Invention Grant
US08366038B2 Device for fastening a turbojet engine to an aircraft fixing strut 有权
用于将涡轮喷气发动机紧固到飞行器固定支柱的装置

  • Patent Title: Device for fastening a turbojet engine to an aircraft fixing strut
  • Patent Title (中): 用于将涡轮喷气发动机紧固到飞行器固定支柱的装置
  • Application No.: US12084393
    Application Date: 2006-10-24
  • Publication No.: US08366038B2
    Publication Date: 2013-02-05
  • Inventor: Hervé Marche
  • Applicant: Hervé Marche
  • Applicant Address: FR Toulouse
  • Assignee: Airbus Operations SAS
  • Current Assignee: Airbus Operations SAS
  • Current Assignee Address: FR Toulouse
  • Agency: Patterson Thuente Christensen Pedersen, P.A.
  • Priority: FR0553304 20051031
  • International Application: PCT/FR2006/051093 WO 20061024
  • International Announcement: WO2007/051938 WO 20070510
  • Main IPC: B64D27/10
  • IPC: B64D27/10
Device for fastening a turbojet engine to an aircraft fixing strut
Abstract:
A front attachment device for fastening a turbojet engine to an aircraft fixing strut. The attachment device is adapted to absorb the turbojet engine thrust loads, and includes a top bracket, and a lower bracket. A thrust load absorption vector results from a first convergence point of primary vectors passing through primary fixing points that couple the top bracket to the lower bracket and a second convergence point of secondary vectors passing through secondary fixing points that couple the lower bracket to the turbojet engine. The thrust load absorption vector transmits the turbojet engine thrust loads to the fixing strut, and extends along a longitudinal axis of the turbojet engine.
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