Engine fastener of a mounting system interposed between an attachment strut and an aircraft engine

Engine fastener of a mounting system interposed between an attachment strut and an aircraft engine

  • CN 101,142,120 A
  • Filed: 03/15/2006
  • Published: 03/12/2008
  • Est. Priority Date: 03/18/2005
  • Status: Active Application
First Claim
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1. engine accessory power rating (16) that is used for assembly system (1), described assembly system is designed to be installed between the rigid construction (4) and driving engine (2) of aircraft engine accessory pillar (6), and wherein, described annex comprises:

  • Main body (130);

    Pedals (146), it is hinged being installed on the described main body (130) by means of first link pin (144);

    AndTwo thrust absorbing rods (150a, 150b), each thrust absorbing rod all has the rear end that is connected in described pedals (146),Wherein said main body (130) is made of first main supporting rod (132a) and second main supporting rod (132b) that is stacked on described first main supporting rod,It is characterized in that, described first link pin (144) is made of the first (144a) of pin and the second portion (144b) of pin, first of wherein said pin (144a) and described first main supporting rod (132a) are made for one, and second portion of described pin (144b) and described second main supporting rod (132b) are made for one, and, the described first and second main supporting rod (132a, 132b) limit stop limit surface (166) jointly, the rotation of described pedals (146) around described first link pin (144) can be limited in described stop limit surface.

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