Attachment structure for a turbojet engine

Attachment structure for a turbojet engine

  • CN 101,959,757 A
  • Filed: 01/09/2009
  • Published: 01/26/2011
  • Est. Priority Date: 03/07/2008
  • Status: Active Application
First Claim
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1. attachment structure (1 that is attached to the turbojet (2) of the fixed sturcture of aircraft via attached hanger (5), 100,300), it is characterized in that, it comprises the roughly single-piece casing section that extends at least in part in every side of the blower-casting (3) of turbojet of axis longitudinally that is used for around the blower-casting (3) of turbojet, and this single-piece casing section comprises the attachment arrangement (201 that is connected to hanger on the one hand, 203), comprise driving engine attachment arrangement (4) on the other hand, this driving engine attachment arrangement turbojet roughly longitudinally every side of axis be arranged on the described casing section, and be used to be connected to the part of turbojet, react on the power that applies thereon in this way.

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