公开(公告)号：EP2951404B1

公开(公告)日：2019-04-10

申请号：EP14786006.8

申请日：2014-01-31

Applicant: United Technologies Corporation

Inventor： PORTER, Steven D. ,  FEINDEL, David T. ,  BUDNICK, Matthew ,  CHUONG, Conway

IPC: F01D25/00 ,  F01D21/00 ,  F01D11/00

公开(公告)号：EP3428490A1

公开(公告)日：2019-01-16

申请号：EP18172186.1

申请日：2018-05-14

Applicant: United Technologies Corporation

Inventor： CHUONG, Conway ,  D'AMBRUOSO, Tara L. ,  WONG, Joey

IPC: F16J15/44 ,  F01D11/02

Abstract: A non-contact seal assembly (28) includes a plurality of seal shoes (54) arranged about a centerline (22) in an annular array, the seal shoes (54) including a first seal shoe (54) extending axially along the centerline (22) between a first shoe end (70) and a second shoe end (72). The non-contact seal assembly (28) may comprise a seal base (52) circumscribing axially offset from the annular array of the seal shoes (54). The non-contact seal assembly (28) may further comprise a plurality of spring elements (56), each of the spring elements (56) radially distal from and connecting to a respective one of the seal shoes (54), and each of the plurality of spring elements (56) is axially adjacent to the seal base (52).

公开(公告)号：EP3296520A2

公开(公告)日：2018-03-21

申请号：EP17175782.6

申请日：2017-06-13

Applicant: United Technologies Corporation

Inventor： CHUONG, Conway

IPC: F01D11/02

Abstract: An assembly (20) includes a plurality of seal shoes (76) arranged about an axial centerline (22) in an annular array. The assembly (20) also includes a seal base (74) and a plurality of spring elements (78). The seal base (74) circumscribes the annular array of the seal shoes (76). A threaded base aperture (84) extends axially through the seal base (74). Each of the spring elements (78) is radially between and connects a respective one of the seal shoes (76) with the seal base (74). The spring elements (78) are formed integral with the seal base (74) and the seal shoes (76) as a unitary body.

Abstract translation: 一个组件（20）包括多个围绕轴向中心线（22）排列成环形阵列的密封垫（76）。 组件（20）还包括密封基座（74）和多个弹簧元件（78）。 密封底座（74）围绕密封瓦（76）的环形阵列。 带螺纹的基座孔（84）轴向延伸穿过密封基座（74）。 每个弹簧元件（78）径向地位于密封座（76）中的相应一个与密封件基座（74）之间并且将其连接。 弹簧元件（78）与密封基座（74）和密封蹄（76）整体形成为一体。

公开(公告)号：EP3284983A1

公开(公告)日：2018-02-21

申请号：EP17175799.0

申请日：2017-06-13

Applicant: United Technologies Corporation

Inventor： CHUONG, Conway

IPC: F16J15/44

Abstract: An assembly (20) includes a monolithic carrier structure (44) and a seal assembly (30). The monolithic carrier structure (44) includes a carrier base (46) and a support ring (48). The carrier base (46) extends axially along the centerline (22). The support ring (48) projects radially inward from the carrier base (46). The seal assembly (30) is nested radially within the carrier base (46) and axially next to the support ring (48). The seal assembly (30) includes a seal base (72), a plurality of spring elements (76) and a plurality of seal shoes (74) arranged about the centerline (22) in an annular array. The seal base (72) circumscribes the annular array of the seal shoes (74). Each of the spring elements (76) is radially between and connects a respective one of the seal shoes (74) with the seal base (72).

Abstract translation: 组件（20）包括整体载体结构（44）和密封组件（30）。 整体式载体结构（44）包括载体基部（46）和支撑环（48）。 载体基座（46）沿中心线（22）轴向延伸。 支撑环（48）从载体基座（46）径向向内突出。 密封组件（30）径向地嵌套在载体基座（46）内并轴向紧靠支撑环（48）。 密封组件（30）包括密封基座（72），多个弹簧元件（76）和围绕中心线（22）布置成环形阵列的多个密封蹄（74）。 密封底座（72）外接密封瓦（74）的环形阵列。 每个弹簧元件（76）径向地位于密封垫（74）中的相应的一个与密封基座（72）之间并且将其连接。

公开(公告)号：EP2938857B1

公开(公告)日：2017-09-27

申请号：EP13868090.5

申请日：2013-12-19

Applicant: United Technologies Corporation

Inventor： BUDNICK, Matthew ,  CHUONG, Conway ,  SCOTT, Jonathan, Ariel

IPC: F02C7/12 ,  F01D25/12 ,  F01D5/08 ,  F01D25/14

CPC classification number: F01D25/14 ,  F01D5/081 ,  F01D9/02 ,  F01D9/065 ,  F01D25/12 ,  F01D25/145 ,  F01D25/162 ,  F01D25/24 ,  F02C7/12 ,  F05D2220/32 ,  F05D2260/231 ,  Y02T50/673 ,  Y02T50/676

Abstract: An assembly for a gas turbine engine includes a strut and a heat shield. The heat shield is disposed adjacent the strut and the heat shield and is adapted to contain a cooling air flow that passes along first cavity between the heat shield and the strut.

Abstract translation: 用于燃气涡轮发动机的组件包括支柱和隔热罩。 隔热屏布置在支柱和隔热屏附近，并且适于容纳通过隔热屏和支柱之间的第一腔的冷却空气流。

公开(公告)号：EP3203032A1

公开(公告)日：2017-08-09

申请号：EP17154476.0

申请日：2017-02-02

Applicant: United Technologies Corporation

Inventor： CHUONG, Conway

IPC: F01D9/04

CPC classification number: F01D9/041 ,  F05D2220/323 ,  F05D2230/10 ,  F05D2230/12 ,  F05D2230/18 ,  F05D2240/122 ,  F05D2260/81

Abstract: A method of calculating a throat area (66) of a section of a machinery includes outlining a boundary (68) of the throat area (66) of the section, selecting a plurality of inspection points (OD1-N, ID1-N, SS1-N, PS1-N) along the boundary (68) of the throat area (66), dividing the throat area (66) into a plurality of sections (S1-S8), calculating an individual area of each of the plurality of sections (S1-S8) and summing the individual areas of each of the plurality of sections (S1-S8) to calculate the throat area (66).

Abstract translation: 计算机器的一部分的喉部区域（66）的方法包括概述该部分的喉部区域（66）的边界（68），选择多个检查点（OD1-N，ID1-N，SS1 （66）的边界（68），将喉部区域（66）分成多个部分（S1-S8），计算多个部分中的每一个的单独区域 （S1-S8）并且对所述多个部分中的每个部分（S1-S8）的各个区域进行求和以计算咽喉区域（66）。

公开(公告)号：EP2938864A1

公开(公告)日：2015-11-04

申请号：EP13868022.8

申请日：2013-12-19

Applicant: United Technologies Corporation

Inventor： CHUONG, Conway ,  BUDNICK, Matthew

IPC: F02C7/20 ,  F01D25/28

CPC classification number: F02C7/28 ,  F01D9/02 ,  F01D11/005 ,  F01D25/162 ,  F01D25/28 ,  F05D2240/55

Abstract: An assembly for a gas turbine engine includes a component, a fairing, and a seal. The fairing is disposed adjacent to the component and defines a primary gas flow path. The fairing has a rib that is located outside of the primary flow path and extends from an outer surface of the fairing. The seal is disposed between the rib and the component.

公开(公告)号：EP2938863A1

公开(公告)日：2015-11-04

申请号：EP13868006.1

申请日：2013-12-17

Applicant: United Technologies Corporation

Inventor： BUDNICK, Matthew ,  CHUONG, Conway ,  SCOTT, Jonathan A.

IPC: F02C7/20 ,  F02C7/24 ,  F01D25/28

CPC classification number: F01D9/041 ,  F01D25/145 ,  F01D25/162 ,  F01D25/24 ,  F01D25/246 ,  F01D25/28 ,  F01D25/30 ,  F05D2220/32 ,  F05D2240/15 ,  F05D2260/231 ,  F05D2260/30 ,  F05D2260/31

Abstract: A turbine exhaust case comprises a frame, a fairing, a heat shield and a mechanical linkage. The frame comprises an outer ring, an inner ring, and a plurality of struts joining the outer ring and the inner ring. The fairing comprising a ring-strut-ring structure disposed within the frame. The heat shield is disposed between the frame and the fairing. The mechanical linkage couples the heat shield to the fairing. In one embodiment, the heat shield comprises a multi-piece heat shield that inhibits heat transfer between the frame and the fairing. In various embodiments, the mechanical linkage comprises a slip joint or a fixed joint for coupling the heat shield to the fairing.

公开(公告)号：EP2938857A1

公开(公告)日：2015-11-04

申请号：EP13868090.5

申请日：2013-12-19

Applicant: United Technologies Corporation

Inventor： BUDNICK, Matthew ,  CHUONG, Conway ,  SCOTT, Jonathan, Ariel

IPC: F02C7/12 ,  F01D25/12

CPC classification number: F01D25/14 ,  F01D5/081 ,  F01D9/02 ,  F01D9/065 ,  F01D25/12 ,  F01D25/145 ,  F01D25/162 ,  F01D25/24 ,  F02C7/12 ,  F05D2220/32 ,  F05D2260/231 ,  Y02T50/673 ,  Y02T50/676

Abstract: An assembly for a gas turbine engine includes a strut and a heat shield. The heat shield is disposed adjacent the strut and the heat shield and is adapted to contain a cooling air flow that passes along first cavity between the heat shield and the strut.

公开(公告)号：EP2938837A1

公开(公告)日：2015-11-04

申请号：EP13868215.8

申请日：2013-12-23

Applicant: United Technologies Corporation

Inventor： CHUONG, Conway ,  BUDNICK, Matthew

IPC: F01D11/02 ,  F01D25/24 ,  F02C7/28

CPC classification number: F01D11/001 ,  F01D11/003 ,  F01D11/005 ,  F01D25/162 ,  F01D25/24 ,  F01D25/246 ,  F02C7/28 ,  F05D2240/55

Abstract: A gas turbine engine assembly includes a second module connected axially to a first module along a joint, and an annular cavity defined between the first module and the second module. The seal assembly is disposed proximate the cavity, and includes a seal support ring, a first finger seal, and a second finger seal. The support ring has a backing portion secured to a radial wall of to the first module, and a first seal land extending axially into the cavity away from the first module. The first finger seal has a free end adapted to contact an inner side of the first seal land. The second finger seal is adapted to seal a radially outer portion of the annular cavity.