公开(公告)号：US20080197233A1

公开(公告)日：2008-08-21

申请号：US11914560

申请日：2006-06-27

Applicant: Stephane Combes ,  Laurent Lafont ,  Stephane Levert

Inventor： Stephane Combes ,  Laurent Lafont ,  Stephane Levert

IPC: B64D27/26

CPC classification number: B64D27/26 ,  Y02T50/44

Abstract: An engine attachment pylon for an aircraft including an aft engine attachment fitted with an aft attachment body and a first shear pin capable of resisting forces applied along a transverse direction of the pylon. The first pin passes through a lower spar of a rigid structure of the pylon and includes a lower end housed in the aft attachment body. The lower end includes a reaming through which a first pin passes, that also passes through the aft attachment body.

Abstract translation: 一种用于飞行器的发动机附接塔架，包括装配有后部附接体的后部发动机附件和能够抵抗沿着塔架的横向方向施加的力的第一剪切销。 第一销穿过塔的刚性结构的下部翼梁，并且包括容纳在后部附接体中的下端。 下端包括第一销通过的铰孔，其也穿过后部附接体。