The present disclosure relates to transparent articles, and more particularly to methods of making transparent articles such as impact resistant windows for aircraft.
Armor is commonly used in vehicles to provide protection against projectiles. In applications where transparency is desired, such as in windows, glass and ceramic materials are typically employed due to the strength, hardness, and the fracture toughness of such materials.
Glass materials can provide effective impact resistance to relatively light projectiles, particularly those projectiles which fall into the category of ball rounds. For impact resistance to large caliber projectiles it is generally necessary to thicken the glass armor structures—commonly to thicknesses of five centimeters and greater—based on the level of protection desired. Such thickness can be prohibitive in aircraft due to the associated weight. In addition, commonly used silicate glasses lack sufficient hardness to defeat armor piercing projectiles.
Ceramic materials, like sapphire and spinel, can provide greater impact resistance than glass materials for a given thickness and weight. This is due to greater strength, hardness and fracture toughness of certain ceramics in comparison to glass. For these same reasons, however, ceramics can be difficult to work into curved or complex shapes of size necessary for transparent articles in aircraft. Suitable ceramics, by nature of their manufacturing, typically requiring slow and/or prohibitively expensive grinding and polishing of all major faces.
Such conventional material and structures have generally been considered satisfactory for their intended purpose. However, there is still a need in the art for improved compositions for transparent armor structures. The present disclosure provides a solution for this need.
A method of making a transparent article includes mixing an oxygen source, a nitrogen source, a magnesium source, a silicon source, and a calcium source. The oxygen source, nitrogen source, magnesium source, silicon source, and calcium source are then heated to form a molten oxynitride glass modified by calcium and magnesium. The molten oxynitride glass is thereafter cooled to form a transparent body having ballistic resistance such that armor piercing test ammunition having a bullet mass of 166 grains fired from a barrel having a 22 inch length and traveling at a velocity of about 2850 feet per second does not penetrate the transparent body when tested in compliance with Level IV of National Institute of Justice Standard 0108.01, September 1985
In certain embodiments, the magnesium source can exclude magnesium hydride. The magnesium source can also exclude magnesium oxide. The magnesium source can include magnesium nitride. The magnesium source can consist essentially of magnesium nitride. The magnesium source can include magnesium oxide. The magnesium source can consist essentially of magnesium oxide. The magnesium source can include both magnesium nitride and magnesium oxide. The magnesium source can consist essentially of magnesium nitride and magnesium oxide.
In accordance with certain embodiments, the nitrogen source can primarily include calcium nitride. The silicon source can be a supplemental nitrogen source, such as silicon nitride. The magnesium source can be a supplemental nitrogen source. Milling the sources can include ball or rod milling the sources. Milling the sources can include anhydrously milling the oxygen, nitrogen, magnesium and calcium sources. Heating the milled sources can include heating the sources in an unpressurized inert atmosphere. It is contemplated that the milled sources can be heated in a nitrogen atmosphere having a pressure of about 1 atmosphere.
It is contemplated that, in accordance with certain embodiments, the oxygen source, nitrogen source, magnesium source, silicon source, and calcium source are milled. Heating the article can include heating the article to between about 1600 and 1700 degrees Celsius. The re-heated article can be shaped by slumping the re-heated article over an arcuate surface of a mandrel. Re-heating the article can include re-heating the article to between about 800 and 1000 degrees Celsius.
A transparent article includes a transparent body formed from oxynitride glass. The oxynitride glass includes magnesium and calcium modifying the oxynitride glass. The transparent body has ballistic resistance such that armor piercing test ammunition having a bullet mass of 166 grains fired from a barrel having a 22 inch length and traveling at a velocity of about 2850 feet per second does not penetrate the transparent body when tested in compliance with Level IV of National Institute of Justice Standard 0108.01, September 1985
In certain embodiments, the oxynitride glass can include selected amounts of calcium, magnesium, silicon, oxygen, and nitrogen. The oxynitride glass can consist essentially of calcium, magnesium, silicon, oxygen, and nitrogen. The oxynitride glass can contain magnesium and calcium in an aggregated atomic percent between about 10 and about 55 atomic percent. The oxynitride glass can contain about 30 to 50 atomic percent oxygen, 10 to 30 atomic percent nitrogen, 10 to 30 atomic percent silicon, substantially none to 25 atomic percent magnesium, and 10 to 30 atomic percent calcium.
Preferably, the oxynitride glass can have about 30 to 50 atomic percent oxygen, 15 to 25 atomic percent nitrogen, 19 to 23 atomic percent silicon, 2 to 10 atomic percent magnesium, and 14 to 20 atomic percent calcium. Most preferably, the oxynitride glass can contain between about 36 to 39 atomic percent oxygen, 17 to 19 atomic percent nitrogen, about 21 atomic percent silicon, about 5.5 atomic percent magnesium, and about 17.5 atomic percent calcium.
In accordance with certain embodiments, the transparent body can have a strike face and an opposed backing face. Either or both of the strike face and the backing face can be an as-melted surface. Either or both the strike face and the backing face can be an unpolished surface. Either or both the strike face and the backing face can be polished.
It is contemplated that the transparent body can have a profile bounded by an arcuate segment. An as-melted surface can define at least a portion of the arcuate segment. An unpolished surface can define at least a portion of the arcuate segment. An unground, polished surface can define at least a portion of the arcuate segment. The profile can be bounded by unground and ground surface segments. The transparent body can be dimensioned as a window, a screen, a canopy, or a dome.
These and other features of the systems and methods of the subject disclosure will become more readily apparent to those skilled in the art from the following detailed description of the preferred embodiments taken in conjunction with the drawings.
So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, embodiments thereof will be described in detail herein below with reference to certain figures, wherein:
Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of a transparent article in accordance with the disclosure is shown in
As used herein the term transparent armor means transmitting light without appreciable scattering in a manner such as ordinary window glass so that objects placed behind the transparent armor are clearly distinguishable. As also used herein the term “suitably sized” means having a monolithic size approximating that of an aircraft windscreen. As additionally used herein, the term “dimensioned” means having, as an unworked blank, length, width, and thickness approximate that of an aircraft windscreen. In certain embodiments the windscreen dimensioning is according to those of windscreens in Supplemental Type Certificate SR01340AT, issued by the FAA to Aeronautical Accessories Incorporated on Apr. 16, 1997, the contents of which is incorporated herein by reference in its entirety.
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In certain embodiments, transparent article 100 has a thickness 116, weight 118, and dimensioning 120 which render transparent article suitable for use as transparent armor in a rotorcraft. For example, thickness 116 can be within a range of about 0.75 inches to about 1 inch. Weight 118 can be on the order of about 12 pounds to about 13 pounds. Dimensioning 120 can be such that transparent article 100 conforms to a conventional aircraft structure, such as a rotorcraft polycarbonate windscreen by way of non-limiting example. For example, in certain embodiments, transparent article 100 can have a surface area that is between about one (1) square foot and about 24 square feet. In accordance with certain embodiments, the surface of transparent article 100 can be planar.
It is contemplated that the surface of transparent article 100 can be curved or arcuate. Curvature of transparent article 100 can be simple or compound, as suitable for an intended application. Transparent article 100 can also be singular, i.e., comprising only one transparent body 102. It is also contemplated that transparent article 100 can be composite, i.e., comprising two or more transparent bodies stacked together. As will be appreciated by those of skill in the art, stacking transparent article 100 with one or more second transparent article 100 as a composite can provide increased impact protection.
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Lattice structure 128 also includes magnesium 110 in an atomic percent magnesium D and calcium 112 in an atomic percent calcium E. Cations of magnesium 110 and calcium 112 modify the network (i.e. lattice 128) otherwise formed by silicon 122, oxygen 124, and nitrogen 126. In this respect, magnesium 110 and calcium 112 distort lattice structure 128, modifying oxynitride glass 104 such that lattice structure 128 is less dense. In certain embodiments, oxynitride glass 104 is less dense without appreciable detriment of the mechanical properties of oxynitride glass 104 which influence ballistic resistance 114 (shown in
Oxynitride glass 104 includes silicon 122 in a silicon amount A between about 10 to 30 atomic percent silicon. In certain embodiments, oxynitride glass 104 includes silicon 122 in a silicon amount A between about 19 to 23 atomic percent silicon. In an illustrative exemplary embodiment, oxynitride glass 104 includes silicon 122 in a silicon amount A that is about 21 atomic percent silicon.
Oxynitride glass 104 includes oxygen 124 in an oxygen amount B between about 30 to 50 atomic percent oxygen. In certain embodiments, oxynitride glass 104 includes oxygen 124 in an oxygen amount B between about 35 to 40 atomic percent oxygen. In an illustrative exemplary embodiment, oxynitride glass 104 includes oxygen 124 in an oxygen amount B between about 36 to 39 atomic percent oxygen.
Oxynitride glass 104 includes nitrogen 126 in a nitrogen amount C between about 10 to 30 atomic percent nitrogen. In certain embodiments, oxynitride glass 104 includes nitrogen 126 in a nitrogen amount C between about 15 to 25 atomic percent nitrogen. In the illustrative exemplary embodiment, oxynitride glass 104 includes nitrogen 126 in a nitrogen amount C between about 36 to 39 atomic percent nitrogen.
Oxynitride glass 104 includes substantially no magnesium, i.e. completely absent or in a trace amount, to a magnesium amount D of about 25 atomic percent magnesium. In certain embodiments, oxynitride glass 104 includes magnesium 110 in a magnesium amount D between about 2 to 10 atomic percent magnesium. In the illustrative exemplary embodiment, oxynitride glass 104 includes magnesium 110 in a magnesium amount D that is about is 5.5 atomic percent magnesium.
Oxynitride glass 104 includes calcium 112 in a calcium amount E between about 10 to 30 atomic percent calcium. In certain embodiments, oxynitride glass 104 includes calcium 112 in a calcium amount E between about 14 to 20 atomic percent calcium. In the illustrative exemplary embodiment, oxynitride glass 104 includes calcium 112 in a calcium amount E of about 15.5 atomic percent calcium.
Because of their size and light weight, magnesium cations 110 and calcium cations 112 reduce the density of oxynitride glass 104 as compared to unmodified oxynitride glass and oxynitride glass modified with rare earth elements. For that reason oxynitride glass 104 includes magnesium 110 and calcium 112 in a ratio that alters selected mechanical properties of modified oxynitride glass 104. For example, the ratio of magnesium 110 to calcium 112 can be selected to alter one or more of hardness, fracture toughness, strength, and/or density to influence ballistic resistance 114 (shown in
In certain embodiments, oxynitride glass 104 can include between about 10 to 30 atomic percent silicon, 30 to 50 atomic percent oxygen, 10 to 30 atomic percent nitrogen, 10 to 30 atomic percent magnesium, and 10 to 30 atomic percent calcium. Preferably, oxynitride glass 104 includes between about 19 to 23 atomic percent silicon, 35 to 40 atomic percent oxygen, 15 to 25 atomic percent nitrogen, 2 to 10 atomic percent magnesium, and 14 to 20 atomic percent calcium. Most preferably, oxynitride glass 104 includes about 21 atomic percent silicon, 36 to 39 atomic percent oxygen, 17 to 19 atomic percent nitrogen, about 5.5 percent magnesium, and about 17.5 atomic percent calcium. Transparent articles, e.g., transparent article 100 (shown in
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As will be appreciated by those of skill in the art, while generally satisfactory as a source of magnesium, MgH is pyrophoric. Specifically, MgH liberates hydrogen during decomposition. The liberated hydrogen is extremely flammable, which can complicate the glass-making process, and in the case of oxynitride glasses, can make the fabrication of transparent bodies of suitable size and transparency for use as certain types of articles—such as transparent armor. For that reason magnesium source 604, in accordance with certain embodiments, excludes MgH.
For example, in an embodiment B, magnesium source 604 excludes MgH and includes MgO. MgO has the advantage that the oxygen generated from the decomposition of MgO is relatively inert compared to hydrogen, which simplifies the manufacture of oxynitride glass 104 (shown in
Alternatively, in an embodiment C, magnesium source 604 excludes MgH and includes MgCOx. MgCOx similarly has the advantage that the decomposition products generated from the decomposition of MgCOx are more inert than hydrogen and can include less oxygen than MgO, which simplifies the manufacture of oxynitride glass 104 (shown in
In a further embodiment D magnesium source 604 includes MgN. As with MgO and MgCOx, use of MgN has the advantage that the decomposition products arising from the decomposition of MgN, i.e., nitrogen, are inert. Accordingly, use of MgN as a source of magnesium simplifies the manufacture of oxynitride glass 104 (shown in
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Heating operation 630 can include heating sources 604-609 in an inert atmosphere, such as a nitrogen atmosphere. Heating under an inert atmosphere can prevent the incorporation of contaminants into molten composition 611, such as elemental oxides. As will be appreciated by those of skill in the art in view of the present disclosure, reducing (or eliminating) contaminant incorporation allows transparent body 102 (shown in
In accordance with certain embodiments, heating operation 630 can include heating sources 604-609 in an inert vessel 20, such as a niobium vessel. Inert vessel 20 can also reduce (or eliminate entirely) incorporation of contamination into molten composition 611. It is to be understood and appreciated that suitably inert vessels can also be constructed from tantalum, molybdenum and/or boron nitride, as suitable for a contemplated application.
In certain embodiments, heating operation 630 can include harvesting magnesium liberated from magnesium source 604 (shown in
In certain embodiments heating operation 630 includes heating furnace 16 to a temperature between about 1550 and 1750 degrees Celsius for a predetermined time period. In accordance with certain embodiments heating operation 630 includes heating furnace 16 to a temperature between about 1625 and about 1725 degrees Celsius for predetermined time period. It is contemplated that heating operation 630 can include heating oxynitride glass 104 to a temperature of between about 1600 and 1700 degrees Celsius. In an exemplary illustrative embodiment heating operation 630 includes heating furnace 16 to about 1675 degrees Celsius for a predetermined time period of about two (2) hours. Due to the relative stability of magnesium nitride, embodiments utilizing magnesium nitride as a source of magnesium allow for heating at relatively low pressure, e.g., at around one (1) atmosphere, simplifying the heating operation.
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Transparent ceramic armor materials with hardness sufficient to defeat armor piercing projectiles have traditionally been limited to materials like spinel and sapphire. While satisfactory for their intended purpose such materials are relatively expensive and difficult to form into structures suitable for armor, such as for aircraft windscreens, covers, and windows.
In embodiments described, oxynitride glass modified with magnesium and calcium are disclosed. While of suitable hardness and density for use as armor, structures of suitable transparency, size, and dimensions have not been available due to the difficulty in manufacturing structures formed from oxynitride glass. Applicant has found that oxynitride structures of suitable transparency, dimensions, and size can be obtained through the selection of the oxynitride glass constituent sources. In this respect, Applicant has demonstrated the ability to fabricate high-hardness oxynitride glass with transparency, size, and dimensions through the use of magnesium and calcium hydride materials, mixed with silicon dioxide, and heated within a nitrogen atmosphere can provide network modifying nitrides (CaN and MgN) that avoid the challenges of adding nitrogen via silicon nitride, which tends to opacify the glass. Applicant has also found that the provision of magnesium to the glass development process through a high surface area provided synthetic magnesium silicate can simplify the fabrication process, through reduction (or elimination entirely) of elemental hydrogen during the glass-making process, and that oxynitride structures of suitable transparency, size and dimension for transparent armor can be formed.
In certain embodiments, the oxynitride glass modified with calcium and magnesium is amenable to re-heating to semi-molten state from the glass material and can be shaped (e.g., curved), reducing the amount of diamond grinding required to produce structures with similar shape formed from materials with high hardness (e.g., spinel, sapphire, etc.). In accordance with certain embodiments the glass materials have relatively few (if any) grain boundaries, reducing the variation in mechanical properties otherwise associated with the grain boundaries present in other high hardness glass materials, e.g., spinel and aluminum oxynitride materials. It is also contemplated that the glass material can be formed using a less volatile, low cost, and readily available synthetic magnesium silicate, simplifying fabrication of transparent article from the modified oxynitride glass constituent element sources.
The methods and systems of the present disclosure, as described above and shown in the drawings, provide for transparent articles with superior properties including transparency, size, and dimensioning suitable for use as transparent armor on aircraft. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the scope of the subject disclosure.