The present invention relates to a plain bearing equipped with a friction coating and to the method for producing said coating.
High-performance plain bearings are needed in various fields particularly in the reduction gearboxes of turbojet engines with high bypass ratios.
The search for high performance has led to the proposal of various improvements to plain bearings. Hence, U.S. Pat. No. 3,644,105 describes a bearing comprising a composite coating of copper and molybdenum disulfide obtained by electrolytic codepositon. A surface layer consisting of a lead-based alloy containing tin and copper completes the coating.
The earlier known solutions are not, however, entirely satisfactory and, particularly in the applications mentioned herein above, there is still a need to develop plain bearings that provide good operating conditions and good service life after the corresponding severe conditions of use. These conditions in particular include resistance to very high pressure, operation at high linear speed, resistance to high temperature and the plain bearings also have to be capable of operating with lubrication by a low-viscosity oil and, for short periods, without oil.
These results are obtained satisfactorily according to the invention by a high-performance plain bearing equipped with friction coating characterized in that the coating comprises a layer of bronze obtained by sintering and the pores of which are filled with a fluoroplastic paste filled with molybdenum disulfide.
Said friction coating is obtained in a way that is remarkable according to the invention using a method characterized in that it involves the following steps:
Particular conditions of production and advantageous parameters are also determined.
Other characteristics and advantages of the invention will be better understood from reading the description which will follow of one exemplary embodiment of the invention, with reference to the attached drawings in which:
A plain bearing especially intended for aeronautical applications such as the reduction gearboxes of turbojet engines with high bypass ratios comprises, in a conventional way, a metallic support schematically depicted as 1 in
As depicted in
The next step (b) of said method consists in ionic cleaning under vacuum so as to obtain activation of the sintered bronze layer.
In step (c), a layer about 1 mm thick of fluoroplastic paste of the PTFE (polytetrafluroethylene) type filled with molybdenum disulfide is applied to the entire sintered bronze surface and the support 1 coated with the sintered bronze layer 4 is then placed in a die 5, as depicted schematically in
In the next step (e), the paste is dried, something which may, for example, be performed at 90° C. for 2 hours. In step (f) the bearing component 1 is shaped by passing it a second time into the die with the addition of the non-stick and anti-wear coating as defined above. Step (g) of sintering the paste is then carried out under determined conditions such as at 375° C. for 40 minutes and the component is then immersed in water.
Finally, in the final step (h) the bearing component 1 is passed through the die, still equipped with the non-stick coating, to size it to its end dimensions.
No further machining of the plain bearing thus obtained is needed. The qualities of adhesion to the support and the anti-friction qualities of the coating according to the invention thus obtained allow the plain bearing to satisfy the high performance demanded for its operation. In particular, the plain bearing obtained resists very high pressures that may exceed 50 mPa in the oil film. It can operate at high linear speeds and at temperatures up to 120° C. It tolerates low-viscosity oil down to 5×10−6 m2/s at 100° C. and the bearing is capable of operating without oil for short periods, at reduced load.
Number | Date | Country | Kind |
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01 07414 | Jun 2001 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR02/01927 | 6/6/2002 | WO |