发明公开
EP1956224A3 Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system 有权
风扇喷嘴具有可变横截面的用于燃气涡轮机的一个凸轮致动系统的风扇壳体

  • 专利标题: Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system
  • 专利标题(中): 风扇喷嘴具有可变横截面的用于燃气涡轮机的一个凸轮致动系统的风扇壳体
  • 申请号: EP08250456.4
    申请日: 2008-02-07
  • 公开(公告)号: EP1956224A3
    公开(公告)日: 2011-09-07
  • 发明人: Baran, Kenneth C.
  • 申请人: United Technologies Corporation
  • 申请人地址: United Technologies Building, 1 Financial Plaza Hartford, CT 06101 US
  • 专利权人: United Technologies Corporation
  • 当前专利权人: United Technologies Corporation
  • 当前专利权人地址: United Technologies Building, 1 Financial Plaza Hartford, CT 06101 US
  • 代理机构: Leckey, David Herbert
  • 优先权: US672589 20070208
  • 主分类号: F02K1/00
  • IPC分类号: F02K1/00 F02K1/12
Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system
摘要:
A fan variable area nozzle (FVAN) (42) includes a flap assembly which varies a fan nozzle exit area through a cam drive ring (58). The flap assembly generally includes a multiple of flaps (50), flap linkages (52) and an actuator system (54). The actuator system (54) rotationally translates the cam drive ring (58) relative an engine centerline axis which results in a follower of the flap linkage (52) following a cam surface (86) to pivot each flap (50) such that the flap assembly dilates about the circumferential hinge line. Rotation of the cam drive ring (58) adjusts dilation of the entire fan nozzle exit area in a symmetrical manner. Another cam drive ring (58' Fig 5A) includes a multiple of movable cams (84) which engages the follower of the flap linkage (52) of each flap (50) such that pivotable movement of a particular number of the multiple of movable cams (84) about a respective cam pivot results in vectoring of the FVAN (42).
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