• Patent Title: THRUST REVERSER FOR THE NACELLE OF AN AIRCRAFT TURBOFAN ENGINE
  • Application No.: US18556312
    Application Date: 2022-04-27
  • Publication No.: US20240209813A1
    Publication Date: 2024-06-27
  • Inventor: Sebastien Laurent Marie PASCALLuigi BISANTI
  • Applicant: SAFRAN NACELLES
  • Applicant Address: FR Gonfreville-L'Orcher
  • Assignee: SAFRAN NACELLES
  • Current Assignee: SAFRAN NACELLES
  • Current Assignee Address: FR Gonfreville-L'Orcher
  • Priority: FR 04530 2021.04.30
  • International Application: PCT/FR2022/050797 2022.04.27
  • Date entered country: 2023-10-19
  • Main IPC: F02K1/72
  • IPC: F02K1/72 F02K1/76
THRUST REVERSER FOR THE NACELLE OF AN AIRCRAFT TURBOFAN ENGINE
Abstract:
A thrust reverser for an aircraft bypass turbojet engine nacelle, this thrust reverser having a generally annular shape around an axis and including in particular flaps for deflecting the secondary flow through gratings, each of these flaps having a rigid wall and sealing elements located on the outer face of this wall, these sealing elements extending along side edges of the flap so as to provide a seal along these edges in the first position.
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