公开(公告)号：US20150239569A1

公开(公告)日：2015-08-27

申请号：US14427189

申请日：2013-09-12

Applicant: SNECMA

Inventor： Francois Gallet ,  Patrick Joyez

IPC: B64D27/26 ,  B64C11/48

CPC classification number: B64D27/26 ,  B64C11/48 ,  B64D27/12 ,  B64D2027/005 ,  B64D2027/264 ,  Y02T50/66

Abstract: A system for pylon attachment for mounting an engine on a structure of an aircraft, or to wings of the aircraft, including a first attachment mechanism that can be secured to the pylon and a second attachment mechanism that can be secured to the structure of the aircraft. A connection mechanism connects the first and second attachment mechanism, the connection mechanism configured to allow movement of the first attachment mechanism in relation to the second attachment mechanism between first and second positions.

Abstract translation: 一种用于将发动机安装在飞行器的结构上或飞机的机翼上的塔架连接系统，包括可固定到塔架的第一连接机构和可固定到飞行器结构的第二附接机构 。 连接机构连接第一和第二附接机构，连接机构构造成允许第一连接机构相对于第二连接机构在第一和第二位置之间移动。

公开(公告)号：US09567090B2

公开(公告)日：2017-02-14

申请号：US14427189

申请日：2013-09-12

Applicant: SNECMA

Inventor： Francois Gallet ,  Patrick Joyez

IPC: B64D27/26 ,  B64D27/12 ,  B64C11/48 ,  B64D27/00

CPC classification number: B64D27/26 ,  B64C11/48 ,  B64D27/12 ,  B64D2027/005 ,  B64D2027/264 ,  Y02T50/66

Abstract: A system for pylon attachment for mounting an engine on a structure of an aircraft, or to wings of the aircraft, is provided. The system includes a first attachment mechanism that can be secured to the pylon and a second attachment mechanism that can be secured to the structure of the aircraft. A connection mechanism connects the first and second attachment mechanism. The connection mechanism allows movement of the first attachment mechanism in relation to the second attachment mechanism between first and second positions.

Abstract translation: 提供了一种用于将发动机安装在飞行器的结构或飞机的机翼上的塔架附接系统。 该系统包括可固定到塔架的第一连接机构和可固定到飞行器结构的第二连接机构。 连接机构连接第一和第二附接机构。 连接机构允许第一连接机构相对于第二连接机构在第一和第二位置之间移动。