公开(公告)号：US20170044931A1

公开(公告)日：2017-02-16

申请号：US14826498

申请日：2015-08-14

Applicant: United Technologies Corporation

Inventor： Paul M. Lutjen ,  Carson A. Roy Thill ,  Dominic J. Mongillo, JR. ,  Kevin D. Tracy ,  Jeffrey A. Perry ,  Thurman C. Dabbs

IPC: F01D25/12 ,  F01D11/08

CPC classification number: F01D25/12 ,  F01D11/08 ,  F05D2220/32 ,  F05D2240/11 ,  F05D2240/24 ,  F05D2250/74 ,  F05D2260/20

Abstract: A gas turbine engine includes a turbine section including a plurality of blade outer air seals (BOAS) disposed therein, the BOAS including a BOAS body including a plurality of cooling holes defined in substantial conformance with a set of Cartesian coordinates as set forth in at least one of Table 1 and Table 2.

Abstract translation: 燃气涡轮发动机包括涡轮部分，其包括设置在其中的多个叶片外部空气密封件（BOAS），所述BOAS包括BOAS主体，该BOAS主体包括基本上符合一组笛卡尔坐标定义的多个冷却孔，至少如 表1和表2之一。

公开(公告)号：US20160010482A1

公开(公告)日：2016-01-14

申请号：US14766469

申请日：2014-02-05

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Mark J Rogers ,  Mark Broomer ,  Craig R McGarrah ,  Timothy M Davis ,  Anthony B Swift ,  Russell E Keene ,  Carson A. Roy Thill ,  Timothy A. Dunbar

IPC: F01D11/08

CPC classification number: F01D11/08 ,  F01D25/246 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2240/10 ,  F05D2240/20 ,  F05D2240/55 ,  F05D2250/14

Abstract: An interface within a gas turbine engine includes a multiple of segmented components, each with a segment flange with a multiple of apertures, at least one of the multiple of apertures a first slot aperture. A full ring component with a ring flange that defines a multiple ring of apertures, at least one of the multiple of ring apertures a second slot aperture, the second slot aperture transverse to the first slot aperture.

Abstract translation: 燃气涡轮发动机内的界面包括多个分段部件，每个部件具有多个孔的段凸缘，多个孔中的至少一个孔是第一槽孔。 具有环形凸缘的整个环形部件，其限定多个孔环，所述多个环形孔中的至少一个具有第二狭槽孔，所述第二狭缝孔横向于所述第一狭缝孔。

公开(公告)号：US20150226132A1

公开(公告)日：2015-08-13

申请号：US14611920

申请日：2015-02-02

Applicant: United Technologies Corporation

Inventor： Carson A. Roy Thill ,  Mark Broomer ,  Timothy M. Davis ,  Craig R. McGarrah ,  Mark J. Rogers ,  Russell E. Keene ,  Anthony B. Swift

IPC: F02C7/28 ,  F01D25/24 ,  F02C3/04

CPC classification number: F02C7/28 ,  F01D11/005 ,  F01D25/24 ,  F01D25/246 ,  F02C3/04 ,  F05D2240/56 ,  F05D2240/58 ,  F05D2260/30 ,  F16J15/0887

Abstract: A seal assembly for a gas turbine engine includes an engine static structure. First and second members fluidly separate cavities from one another. A seal assembly is captured by the engine structure. The seal assembly includes a carrier and a seal that engages the first member. The second member is captured by the carrier.

Abstract translation: 用于燃气涡轮发动机的密封组件包括发动机静止结构。 第一和第二构件将空腔彼此流体地分开。 密封组件由发动机结构捕获。 密封组件包括承载件和接合第一构件的密封件。 第二个成员由承运人捕获。