An aircraft includes an airframe and a rotary component rotatably connected to the airframe by way of a plain bearing. The rotary component is part of a rotorcraft control system. The plain bearing includes an inner member rotatably engaged in at least two axes of rotation to an outer member. The inner member has a coefficient of thermal expansion (CTE) substantially less than that of the outer member.
Self-lubricated bearings
2018-12-25
Patent
Electronic Resource
English
The Influence of Misalignment on Self-Lubricated Bearings
Automotive engineering | 1983
|The Application of Self-Lubricated and Pre-Lubricated Bearings to Off-Highway Equipment
SAE Technical Papers | 1982
|The Application of Self-Lubricated and Pre-Lubricated Bearings to Off-Highway Equipment
Automotive engineering | 1982
|The application of self-lubricated and pre-lubricated bearings to off-highway equipment
Tema Archive | 1982
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