发明申请
US20130236294A1 TURBOJET ENGINE NACELLE WITH VARIABLE VENTILATION OUTLET CROSS SECTION 有权
涡轮发动机带有可变通风口的交叉部分

  • 专利标题: TURBOJET ENGINE NACELLE WITH VARIABLE VENTILATION OUTLET CROSS SECTION
  • 专利标题(中): 涡轮发动机带有可变通风口的交叉部分
  • 申请号: US13870369
    申请日: 2013-04-25
  • 公开(公告)号: US20130236294A1
    公开(公告)日: 2013-09-12
  • 发明人: Guy Bernard VauchelLaurence Lemains
  • 申请人: AIRCELLE
  • 申请人地址: FR GONFREIVILLE L'ORCHER
  • 专利权人: AIRCELLE
  • 当前专利权人: AIRCELLE
  • 当前专利权人地址: FR GONFREIVILLE L'ORCHER
  • 优先权: FR10/58712 20101025
  • 主分类号: F01D25/24
  • IPC分类号: F01D25/24
TURBOJET ENGINE NACELLE WITH VARIABLE VENTILATION OUTLET CROSS SECTION
摘要:
A turbojet engine nacelle includes a rear section having an internal structure. The internal structure surrounds a rear part of an engine compartment and delimits, with an ejection jet pipe, an outlet cross section for the ventilation of the engine compartment. The engine nacelle includes a moving element associated with a corresponding controller. The moving element is able to move between a withdrawn position in which the outlet cross section for ventilation is at a maximum and an engaged position in which the moving element partially reduces the outlet cross section for ventilation by comparison with the retracted position. The controller is capable of moving the moving element between the retracted and engaged positions.
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