Invention Application
US20160016669A1 FRONT FRAME FOR A CASCADE THRUST REVERSER STRUCTURE 有权
一个CASCADE扭转反向结构的前框架

  • Patent Title: FRONT FRAME FOR A CASCADE THRUST REVERSER STRUCTURE
  • Patent Title (中): 一个CASCADE扭转反向结构的前框架
  • Application No.: US14633269
    Application Date: 2015-02-27
  • Publication No.: US20160016669A1
    Publication Date: 2016-01-21
  • Inventor: Xavier CAZUCJean-Philippe Joret
  • Applicant: AIRCELLE
  • Priority: FR12/58173 20120903
  • Main IPC: B64D29/06
  • IPC: B64D29/06 F02K1/70 F01D25/28
FRONT FRAME FOR A CASCADE THRUST REVERSER STRUCTURE
Abstract:
The present disclosure relates to a front frame for an aircraft nacelle comprising a turbojet mounted on a suspension strut, said nacelle comprising a thrust reverser including an actuator designed to open a thrust reversal cowling. The front frame comprises a tubular torsion box, a first straight attachment edge intended to attach the box to a turbojet casing and a second straight attachment edge intended to attach the box to air flow diversion means. The front frame is arranged to transmit tensile and compressive loads between the turbojet casing and the air flow diversion means and torsion loads absorbed by the suspension strut. The front frame is characterized in that the tubular torsion box has a semi-elliptical or elliptical cross-section.
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