公开(公告)号：EP2935799A1

公开(公告)日：2015-10-28

申请号：EP13866382.8

申请日：2013-12-19

Applicant: United Technologies Corporation

Inventor： DUELM, Shelton O. ,  MCCAFFREY, Michael G.

IPC: F01D9/04 ,  F01D9/02 ,  F02C7/00

CPC classification number: F01D5/284 ,  F01D9/041 ,  F01D25/162 ,  F05D2230/23 ,  F05D2300/6033 ,  Y02T50/672 ,  Y02T50/673

Abstract: A vane assembly for a gas turbine engine is disclosed and includes a plurality of individual vane segments forming an annular ring. Each of the plurality of vane segments is formed of a ceramic matrix composite including at least one airfoil extending between an inner platform and an outer platform. An outer wrap is disposed about an outer periphery of the annular ring and over an interface between outer platforms of adjacent ones of the plurality of vane segments.

公开(公告)号：EP3239471B1

公开(公告)日：2020-05-27

申请号：EP17167027.6

申请日：2017-04-19

Applicant: United Technologies Corporation

Inventor： PETERS, Christopher J. ,  DUELM, Shelton O.

IPC: F01D11/00 ,  F01D11/02 ,  F02C7/28 ,  F16J15/44

公开(公告)号：EP2961938B1

公开(公告)日：2019-12-18

申请号：EP14798232.6

申请日：2014-02-12

Applicant: United Technologies Corporation

Inventor： DUELM, Shelton O. ,  MCCAFFREY, Michael G.

IPC: F01D9/02 ,  F01D5/28 ,  F04D29/38 ,  F01D9/06 ,  F01D9/04 ,  F01D25/16

公开(公告)号：EP2984292B1

公开(公告)日：2018-06-06

申请号：EP14836531.5

申请日：2014-04-11

Applicant: United Technologies Corporation

Inventor： DUELM, Shelton O. ,  RUGG, Kevin L.

IPC: F01D9/02 ,  F01D25/28 ,  F02C7/20 ,  F01D5/22 ,  F01D9/04 ,  F01D25/24

CPC classification number: F01D9/042 ,  F01D25/246 ,  Y02T50/672 ,  Y02T50/673

Abstract: Disclosed is a gas turbine engine that includes a plurality of stator vanes. Each of the stator vanes includes an airfoil section and a platform provided at an end of the airfoil section. The platforms are provided with flanges on opposed ends thereof, and the flanges are fastened to corresponding flanges of an adjacent one of the plurality of stator vanes.

公开(公告)号：EP3239471A1

公开(公告)日：2017-11-01

申请号：EP17167027.6

申请日：2017-04-19

Applicant: United Technologies Corporation

Inventor： PETERS, Christopher J. ,  DUELM, Shelton O.

IPC: F01D11/00 ,  F01D11/02 ,  F02C7/28 ,  F16J15/44

Abstract: Aspects of the disclosure are directed to a seal (300) comprising a support ring (204), at least one beam (310) coupled to the support ring (204), and a shoe (316) coupled to the at least one beam (310), the shoe (316) having an axial shoe face (316a) that includes a rounded edge that is configured to contact a support structure (222) face of a support structure (222) when the seal (300) is subjected to a load (350; 350'; 350") that is equal to or greater than a first threshold.

Abstract translation: 本公开的多个方面涉及包括支撑环（204），联接到支撑环（204）的至少一个梁（310）以及联接到所述至少一个梁（316）的鞋（316）的密封件（300） 所述鞋（316）具有轴向鞋面（316a），所述鞋面（316a）包括圆形边缘，所述圆形边缘构造成当所述密封件（300）经受所述密封件（300）时与支撑结构（222）的支撑结构 负载（350; 350'; 350“）等于或大于第一阈值。

公开(公告)号：EP3009608A1

公开(公告)日：2016-04-20

申请号：EP15187544.0

申请日：2015-09-30

Applicant: United Technologies Corporation

Inventor： CARR, Jesse M. ,  DUBE, Bryan P. ,  DUELM, Shelton O.

IPC: F01D9/04

Abstract: A vane assembly (60;... 560) includes inner and outer rings (62a, 62b; 162a, 162b), a plurality of segmented vane structures (64; 164) circumferentially-spaced around a central axis (A) and between the inner and outer rings (62a, 62b; 162a, 162b), and at least one spring (74;... 674) that mechanically traps the segmented vane structures (64; 164) in radial compression between the inner and outer rings (62a, 62b; 162a, 162b). Corresponding method for a vane assembly (60;... 560).

Abstract translation: 叶片组件（60; ... 560）包括内环和外环（62a，62b; 162a，162b），围绕中心轴线（A）周向间隔开的多个分段叶片结构（64; 164） 内部和外部环（62a，62b; 162a，162b）以及至少一个弹簧（74; ... 674），其在所述内圈和外圈（62a）之间以径向压缩机械地捕集所述分段的叶片结构（64; 164） ，62b; 162a，162b）。 叶片组件（60; ... 560）的相应方法。

公开(公告)号：EP2956625A1

公开(公告)日：2015-12-23

申请号：EP14751134.9

申请日：2014-01-29

Applicant: United Technologies Corporation

Inventor： CHANG, Hoyt Y. ,  DUELM, Shelton O.

IPC: F01D5/14 ,  F02C7/00

CPC classification number: F01D9/02 ,  F01D5/147 ,  F01D5/18 ,  F01D5/282 ,  F01D5/284 ,  F01D9/041 ,  F01D25/162 ,  F05D2220/32 ,  F05D2230/23 ,  F05D2230/60 ,  F05D2240/12 ,  F05D2240/121 ,  F05D2240/303 ,  F05D2300/2261 ,  F05D2300/44 ,  F05D2300/6012 ,  F05D2300/6033 ,  Y02T50/672 ,  Y02T50/673

Abstract: A vane assembly within a mid-turbine frame of a gas turbine engine includes an airfoil that extends between an outer platform and an inner platform. The airfoil includes an outer wall defining a leading edge of a first radius. An inner wall of the airfoil defines an inner cavity including a forward portion proximate the leading edge defining a second radius different than the first radius.

公开(公告)号：EP3049626B1

公开(公告)日：2020-11-25

申请号：EP14846447.2

申请日：2014-09-15

Applicant: United Technologies Corporation

Inventor： DUELM, Shelton O. ,  MCCAFFREY, Michael G.

IPC: F01D5/28 ,  F01D9/04

公开(公告)号：EP2935799B1

公开(公告)日：2020-05-06

申请号：EP13866382.8

申请日：2013-12-19

Applicant: United Technologies Corporation

Inventor： DUELM, Shelton O. ,  MCCAFFREY, Michael G.

IPC: F01D9/04 ,  F01D9/02 ,  F02C7/00 ,  F01D25/16

公开(公告)号：EP3009608B1

公开(公告)日：2019-10-30

申请号：EP15187544.0

申请日：2015-09-30

Applicant: United Technologies Corporation

Inventor： CARR, Jesse M. ,  DUBE, Bryan P. ,  DUELM, Shelton O.

IPC: F01D9/04