公开(公告)号：WO2014035621A1

公开(公告)日：2014-03-06

申请号：PCT/US2013/053882

申请日：2013-08-07

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： ROMANOV, Dmitriy A. ,  PELLETIER, Brian R. ,  KEENE, Russell E.

IPC: F02C7/00 ,  F02C7/28

CPC classification number: F01D5/20 ,  F01D11/08 ,  F05D2230/90 ,  F05D2260/22141 ,  Y02T50/676 ,  Y10T29/49336

Abstract: An example blade outer air seal assembly for a gas turbine engine includes a main body portion extending along an axis. The main body portion has a radially inward facing surface and at least one radially outward facing surface. A passage is provided in the main body portion between the at least one radially inward facing surface and the at least one radially outward facing surface. The passage has a first portion and a second portion transverse to the first portion, and at least one rib disposed along the axis radially outward of the second portion.

Abstract translation: 用于燃气涡轮发动机的示例性叶片外部空气密封组件包括沿轴线延伸的主体部分。 主体部分具有径向向内的表面和至少一个径向向外的表面。 在主体部分之间的至少一个径向向内的表面和至少一个径向向外的表面之间提供通道。 通道具有横向于第一部分的第一部分和第二部分，以及沿着第二部分的径向向外的轴线设置的至少一个肋。

公开(公告)号：WO2014123965A1

公开(公告)日：2014-08-14

申请号：PCT/US2014/014811

申请日：2014-02-05

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： ROGERS, Mark J. ,  BROOMER, Mark ,  MCGARRAH, Craig R. ,  DAVIS, Timothy M. ,  SWIFT, Anthony B. ,  KEENE, Russell E. ,  ROY THILL, Carson A. ,  DUNBAR, Timothy A.

IPC: F01D11/08 ,  F01D5/12 ,  F01C7/00

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缝孔，所述第二狭缝孔横向于所述第一狭缝孔。

公开(公告)号：WO2014150353A1

公开(公告)日：2014-09-25

申请号：PCT/US2014/023017

申请日：2014-03-11

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： BROOMER, Mark ,  KEENE, Russell E. ,  DAVIS, Timothy M. ,  ROGERS, Mark J.

IPC: F01D25/28 ,  F01D25/24 ,  F02C7/00

CPC classification number: F16L23/02 ,  F01D11/003 ,  F01D11/122 ,  F01D25/24 ,  F01D25/246 ,  F05D2230/642 ,  F05D2240/11 ,  F05D2260/38 ,  F16L23/16 ,  F16L25/0018

Abstract: A turbine shroud for incorporation in a turbine of a gas turbine engine has a plurality of butted shroud segments circumferentially arrayed to form a ring. Each of the shroud segments has an arcuate main shroud body portion, a radially inward extending annular flange attached to a first end of the main body portion, and a radially outward extending flange with a plurality of mounting apertures attached to a second end of the main shroud body portion. A first mounting aperture is sized smaller than an adjacent second mounting aperture in the radially outward extending flange.

Abstract translation: 用于结合在燃气涡轮发动机的涡轮机中的涡轮机罩具有周向排列以形成环的多个对接护罩段。 每个护罩段具有弓形主护罩主体部分，附接到主体部分的第一端的径向向内延伸的环形凸缘以及径向向外延伸的凸缘，多个安装孔附接到主体的第二端 护罩主体部分。 第一安装孔的尺寸小于径向向外延伸的凸缘中相邻的第二安装孔。

公开(公告)号：WO2014138078A1

公开(公告)日：2014-09-12

申请号：PCT/US2014/020342

申请日：2014-03-04

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： BROOMER, Mark ,  ROY THILL, Carson A. ,  DAVIS, Timothy M. ,  CHEROLIS, Anthony P. ,  HAZZARD, Robert L. ,  MCGARRAH, Craig R. ,  CHOUNG, Conway ,  KEENE, Russell E.

IPC: F01D11/02 ,  F01D11/00 ,  F02C7/28

CPC classification number: F01D11/08 ,  F01D5/14 ,  F01D9/02 ,  F01D11/003 ,  F01D11/005 ,  F01D25/246

Abstract: An assembly for a turbine engine includes a turbine engine first component, a turbine engine second component and a flexible seal that is attached to the first component. The flexible seal at least partially seals a gap between the first component and the second component. The flexible seal includes a mount and a finger seal that sealingly engages the second component. The mount includes a boss that sealingly engages the first component.

Abstract translation: 用于涡轮发动机的组件包括涡轮发动机第一部件，涡轮发动机第二部件和附接到第一部件的柔性密封件。 柔性密封件至少部分地密封第一部件和第二部件之间的间隙。 柔性密封件包括安装件和密封地接合第二部件的手指密封件。 安装件包括密封地接合第一部件的凸台。

公开(公告)号：WO2014070817A1

公开(公告)日：2014-05-08

申请号：PCT/US2013/067377

申请日：2013-10-30

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： ROMANOV, Dmitriy A. ,  DUGUAY, Brian ,  KEENE, Russell E.

IPC: F01D11/08 ,  F01D5/20 ,  F02C7/00

CPC classification number: F01D25/246 ,  F01D9/04 ,  F01D11/08 ,  F05D2240/11 ,  F05D2260/201 ,  F05D2260/221 ,  Y02T50/676

Abstract: A blade outer air seal for a gas turbine engine includes a first side surface, a second side surface, and a wall. The wall extends between the first side surface and the second side surface and has one or more holes formed therein. The holes are spaced from the first side surface and/or the second side surface and have areas between about 0.005% and 0.450% of a surface area of the blade outer air seal.

Abstract translation: 用于燃气涡轮发动机的叶片外部空气密封件包括第一侧表面，第二侧表面和壁。 该壁在第一侧表面和第二侧表面之间延伸并且在其中形成有一个或多个孔。 孔与第一侧表面和/或第二侧表面间隔开并且具有在叶片外部空气密封件的表面积的约0.005％至0.450％之间的面积。