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 |