公开(公告)号：WO2014189588A2

公开(公告)日：2014-11-27

申请号：PCT/US2014020264

申请日：2014-03-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ZHENG ZHIJUN ,  FOSTER JOSEPH P ,  DAILEY STEPHEN P ,  SANDY DAVID F

IPC: F02C7/20 ,  B64D27/00 ,  F16B21/10

CPC classification number: B64D27/26 ,  B64D2027/266 ,  B64D2027/268 ,  F01D25/24 ,  F01D25/28 ,  F02C7/20 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2230/642 ,  F05D2240/90 ,  F05D2260/311 ,  F16B5/025 ,  Y02T50/44 ,  Y02T50/671

Abstract: An engine mount may include a clevis and a lug defining a hole therethrough. A pin may be joined to the clevis and may extend through the hole of the lug with the pin and the lug defining a clearance therebetween. A trigger system may be disposed on the lug and operatively associated with the pin.

Abstract translation: 发动机支架可以包括U形夹和限定穿过其中的孔的凸耳。 销可以连接到U形夹，并且可以通过销延伸穿过凸耳的孔，并且凸耳在其间限定间隙。 触发器系统可以设置在凸耳上并且与销可操作地相关联。

公开(公告)号：EP2893172A4

公开(公告)日：2016-06-01

申请号：EP13833645

申请日：2013-09-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SANDY DAVID F ,  ZHENG ZHIJUN ,  DAILEY STEPHEN P ,  FOSTER JOSEPH P

IPC: F02C7/32 ,  B64D27/26 ,  F02C7/36 ,  F02K3/06

CPC classification number: B64D27/26 ,  B64D2027/266 ,  B64D2027/268 ,  F02C7/20 ,  F02K3/06

Abstract: An assembly for mounting a turbine engine to a pylon includes a mounting beam, a plurality of fasteners, a first mounting linkage and a second mounting linkage. The mounting beam includes a mount beam fitting that extends axially between a first mount beam end and a second mount beam end, and a mount beam flange that extends radially out from the mount beam fitting at the first mount beam end. A first fastener aperture extends radially through the mount beam fitting, and a second fastener aperture extends axially through the mount beam flange. The fasteners connect the mounting beam to the pylon. A first of the fasteners is mated with the first fastener aperture, and a second of the fasteners is mated with the second fastener aperture. The first mounting linkage connects the first mount beam end to a first engine attachment. The second mounting linkage connects the second mount beam end to second engine attachments.

公开(公告)号：EP2969763A4

公开(公告)日：2016-11-23

申请号：EP14769280

申请日：2014-03-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SAWYERS-ABBOTT NIGEL DAVID ,  FOSTER JOSEPH P

IPC: B64D33/02 ,  F02C7/04

CPC classification number: F01D25/265 ,  B64D29/06 ,  F01D21/00 ,  F02C7/20 ,  F02K1/32 ,  F05D2220/32 ,  F05D2260/30

Abstract: A nacelle for a gas turbine engine includes a upper and lower bifurcations, an inner diameter cowl and a first latch system. The inner diameter cowl extends between the upper and lower bifurcations and the first latch system is mounted on the inner diameter cowl. The first latch system is spaced along the inner diameter cowl between the upper and lower bifurcations.

公开(公告)号：EP2971679A4

公开(公告)日：2016-11-23

申请号：EP14801436

申请日：2014-03-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ZHENG ZHIJUN ,  FOSTER JOSEPH P ,  DAILEY STEPHEN P ,  SANDY DAVID F

IPC: F02C7/20 ,  B64D27/00 ,  F16B21/10

CPC classification number: B64D27/26 ,  B64D2027/266 ,  B64D2027/268 ,  F01D25/24 ,  F01D25/28 ,  F02C7/20 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2230/642 ,  F05D2240/90 ,  F05D2260/311 ,  F16B5/025 ,  Y02T50/44 ,  Y02T50/671