IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0447341
(2003-05-29)
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발명자
/ 주소 |
- Adams,Robbie
- Giles,Todd
- Brault,Sharon
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출원인 / 주소 |
- Honeywell International, Inc.
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
16 인용 특허 :
32 |
초록
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A bearing for a high-speed and high-momentum rotating flywheel system for satellite or other applications that enables better recovery when unintended physical contact occurs. This better recovery is achieved through increased impact resistance and wear resistance by using a flat annulus connected t
A bearing for a high-speed and high-momentum rotating flywheel system for satellite or other applications that enables better recovery when unintended physical contact occurs. This better recovery is achieved through increased impact resistance and wear resistance by using a flat annulus connected to the main shaft of the primary bearing and secondary metal bearing and coating both annuli with rhenium or its alloys. Rhenium has a very high melting point but in the annealed condition is ductile so the rhenium coating is hardened to a very high strength and wear resistance but the rhenium beneath is still ductile. This combination of hard and soft material provides good wear resistance and impact resistance for those times when the primary bearing ceases to operate and contact is made with the secondary bearing.
대표청구항
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What is claimed is: 1. A secondary bearing system, the secondary bearing system comprising: a primary bearing shaft having a first contact surface coated with a first material comprising rhenium; and a secondary bearing shaft having a second contact surface coated with a second material comprising
What is claimed is: 1. A secondary bearing system, the secondary bearing system comprising: a primary bearing shaft having a first contact surface coated with a first material comprising rhenium; and a secondary bearing shaft having a second contact surface coated with a second material comprising rhenium, the second contact surface being initially separated from the first contact surface. 2. The secondary bearing system as set forth in claim 1, wherein the first and second contact surfaces are adapted to rotate at high speed with respect to one another while withstanding contact with one another. 3. The secondary bearing system as set forth in claim 1, wherein the secondary bearing shaft comprises a socket hollow that is adjacent to the second contact surface; and the primary bearing shaft comprises a stub that is adjacent to the first contact surface and adapted to fit within the socket hollow when the first contact surface contacts the second contact surface. 4. The secondary bearing system as set forth in claim 1, wherein the primary bearing shaft comprises a first support annulus that includes the first contact surface; and the secondary bearing shaft comprises a second support annulus that includes the second contact surface. 5. The secondary bearing system as set forth in claim 1, wherein the first and second contact surfaces are adapted to engage each other, whereby the secondary mechanical bearing engages and supports the primary bearing shaft. 6. The secondary bearing system as set forth in claim 1, wherein the primary and secondary bearing shafts are components of an integrated power and attitude control system. 7. The secondary bearing system as set forth in claim 1, wherein each of the first and second materials is a mixture of a powdered ceramic and powdered metal comprising rhenium. 8. The secondary bearing system as set forth in claim 7, wherein each of the primary and secondary bearing shafts comprises steel. 9. The secondary bearing system as set forth in claim 8, wherein each of the primary and secondary bearing shafts comprises an aluminum alloy of steel. 10. The secondary bearing system as set forth in claim 9, wherein each of the primary and secondary bearing shafts comprises aluminum alloys of steel selected from the group consisting of 135M, Nitralloy 135M, Nitralloy EZ, Nitralloy Gi, Nitralloy N, SAE 7140, AMS 6470, AMS 6475, Nitralloy N135M, thermally conductive steels, and steels having at least 0.011% by weight of aluminum. 11. The secondary bearing system as set forth in claim 7, wherein the powdered ceramic further comprises silicon carbide (SiC). 12. The secondary bearing system as set forth in claim 7, wherein the powdered ceramic further comprises powdered ceramic selected from the group consisting of alumina, alumina titanate, aluminum nitride, and mixtures thereof, beryllium oxide, boron nitride, braided ceramic fibers, carbide/cobalt hardmetal, cast carbide, ceramic eutectic composites, coarse-grained tungsten, coated silicon nitride, cobalt oxide, conventional carburized tungsten carbide, diamond, entatite, fosterite, hot-press matrices, infiltration matrices, macrocrystalline tungsten carbide powder, macrocrystalline tungsten carbide sintered tungsten, metal matrix composites, multi-layered PVD coatings, nickel oxide, niobium carbide powder, physical vapor deposition coatings, reaction bonded silicon nitride, reaction bonded tungsten carbide, reaction bonded tungsten carbide and sintered tungsten carbide, silica zirconia, silicon carbide whiskers, silicon carbide fibers, silicon carbide whisker-reinforced alumina ceramic, silicon nitride, sintered tungsten carbide, tantalum carbide powder tantalum niobium carbide powder, titanium carbide, titanium carbide-titanium nitride, titanium carbide-titanium nitride-based carbide and ceramic substrates, titanium carbide-titanium nitride-based carbide substrates, titanium carbide-titanium nitride-based ceramic substrates, titanium carbonitride powder, titanium diboride, titanium nitride powder, tungsten carbide macrocrystalline tungsten carbide, tungsten disulfide, tungsten metal powder, tungsten sulfide, tungsten titanium carbide powder, zirconia, and mixtures thereof. 13. The secondary bearing system as set forth in claim 7, wherein the powdered metal is powdered rhenium. 14. The secondary bearing system as set forth in claim 7, wherein the powdered metal is a powdered rhenium-based alloy. 15. The secondary bearing system as set forth in claim 7, wherein the mixture of powdered ceramic and powdered metal have been fused to the primary and secondary bearing shafts by sintering. 16. The secondary bearing system as set forth in claim 1, wherein each of the first and second materials is rhenium. 17. The secondary bearing system as set forth in claim 1, wherein each of the first and second materials is a rhenium alloy. 18. A secondary bearing system, comprising: a primary bearing shaft having a stub and an adjacent first support annulus that comprises a first contact surface coated with a first material comprising rhenium; a secondary bearing shaft having a socket hollow and an adjacent second support annulus that comprises a second contact surface coated with a second material comprising rhenium; the first and second contact surfaces being adapted to rotate at high speed with respect to one another and withstanding contact with one another while resisting spalling; and the stub fitting within the socket hollow when the first contact surface contacts the second contact surface. 19. The secondary bearing system as set forth in claim 18, wherein the first and second contact surfaces are adapted to engage each other, whereby the secondary mechanical bearing engages and supports the primary bearing shaft. 20. The secondary bearing system as set forth in claim 19, wherein the primary and secondary bearing shafts are components of an integrated power and attitude control system. 21. The secondary bearing system as set forth in claim 18, wherein each of the first and second materials is rhenium. 22. The secondary bearing system as set forth in claim 18, wherein each of the first and second materials is a rhenium alloy. 23. A secondary bearing system, the secondary bearing system comprising: a primary bearing shaft having a first surface that is reinforced with a rhenium-containing material; and a secondary component having a second surface that is reinforced with a rhenium-containing material, the second surface being adapted to mate the primary bearing shaft and a generally oppositely opposed the first surface. 24. The secondary bearing system as set forth in claim 23, wherein each of the first and second surfaces is reinforced by a mixture of powdered ceramic and powdered refractory metal that have been fused to a respective substrate. 25. The secondary bearing system as set forth in claim 24, wherein the powdered ceramic further comprises silicon carbide (SiC). 26. The secondary bearing system as set forth in claim 24, wherein the powdered ceramic further comprises powdered ceramic selected from the group consisting of alumina, alumina titanate, aluminum nitride, and mixtures thereof, beryllium oxide, boron nitride, braided ceramic fibers, carbide/cobalt hardmetal, cast carbide, ceramic eutectic composites, coarse-grained tungsten, coated silicon nitride, cobalt oxide, conventional carburized tungsten carbide, diamond, entatite, fosterite, hot-press matrices, infiltration matrices, macrocrystalline tungsten carbide powder, macrocrystalline tungsten carbide sintered tungsten, metal matrix composites, multi-layered PVD coatings, nickel oxide, niobium carbide powder, physical vapor deposition coatings, reaction bonded silicon nitride, reaction bonded tungsten carbide, reaction bonded tungsten carbide and sintered tungsten carbide, silica zirconia, silicon carbide whiskers, silicon carbide fibers, silicon carbide whisker-reinforced alumina ceramic, silicon nitride, sintered tungsten carbide, tantalum carbide powder, tantalum niobium carbide powder, titanium carbide, titanium carbide-titanium nitride, titanium carbide-titanium nitride-based carbide and ceramic substrates, titanium carbide-titanium nitride-based carbide substrates, titanium carbide-titanium nitride-based ceramic substrates, titanium carbonitride powder, titanium diboride, titanium nitride powder, tungsten carbide macrocrystalline tungsten carbide, tungsten disulfide, tungsten metal powder, tungsten sulfide, tungsten titanium carbide powder, zirconia, and mixtures thereof. 27. The secondary bearing system as set forth in claim 24, wherein the powdered metal is powdered rhenium. 28. The secondary bearing system as set forth in claim 24, wherein the powdered metal is a powdered rhenium-based alloy. 29. The secondary bearing system as set forth in claim 24, wherein the mixture of powdered ceramic and powdered metal have been fused to the primary and secondary bearing shafts by sintering. 30. The secondary bearing system as set forth in claim 24, wherein each of the primary and secondary bearing shafts comprises steel. 31. The secondary bearing system as set forth in claim 30, wherein each of the primary and secondary bearing shafts comprises an aluminum alloy of steel. 32. The secondary bearing system as set forth in claim 31, wherein each of the primary and secondary bearing shafts comprises aluminum alloys of steel selected from the group consisting of 135M, Nitralloy 135M, Nitralloy EZ, Nitralloy G, Nitralloy N, SAE 7140, AMS 6470, AMS 6475, Nitralloy N135M, thermally conductive steels, and steels having at least 0.011% by weight of aluminum. 33. The secondary bearing system as set forth in claim 23, wherein each of the first and second surfaces is reinforced by rhenium. 34. The secondary bearing system as set forth in claim 23, wherein each of the first and second surfaces is reinforced by a rhenium alloy.
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