公开(公告)号：WO2014092835A3

公开(公告)日：2014-08-21

申请号：PCT/US2013061333

申请日：2013-09-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LIOR RAPHAEL ,  SNAPE NATHAN

IPC: F01D25/28 ,  F01D25/00 ,  F02C7/00

CPC classification number: F02C7/00 ,  F05D2220/76 ,  F05D2230/72 ,  F05D2260/30 ,  Y10T29/49229

Abstract: A gas turbine engine component assembly according to an exemplary aspect of the present disclosure includes, among other things, a nacelle including a moveable portion. A generator is configured to be received within a space established by the nacelle. A plurality of cables are at least partially supported on the moveable portion of the nacelle, the plurality of cables being selectively electrically coupled with the generator.

Abstract translation: 根据本公开的示例性方面的燃气涡轮发动机部件组件包括其中包括包括可移动部分的机舱。 发电机被配置为接收在由机舱建立的空间内。 多个电缆至少部分地支撑在机舱的可移动部分上，多个电缆选择性地与发电机电耦合。

公开(公告)号：EP2971702A4

公开(公告)日：2016-11-16

申请号：EP14775865

申请日：2014-03-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LIOR RAPHAEL ,  PAVLIK MARK G

IPC: F02C9/18 ,  F01D17/10 ,  F02C7/232 ,  F16K31/50

CPC classification number: F02C9/18 ,  F01D25/32 ,  F02C6/08 ,  F02C7/057 ,  F02C7/06 ,  F02C7/232 ,  F02C9/52 ,  F05D2220/32 ,  F05D2260/606 ,  F16K1/34 ,  F16K24/04 ,  F16K27/02

Abstract: A bleed valve assembly according to an exemplary aspect of the present disclosure includes, among other things, a bleed adaptor having an inlet portion, a fitting opposite the inlet portion, an adaptor body that extends between the inlet portion and the fitting, and a bleed opening disposed on the adaptor body that is selectively exposed to direct fluid into the bleed adaptor.

公开(公告)号：EP2901064A4

公开(公告)日：2015-12-02

申请号：EP13841174

申请日：2013-07-19

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LIOR RAPHAEL ,  DEROSA ROBERT J

IPC: F16L21/00 ,  F01D25/14 ,  F01D25/28 ,  F02C7/22 ,  F02C7/25 ,  F16L57/00

CPC classification number: F02C7/24 ,  F01D25/14 ,  F01D25/28 ,  F02C7/22 ,  F02C7/25 ,  F05D2300/21 ,  F05D2300/614 ,  F16L57/00 ,  F23R3/60 ,  Y02T50/672 ,  Y02T50/675 ,  Y10T29/49229

Abstract: A flexible shield for fluid connectors of a gas turbine engine is disclosed. The flexible shield may comprise a flexible sleeve adapted to surround the fluid connector, and a coupling configured to secure the flexible sleeve onto a fluid tube proximate the fluid connector. A gas turbine engine employing such a flexible shield is also disclosed, as is a method of enclosing a fluid connector in a gas turbine engine using such a flexible shield.