发明名称 SHAFT DISPLACEMENT CONTROL
摘要 <p>An aircraft powerplant (52) has a shaft (54) with a bladed air moving device (56, 58) disposed within an enclosure that forms a flow path, a bearing assembly (60) supportingly coupled to the shaft and a squeeze-film damper (62) positioned between the bearing assembly and a housing. The squeeze-film damper includes a plurality of sectors (64) that are each in fluid communication with a fluid pressure source. A controller (72) is used to operate upon sensed aircraft motion and regulate pressure in the plurality of sectors to influence a clearance between the bladed air moving device and the enclosure.</p>
申请公布号 WO2014130121(A1) 申请公布日期 2014.08.28
申请号 WO2013US72771 申请日期 2013.12.03
申请人 COPELAND, ANDREW D.;COOKERLY, ALAN B. 发明人 COPELAND, ANDREW D.;COOKERLY, ALAN B.
分类号 F01D11/20;F01D25/16;F02C7/06;F16C33/10;F16F15/023 主分类号 F01D11/20
代理机构 代理人
主权项
地址