Field of the Technology
The present disclosure is directed to thread rolling dies used for producing threads on one machine component in order to fasten it to another machine component, and to methods of manufacturing thread rolling dies. More specifically, the disclosure is directed to thread rolling dies comprising sintered cemented carbide thread rolling regions, and to methods of making the thread rolling dies.
Description of the Background of the Technology
Threads are commonly used as a means of fastening one machine component to another. Machining techniques such as turning, using single point or form tools, and grinding, using single contact or form wheels, are employed as metal removal methods to create the desired thread geometry in a workpiece. These methods are commonly referred to as thread cutting methods.
Thread cutting techniques suffer from some inherent disadvantages. Thread cutting techniques are generally slow and costly, and require the use of expensive machine tools, including special tooling. The thread cutting techniques are not cost-effective for processing large production batches. Because thread cutting involves machining a blank, waste material in the form of cut chips is produced. Additionally, the finish of cut threads may be less than desirable.
An alternative method of forming threads in machine components involves the use of “chipless” metal forming techniques, i.e., thread forming techniques in which the workpiece is not cut and chips are not formed. An example of a chipless thread forming technique is the thread rolling technique. The thread rolling technique involves rolling threads onto a cylindrical metal component positioned between two or more thread rolling dies including a working surface having a mirror-image of the desired thread geometry. Traditionally, thread rolling dies may be circular or flat. The thread geometry is created on a workpiece as it is compressed between the dies and the dies move relative to one another. Circular thread rolling dies are rotated relative to one another. Flat thread rolling dies are moved in a linear or reciprocating fashion relative to one another. Thread rolling is therefore a method of cold forming, or moving rather than removing the workpiece material to form the threads. This is illustrated schematically in
Thread rolling offers several advantages over machining or cutting techniques for forming threads on a workpiece. For example, a significant amount of material may be saved from becoming waste because of the “chipless” nature of the thread rolling technique. Also, because thread rolling forms the threads by flowing the material upward and outward, the blank may be smaller than that required for when forming the threads by thread cutting, resulting in additional material savings. In addition, thread rolling can produce threads and related forms at high threading speeds and with longer comparable tool life. Therefore, thread rolling is a viable technique for high volume production. Thread rolling also is cold forming technique in which there is no abrasive wear, and the thread rolling dies can operate throughout their useful life without the need for periodic sizing.
Thread rolling also results in a significant increase in the hardness and yield strength of the material in the thread region of the workpiece due to work hardening caused by the compressive forces exerted during the thread rolling operation. Thread rolling can produce threads that are, for example, up to 20% stronger than cut threads. Rolled threads also exhibit reduced notch sensitivity and improved fatigue resistance. Thread rolling, which is a cold forming technique, also typically results in threads having excellent microstructure, a smooth mirror surface finish, and improved grain structure for higher strength.
Advantages of thread rolling over thread cutting are illustrated schematically in
Conventional thread rolling dies are typically made from high speed steels as well as other tool steels. Thread rolling dies made from steels have several limitations. The compressive strength of high speed steels and tool steels may not be significantly higher than the compressive strength of common workpiece materials such as alloy steels and other structural alloys. In fact, the compressive strength of conventional thread rolling die materials may be lower than the compressive strength of high strength workpiece materials such as, for example, nickel-base and titanium-base aerospace alloys and certain corrosion resistant alloys. In general, the compressive yield strength of tool steels used to make thread rolling dies falls bellow about 275,000 psi. When the compressive strength of the thread rolling die material does not substantially exceed the compressive strength of the workpiece material, the die is subject to excessive plastic deformation and premature failure.
In addition to having relatively high compressive strength, thread rolling die materials should possess substantially greater stiffness than the workpiece material. In general, however, the high speed steels and tool steels that are currently used in thread rolling dies do not possess stiffness that is higher than common workpiece materials. The stiffness (i.e., Young's Modulus) of these tool steels falls below about 32×106 psi. Thread rolling dies made from these high speed steels and tool steels may undergo excessive elastic deformation during the thread rolling process, making it difficult to hold close tolerances on the thread geometry.
In addition, thread rolling dies made from high speed steels and tool steels can be expected to exhibit only modestly higher wear resistance compared to many common workpiece materials. For example, the abrasion wear volume of certain tool steels used in thread rolling dies, measured as per ASTM G65-04, “Standard Test Method for Measuring Abrasion Using the Dry Sand/Rubber Wheel Apparatus”, is about 100 mm3. Therefore, die lifetime may be limited due to excessive wear.
Accordingly, there is a need for thread rolling dies made from materials that exhibit superior combinations of strength, particularly compressive strength, stiffness, and wear resistance compared to high speed and other tool steels conventionally used in thread rolling dies. Such materials would provide increased die service life and also may allow the dies to be used to produce threads on workpiece materials that cannot readily be processed using conventional dies.
In a non-limiting embodiment according to the present disclosure, a thread rolling die comprises a thread rolling region including a working surface comprising a thread form. The thread rolling region comprises a sintered cemented carbide material having a hardness in the range of 78 HRA to 89 HRA.
In another non-limiting embodiment according to the present disclosure, a thread rolling die comprises a thread rolling region including a working surface comprising a thread form, wherein the thread rolling region includes a sintered cemented carbide material having at least one of a compressive yield strength of at least 400,000 psi; a Young's modulus in the range of 50×106 psi to 80×106 psi; an abrasion wear volume in the range of 5 mm3 to 30 mm3 evaluated according to ASTM G65-04; a fracture toughness of at least 15 ksi·in1/2; and a transverse rupture strength of at least 300 ksi.
In yet another non-limiting embodiment according to this disclosure, a thread rolling die comprises a thread rolling region including a working surface comprising a thread form, wherein at least the working surface of the thread rolling region comprises a sintered cemented carbide material. In certain non-limiting embodiments, the thread rolling die includes at least one non-cemented carbide piece metallurgically bonded to the thread rolling region in an area of the thread rolling region that does not prevent the working surface from contacting a workpiece. In certain non-limiting embodiments, the non-cemented carbide piece comprises at least one of a metallic region and a metal matrix composite region.
In yet another non-limiting embodiment according to the present disclosure, a thread rolling die comprises a thread rolling region including a working surface comprising a thread form, and a non-cemented carbide piece metallurgically bonded to the thread rolling region, wherein at least the working surface of the thread rolling region comprises a sintered cemented carbide material having at least one of a compressive yield strength of at least 400,000 psi; a Young's modulus in the range of 50×106 psi to 80×106 psi; an abrasion wear volume in the range of 5 mm3 to 30 mm3 evaluated according to ASTM G65-04; a hardness in the range of 78 HRA to 89 HRA; a fracture toughness of at least 15 ksi·in1/2; and a transverse rupture strength of at least 300 ksi.
The features and advantages of articles and methods described herein may be better understood by reference to the accompanying drawings in which:
The reader will appreciate the foregoing details, as well as others, upon considering the following detailed description of certain non-limiting embodiments according to the present disclosure.
In the present description of non-limiting embodiments, other than in the operating examples or where otherwise indicated, all numbers expressing quantities or characteristics are to be understood as being modified in all instances by the term “about”. Accordingly, unless indicated to the contrary, any numerical parameters set forth in the following description are approximations that may vary depending on the desired properties one seeks to obtain in the articles and methods according to the present disclosure. 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 described in the present description should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques.
Any patent, publication, or other disclosure material, in whole or in part, that is said to be incorporated by reference herein is incorporated herein only to the extent that the incorporated material does not conflict with existing definitions, statements, or other disclosure material set forth in this disclosure. As such, and to the extent necessary, the disclosure as set forth herein supersedes any conflicting material incorporated herein by reference. Any material, or portion thereof, that is said to be incorporated by reference herein, but which conflicts with existing definitions, statements, or other disclosure material set forth herein is only incorporated to the extent that no conflict arises between that incorporated material and the existing disclosure material.
One non-limiting embodiment of a circular thread rolling die 10 according to the present disclosure is depicted in
In a non-limiting embodiment, the sintered cemented carbide material of the thread rolling region 12 may have a compressive yield strength of at least 400,000 psi. In another non-limiting embodiment, the sintered cemented carbide material of the thread rolling region 12 may have a Young's modulus of at least 50×106 psi. A non-limiting embodiment of the thread rolling die 10 comprises a sintered cemented carbide thread rolling region 12, wherein the sintered cemented carbide material has a Young's modulus in the range of 50×106 psi to 80×106 psi. In still another non-limiting embodiment, the sintered cemented carbide material of the thread rolling region 12 may have an abrasion wear volume no greater than 30 mm3 as evaluated according to ASTM G65-04. In one non-limiting embodiment, the sintered cemented carbide material of the thread rolling region 12 has an abrasion wear volume in the range of 5 mm3 to 30 mm3 as evaluated according to ASTM G65-04.
According to one non-limiting embodiment of a thread rolling die 10, 30 according to the present disclosure, the sintered cemented carbide material of the thread rolling region 12 may have a combination of properties including a compressive yield strength of at least 400,000 psi; a Young's modulus of at least 50×106 psi; and an abrasion wear volume no greater than 30 mm3 evaluated according to ASTM G65-04. In another non-limiting embodiment, the sintered cemented carbide material of the thread rolling region 12 may have a fracture toughness of at least 15 ksi·in1/2. In still another non-limiting embodiment, the sintered cemented carbide material of the thread rolling region 12 may have a transverse rupture strength of at least 300 ksi.
According to certain other non-limiting embodiments, the sintered cemented carbide material of the thread rolling region 12 of thread rolling dies 10, 30 has one or more of a compressive yield strength of at least 400,000 psi; a Young's modulus in the range of 50×106 psi to 80×106 psi; an abrasion wear volume in the range of 5 mm3 to 30 mm3 as evaluated according to ASTM G65-04; a hardness in the range of 78 HRA to 89 HRA; a fracture toughness of at least 15 ksi·in1/2; and a transverse rupture strength of at least 300 ksi.
According to certain non-limiting embodiments according to the present disclosure, the thread form 16 of the working surface 14 of thread rolling dies 10, 30 may include one of V-type threads, Acme threads, Knuckle threads, and Buttress threads. It will be understood, however, that such thread form patterns are not exhaustive and that any suitable thread form known now or here hereafter to a person skilled in the art may be included on a thread rolling die according to the present disclosure.
In certain non-limiting embodiments, sintered cemented carbide included in the thread rolling region and, optionally, sintered cemented carbide material included in other regions of the thread rolling dies according to the present disclosure are made using conventional powder metallurgy techniques. Such techniques include, for example: mechanically or isostatically pressing a blend of metal powders to form a “green” part having a desired shape and size; optionally, heat treating or “presintering” the green part at a temperature in the range of 400° C. to 1200° C. to provide a “brown” part; optionally, machining the part in the green or brown state to impart certain desired shape features; and heating the part at a sintering temperature, for example, in the range of 1350° C. to 1600° C. Other techniques and sequences of steps for providing sintered cemented carbide material will be evident to those having ordinary skill in the art. In appropriate circumstances, one or more of such other techniques may be used to provide sintered cemented carbide material included in thread rolling dies according to the present disclosure, and it will become evident to those having ordinary skill, upon reading the present disclosure, how to adapt such one or more techniques for use in providing the present thread rolling dies.
In certain non-limiting embodiments of thread rolling dies according to the present disclosure, sintered cemented carbide material included in the thread rolling dies according to the present disclosure may be finish-machined using operations such, for example, turning, milling, grinding, and electro-discharge machining. Also, in certain non-limiting embodiments of thread rolling dies according to the present disclosure, finish-machined material included in the thread rolling dies may be coated with materials providing wear resistance and/or other advantageous characteristics. Such coatings may be applied using conventional coating techniques such as, for example, chemical vapor deposition (CVD) and/or physical vapor deposition (PVD). Non-limiting examples of wear resistant materials that may be provided as a coating on all or a region of cemented carbide materials included in thread rolling dies according to the present disclosure include Al2O3, TiC, Ti(C,N), either in single layers or in combinations of multiple layers. Other possible materials that may be provided as coatings on cemented carbide materials, either as a single-layer or as part of a multiple-layer coating, included in thread rolling dies according to the present disclosure will be known to those having ordinary skill and are encompassed herein.
In certain non-limiting embodiments, cemented carbide material included in the thread rolling region of thread rolling dies according to the present disclosure includes a discontinuous, dispersed phase and a continuous binder phase. The discontinuous, dispersed phase includes hard particles of a carbide compound of at least one metal selected from Groups IVB, a Group VB, or a Group VIB of the Periodic Table. Such metals include, for example, titanium, zirconium, hafnium, vanadium, niobium, tantalum, chromium, molybdenum, and tungsten. The continuous binder phase comprises one or more of cobalt, a cobalt alloy, nickel, a nickel alloy, iron, and an iron alloy. In certain non-limiting embodiments, the sintered cemented carbide material included in the thread rolling region comprises 60 weight percent up to 98 weight percent of the dispersed phase and 2 weight percent to 40 weight percent of the continuous binder phase. According to certain non-limiting embodiment, hard carbide particles of the dispersed phase have an average grain size in the range of 0.3 μm to 20 μm.
In a non-limiting embodiment, the continuous binder phase of sintered cemented carbide material included in the thread rolling region of a thread rolling die according to the present disclosure comprises at least one additive selected from tungsten, chromium, titanium, vanadium, niobium and carbon in a concentration up to the solubility limit of the additive in the continuous binder phase. In certain non-limiting embodiments, the continuous binder phase of sintered cemented carbide material in the thread rolling region comprises at least one additive selected from silicon, boron, aluminum copper, ruthenium, and manganese in a total concentration of up to 5% by weight, based on the total weight of the continuous binder phase.
In certain non-limiting embodiments of thread rolling dies according to the present disclosure, the working surface of the thread rolling region comprises sintered cemented carbide material having a surface hardness in the range of 78 HRA to 89 HRA. Grades of sintered cemented having this particular surface hardness include, but are not limited to, grades including a dispersed, discontinuous phase including tungsten carbide particles and a continuous binder phase comprising cobalt. Various commercially available powder blends used to produce grades of sintered cemented carbide materials are known to those of ordinary skill and may be obtained from various sources such as, for example, ATI Engineered Products, Grant, Ala., USA. Non-limiting examples of commercially available cemented carbide grades that may be used in various embodiments of thread rolling dies according to the present disclosure include ATI Firth Grades FL10, FL15, FL20, FL25, FL30, FL35, H20, H25, ND20, ND25, ND30, H71, R52, and R61. The various cemented carbide grades typically differ in one or more of carbide particle composition, carbide particle grain size, binder phase volume fraction, and binder phase composition, and these variations influence the final physical and mechanical properties of the sintered cemented carbide material.
Again referring to the schematic illustration of
In a non-limiting embodiment of thread rolling die 40, the second layer 46 may comprise a cemented carbide grade with hardness less than the hardness of the working surface 44 layer in order to better transfer stresses experienced during the thread rolling operation, and minimize cracking of the sintered cemented carbide material at the working surface 44 and in the thread rolling region 42. Sintered cemented carbide layers 48, 50, 52 progressively decrease in hardness in order to transfer stresses from the relatively harder working surface 44, and thus avoid cracking of the sintered cemented carbide at the working surface 44 and in the thread rolling region 42. In is noted that in the non-limiting embodiment of a circular thread rolling die depicted in
In a non-limiting embodiment of a thread rolling die comprising a plurality of different grades of cemented carbide arranged in a layered fashion as depicted in
Certain non-limiting methods for producing articles comprising areas of sintered ceramic carbide materials having differing properties is described in U.S. Pat. No. 6,511,265, which is hereby incorporated by reference herein in its entirety. One such method includes placing a first metallurgical powder blend comprising hard particles and binder particles into a first region of a void of a mold. The mold may be, for example, a dry-bag rubber mold. A second metallurgical powder blend having a different composition comprising hard particles and binder particles is placed into a second region of the void of the mold. Depending on the number of regions of different cemented carbide materials desired in the thread rolling die, the mold may be partitioned into additional regions in which particular metallurgical powder blends are disposed. The mold may be segregated into such regions, for example, by placing physical partitions in the void of the mold to define the several regions. In certain embodiments the physical partition may be a fugitive partition, such as paper, that the partition decomposes and dissipates during the subsequent sintering step. The metallurgical powder blends are chosen to achieve the desired properties in the corresponding regions of the thread rolling die as described above. In certain embodiments, a portion of at least the first region and the second region and any other adjacent regions partitioned in the void of the mold are brought into contact with each other, and the materials within the mold are then isostatically compressed to densify the metallurgical powder blends and form a green compact of consolidated powders. The compact is then sintered to further densify the compact and to form an autogenous bond between the first, second, and, if present, any other regions. The sintered compact provides a blank that may be machined to particular desired thread rolling die geometry. Such geometries are known to those having ordinary skill in the art and are not specifically described herein.
In one non-limiting embodiment of a thread rolling die having a construction as depicted in
In one non-limiting embodiment of a thread rolling die according to the present disclosure, the thread rolling die includes a hybrid cemented carbide in which the binder concentration of the dispersed phase of the hybrid cemented carbide is 2 to 15 weight percent of the dispersed phase, and the binder concentration of the continuous binder phase of the hybrid cemented carbide is 6 to 30 weight percent of the continuous binder phase.
Hybrid cemented carbides included in certain non-limiting embodiments of articles according to the present disclosure may have relatively low contiguity ratios, thereby improving certain properties of the hybrid cemented carbides relative to other cemented carbides. Non-limiting examples of hybrid cemented carbides that may be used in embodiments of thread rolling dies according to the present disclosure are described in U.S. Pat. No. 7,384,443, which is hereby incorporated by reference herein in its entirety. Certain embodiments of hybrid cemented carbide composites that may be included in articles herein have a contiguity ratio of the dispersed phase that is no greater than 0.48. In some embodiments, the contiguity ratio of the dispersed phase of the hybrid cemented carbide may be less than 0.4, or less than 0.2. Methods of forming hybrid cemented carbides having relatively low contiguity ratios include, for example: partially or fully sintering granules of the dispersed grade of cemented carbide; blending these “presintered” granules with the unsintered or “green” second grade of cemented carbide powder; compacting the blend; and sintering the blend. Details of such a method are detailed in the incorporated U.S. Pat. No. 7,384,443 and, therefore, will be known to those having ordinary skill. A metallographic technique for measuring contiguity ratios is also detailed in the incorporated U.S. Pat. No. 7,384,443 and will be known to those having ordinary skill.
Referring now to
In yet another non-limiting embodiment of a thread rolling die according to the present disclosure, the metal matrix composite of the non-cemented carbide piece comprises at least one of hard particles and metallic particles bound together by a metallic matrix material, wherein the melting temperature of the metallic matrix material is less than a melting temperature of the hard particles and/or the metallic particles of the metal matrix composite.
In certain other non-limiting embodiments, a non-cemented carbide piece included in a non-working region 18 of a thread rolling die 10, 30 is a composite material including metal or metallic alloy grains, particles, and/or powder dispersed in a continuous metal or metallic alloy matrix composite. In certain non-limiting embodiments, a non-cemented carbide piece in a non-working region 18 comprises a composite material including particles or grains of a metallic material selected from tungsten, a tungsten alloy, tantalum, a tantalum alloy, molybdenum, a molybdenum alloy, niobium, a niobium alloy, titanium, a titanium alloy, nickel, a nickel alloy, cobalt, a cobalt alloy, iron, and an iron alloy. In one particular non-limiting embodiment, a non-cemented carbide piece in a non-working region 18 included in a thread rolling die 10, 30 according to the present disclosure comprises tungsten grains dispersed in a matrix of a metal or a metallic alloy.
Another non-limiting embodiment of a thread rolling die according to the present disclosure includes a metal matrix composite piece comprising hard particles. A non-limiting embodiment includes a non-cemented carbide piece comprising hard particles of at least one carbide of a metal selected from Groups IVB, VB, and VIB of the Periodic Table. In one non-limiting embodiment, the hard particles of the metal matrix composite comprise particles of at least one of carbides, oxides, nitrides, borides and silicides.
According to one non-limiting embodiment, the metal matrix material includes at least one of copper, a copper alloy, aluminum, an aluminum alloy, iron, an iron alloy, nickel, a nickel alloy, cobalt, a cobalt alloy, titanium, a titanium alloy, a bronze alloy, and a brass alloy. In one non-limiting embodiment, the metal matrix material is a bronze alloy consisting essentially of 78 weight percent copper, 10 weight percent nickel, 6 weight percent manganese, 6 weight percent tin, and incidental impurities. In another non-limiting embodiment, the metal matrix material consists essentially of 53 weight percent copper, 24 weight percent manganese, 15 weight percent nickel, 8 weight percent zinc, and incidental impurities. In non-limiting embodiments, the metal matrix material may include up to 10 weight percent of an element that will reduce the melting point of the metal matrix material, such as, but not limited to, at least one of boron, silicon, and chromium.
In certain embodiments, a non-cemented carbide piece included in a thread rolling die 10, 30 may be machined to include threads or other features so that the thread rolling die 10, 30 may be mechanically attached to a thread rolling machine (not shown).
As depicted in
According to one aspect of the present disclosure, a non-limiting method for forming a sintered cemented carbide thread rolling die that comprises a non-cemented carbide piece or region includes providing a sintered cemented carbide thread rolling region or sintered cemented carbide thread rolling die. Optionally, one or more non-cemented carbide pieces comprising a metal or metal alloy, as disclosed hereinabove may be placed adjacent to a non-working area of the sintered cemented carbide thread rolling region or sintered cemented carbide thread rolling die in a void of a mold. The space between the sintered ceramic thread rolling region or thread rolling die and the optional solid metal or metal alloy pieces defines an unoccupied space. A plurality of inorganic particles are added to at least a portion of the unoccupied space. The inorganic particles may comprise one or more of hard particles, metal grains, particles, and powders The remaining void space between the plurality of inorganic particles and the sintered cemented carbide thread rolling region or thread rolling die and the optional solid metallic pieces defines a remainder space. The remainder space is at least partially filled by infiltration with a molten metal or metal alloy matrix material that has a lower melting temperature than any of the inorganic particles which, together with the inorganic particles, forms a metal matrix composite material. Upon cooling, the metal of the metal matrix composite material bonds together the inorganic particles and the sintered cemented carbide thread rolling die and, if present, any non-cemented carbide metal or metal alloy pieces. Upon removal from the mold, the sintered cemented carbide thread rolling die with a non-cemented carbide piece comprising at least one of a metal or metal alloy region and a metal matrix composite region may be machined and finished to a desired shape. This infiltration process is disclosed in U.S. patent application Ser. No. 12/196,815, which is hereby incorporated herein by reference in its entirety.
Still another non-limiting embodiment of a thread rolling die encompassed by this disclosure comprises a thread rolling region comprising a working surface having a thread form, wherein at least the working surface of the thread rolling region comprises a sintered cemented carbide material, and at least one non-cemented carbide piece is metallurgically bonded to the thread rolling region in an area of the thread rolling region that does not prevent access of a workpiece to the working surface. The non-cemented carbide piece comprises at least one of a metallic region and a metal matrix composite region. The non-cemented carbide piece may be machinable in order to facilitate, for example, mounting of the sintered ceramic thread rolling die to a thread rolling machine.
In a non-limiting embodiment, the sintered cemented carbide of the thread rolling region has a compressive yield strength of at least 400,000 psi, a Young's modulus in the range of 50×106 psi to 80×106 psi, an abrasion wear volume in the range of 5 mm3 to 30 mm3 evaluated according to ASTM G65-04, a hardness in the range of 78 HRA to 89 HRA, a fracture toughness of at least 15 ksi·in1/2, and a transverse rupture strength of at least 300 ksi.
The properties of the thread rolling die illustrated in
A circular sintered cemented carbide thread rolling die is prepared as described in Example 1 and is placed in a graphite mold. Powdered tungsten is added to the mold to cover the thread rolling die. An infiltrant powder blend consisting essentially of 78 weight percent copper, 10 weight percent nickel, 6 weight percent manganese, 6 weight percent tin, and incidental impurities is placed in a funnel positioned above the graphite mold. The assembly is placed in a vacuum furnace at a temperature of 1350° C., which is greater than the melting point of the infiltrant powder blend. The molten material formed on melting the infiltrant powder blend infiltrates the space between the tungsten powder and the thread rolling die. As the molten material cools and solidifies, it binds tungsten carbide particles formed from the powdered tungsten to the die and forms a non-cemented carbide non-working portion. Subsequently, the rolling die is machined to form a sintered ceramic thread rolling die comprising a non-cemented carbide non-working region 18 as schematically depicted in
It will be understood that the present description illustrates those aspects of the invention relevant to a clear understanding of thread rolling dies according to the present disclosure. Certain aspects that would be apparent to those of ordinary skill in the art and that, therefore, would not facilitate a better understanding of the subject matter herein have not been presented in order to simplify the present description. Although only a limited number of embodiments are necessarily described herein, one of ordinary skill in the art will, upon considering the foregoing description, recognize that many modifications and variations may be employed. All such variations and modifications are intended to be covered by the foregoing description and the following claims.
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20110107811 A1 | May 2011 | US |