公开(公告)号：US20160003161A1

公开(公告)日：2016-01-07

申请号：US14765393

申请日：2014-03-06

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Gary L. Grogg ,  Garth J. Vdovak ,  Marshall Thayer

IPC: F02C7/24 ,  F02C7/20 ,  F02C7/06

CPC classification number: F02C7/24 ,  F01D25/00 ,  F01D25/162 ,  F01D25/243 ,  F01D25/30 ,  F02C7/00 ,  F02C7/06 ,  F02C7/20 ,  F05D2260/30 ,  F05D2260/31

Abstract: An attachment interface assembly for a gas turbine engine has a component configured for attachment to an engine static structure. A fastener has a threaded body portion and an enlarged head portion. The threaded body portion is inserted through aligned holes in the component and engine static structure. A clip has a center opening that receives the threaded body portion such that the clip is positioned between the enlarged head portion and the component.

Abstract translation: 用于燃气涡轮发动机的附接接口组件具有构造成附接到发动机静态结构的部件。 紧固件具有螺纹体部分和扩大的头部。 螺纹体部分通过部件和发动机静态结构中的对准的孔插入。 夹子具有容纳螺纹本体部分的中心开口，使得夹子位于扩大头部和部件之间。