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。

公开(公告)号：US09879558B2

公开(公告)日：2018-01-30

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 ,  F01D25/24

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.

公开(公告)号：US09670791B2

公开(公告)日：2017-06-06

申请号：US14772194

申请日：2014-03-04

Applicant: United Technologies Corporation

Inventor： Mark Broomer ,  Carson A. Roy Thill ,  Timothy M. Davis ,  Anthony P. Cherolis ,  Robert L. Hazzard ,  Craig R. McGarrah ,  Conway Choung ,  Russell E. Keene

IPC: F16J15/32 ,  F01D25/30 ,  F01D11/08 ,  F01D11/00 ,  F01D5/14 ,  F01D9/02 ,  F01D25/24

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.

公开(公告)号：US20160017738A1

公开(公告)日：2016-01-21

申请号：US14770678

申请日：2014-02-24

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Mark J. Rogers ,  Timothy M. Davis ,  Mark Broomer ,  Kevin W. White ,  Craig McGarrah ,  Carson A. Roy Thill

IPC: F01D11/00 ,  F01D25/26

CPC classification number: F01D11/005 ,  F01D25/26 ,  F02C7/28 ,  F05D2220/30 ,  F05D2240/11 ,  F05D2240/55 ,  F05D2260/97 ,  F16J15/061 ,  F16J15/0812

Abstract: An assembly for a turbine engine includes a turbine engine first component, a turbine engine second component and a seal assembly. The first component includes a groove and a groove surface. The second component includes a tongue that extends into the groove to a tongue surface. The seal assembly at least partially seals a gap between the groove surface and the tongue surface. The seal assembly includes a rope seal and a clip that attaches the rope seal to the tongue. The rope seal is arranged within the groove between the groove surface and the tongue surface.

Abstract translation: 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密封组件。 第一部件包括凹槽和凹槽表面。 第二部件包括延伸到凹槽中的舌部到舌部表面。 密封组件至少部分地密封槽表面和舌表面之间的间隙。 密封组件包括绳索密封件和将绳索密封件附接到舌头的夹子。 绳密封件布置在槽表面和舌表面之间的槽内。

公开(公告)号：US20160003081A1

公开(公告)日：2016-01-07

申请号：US14772194

申请日：2014-03-04

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Mark Broomer ,  Carson A. Roy Thill ,  Timothy M. Davis ,  Anthony P. Cherolis ,  Robert L. Hazzard ,  Craig R. McGarrah ,  Conway Choung ,  Russell E. Keene

IPC: F01D11/08 ,  F01D5/14 ,  F01D9/02

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：US10731493B2

公开(公告)日：2020-08-04

申请号：US14783048

申请日：2014-04-10

Applicant: United Technologies Corporation

Inventor： Timothy M. Davis ,  Mark J. Rogers ,  Mark Broomer ,  Craig R. McGarrah ,  Carson A. Roy Thill

IPC: F01D11/00 ,  F01D9/04 ,  F01D11/08 ,  F01D25/24

Abstract: A seal for sealing a radially outer component of a gas turbine engine stator to a radially inner component thereof includes an axially resilient seal carrier adapted for mounting the seal carrier and including at a radially inner portion thereof, a pair of radially spaced, axially extending, radially resilient jaws adapted to clamp a sealing element such as a rope seal there between in sealing engagement with a radially inner component of the engine stator.

公开(公告)号：US20160061047A1

公开(公告)日：2016-03-03

申请号：US14783048

申请日：2014-04-10

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Timothy M. Davis ,  Mark J. Rogers ,  Mark Broomer ,  Craig R. McGarrah ,  Carson A. Roy Thill

IPC: F01D11/00 ,  F01D11/08 ,  F01D25/24 ,  F01D9/04

Abstract: A seal for sealing a radially outer component of a gas turbine engine stator to a radially inner component thereof includes an axially resilient seal carrier adapted for mounting the seal carrier and including at a radially inner portion thereof, a pair of radially spaced, axially extending, radially resilient jaws adapted to clamp a sealing element such as a rope seal there between in sealing engagement with a radially inner component of the engine stator.

Abstract translation: 用于将燃气涡轮发动机定子的径向外部部件密封到其径向内部部件的密封件包括轴向弹性的密封载体，其适于安装密封载体并且在其径向内部包括一对径向间隔开的轴向延伸的， 径向弹性夹爪，其适于将密封元件（例如其间的绳索密封件）与发动机定子的径向内部部件密封接合。

公开(公告)号：US10451204B2

公开(公告)日：2019-10-22

申请号：US14765849

申请日：2014-03-11

Applicant: United Technologies Corporation

Inventor： Mark Broomer ,  Russell E. Keene ,  Timothy M. Davis ,  Mark J. Rogers

IPC: F16L23/02 ,  F01D11/00 ,  F01D25/24 ,  F16L23/16 ,  F16L25/00 ,  F01D11/12

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.

公开(公告)号：US10280778B2

公开(公告)日：2019-05-07

申请号：US14770678

申请日：2014-02-24

Applicant: United Technologies Corporation

Inventor： Mark J. Rogers ,  Timothy M. Davis ,  Mark Broomer ,  Kevin W. White ,  Craig McGarrah ,  Carson A. Roy Thill

IPC: F01D11/00 ,  F02C7/28 ,  F16J15/08 ,  F16J15/06 ,  F01D25/26

Abstract: An assembly for a turbine engine includes a turbine engine first component, a turbine engine second component and a seal assembly. The first component includes a groove and a groove surface. The second component includes a tongue that extends into the groove to a tongue surface. The seal assembly at least partially seals a gap between the groove surface and the tongue surface. The seal assembly includes a rope seal and a clip that attaches the rope seal to the tongue. The rope seal is arranged within the groove between the groove surface and the tongue surface.