Invention Grant
US09476383B2 Aircraft turbojet engine thrust reverser with a reduced number of latches 有权
飞机涡轮喷气发动机推力反向器具有减少的锁存数量

  • Patent Title: Aircraft turbojet engine thrust reverser with a reduced number of latches
  • Patent Title (中): 飞机涡轮喷气发动机推力反向器具有减少的锁存数量
  • Application No.: US13944187
    Application Date: 2013-07-17
  • Publication No.: US09476383B2
    Publication Date: 2016-10-25
  • Inventor: Pierre Caruel
  • Applicant: AIRCELLE
  • Applicant Address: unknown Gonfreville l'Orcher
  • Assignee: AIRCELLE
  • Current Assignee: AIRCELLE
  • Current Assignee Address: unknown Gonfreville l'Orcher
  • Agency: Burris Law, PLLC
  • Priority: FR1150342 20110117
  • Main IPC: F02K1/54
  • IPC: F02K1/54 B64D33/04 F02K1/72 F02K1/76
Aircraft turbojet engine thrust reverser with a reduced number of latches
Abstract:
A thrust reverser with grids includes a jet engine pylon, a one piece cowl either directly or indirectly slidably mounted on the jet engine pylon between a direct jet position and a reverse jet position, and a system for locking this cowl on a beam. The system has a single tertiary lock, which is positioned on one side of the jet engine pylon being capable of locking a corresponding upper edge of the cowl. In addition, the tertiary lock includes a locker to lock the cowl, a blocker for blocking the locker, and a position detector in order to detect the position of the locker. The system further includes another detector to detect proper closing of the other upper edge of the cowl.
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