发明授权
US08978356B2 Thrust reverser and variable area fan nozzle actuation system and method
有权
推力反向器和可变面积风扇喷嘴致动系统及方法
- 专利标题: Thrust reverser and variable area fan nozzle actuation system and method
- 专利标题(中): 推力反向器和可变面积风扇喷嘴致动系统及方法
-
申请号: US12960442申请日: 2010-12-03
-
公开(公告)号: US08978356B2公开(公告)日: 2015-03-17
- 发明人: Michael John Burgess
- 申请人: Michael John Burgess
- 申请人地址: US IL Chicago
- 专利权人: The Boeing Company
- 当前专利权人: The Boeing Company
- 当前专利权人地址: US IL Chicago
- 主分类号: F02K3/02
- IPC分类号: F02K3/02 ; F02K1/76 ; F02K1/06 ; F02K1/08 ; F02K1/09 ; F02K1/54 ; F02K1/16 ; F15B15/08 ; F15B15/26 ; F02K1/64
摘要:
There is provided an actuation system for a gas turbine engine including a thrust reverser and a variable area fan nozzle. The system has a plurality of linear actuators each having a first outer piston concentric with a second inner piston. The first outer piston is operatively connected to a thrust reverser. The second inner piston is operatively connected to a variable area fan nozzle. The system further has a piston lock assembly for selectively locking the first outer piston to the second inner piston. The system further has a control system coupled to the plurality of linear actuators for operating the variable area fan nozzle between a stowed position and a deployed position.
公开/授权文献
信息查询