
15.28
15.36
15.57
15.36
15.57
15.36

Fe₂O₃
0.29
0.29
0.29
0.29
0.29
0.29

CaO
15.43
13.18
12.51
13.18
12.51
13.18

MgO
6.12
6.26
6.21
6.26
6.21
6.26

Na₂O
0.05
0.05
0.05
0.05
0.05
0.05

K₂O
0.09
0.09
0.09
0.09
0.09
0.09

Sc₂O₃
0.00
2.08
2.68
0.00
0.00
0.00

Y₂O₃
0.00
0.00
0.00
2.08
2.68
0.00

La₂O₃
0.00
0.00
0.00
0.00
0.00
2.08

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.50
0.50
0.51
0.50
0.51
0.50

Li₂O
0.74
0.72
0.72
0.72
0.72
0.72

SO₃
0.01
0.01
0.01
0.01
0.01
0.01

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

T_L(° C.)
1198
1197
1241
1197
1201
1199

T_F(° C.)
1285
1288
1296
1306
1312
1300

ΔT (° C.)
87
91
55
109
111
101

T_m(° C.)
1489
1485
1495
1509
1513
1507

Fiber Density
2.62
2.62
2.62
2.62
2.63
2.63

(g/cm³)

Fiber Modulus
89.2
91.0
91.6
90.6
90.2
88.0

(GPa)

Fiber Strength
3570
4108
4376
4264
4727
4321

(MPa)

Fiber Failure
4.0
4.5
4.8
4.7
5.2
4.9

Strain (%)

Specific Fiber
3.5
3.6
3.6
3.5
3.5
3.4

Modulus (×10⁶m)

Specific Fiber
139
160
171
166
184
168

Strength (×10³m)

7
8
9
10
11
12

SiO₂
61.37
61.46
61.37
59.74
59.73
59.73

Al₂O₃
15.57
15.36
15.57
16.00
17.46
17.46

Fe₂O₃
0.29
0.29
0.29
0.27
0.29
0.29

CaO
12.51
13.18
12.51
9.63
7.46
7.46

MgO
6.21
6.26
6.21
8.58
7.13
7.13

Na₂O
0.05
0.05
0.05
0.19
0.19
0.19

K₂O
0.09
0.09
0.09
0.09
0.09
0.09

Sc₂O₃
0.00
0.00
0.00
4.24
6.34
4.44

Y₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

La₂O₃
2.68
0.00
0.00
0.00
0.00
1.90

Nd₂O₃
0.00
2.08
2.68
0.00
0.00
0.00

TiO₂
0.51
0.50
0.51
0.63
0.69
0.69

Li₂O
0.72
0.72
0.72
0.61
0.61
0.61

SO₃
0.01
0.01
0.01
0.02
0.02
0.02

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

T_L(° C.)
1198
1201
1201
1355

1376

T_F(° C.)
1309
1300
1308
1308
1349
1315

ΔT (° C.)
111
99
107
−47

−61

T_m(° C.)
1515
1506
1513
1491
1515
1507

Fiber Density
2.63
2.62
2.62
2.63

(g/cm³)

Fiber Modulus
88.4
88.1
88.9
92.1

(GPa)

Fiber Strength
4639

(MPa)

Fiber Failure
5.3

Strain (%)

Specific Fiber
3.4
3.4
3.5
3.6

Modulus (×10⁶m)

Specific Fiber
180

Strength (×10³m)

13
14
15
16
17
18

SiO₂
59.73
59.74
59.73
59.73
59.73
59.73

Al₂O₃
17.46
16.00
17.46
17.46
17.46
17.46

Fe₂O₃
0.29
0.27
0.29
0.29
0.29
0.29

CaO
7.46
9.63
7.46
7.46
7.46
7.46

MgO
7.13
8.58
7.13
7.13
7.13
7.13

Na₂O
0.19
0.19
0.19
0.19
0.19
0.19

K₂O
0.09
0.09
0.09
0.09
0.09
0.09

Sc₂O₃
3.17
0.00
0.00
0.00
0.00
4.44

Y₂O₃
0.00
4.24
6.34
4.44
3.17
0.00

La₂O₃
3.17
0.00
0.00
1.90
3.17
0.00

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.69
0.63
0.69
0.69
0.69
2.59

Li₂O
0.61
0.61
0.61
0.61
0.61
0.61

SO₃
0.02
0.02
0.02
0.02
0.02
0.02

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

T_L(° C.)
1302
1194
1194
1193
1197

T_F(° C.)
1317
1287
1327
1326
1330

ΔT (° C.)
15
93
133
133
133

T_m(° C.)
1512
1476
1515
1523
1532

Fiber Density
2.64
2.65
2.65
2.65
2.65

(g/cm³)

Fiber Modulus
91.8
92.1
92.2
91.5
91.9

(GPa)

Fiber Strength

5255
5181
5195

(MPa)

Fiber Failure

5.7
5.7
5.7

Strain (%)

Specific Fiber
3.5
3.5
3.5
3.5
3.5

Modulus (×10⁶m)

Specific Fiber

202
199
200

Strength (×10³m)

19
20
21
22
23
24

SiO₂
59.73
60.31
60.22
59.85
59.85
60.37

Al₂O₃
17.46
15.62
16.28
15.58
15.58
14.48

Fe₂O₃
0.29
0.23
0.28
0.27
0.27
0.25

CaO
7.46
13.84
13.06
11.05
11.05
5.46

MgO
7.13
8.63
8.61
8.70
8.70
8.03

Na₂O
0.19
0.06
0.06
0.20
0.20
0.18

K₂O
0.09
0.07
0.09
0.09
0.09
0.08

Sc₂O₃
4.44
0.00
0.00
2.88
0.00
0.00

Y₂O₃
0.00
0.00
0.00
0.00
2.88
0.00

La₂O₃
0.00
0.00
0.00
0.00
0.00
9.87

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.69
0.45
0.64
0.61
0.61
0.57

Li₂O
0.61
0.78
0.75
0.76
0.76
0.70

SO₃
0.02
0.02
0.02
0.02
0.02
0.01

ZrO₂
1.90
0.00
0.00
0.00
0.00
0.00

B₂O₃

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

T_L(° C.)

1211
1225
1240
1195
1260

T_F(° C.)

1251
1265
1264
1268
1320

ΔT (° C.)

40
40
24
73
60

T_m(° C.)

1441
1457
1450
1458
1523

Fiber Density

2.62
2.62
2.64
2.64
2.70

(g/cm³)

Fiber Modulus

90.2
90.5
92.4
91.1
89.5

(GPa)

Fiber Strength

4622
4739
4913
4759
4978

(MPa)

Fiber Failure

5.13
5.2
5.3
5.2
5.6

Strain (%)

Specific Fiber

3.51
3.5
3.6
3.5
3.4

Modulus (×10⁶m)

Specific Fiber

180
185
190
184
188

Strength (×10³m)

25
26
27
28
29
30

SiO₂
59.54
59.73
59.77
62.85
54.20
59.94

Al₂O₃
17.28
17.35
17.36
19.78
15.20
15.66

Fe₂O₃
0.30
0.29
0.28
0.32
0.26
0.25

CaO
9.68
4.99
0.69
2.77
6.41
13.03

MgO
11.28
11.25
11.20
7.00
6.73
7.80

Na₂O
1.12
1.12
1.12
2.40
0.03
0.03

K₂O
0.10
0.09
0.09
0.00
0.07
0.09

Sc₂O₃
0.00
0.00
0.00
3.16
3.88
0.00

Y₂O₃
0.00
0.00
0.00
0.00
0.00
1.99

La₂O₃
0.00
4.49
8.78
0.00
3.88
0.00

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.68
0.68
0.68
0.78
0.02
0.52

Li₂O
0.00
0.00
0.00
0.00
0.59
0.65

SO₃
0.02
0.02
0.02
0.02
0.02
0.02

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.93
8.71
0

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

T_L(° C.)
1265
1268
1324
1344
1300
1211

T_F(° C.)
1285
1316
1361
1397
1414
1275

ΔT (° C.)
20
48
37
53
114
64

T_m(° C.)
1471
1508
1559
1613
1631
1466

Fiber Density
2.61
2.64
2.67
2.51
2.53
2.64

(g/cm³)

Fiber Modulus
90.0
90.5
90.1
87.1
85.9
90.4

(GPa)

Fiber Strength
5105
5294
5445
5503
5492

(MPa)

Fiber Failure
5.7
5.9
6.0
6.3
6.4

Strain (%)

Specific Fiber
3.5
3.5
3.4
3.5
3.5
3.5

Modulus (×10⁶m)

Specific Fiber
199.7
204.8
208.0
223.4
221.8

Strength (×10³m)

31
32
33
34
35
36

SiO₂
59.94
59.94
60.85
61.67
61.67
59.52

Al₂O₃
15.66
15.66
15.90
16.33
16.33
17.24

Fe₂O₃
0.25
0.25
0.25
0.26
0.26
0.27

CaO
13.03
13.03
13.23
6.01
6.01
6.35

MgO
7.80
7.80
7.92
10.26
10.26
10.85

Na₂O
0.03
0.03
0.03
0.16
0.16
0.17

K₂O
0.09
0.09
0.10
0.09
0.09
0.10

Sc₂O₃
0.00
1.99
0.51
0.00
0.00
0.00

Y₂O₃
0.00
0.00
0.00
4.21
0.00
4.44

La₂O₃
1.99
0.00
0.00
0.00
4.21
0.00

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.52
0.52
0.53
0.58
0.58
0.61

Li₂O
0.65
0.65
0.66
0.42
0.42
0.44

SO₃
0.02
0.02
0.02
0.00
0.00
0.00

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0
0
0
0
0
0

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

T_L(° C.)
1209
1212
1213
1258
1247
1232

T_F(° C.)
1265
1263
1270
1329
1331
1300

ΔT (° C.)
56
51
57
71
84
68

T_m(° C.)
1458
1451
1466
1529
1535
1489

Fiber Density
2.64
2.64

2.62
2.62
2.65

(g/cm³)

Fiber Modulus
90.6
90.3

92.2
90.9
94.1

(GPa)

Fiber Strength

5224

(MPa)

Fiber Failure

5.6

Strain (%)

Specific Fiber
3.5
3.5

3.6
3.5
3.6

Modulus (×10⁶m)

Specific Fiber

201

Strength (×10³m)

37
38
39
40
41
42

SiO₂
59.52
59.00
59.52
60.36
59.84
61.69

Al₂O₃
17.24
17.25
17.40
17.65
18.14
21.64

Fe₂O₃
0.27
0.29
0.29
0.29
0.30
0.34

CaO
6.35
6.18
5.37
4.05
3.57
1.01

MgO
10.85
10.65
10.73
10.86
11.85
10.12

Na₂O
0.17
0.02
0.02
0.02
0.02
0.02

K₂O
0.10
0.09
0.09
0.09
0.09
0.11

Sc₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Y₂O₃
0.00
5.84
5.90
5.98
5.47
4.21

La₂O₃
4.44
0.00
0.00
0.00
0.00
0.00

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.61
0.68
0.68
0.69
0.71
0.85

Li₂O
0.44
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

T_L(° C.)
1237
1276
1297
1336
1316

T_F(° C.)
1302
1315
1324
1340
1332
1392

ΔT (° C.)
65
39
27
4
16

T_m(° C.)
1496
1500
1509
1529
1518
1599

T_soft(° C.)

951
958
978
962
995

CTE (10⁻⁶/° C.)

3.1

Fiber Density
2.66
2.63
2.66
2.65
2.65
2.58

(g/cm³)

Fiber Modulus
92.8
92.8
93.2
94.1
93.6
92.4

(GPa)

Fiber Strength

5076

(MPa)

Fiber Failure

5.5

Strain (%)

Specific Fiber
3.6
3.6
3.6
3.6
3.6
3.6

Modulus (×10⁶m)

Specific Fiber

197

Strength (×10³m)

43
44
45
46
47
48

SiO₂
61.69
60.82
60.82
59.40
60.03
60.48

Al₂O₃
21.64
21.34
21.34
17.25
17.40
17.67

Fe₂O₃
0.34
0.34
0.34
0.25
0.26
0.26

CaO
1.01
0.99
0.99
5.78
5.93
4.95

MgO
10.12
9.98
9.98
10.78
10.83
10.64

Na₂O
0.02
0.02
0.02
0.05
0.04
0.04

K₂O
0.11
0.11
0.11
0.10
0.10
0.10

Sc₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Y₂O₃
0.00
5.56
0.00
4.79
4.03
4.34

La₂O₃
4.21
0.00
5.56
0.00
0.00
0.00

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.85
0.84
0.84
0.52
0.57
0.56

Li₂O
0.00
0.00
0.00
1.06
0.81
0.95

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

T_L(° C.)

1235
1237
1232

T_F(° C.)
1401
1397
1390
1273
1289
1299

ΔT (° C.)

38
52
67

T_soft(° C.)
992
993
990

T_m(° C.)
1603
1595
1589
1467
1484
1499

Fiber Density
2.58
2.60
2.61
2.65
2.64
2.63

(g/cm³)

Fiber Modulus
91.6
92.7
92.0
94.7
93.8
93.1

(GPa)

Fiber Strength

5307
5237
5357

(MPa)

Fiber Failure

5.6
5.6
5.8

Strain (%)

Specific Fiber
3.6
3.6
3.6
3.6
3.6
3.6

Modulus (×10⁶m)

Specific Fiber

204
203
207

Strength (×10³m)

Dielectric
5.69
5.82
5.87

Constant @1 GHz

Dissipation loss @
0.0020
0.0018
0.0017

1 GHz

49
50
51
52
53
54

SiO₂
59.90
56.85
54.76
57.72
60.07
59.40

Al₂O₃
16.54
15.70
15.12
16.67
17.56
17.25

Fe₂O₃
0.24
0.23
0.22
0.22
0.22
0.25

CaO
5.38
5.10
4.92
4.63
4.65
5.78

MgO
11.55
10.96
10.56
9.94
9.97
10.78

Na₂O
0.05
0.04
0.04
0.06
0.07
0.05

K₂O
0.10
0.09
0.09
0.11
0.12
0.10

Sc₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Y₂O₃
4.71
9.56
12.89
8.67
4.88
2.40

La₂O₃
0.00
0.00
0.00
0.00
0.00
2.40

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.50
0.48
0.46
0.43
0.39
0.52

Li₂O
1.03
0.98
0.94
1.55
2.08
1.06

SO₃
0.00
0.00
0.00
0.00
0.00
0.01

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.01

T_L(° C.)
1252
1223
1225
1201
1216
1240

T_F(° C.)
1273
1247
1232
1252
1262
1273

ΔT (° C.)
21
24
7
51
46
33

T_m(° C.)
1464
1427
1403
1441
1465
1467

Fiber Density
2.65
2.74
2.81
2.71

(g/cm³)

Fiber Modulus
93.8
96.4
97.6
95.3

(GPa)

Fiber Strength

5013

(MPa)

Fiber Failure

5.3

Strain (%)

Specific Fiber
3.6
3.6
3.5
3.6

Modulus (×10⁶m)

Specific Fiber

182

Strength (×10³m)

55
56
57
58
59
60

SiO₂
59.40
60.03
60.03
60.16
60.16
59.43

Al₂O₃
17.25
17.40
17.40
18.32
18.32
18.10

Fe₂O₃
0.25
0.26
0.26
0.28
0.28
0.27

CaO
5.78
5.93
5.93
5.43
5.43
5.36

MgO
10.78
10.83
10.83
10.19
10.19
10.07

Na₂O
0.05
0.04
0.04
0.04
0.04
0.04

K₂O
0.10
0.10
0.10
0.11
0.11
0.10

Sc₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Y₂O₃
0.00
2.02
0.00
4.09
0.00
0.00

La₂O₃
4.79
2.02
4.03
0.00
4.09
5.25

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.52
0.57
0.57
0.61
0.61
0.60

Li₂O
1.06
0.81
0.81
0.79
0.79
0.78

SO₃
0.01
0.01
0.01
0.00
0.00
0.00

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.01
100.00
100.00
100.00
100.00

T_L(° C.)
1245
1240
1245
1233
1233
1227

T_F(° C.)
1275
1288
1290
1305
1302
1298

ΔT (° C.)
30
48
45
71
69
71

T_m(° C.)
1473
1483
1487
1503
1503
1495

Fiber Density

2.64
2.64
2.63
2.63
2.65

(g/cm³)

Fiber Modulus

93.1
92.9
92.8
91.4
91.6

(GPa)

Fiber Strength

5368

(MPa)

Fiber Failure

5.8

Strain (%)

Specific Fiber

3.60

3.6

Modulus (×10⁶m)

Specific Fiber

207

Strength (×10³m)

61
62
63
64
65
66

SiO₂
59.99
60.51
60.39
60.20
59.60
58.69

Al₂O₃
17.86
15.46
15.43
15.39
15.23
15.00

Fe₂O₃
0.27
0.26
0.26
0.26
0.25
0.25

CaO
4.49
14.49
14.46
14.42
14.27
14.05

MgO
9.92
8.17
8.15
8.13
8.05
7.93

Na₂O
0.04
0.03
0.03
0.03
0.03
0.03

K₂O
0.10
0.09
0.09
0.09
0.09
0.09

Sc₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Y₂O₃
0.00
0.00
0.20
0.50
1.50
3.00

La₂O₃
5.97
0.00
0.00
0.00
0.00
0.00

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.59
0.55
0.54
0.54
0.54
0.53

Li₂O
0.77
0.43
0.43
0.43
0.43
0.42

SO₃
0.00
0.01
0.01
0.01
0.01
0.01

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
99.99
99.99
99.99
99.99
99.99

T_L(° C.)
1240
1205
1208
1200
1202
1209

T_F(° C.)
1316
1273
1268
1271
1269
1256

ΔT (° C.)
76
68
60
71
67
47

T_m(° C.)
1518
1468
1462
1465
1459
1440

Fiber Density
2.65
2.63

(g/cm³)

Fiber Modulus
91.8
89.5

(GPa)

Fiber Strength

(MPa)

Fiber Failure

Strain (%)

Specific Fiber
3.5

Modulus (×10⁶m)

Specific Fiber

Strength (×10³m)

67
68
69
70
71
72

SiO₂
58.08
57.48
56.27
60.39
60.20
59.60

Al₂O₃
14.84
14.69
14.38
15.43
15.39
15.23

Fe₂O₃
0.25
0.24
0.24
0.26
0.26
0.25

CaO
13.91
13.76
13.47
14.46
14.42
14.27

MgO
7.84
7.76
7.60
8.15
8.13
8.05

Na₂O
0.03
0.03
0.03
0.03
0.03
0.03

K₂O
0.09
0.09
0.09
0.09
0.09
0.09

Sc₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Y₂O₃
4.00
5.00
7.00
0.00
0.00
0.00

La₂O₃
0.00
0.00
0.00
0.20
0.50
1.50

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.52
0.52
0.51
0.54
0.54
0.54

Li₂O
0.42
0.41
0.40
0.43
0.43
0.43

SO₃
0.01
0.01
0.01
0.01
0.01
0.01

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
99.99
100.00
100.00
99.99
99.99
99.99

T_L(° C.)
1206
1208
1212
1207
1205
1204

T_F(° C.)
1260
1255
1244
1265
1265
1259

ΔT (° C.)
54
47
32
58
60
55

T_m(° C.)
1444
1463
1480
1456
1457
1447

Fiber Density

(g/cm³)

Fiber Modulus

(GPa)

Fiber Strength

(MPa)

Fiber Failure

Strain (%)

Specific Fiber

Modulus (×10⁶m)

Specific Fiber

Strength (×10³m)

73
74
75
76
77
78
79
80

SiO₂
58.69
58.08
57.48
56.27
60.72
60.81
58.91
58.91

Al₂O₃
15.00
14.84
14.69
14.38
15.57
13.01
16.95
16.95

Fe₂O₃
0.25
0.25
0.24
0.24
0.27
0.23
0.25
0.25

CaO
14.05
13.91
13.76
13.47
22.52
19.17
4.35
4.35

MgO
7.93
7.84
7.76
7.60
0.19
0.16
10.49
10.49

Na₂O
0.03
0.03
0.03
0.03
0.01
0.01
0.04
0.04

K₂O
0.09
0.09
0.09
0.09
0.08
0.07
0.10
0.10

Sc₂O₃
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

Y₂O₃
0.00
0.00
0.00
0.00
0.00
6.01
3.98
0.00

La₂O₃
3.00
4.00
5.00
7.00
0.00
0.00
0.00
3.98

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.53
0.52
0.52
0.51
0.63
0.53
2.09
2.09

Li₂O
0.42
0.42
0.41
0.40
0.00
0.00
0.78
0.78

SO₃
0.01
0.01
0.01
0.01
0.00
0.00
0.00
0.00

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00
2.05
2.05

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
99.99
99.99
100.00
100.00
100.00
100.00
100.00
100.00

T_L(° C.)
1202
1199
1196

1231
1272

T_F(° C.)
1253
1248
1245

1325
1346
1297
1298

ΔT (° C.)
51
49
49

94
74

T_m(° C.)
1440
1432
1427

1528
1543
1491
1496

T_soft(° C.)

943
962
912
904

T_g(° C.)

722
716

CTE (10⁻⁶/° C.)

4.11
4.13

Fiber Density

2.62
2.68
2.66
2.66

(g/cm³)

Fiber Modulus

82.0
83.7
93.8
92.4

(GPa)

Fiber Strength

3948
4029

(MPa)

Fiber Failure

4.8
4.8

Strain (%)

Specific Fiber

3.2
3.2
3.6
3.5

Modulus (×10⁶m)

Specific Fiber

154
153

Strength (×10³m)

81
82
83
84
85
86
87
88
89

SiO₂
61.43
59.81
59.04
58.66
57.41
58.17
54.56
56.41
51.18

Al₂O₃
15.14
14.74
14.55
14.45
14.15
14.33
13.44
13.90
12.61

Fe₂O₃
0.26
0.26
0.25
0.25
0.25
0.25
0.23
0.24
0.22

CaO
14.70
12.52
11.46
10.95
10.72
12.17
9.36
11.80
8.78

MgO
7.98
7.77
7.67
7.62
7.45
7.55
7.08
7.32
6.65

Na₂O
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

K₂O
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

Sc₂O₃
0.00
4.43
6.56
7.60
9.56
0.00
0.00
0.00
0.00

Y₂O₃
0.00
0.00
0.00
0.00
0.00
7.05
14.88
0.00
0.00

La₂O₃
0.00
0.00
0.00
0.00
0.00
0.00
0.00
9.87
20.15

Nd₂O₃
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

TiO₂
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

Li₂O
0.49
0.48
0.47
0.47
0.46
0.47
0.44
0.45
0.41

SO₃
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

ZrO₂
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.0
100.0
100.0
100.0
100.0
100.0
100.0
100.0
100.0

T_L(° C.)
1199
1337
1434
1462
1516
1204
1294
1184
1158

T_F(° C.)
1296
1285
1284
1307
1348
1280
1260
1266
1237

ΔT (° C.)
97
−52
−150
−155
−168
76
−34
82
79

T_m(° C.)
1495
1471
1458
1447
1449
1464
1426
1450
1406

T_soft(° C.)
898
917
920
925
931
911
922
899
903

T_g(° C.)
717
740
750
759
757
734
748
721
729

CTE (10⁻⁶/° C.)
4.63
4.61
4.54
4.54
4.44

Fiber Density
2.60
2.64

2.70

2.78

(g/cm³)

Fiber Modulus
89.4
92.4

91.6

90.8

(GPa)

Fiber Strength

(MPa)

Fiber Failure

Strain (%)

Specific Fiber
3.5
3.6

3.5

3.3

Modulus (×10⁶m)

Specific Fiber

Strength (×10³m)

90
91
92
93

SiO₂
63.08
65.03
65.03
64.49

Al₂O₃
16.16
15.35
15.35
14.61

Fe₂O₃
0.24
0.23
0.23
0.19

CaO
4.40
3.37
3.37
3.00

MgO
10.63
10.86
10.86
9.67

Na₂O
0.04
0.04
0.04
0.03

K₂O
0.09
0.09
0.09
0.08

Sc₂O₃
0.00
0.00
0.00
0.00

Y₂O₃
0.00
0.00
3.68
0.00

La₂O₃
4.04
3.68
0.00
4.33

Nd₂O₃
0.00
0.00
0.00
0.00

TiO₂
0.52
0.47
0.47
0.39

Li₂O
0.79
0.89
0.89
0.79

SO₃
0.00
0.00
0.00
0.00

ZrO₂
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00

P₂O₅
0.00
0.00
0.00
2.42

TOTAL
100.0
100.0
100.0
100.0

T_L(° C.)
1267

T_F(° C.)
1332
1355
1350
1396

ΔT (° C.)
65

T_m(° C.)
1542
1572
1562
1619

Fiber Density
2.60

(g/cm³)

Fiber Modulus
91.4

(GPa)

Fiber Strength

(MPa)

Fiber Failure

Strain (%)

Specific Fiber
3.6

Modulus (×10⁶m)

Specific Fiber

Strength (×10³m)

Certain of these data were plotted in FIGS. 1-4. FIG. 1 is a chart showing Young's modulus values relative to the amount of rare earth oxides (RE₂O₃) for the glass compositions in Examples 1-17, 22, and 23. FIG. 2 is a chart showing pristine fiber tensile strength values relative to the amount of rare earth oxides (RE₂O₃) for the glass compositions in Examples 1-17, 22, and 23. FIG. 3 is a chart showing softening and glass transition temperatures relative to the amount of rare earth oxides (RE₂O₃) for the glass compositions of Examples 81-89. FIG. 4 is a chart showing linear coefficient of thermal expansion relative to the amount of scandium oxide (Sc₂O₃) for the glass compositions of Examples 81-89.

Table 2 provides a plurality of fiberizable glass compositions according to various embodiments of the present invention as well as data relating to various properties of such compositions. The embodiments of Table 2 were produced in the same manner as those in Table 1. The melt properties and mechanical properties of the embodiments of Table 2 were determined in the same manner as for those in Table 1.

TABLE 2

94
95
96
97
98
99

SiO₂
61.42
60.85
60.07
61.02
61.28
60.18

Al₂O₃
17.85
17.62
17.52
17.80
17.87
16.77

CaO
5.42
5.64
5.92
6.00
6.01
7.18

MgO
8.81
9.18
9.63
8.22
6.29
8.05

BaO
0.00
0.00
0.00
0.00
0.00
0.00

SrO
0.00
0.00
0.00
0.00
0.00
0.00

ZnO
0.00
0.00
0.00
0.00
0.00
0.00

Na₂O
0.04
0.05
0.04
0.04
0.04
0.04

K₂O
0.11
0.10
0.10
0.11
0.11
0.10

Li₂O
0.96
1.00
0.91
0.93
0.93
1.01

Fe₂O₃
0.37
0.37
0.37
0.38
0.38
0.37

TiO₂
0.56
0.55
0.56
0.57
2.13
1.36

Y₂O₃
4.45
4.64
4.87
4.94
4.96
4.93

La₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Cu₂O
0.00
0.00
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
3.44
3.45
3.43
3.43
3.43
3.59

MgO/CaO
1.63
1.63
1.63
1.37
1.05
1.12

CaO + MgO +
14.23
14.82
15.55
14.21
12.29
15.24

BaO + SrO

BaO + SrO + ZnO
0.00
0.00
0.00
0.00
0.00
0.00

T_L(° C.)
1188
1188
1200
1185
1208
1154

T_F(° C.)
1319
1307
1297
1320
1338
1294

ΔT (° C.)
131
119
97
135
130
140

T_m(° C.)
1522
1508
1494
1521
1549
1493

Fiber Density
2.61
2.62
2.63
2.62
2.61

(g/cm³)

Fiber Modulus (GPa)
92.3
92.0
92.8
91.9
90.0

Fiber Strength (MPa)
5490
5492
5340
5467

Fiber Failure Strain (%)
5.9
6.0
5.8
5.9

Specific Fiber
3.6
3.6
3.6
3.6
3.5

Modulus (×10⁶m)

Specific Fiber
215.0
214.2
207.0
213.2
0.0

Strength (×10³m)

100
101
102
103
104
105

SiO₂
61.28
60.18
60.83
60.12
59.78
61.00

Al₂O₃
17.87
16.77
15.23
17.84
17.99
16.75

CaO
6.01
7.18
7.90
5.88
5.93
4.67

MgO
6.29
8.05
8.86
9.47
9.55
10.20

BaO
0.00
0.00
0.00
0.00
0.00
0.00

SrO
0.00
0.00
0.00
0.00
0.00
2.46

ZnO
0.00
0.00
0.00
0.00
0.00
0.00

Na₂O
0.04
0.04
0.04
0.04
0.04
0.04

K₂O
0.11
0.10
0.09
0.10
0.10
0.10

Li₂O
0.93
1.01
0.77
0.77
0.78
0.72

Fe₂O₃
0.38
0.37
0.37
0.39
0.40
0.25

TiO₂
0.56
0.56
1.41
0.59
0.59
0.55

Y₂O₃
4.96
4.93
4.50
4.80
4.84
3.25

La₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Cu₂O
1.57
0.80
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
3.43
3.59
3.99
3.37
3.32
3.64

MgO/CaO
1.05
1.12
1.12
1.61
1.61
2.19

CaO + MgO +
12.29
15.24
16.76
15.35
15.48
17.33

BaO + SrO

BaO + SrO + ZnO
0.00
0.00
0.00
0.00
0.00
2.46

T_L(° C.)
1153
1167
1219
1226
1201
1235

T_F(° C.)
1336
1291
1289
1307
1299
1320

ΔT (° C.)
183
124
70
81
98
85

T_m(° C.)
1547
1447
1491
1501
1493
1519

Fiber Density
2.62

2.64

2.63

(g/cm³)

Fiber Modulus
91.1

91.8

92.6

(GPa)

Fiber Strength
5321

5243

5583

(MPa)

Fiber Failure Strain (%)
5.8

5.7

6.03

Specific Fiber
3.5

3.5

3.6

Modulus (×10⁶m)

Specific Fiber
207.0

202.5

216.6

Strength (×10³m)

106
107
108
109
110
111

SiO₂
60.48
62.01
64.00
66.00
65.00
63.00

Al₂O₃
17.67
16.98
16.09
15.21
15.16
16.02

CaO
4.95
4.76
4.51
4.26
3.62
3.83

MgO
10.64
10.22
9.68
9.14
10.83
11.45

BaO
0.00
0.00
0.00
0.00
0.00
0.00

SrO
0.00
0.00
0.00
0.00
0.00
0.00

ZnO
0.00
0.00
0.00
0.00
0.00
0.00

Na₂O
0.04
0.04
0.04
0.04
0.04
0.04

K₂O
0.10
0.10
0.09
0.09
0.09
0.09

Li₂O
0.95
0.90
0.86
0.80
0.80
0.85

Fe₂O₃
0.26
0.25
0.24
0.23
0.23
0.24

TiO₂
0.56
0.54
0.51
0.48
0.48
0.50

Y₂O₃
4.33
4.20
3.98
3.75
3.74
3.96

La₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Cu₂O
0.00
0.00
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.004
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
3.42
3.65
3.98
4.34
4.29
3.93

MgO/CaO
2.15
2.15
2.15
2.15
2.99
2.99

CaO + MgO +
15.60
14.99
14.19
13.40
14.46
15.29

BaO + SrO

BaO + SrO + ZnO
0.00
0.00
0.00
0.00
0.00
0.00

T_L(° C.)
1232
1234
1282
1332
1329
1288

T_F(° C.)
1299
1321
1348
1383
1358
1329

ΔT (° C.)
67
87
66
51
29
41

T_m(° C.)
1499
1522
1558
1601
1567
1532

Fiber Density
2.63
2.61
2.58
2.56
2.57
2.60

(g/cm³)

Fiber Modulus
93.1
92.6
91.7
89.2
90.8
92.7

(GPa)

Fiber Strength
5357.0
5462
5456

(MPa)

Fiber Failure Strain (%)
5.8
5.9
6.0

Specific Fiber
3.54
3.55
3.55
3.49
3.53
3.57

Modulus (×10⁶m)

Specific Fiber
203.8
209.5
211.5

Strength (×10³m)

112
113
114
115
116
117

SiO₂
61.00
60.43
62.00
64.00
65.00
63.50

Al₂O₃
16.88
17.70
17.00
16.11
15.67
14.91

CaO
4.04
0.10
0.10
0.09
0.09
5.11

MgO
12.08
10.65
10.22
9.68
9.41
10.11

BaO
0.00
0.00
0.00
0.00
0.00
0.00

SrO
0.00
0.00
0.00
0.00
0.00
0.00

ZnO
0.00
4.90
4.70
4.46
4.33
0.00

Na₂O
0.04
0.04
0.04
0.04
0.04
0.03

K₂O
0.10
0.10
0.10
0.09
0.09
0.08

Li₂O
0.91
0.95
0.91
0.86
0.84
0.50

Fe₂O₃
0.25
0.25
0.24
0.23
0.23
0.24

TiO₂
0.52
0.56
0.54
0.51
0.49
0.50

Y₂O₃
4.17
4.30
4.14
3.92
3.80
5.01

La₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Cu₂O
0.00
0.00
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
3.61
3.41
3.65
3.97
4.15
4.26

MgO/CaO
2.99
102.58
102.58
102.58
102.58
1.98

CaO + MgO +
16.13
10.76
10.33
9.78
9.51
15.23

BaO + SrO

BaO + SrO + ZnO
0.00
4.90
4.70
4.46
4.33
0.00

T_L(° C.)
1242
1296
1321
1361
1378
1330

T_F(° C.)
1301
1315
1338
1362
1381
1360

ΔT (° C.)
59
19
17
1
3
30

T_m(° C.)
1496
1516
1546
1577
1600
1572

Fiber Density
2.62

(g/cm³)

Fiber Modulus
94.8

(GPa)

Fiber Strength
5395

(MPa)

Fiber Failure Strain (%)
5.7

Specific Fiber
3.62

Modulus (×10⁶m)

Specific Fiber
206.1

Strength (×10³m)

118
119
120
121
122
123

SiO₂
64.01
62.50
64.01
62.49
64.00
62.51

Al₂O₃
13.57
16.93
17.34
16.70
17.37
16.93

CaO
5.34
2.41
0.09
1.30
0.09
4.70

MgO
10.55
9.10
9.28
10.49
9.28
10.20

BaO
0.00
0.00
0.00
3.05
3.20
0.00

SrO
0.00
3.04
3.23
0.00
0.00
0.00

ZnO
0.00
0.00
0.00
0.00
0.00
0.00

Na₂O
0.03
0.03
0.03
0.03
0.03
0.03

K₂O
0.08
0.09
0.09
0.09
0.09
0.10

Li₂O
0.51
0.55
0.57
0.53
0.56
0.60

Fe₂O₃
0.22
0.26
0.26
0.25
0.26
0.26

TiO₂
0.46
0.58
0.60
0.58
0.60
0.58

Y₂O₃
5.23
4.51
4.51
4.49
4.51
4.09

La₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Cu₂O
0.00
0.00
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
4.72
3.69
3.69
3.74
3.68
3.69

MgO/CaO
1.98
3.78
104.76
8.09
104.83
2.17

CaO + MgO +
15.90
14.55
12.60
14.84
12.57
14.90

BaO + SrO

BaO + SrO + ZnO
0.00
3.04
3.23
3.05
3.20
0.00

T_L(° C.)
1352
1317
1348
1327
1347
1290

T_F(° C.)
1347
1381
1415
1378
1428
1350

ΔT (° C.)
−5
64
67
51
81
60

T_m(° C.)
1552
1590
1633
1587
1648
1553

Fiber Density

2.611
2.5728

(g/cm³)

Fiber Modulus

90.5
89.99

(GPa)

Fiber Strength

(MPa)

Fiber Failure Strain (%)

Specific Fiber

3.46
3.50

Modulus (×10⁶m)

Specific Fiber

Strength (×10³m)

124
125
126
127
128
129

SiO₂
62.25
62.39
62.31
62.01
64.00
66.00

Al₂O₃
16.72
16.63
16.85
16.98
16.09
15.21

CaO
4.78
5.01
4.97
4.76
4.51
4.26

MgO
10.20
10.01
9.93
10.22
9.68
9.14

BaO
0.00
0.00
0.00
0.00
0.00
0.00

SrO
0.00
0.00
0.00
0.00
0.00
0.00

ZnO
0.00
0.00
0.00
0.00
0.00
0.00

Na₂O
0.03
0.03
0.03
0.04
0.04
0.04

K₂O
0.09
0.09
0.09
0.10
0.09
0.09

Li₂O
0.60
0.50
0.50
0.90
0.86
0.80

Fe₂O₃
0.26
0.26
0.26
0.25
0.24
0.23

TiO₂
0.57
0.58
0.59
0.54
0.50
0.48

Y₂O₃
4.49
4.50
4.46
0.00
0.00
0.00

La₂O₃
0.00
0.00
0.00
4.20
3.98
3.75

Cu₂O
0.00
0.00
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
3.72
3.75
3.70
3.65
3.98
4.34

MgO/CaO
2.13
2.00
2.00
2.15
2.15
2.15

CaO + MgO +
14.98
15.01
14.90
14.99
14.19
13.40

BaO + SrO

BaO + SrO + ZnO
0.00
0.00
0.00
0.00
0.00
0.00

T_L(° C.)
1288
1292
1292
1234
1283
1338

T_F(° C.)
1339
1348
1346
1321
1363
1386

ΔT (° C.)
51
56
54
87
80
48

T_m(° C.)
1539
1550
1548
1527
1579
1608

Fiber Density

(g/cm³)

Fiber Modulus

(GPa)

Fiber Strength

5365

(MPa)

Fiber Failure Strain (%)

Specific Fiber

Modulus (×10⁶m)

Specific Fiber

Strength (×10³m)

130
131
132
133
134
135

SiO₂
65.00
63.00
61.00
60.43
62.00
64.00

Al₂O₃
15.16
16.02
16.88
17.70
17.00
16.11

CaO
3.62
3.83
4.04
0.10
0.10
0.09

MgO
10.83
11.45
12.08
10.65
10.22
9.68

BaO
0.00
0.00
0.00
0.00
0.00
0.00

SrO
0.00
0.00
0.00
0.00
0.00
0.00

ZnO
0.00
0.00
0.00
4.90
4.70
4.46

Na₂O
0.04
0.04
0.04
0.04
0.04
0.04

K₂O
0.09
0.09
0.10
0.10
0.10
0.09

Li₂O
0.80
0.85
0.90
0.95
0.90
0.86

Fe₂O₃
0.23
0.24
0.25
0.25
0.24
0.23

TiO₂
0.48
0.50
0.52
0.56
0.54
0.50

Y₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

La₂O₃
3.74
3.96
4.18
4.31
4.14
3.92

Cu₂O
0.00
0.00
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
4.29
3.93
3.61
3.41
3.65
3.97

MgO/CaO
2.99
2.99
2.99
102.58
102.58
102.58

CaO + MgO +
14.46
15.29
16.13
10.76
10.33
9.78

BaO + SrO

BaO + SrO + ZnO
0.00
0.00
0.00
4.90
4.70
4.46

T_L(° C.)
1313
1263
1259
1307
1315
1352

T_F(° C.)
1359
1325
1298
1324
1348
1380

ΔT (° C.)
46
62
39
17
33
28

T_m(° C.)
1574
1532
1496
1530
1563
1606

Fiber Density

(g/cm³)

Fiber Modulus

(GPa)

Fiber Strength

5355

(MPa)

Fiber Failure Strain (%)

Specific Fiber

Modulus (×10⁶m)

Specific Fiber

Strength (×10³m)

136
137
138
139
140
141

SiO₂
65.00
61.42
61.02
60.85
62.50
62.49

Al₂O₃
15.67
17.85
17.80
17.62
16.93
16.70

CaO
0.09
5.42
6.00
5.64
2.41
1.30

MgO
9.41
8.81
8.22
9.18
9.10
10.49

BaO
0.00
0.00
0.00
0.00
0.00
3.05

SrO
0.00
0.00
0.00
0.00
3.04
0.00

ZnO
4.33
0.00
0.00
0.00
0.00
0.00

Na₂O
0.04
0.04
0.04
0.05
0.03
0.03

K₂O
0.09
0.11
0.11
0.10
0.09
0.09

Li₂O
0.84
0.96
0.93
1.00
0.55
0.53

Fe₂O₃
0.23
0.37
0.38
0.37
0.26
0.25

TiO₂
0.49
0.56
0.57
0.55
0.58
0.58

Y₂O₃
0.00
4.45
4.94
4.64
4.51
4.49

La₂O₃
3.80
0.00
0.00
0.00
0.00
0.00

Cu₂O
0.00
0.00
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
4.15
3.44
3.43
3.45
3.69
3.74

MgO/CaO
102.58
1.63
1.37
1.63
3.78
8.09

CaO + MgO +
9.51
14.23
14.21
14.82
14.55
14.84

BaO + SrO

BaO + SrO + ZnO
4.33
0.00
0.00
0.00
3.04
3.05

T_L(° C.)
1371
1188
1185
1188
1317
1327

T_F(° C.)
1398
1319
1320
1307
1381
1378

ΔT (° C.)
27
131
135
119
64
51

T_m(° C.)
1625
1522
1521
1508
1590
1587

Fiber Density

2.61
2.62
2.62
2.61

(g/cm³)

Fiber Modulus

92.3
91.9
92.0
90.5

(GPa)

Fiber Strength

5490
5467
5492

(MPa)

Fiber Failure Strain (%)

5.9
5.9
6.0

Specific Fiber

3.6
3.6
3.6
3.46

Modulus (×10⁶m)

Specific Fiber

215.0
213.2
214.2

Strength (×10³m)

142
143
144
145
146
147

SiO₂
64.01
64.00
61.28
61.28
60.18
60.18

Al₂O₃
17.34
17.37
17.87
17.87
16.77
16.77

CaO
0.09
0.09
6.01
6.01
7.18
7.18

MgO
9.28
9.28
6.29
6.29
8.05
8.05

BaO
0.00
3.20
0.00
0.00
0.00
0.00

SrO
3.23
0.00
0.00
0.00
0.00
0.00

ZnO
0.00
0.00
0.00
0.00
0.00
0.00

Na₂O
0.03
0.03
0.04
0.04
0.04
0.04

K₂O
0.09
0.09
0.11
0.11
0.10
0.10

Li₂O
0.57
0.56
0.93
0.93
1.01
1.01

Fe₂O₃
0.26
0.26
0.38
0.38
0.37
0.37

TiO₂
0.60
0.60
2.13
0.56
1.36
0.56

Y₂O₃
4.51
4.51
4.96
4.96
4.93
4.93

La₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Cu₂O
0.00
0.00
0.00
1.57
0.00
0.80

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
3.69
3.68
3.43
3.43
3.59
3.59

MgO/CaO
104.76
104.83
1.05
1.05
1.12
1.12

CaO + MgO +
12.60
12.57
12.29
12.29
15.24
15.24

BaO + SrO

BaO + SrO + ZnO
3.23
3.20
0.00
0.00
0.00
0.00

T_L(° C.)
1348
1347
1208
1153
1154
1167

T_F(° C.)
1415
1428
1338
1336
1294
1291

ΔT (° C.)
67
81
130
183
140
124

T_m(° C.)
1633
1648
1549
1547
1493
1447

Fiber Density
2.57

2.61
2.62

(g/cm³)

Fiber Modulus
89.99

90.0
91.1

(GPa)

Fiber Strength

5321

(MPa)

Fiber Failure Strain (%)

5.8

Specific Fiber
3.50

3.5
3.5

Modulus (×10⁶m)

Specific Fiber

0.0
207.0

Strength (×10³m)

148
149
150
151
152
153

SiO₂
60.83
61.00
60.12
59.78
60.07
64.01

Al₂O₃
15.23
16.75
17.84
17.99
17.52
13.57

CaO
7.90
4.67
5.88
5.93
5.92
5.34

MgO
8.86
10.20
9.47
9.55
9.63
10.55

BaO
0.00
0.00
0.00
0.00
0.00
0.00

SrO
0.00
2.46
0.00
0.00
0.00
0.00

ZnO
0.00
0.00
0.00
0.00
0.00
0.00

Na₂O
0.04
0.04
0.04
0.04
0.04
0.03

K₂O
0.09
0.10
0.10
0.10
0.10
0.08

Li₂O
0.77
0.72
0.77
0.78
0.91
0.51

Fe₂O₃
0.37
0.25
0.39
0.40
0.37
0.22

TiO₂
1.41
0.55
0.59
0.59
0.56
0.46

Y₂O₃
4.50
3.25
4.80
4.84
4.87
5.23

La₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Cu₂O
0.00
0.00
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
0.00
0.00
0.00
0.00
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
3.99
3.64
3.37
3.32
3.43
4.72

MgO/CaO
1.12
2.19
1.61
1.61
1.63
1.98

CaO + MgO +
16.76
17.33
15.35
15.48
15.55
15.90

BaO + SrO

BaO + SrO + ZnO
0.00
2.46
0.00
0.00
0.00
0.00

T_L(° C.)
1219
1235
1226
1201
1200
1352

T_F(° C.)
1289
1320
1307
1299
1297
1347

ΔT (° C.)
70
85
81
98
97
−5

T_m(° C.)
1491
1519
1501
1493
1494
1552

Fiber Density
2.64
2.63

2.63
2.62

(g/cm³)

Fiber Modulus
91.8
92.6

92.8
85.2

(GPa)

Fiber Strength
5243
5583

5340

(MPa)

Fiber Failure Strain (%)
5.7
6.03

5.8

Specific Fiber
3.5
3.6

3.6

Modulus (×10⁶m)

Specific Fiber
202.5
216.6

207.0

Strength (×10³m)

154
155
156
157
158
159

SiO₂
60.61
58.73
59.81
62.19
64.78
63.74

Al₂O₃
15.26
14.78
15.06
15.66
16.31
16.05

CaO
7.01
4.75
0.06
0.03
0.03
0.03

MgO
5.49
5.29
6.07
2.38
2.48
2.44

BaO
0.00
0.00
0.00
0.00
0.00
0.00

SrO
0.00
0.00
0.00
0.00
0.00
0.00

ZnO
0.00
0.00
0.00
0.00
0.00
0.00

Na₂O
0.04
0.04
0.04
0.04
0.04
0.04

K₂O
0.09
0.09
0.08
0.09
0.09
0.09

Li₂O
0.83
0.81
0.82
0.86
0.89
0.88

Fe₂O₃
0.22
0.21
0.21
0.21
0.22
0.22

TiO₂
2.00
7.11
6.50
6.76
7.04
6.93

Y₂O₃
3.89
3.77
3.84
4.00
0.00
1.61

La₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

Cu₂O
0.00
0.00
0.00
0.00
0.00
0.00

MnO
0.00
0.00
0.00
0.00
0.00
0.00

MnO₂
4.55
4.41
7.49
7.79
8.12
7.99

B₂O₃
0.00
0.00
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
3.97
3.97
3.97
3.97
3.97
3.97

MgO/CaO
0.78
1.11
99.34
86.24
86.24
86.24

CaO + MgO +
12.50
10.05
6.14
2.41
2.51
2.47

BaO + SrO

BaO + SrO + ZnO
0.00
0.00
0.00
0.00
0.00
0.00

T_L(° C.)
1232
1350
1342
1356
1339
1347

T_F(° C.)
1362
1341
1321
1405
1444
1428

ΔT (° C.)
130
−9
−21
49
105
81

T_m(° C.)
1600
1579
1538
1645
1694
1677

Fiber Density
2.62
2.63
2.58
2.50
2.53

(g/cm³)

Fiber Modulus
85.4
88.9
85.4
82.9
83.9

(GPa)

Fiber Strength

(MPa)

Fiber Failure Strain (%)

Specific Fiber

Modulus (×10⁶m)

Specific Fiber

Strength (×10³m)

160
161
162
163

SiO₂
63.40
69.97
63.25
60.85

Al₂O₃
14.65
16.98
22.00
15.16

CaO
0.03
2.11
0.06
1.52

MgO
2.78
3.82
6.77
0.05

BaO
0.00
0.00
0.00
0.00

SrO
0.00
0.00
0.00
0.00

ZnO
0.00
0.00
0.00
0.00

Na₂O
0.02
0.03
0.02
0.04

K₂O
0.07
0.09
0.11
0.09

Li₂O
0.00
0.54
0.00
0.79

Fe₂O₃
0.23
0.25
0.34
0.21

TiO₂
7.89
3.40
5.33
8.29

Y₂O₃
1.83
0.94
0.00
5.07

La₂O₃
0.00
0.00
0.00
0.00

Cu₂O
0.00
0.00
0.00
0.00

MnO
0.00
0.00
2.11
7.95

MnO₂
9.11
1.86
0.00
0.00

B₂O₃
0.00
0.00
0.00
0.00

SO₃
0.00
0.00
0.00
0.00

TOTAL
100.00
100.00
100.00
100.00

SiO₂/Al₂O₃
4.33
4.12
2.87
4.01

MgO/CaO
110.30
1.81
109.95
0.03

CaO + MgO +
2.81
5.94
6.83
1.56

BaO + SrO

BaO + SrO + ZnO
0.00
0.00
0.00
0.00

T_L(° C.)
1456
1387
1389
1392

T_F(° C.)
1450
1547
1426
1385

ΔT (° C.)
−6
160
37
−7

T_m(° C.)
1684
1812
1646
1626

Fiber Density
2.44
2.55

(g/cm³)

Fiber Modulus
83.3
83.9

(GPa)

Fiber Strength

(MPa)

Fiber Failure Strain (%)

Specific Fiber

Modulus (×10⁶m)

Specific Fiber

Strength (×10³m)

Desirable characteristics that can be exhibited by various but not necessarily all embodiments of the present invention can include, but are not limited to, the following: the provision of glass fibers, fiber glass strands, glass fiber fabrics, composites, and related products having a relatively low density; the provision of glass fibers, fiber glass strands, glass fiber fabrics, composites, and laminates having a relatively high tensile strength; the provision of glass fibers, fiber glass strands, glass fiber fabrics, composites, and related products having a relatively low density; the provision of glass fibers, fiber glass strands, glass fiber fabrics, composites, and laminates having a relatively high modulus; the provision of glass fibers, fiber glass strands, glass fiber fabrics, composites, and laminates having a relatively high elongation; the provision of glass fibers, fiber glass strands, glass fiber fabrics, prepregs, and other products useful for reinforcement applications; and others.

It is to be understood that the present description illustrates aspects of the invention relevant to a clear understanding of the invention. Certain aspects of the invention that would be apparent to those of ordinary skill in the art and that, therefore, would not facilitate a better understanding of the invention have not been presented in order to simplify the present description. Although the present invention has been described in connection with certain embodiments, the present invention is not limited to the particular embodiments disclosed, but is intended to cover modifications that are within the spirit and scope of the invention.

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Number	Date	Country
103781736	May 2014	CN
20 2007 01087	Oct 2007	DE
202007010874	Oct 2007	DE
2 233 643	Jan 1991	GB
58-064243	Apr 1983	JP
58-167444	Oct 1983	JP
3-228849	Oct 1991	JP
1366488	Jan 1988	SU
WO 2013036736	Mar 2013	WO
WO 2014062715	Apr 2014	WO
WO 2014062987	Apr 2014	WO

	Number	Date	Country
Parent	14325854	Jul 2014	US
Child	15019172		US

	Number	Date	Country
Parent	15019172	Feb 2016	US
Child	15385083		US

Glass compositions, fiberizable glass compositions, and glass fibers made therefrom

Information

Patent Number

Date Filed

Date Issued

Inventors

Examiners

Agents

CPC

Field of Search

CPC

International Classifications

Disclaimer

Abstract

Description

Claims

CROSS-REFERENCE TO RELATED APPLICATIONS

US Referenced Citations (28)

Foreign Referenced Citations (11)

Non-Patent Literature Citations (9)

Related Publications (1)

Provisional Applications (1)

Continuations (1)

Continuation in Parts (1)

Entry
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