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Invention Application
US20160115902A1 NACELLE FOR A TURBOJET ENGINE WITH A VARIABLE NOZZLE 审中-公开
具有可变喷嘴的涡轮发动机的NACELLE

  • Patent Title: NACELLE FOR A TURBOJET ENGINE WITH A VARIABLE NOZZLE
  • Patent Title (中): 具有可变喷嘴的涡轮发动机的NACELLE
  • Application No.: US14987302
    Application Date: 2016-01-04
  • Publication No.: US20160115902A1
    Publication Date: 2016-04-28
  • Inventor: Olivier KERBLER , Olivier GILO , Patrick GONIDEC
  • Applicant: AIRCELLE
  • Applicant Address: FR Gonfreville L'Orcher
  • Assignee: AIRCELLE
  • Current Assignee: AIRCELLE
  • Current Assignee Address: FR Gonfreville L'Orcher
  • Priority: FR1356536 20130704
  • Main IPC: F02K1/12
  • IPC: F02K1/12
NACELLE FOR A TURBOJET ENGINE WITH A VARIABLE NOZZLE
Abstract:
The present disclosure provides a turbojet engine nacelle having a downstream section including a cowl which is ended with a hinged flap constituting a nozzle. In particular, the hinged flap is hingedly and translatably hinged to the cowl.
Abstract(Chinese):

本公开提供了一种涡轮喷气发动机机舱，其具有包括整流罩的下游部分，该整流罩以构成喷嘴的铰接折片结束。 特别地，铰链翼片铰接并可平移地铰接到整流罩。

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