WO1994002750A1 - Bearings - Google Patents
Bearings Download PDFInfo
- Publication number
- WO1994002750A1 WO1994002750A1 PCT/GB1993/001537 GB9301537W WO9402750A1 WO 1994002750 A1 WO1994002750 A1 WO 1994002750A1 GB 9301537 W GB9301537 W GB 9301537W WO 9402750 A1 WO9402750 A1 WO 9402750A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- bearing
- nickel
- race
- titanium
- fluorocarbon
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
- F16C23/02—Sliding-contact bearings
- F16C23/04—Sliding-contact bearings self-adjusting
- F16C23/043—Sliding-contact bearings self-adjusting with spherical surfaces, e.g. spherical plain bearings
- F16C23/045—Sliding-contact bearings self-adjusting with spherical surfaces, e.g. spherical plain bearings for radial load mainly, e.g. radial spherical plain bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/121—Use of special materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/20—Sliding surface consisting mainly of plastics
- F16C33/201—Composition of the plastic
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2204/00—Metallic materials; Alloys
- F16C2204/40—Alloys based on refractory metals
- F16C2204/42—Alloys based on titanium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2204/00—Metallic materials; Alloys
- F16C2204/40—Alloys based on refractory metals
- F16C2204/44—Alloys based on chromium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/43—Aeroplanes; Helicopters
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S384/00—Bearings
- Y10S384/90—Cooling or heating
- Y10S384/909—Plastic
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S384/00—Bearings
- Y10S384/90—Cooling or heating
- Y10S384/913—Metallic compounds
Definitions
- This invention relates to bearings, especially sliding contact bearings used in aircraft landing gear and incorporating titanium components in surface-to-surface sliding contact.
- Titanium is used in aircraft construction because it is lightweight compared with steel, but when used in bearings such as landing gear trunnion bearings that experience large shock loads, there can be problems with galling and seizure between titanium surfaces sliding on one another. It has been proposed in US 4848934 to overcome this problem by coating the surface of one titanium bearing component with chromium oxide and forming the other component of copper. Although chromium oxide is a brittle material, it is considered . satisfactory provided the complementary bearing surface with which it cooperates includes copper or copper alloys.
- a sliding contact bearing comprises two bearing members composed of titanium or a titanium alloy with cooperating sliding surfaces, characterised in that a first one of said surfaces is chromium plated and the second one of said surfaces is coated with nickel and fluorocarbon polymer.
- the nickel is preferably applied by an electroless plating process and provides a high level of wear and corrosion resistance.
- the fluorocarbon polymer is deposited on the metal surface so as to provide permanent lubrication between the two surfaces.
- a suitable nickel/fluorocarbon polymer coating may be provided by the General agnaplate Corporation under their trade mark "NEDOX" .
- bearing according to the invention offers comparable performance and durability to that of conventional bearings comprising a chromium plated steel member in sliding cooperation with an aluminium bronze member and superior performance compared to bearings involving chromium plated, or chromium oxide coated or bronze coated bearing surfaces. Further, bearings according to the invention offer the advantage of limiting the friction between the bearing surfaces due to the effect of the fluorocarbon polymer used.
- Figure 1 is a diametral cross-section through an aircraft landing gear trunnion bearing according to the invention.
- Figure 2 is a graph of friction against bearing life for a bearing as shown in Figure 1 compared with a similar bearing in which the outer race is aluminium bronze and the inner spherical member is chromium plated steel.
- the aircraft landing gear trunnion bearing of Figure 1 comprises an outer ring-shaped bearing race 1 with an inner bearing surface 2 formed on a sphere, and an inner ring-shaped bearing member 3 located within the outer bearing race 1 with an outer bearing surface 4 formed on a sphere so as to cooperate with the inner bearing surface 2 of the race 1 and allow relative rotary and sliding contact between the two bearing members 1, 3.
- the outer bearing race 1 is adapted for connection to one part of aircraft landing gear
- the inner bearing member 3 is formed with a bore 5 to receive the journal of a trunnion on the leg of the landing gear.
- the two bearing members 1 and 3 are composed of titanium or titanium alloy, and to avoid galling between the cooperating surfaces of these bearing members, the inner surface 2 of the outer bearing race 1 is chromium plated, and the outer surface 4 of the inner bearing member 3 is coated with nickel and fluorocarbon polymer.
- the nickel is applied by an electroless plating process and the fluorocarbon polymer is subsequently infused into pores in the plating, and the coating is heat treated to create a smooth surface.
- This nickel/polymer coating is typically that provided by General Magnaplate Corporation under their trade mark "NEDOX" .
- the coating is 0.025 to 0.041mm thick and has a hardness in the range 750-1000 VPN.
- the bearing as described above and a similar "standard" bearing with the outer bearing race 1 composed of chromium plated steel and the inner bearing 3 composed of aluminium bronze were subjected to successive simulated flight tests with a maximum load of 214 KN.
- the cooperating surfaces of the bearing were in good condition after 30,000 flight tests, and were still in good condition after 60,000 flight tests with the bearing according to the invention, but were showing slight wear with the "standard” bearing having aluminium bronze and s eel/chromium plated members.
- the friction between the cooperating surfaces of both bearings were measured at regular intervals and the results shown in Figure 2 obtained, the friction units shown being dimensionless scaled friction coefficient units used for ease of comparison.
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/373,255 US5660482A (en) | 1992-07-21 | 1993-07-21 | Bearings |
JP50429294A JP3431152B2 (en) | 1992-07-21 | 1993-07-21 | bearing |
DE69307321T DE69307321T2 (en) | 1992-07-21 | 1993-07-21 | CAMP |
EP93917881A EP0651862B1 (en) | 1992-07-21 | 1993-07-21 | Bearings |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9215470.7 | 1992-07-21 | ||
GB9215470A GB2268982B (en) | 1992-07-21 | 1992-07-21 | Bearings |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1994002750A1 true WO1994002750A1 (en) | 1994-02-03 |
Family
ID=10719042
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GB1993/001537 WO1994002750A1 (en) | 1992-07-21 | 1993-07-21 | Bearings |
Country Status (6)
Country | Link |
---|---|
US (1) | US5660482A (en) |
EP (1) | EP0651862B1 (en) |
JP (1) | JP3431152B2 (en) |
DE (1) | DE69307321T2 (en) |
GB (1) | GB2268982B (en) |
WO (1) | WO1994002750A1 (en) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1264662B1 (en) * | 1993-07-05 | 1996-10-04 | Ausimont Spa | PERFLURODIOSSOLS THEIR HOMOPOLYMERS AND COPOLYMERS AND THEIR USE FOR THE COATING OF ELECTRIC CABLES |
US5961218A (en) * | 1996-02-20 | 1999-10-05 | Ebara Corporation | Water lubricated machine component having contacting sliding surfaces |
WO1999060847A1 (en) * | 1998-05-27 | 1999-12-02 | Berkley Inc. | Metallic fishing line guides |
JP2001193741A (en) * | 2000-01-05 | 2001-07-17 | Minebea Co Ltd | Spherical sliding bearing and manufacturing method |
US6520703B1 (en) | 2000-09-13 | 2003-02-18 | Honeywell International, Inc. | Coupling with tribological coating system |
US20020173853A1 (en) * | 2001-05-17 | 2002-11-21 | Corl Harry E. | Movable joint and method for coating movable joints |
US20030234183A1 (en) * | 2001-05-17 | 2003-12-25 | Noble Medical Coatings, Llc | Movable joint and method for coating movable joints |
US20050211562A1 (en) * | 2001-05-17 | 2005-09-29 | Rowe Thomas G | Method for coating joint surfaces of metals used to form prostheses |
DE10220611A1 (en) * | 2002-02-15 | 2003-08-28 | Brueninghaus Hydromatik Gmbh | rotary bearings |
WO2003069174A1 (en) * | 2002-02-15 | 2003-08-21 | Brueninghaus Hydromatik Gmbh | Swivel slide bearing |
US6619758B1 (en) * | 2002-02-25 | 2003-09-16 | Amara Ross | Wheel and bearing assembly |
GB2406622B (en) * | 2003-10-02 | 2005-08-17 | Minebea Co Ltd | Self-lubricating bearings |
GB2412701B (en) * | 2004-03-31 | 2006-03-22 | Minebea Co Ltd | A metal-to-metal spherical bearing |
US20070164151A1 (en) * | 2006-01-13 | 2007-07-19 | Luce William E | Aircraft shock strut and improved bearings therefor |
DE602007011406D1 (en) * | 2006-01-13 | 2011-02-03 | Goodrich Corp | PLANE SPRING LEG WITH IMPROVED CYLINDER AND IMPROVED STORAGE |
US20090010580A1 (en) * | 2006-07-19 | 2009-01-08 | Roller Bearing Company Of America, Inc. | Spherical plain bearing with spread sealing means |
US20080019625A1 (en) * | 2006-07-19 | 2008-01-24 | Roller Bearing Company Of America, Inc. | Spherical plain bearing with contoured lubrication grooves |
US8926185B2 (en) | 2006-07-19 | 2015-01-06 | Roller Bearing Company Of America, Inc. | Spherical plain bearing with lubrication groove |
US20090003743A1 (en) * | 2007-06-26 | 2009-01-01 | Roller Bearing Company Of America, Inc. | Bearing for kingpin or other shaft assembly |
US9192975B2 (en) * | 2009-01-30 | 2015-11-24 | Larry John Verbowski | Vehicle suspension module |
DE102011077735B4 (en) | 2011-06-17 | 2019-02-28 | Schaeffler Technologies AG & Co. KG | Spherical plain bearings |
GB2508043B (en) | 2013-04-17 | 2015-07-22 | Messier Dowty Ltd | Dynamic bearing |
FR3018322B1 (en) * | 2014-03-10 | 2016-11-04 | Skf Aerospace France | PERMANENT LUBRICATING JOINT BONDING MEMBER |
US10724575B2 (en) * | 2017-06-15 | 2020-07-28 | Schaublin Sa | Metallic lined trunnion bearing for aircraft landing gear |
US10480569B2 (en) * | 2017-06-15 | 2019-11-19 | Schaublin Sa | Hybrid lined trunnion bearing for aircraft landing gear |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2218797A5 (en) * | 1973-02-16 | 1974-09-13 | Metallisation Ste Nle | Self-lubricating surface mfr. - by flame spraying a layer of metal and filling the pores with polymer |
US4846122A (en) * | 1985-09-26 | 1989-07-11 | Sycon Corporation | Pneumatic starter for internal combustion engine |
US4848934A (en) * | 1985-01-11 | 1989-07-18 | The Boeing Company | Lightweight high performance titanium sliding contact bearing |
US4938850A (en) * | 1988-09-26 | 1990-07-03 | Hughes Aircraft Company | Method for plating on titanium |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61596A (en) * | 1985-05-23 | 1986-01-06 | Canon Inc | Formation of chromium plated film having metallic luster |
JPH0819951B2 (en) * | 1987-12-15 | 1996-03-04 | 本田技研工業株式会社 | Sliding member of internal combustion engine |
US5325732A (en) * | 1989-12-15 | 1994-07-05 | Vogel Ferdinand L | Motion-transmitting combination comprising a castable, self-lubricating composite and methods of manufacture thereof |
JP3002300B2 (en) * | 1991-07-12 | 2000-01-24 | 日本トムソン株式会社 | Spherical plain bearing and manufacturing method thereof |
-
1992
- 1992-07-21 GB GB9215470A patent/GB2268982B/en not_active Expired - Fee Related
-
1993
- 1993-07-21 DE DE69307321T patent/DE69307321T2/en not_active Expired - Lifetime
- 1993-07-21 WO PCT/GB1993/001537 patent/WO1994002750A1/en active IP Right Grant
- 1993-07-21 EP EP93917881A patent/EP0651862B1/en not_active Expired - Lifetime
- 1993-07-21 JP JP50429294A patent/JP3431152B2/en not_active Expired - Fee Related
- 1993-07-21 US US08/373,255 patent/US5660482A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2218797A5 (en) * | 1973-02-16 | 1974-09-13 | Metallisation Ste Nle | Self-lubricating surface mfr. - by flame spraying a layer of metal and filling the pores with polymer |
US4848934A (en) * | 1985-01-11 | 1989-07-18 | The Boeing Company | Lightweight high performance titanium sliding contact bearing |
US4846122A (en) * | 1985-09-26 | 1989-07-11 | Sycon Corporation | Pneumatic starter for internal combustion engine |
US4938850A (en) * | 1988-09-26 | 1990-07-03 | Hughes Aircraft Company | Method for plating on titanium |
Non-Patent Citations (2)
Title |
---|
PATENT ABSTRACTS OF JAPAN vol. 10, no. 139 (C-348)22 May 1986 * |
PATENT ABSTRACTS OF JAPAN vol. 13, no. 420 (M-872)19 September 1989 * |
Also Published As
Publication number | Publication date |
---|---|
GB2268982A (en) | 1994-01-26 |
DE69307321T2 (en) | 1997-04-24 |
GB2268982B (en) | 1996-03-13 |
EP0651862B1 (en) | 1997-01-08 |
JPH07509298A (en) | 1995-10-12 |
JP3431152B2 (en) | 2003-07-28 |
EP0651862A1 (en) | 1995-05-10 |
DE69307321D1 (en) | 1997-02-20 |
GB9215470D0 (en) | 1992-09-02 |
US5660482A (en) | 1997-08-26 |
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