公开(公告)号：EP2971547B1

公开(公告)日：2020-01-01

申请号：EP13880304.4

申请日：2013-11-08

Applicant: United Technologies Corporation

Inventor： ALVANOS, Ioannis

IPC: F01D5/20 ,  F01D5/12 ,  F01D9/02 ,  F04D29/68

公开(公告)号：EP2820253B1

公开(公告)日：2019-08-28

申请号：EP13754366.6

申请日：2013-02-11

Applicant: United Technologies Corporation

Inventor： SUCIU, Gabriel L. ,  ALVANOS, Ioannis

IPC: F01D9/02 ,  F01D25/08 ,  F02C7/12 ,  F01D5/08 ,  F02C6/08 ,  F02C7/08

公开(公告)号：EP2820271B1

公开(公告)日：2019-04-03

申请号：EP13754271.8

申请日：2013-02-20

Applicant: United Technologies Corporation

Inventor： SUCIU, Gabriel L. ,  ALVANOS, Ioannis

IPC: F02C7/18 ,  F01D25/12 ,  F01D9/06

公开(公告)号：EP3208425A3

公开(公告)日：2017-11-08

申请号：EP17160228.7

申请日：2012-05-24

Applicant: United Technologies Corporation

Inventor： SUCIU, Gabriel L. ,  ALVANOS, Ioannis ,  DYE, Christopher M. ,  LEVASSEUR, Glenn

IPC: F01D5/28 ,  C04B35/80 ,  F01D5/14 ,  F01D5/22 ,  F01D11/00 ,  F01D25/24

CPC classification number: F01D25/246 ,  F01D5/147 ,  F01D5/225 ,  F01D5/282 ,  F01D5/284 ,  F01D11/008 ,  F05D2300/6033

Abstract: A Ceramic Matrix Composite (CMC) platform for an airfoil (66C) of a gas turbine engine (20) includes a CMC platform segment (86, 88) which at least partially defines an airfoil profile. A corresponding rotor disk assembly (64c) is also provided.

公开(公告)号：EP3208425A2

公开(公告)日：2017-08-23

申请号：EP17160228.7

申请日：2012-05-24

Applicant: United Technologies Corporation

Inventor： SUCIU, Gabriel L. ,  ALVANOS, Ioannis ,  DYE, Christopher M. ,  LEVASSEUR, Glenn

IPC: F01D5/28 ,  C04B35/80 ,  F01D5/14 ,  F01D5/22 ,  F01D11/00 ,  F01D25/24

CPC classification number: F01D25/246 ,  F01D5/147 ,  F01D5/225 ,  F01D5/282 ,  F01D5/284 ,  F01D11/008 ,  F05D2300/6033

Abstract: A Ceramic Matrix Composite (CMC) platform for an airfoil (66C) of a gas turbine engine (20) includes a CMC platform segment (86, 88) which at least partially defines an airfoil profile. A corresponding rotor disk assembly (64c) is also provided.

Abstract translation: 用于燃气涡轮发动机（20）的翼型件（66C）的陶瓷基质复合材料（CMC）平台包括CMC平台段（86,88），其至少部分地限定翼型轮廓。 还提供了相应的转子盘组件（64c）。

公开(公告)号：EP2969319A2

公开(公告)日：2016-01-20

申请号：EP13878807.0

申请日：2013-12-30

Applicant: United Technologies Corporation

Inventor： SUCIU, Gabriel L ,  DAS, Gopal ,  ALVANOS, Ioannis ,  MERRY, Brian D. ,  HILL, James D ,  PENDA, Allan R

IPC: B22F3/105 ,  B22F7/02

CPC classification number: B23K26/342 ,  B22F3/1055 ,  B22F5/009 ,  B33Y10/00 ,  C22C1/0458 ,  C22C1/0491 ,  Y02P10/295

Abstract: A process for manufacturing a turbine engine component includes the steps of: providing a powder containing gamma titanium aluminide; and forming a turbine engine component from said powder using a direct metal laser sintering technique.

公开(公告)号：EP2935837A1

公开(公告)日：2015-10-28

申请号：EP13865215.1

申请日：2013-12-19

Applicant: United Technologies Corporation

Inventor： HILL, James D. ,  SUCIU, Gabriel L. ,  ALVANOS, Ioannis ,  MERRY, Brian D.

IPC: F02C7/28 ,  F01D25/00 ,  F01D11/00

CPC classification number: F01D11/122 ,  F01D5/06 ,  F01D11/001 ,  F01D11/008 ,  F05D2220/32 ,  F05D2240/24 ,  F05D2240/55 ,  F05D2250/71

Abstract: A seal segment according to an exemplary aspect of the present disclosure includes, among other things, a first axial wall, a second axial wall radially spaced from the first axial wall and a radially outer wall that interconnects the first axial wall and the second axial wall. At least one curved member is radially inwardly offset from the radially outer wall and extending between the first and second axial walls.

公开(公告)号：EP2820253A1

公开(公告)日：2015-01-07

申请号：EP13754366.6

申请日：2013-02-11

Applicant: United Technologies Corporation

Inventor： SUCIU, Gabriel L. ,  ALVANOS, Ioannis

IPC: F01D9/02 ,  F01D25/08 ,  F02C7/12

CPC classification number: F02C6/08 ,  F01D5/08 ,  F02C7/08

Abstract: A gas turbine engine includes a heat exchanger, a diffuser case, a passageway and a nozzle assembly. The heat exchanger exchanges heat with a bleed airflow to provide a conditioned airflow. The diffuser case includes a plenum that receives the conditioned airflow. The passageway is fluidly connected between the heat exchanger and the diffuser case, and the conditioned airflow is communicated through the passageway and into the plenum. The nozzle assembly is in fluid communication with the plenum of the diffuser case to receive the conditioned airflow from the plenum.

Abstract translation: 燃气涡轮发动机包括热交换器，扩散器壳体，通道和喷嘴组件。 热交换器与排气流交换热量以提供调节气流。 扩散器壳体包括接收经调节气流的充气室。 通道在热交换器和扩散器壳体之间流体连接，并且经调节的气流通过通道并且进入增压室。 喷嘴组件与扩散器壳体的充气室流体连通以接收来自充气室的经调节的气流。

公开(公告)号：EP3640434A2

公开(公告)日：2020-04-22

申请号：EP19196577.1

申请日：2012-05-24

Applicant: United Technologies Corporation

Inventor： SUCIU, Gabriel L. ,  ALVANOS, Ioannis ,  DYE, Christopher M. ,  LEVASSEUR, Glenn

IPC: F01D5/28 ,  C04B35/80 ,  F01D5/14 ,  F01D5/22 ,  F01D11/00 ,  F01D25/24

Abstract: A Ceramic Matrix Composite (CMC) platform for an airfoil (66C) of a gas turbine engine (20) includes a CMC platform segment (86,88) which at least partially defines an airfoil profile.

公开(公告)号：EP3009613B1

公开(公告)日：2019-01-30

申请号：EP15178341.2

申请日：2015-07-24

Applicant: United Technologies Corporation

Inventor： ALVANOS, Ioannis

IPC: F01D11/04 ,  F01D11/00