Invention Grant
US08015797B2 Thrust reverser nozzle for a turbofan gas turbine engine 有权
涡轮风力发电机的推力反向喷嘴

  • Patent Title: Thrust reverser nozzle for a turbofan gas turbine engine
  • Patent Title (中): 涡轮风力发电机的推力反向喷嘴
  • Application No.: US11534202
    Application Date: 2006-09-21
  • Publication No.: US08015797B2
    Publication Date: 2011-09-13
  • Inventor: Jean-Pierre Lair
  • Applicant: Jean-Pierre Lair
  • Agent Francis L. Conte
  • Main IPC: F02K3/02
  • IPC: F02K3/02 F02K1/54
Thrust reverser nozzle for a turbofan gas turbine engine
Abstract:
The thrust reverser comprises a first reverser door and a second reverser door asymmetrically pivotable between a stowed position and a deployed position, one having a pivot axis closer to the central axis than the other.
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