发明名称 Hybrid sliding element and elastomeric bearing
摘要 According to one embodiment, a bearing is situated in a rotor system. The bearing features a housing having a first opening therethrough, a first member disposed within the first opening and having a second opening therethrough, and an elastomeric bearing disposed within the second opening and having a third opening therethrough configured to receive a shaft. The first member having at least one substantially curved surface. A sliding element bearing disposed between the housing and the first member.
申请公布号 US9399512(B2) 申请公布日期 2016.07.26
申请号 US201313875977 申请日期 2013.05.02
申请人 Bell Helicopter Textron Inc. 发明人 Davis Hunter;Stamps Frank B.
分类号 B64C27/35;F16C11/08;F16C11/06 主分类号 B64C27/35
代理机构 Bell Helicopter Textron Inc. 代理人 Bell Helicopter Textron Inc.
主权项 1. A rotorcraft, comprising: a body; a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source; a hub; a rotor blade coupled to the hub; a swashplate positioned about the drive shaft; a pitch link coupled between the swashplate and the hub corresponding to the rotor blade; and a bearing coupled between the hub and the drive shaft, the bearing comprising: a housing having a first opening therethrough; a first member disposed within the first opening and having a second opening therethrough, the first member having at least one substantially curved surface; an elastomeric bearing disposed within the second opening and having a third opening therethrough, the drive shaft disposed at least partially through the third opening; and a sliding element bearing disposed between the elastomeric bearing and the first member.
地址 Fort Worth TX US