公开(公告)号：EP2834471A4

公开(公告)日：2016-06-01

申请号：EP13813158

申请日：2013-03-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DUBE DAVID P ,  HAYFORD RICHARD K

IPC: F01D9/02 ,  F01D5/10 ,  F01D17/16 ,  F02C9/22 ,  F04D29/56

CPC classification number: F01D17/162 ,  F01D5/10 ,  F04D29/023 ,  F04D29/563 ,  F04D29/668 ,  F05D2230/23 ,  F05D2260/96 ,  F05D2300/43 ,  F05D2300/431 ,  F05D2300/437 ,  Y10T29/49863

Abstract: A variable vane assembly includes a damper positioned between a platform and a trunnion. The damper is comprised of a resilient material.

公开(公告)号：EP3097270A4

公开(公告)日：2017-09-13

申请号：EP14879918

申请日：2014-12-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HAYFORD RICHARD K ,  ROGERS MARK J ,  CARMAN KENNETH E ,  RICHARDSON CARL S ,  EARL JONATHAN J

IPC: F01D9/02 ,  F01D9/04 ,  F01D25/24 ,  F04D29/02

CPC classification number: F04D29/542 ,  F01D9/042 ,  F04D29/023 ,  F04D29/522 ,  F04D29/644 ,  F05B2220/302 ,  F05B2240/124 ,  F05B2280/10743 ,  F05B2280/50032 ,  F05D2220/3219 ,  F05D2230/642 ,  F05D2240/129 ,  F05D2300/177 ,  F05D2300/50212

Abstract: A gas turbine engine includes a circumferential array of vanes slidably supported in an inner case shroud segment. Multiple segments are secured to one another to provide an annular engine static structure section. The inner case shroud segment and the vanes have different material properties than one another.

Abstract translation: 燃气涡轮发动机包括可滑动地支撑在内壳罩段中的周向叶片阵列。 多个部分彼此固定以提供环形发动机静态结构部分。 内壳罩段和叶片具有彼此不同的材料特性。

公开(公告)号：EP2971611A4

公开(公告)日：2016-10-19

申请号：EP14776516

申请日：2014-02-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HAYFORD RICHARD K ,  LUTJEN PAUL M

IPC: F01D25/24 ,  F01D11/08 ,  F01D25/00 ,  F04D29/02 ,  F04D29/08 ,  F04D29/16 ,  F04D29/52 ,  F04D29/64 ,  F16L23/032

CPC classification number: F01D25/28 ,  F01D11/08 ,  F01D25/24 ,  F01D25/243 ,  F02C3/04 ,  F02C7/28 ,  F04D29/023 ,  F04D29/083 ,  F04D29/164 ,  F04D29/526 ,  F04D29/644 ,  F05D2220/30 ,  F05D2230/31 ,  F05D2230/60 ,  F05D2240/11 ,  F05D2240/55 ,  F05D2300/50212

Abstract: A turbine engine case spacer includes an air seal and a flange. The air seal is snap fit to the flange, and each flange includes at least two distinct material layers.

公开(公告)号：EP3097274A4

公开(公告)日：2017-10-04

申请号：EP14876467

申请日：2014-12-19

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BLANEY KEN F ,  HAYFORD RICHARD K ,  JAROCHYM CHRISTOPHER M

IPC: F01D11/22

CPC classification number: F01D11/20 ,  F01D5/12 ,  F01D11/22 ,  F01D25/24 ,  F05D2240/11 ,  F05D2270/64 ,  F05D2270/65

公开(公告)号：EP2825759A4

公开(公告)日：2015-03-25

申请号：EP13761620

申请日：2013-03-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HAYFORD RICHARD K ,  DUBE DAVID P

IPC: F01D17/16 ,  F01D11/00

CPC classification number: F01D17/162 ,  F01D11/005 ,  F04D29/563 ,  F05D2300/43 ,  Y10T29/49321

Abstract: A variable stator vane assembly for a gas turbine engine includes a variable stator vane and a non-structural fairing on the variable stator vane.

公开(公告)号：EP3052766A4

公开(公告)日：2017-08-09

申请号：EP14864145

申请日：2014-09-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROGERS MARK J ,  RICHARDSON CARL S ,  HAYFORD RICHARD K ,  CARMEN KENNETH E ,  EARL JONATHAN

IPC: F01D11/00 ,  B01D46/00 ,  F01D9/04

CPC classification number: F01D11/005 ,  F01D9/041 ,  F01D11/001 ,  F01D11/08 ,  F01D25/04 ,  F05D2220/32 ,  F05D2260/52

Abstract: A vane seal system includes a first non-rotatable vane segment that has a first airfoil with a first pocket at one end thereof. A second non-rotatable vane segment includes a second airfoil with a second pocket at one end thereof spaced by a gap from the first pocket. A seal member spans across the gap and extends in the first pocket and the second pocket. The seal member includes a seal element and at least one spring portion configured to positively locate the seal member in a sealing direction. Also disclosed is a seal for a vane seal system and a method related thereto for damping relative movement between a first pocket and a second pocket.

Abstract translation: 叶片密封系统包括第一不可旋转的叶片段，该第一不可旋转叶片段具有第一翼型，其一端具有第一凹穴。 第二不可旋转叶片段包括第二翼型件，该第二翼型件在其一端具有与第一凹口间隔开间隙的第二凹口。 密封构件跨越间隙并延伸在第一袋和第二袋中。 密封构件包括密封元件和构造成将密封构件沿密封方向可靠地定位的至少一个弹簧部分。 还公开了一种用于叶片密封系统的密封件及其相关方法，用于阻尼第一袋和第二袋之间的相对运动。

公开(公告)号：EP2941540A4

公开(公告)日：2016-10-19

申请号：EP13868210

申请日：2013-12-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HAYFORD RICHARD K ,  LUTJEN PAUL M

IPC: F01D5/28 ,  F01D5/14

CPC classification number: F01D5/28 ,  F01D5/148 ,  F02C3/04 ,  F05D2220/32 ,  F05D2300/10 ,  F05D2300/50212 ,  Y02T50/673

Abstract: An airfoil includes an airfoil body having a first section and a second section that differ by coefficient of thermal expansion. The second section is arranged in thermomechanical juxtaposition with the first section such that the first section and the second section cooperatively thermomechanically control a profile of the airfoil body responsive to varying thermal conditions.

公开(公告)号：EP2935841A4

公开(公告)日：2016-08-31

申请号：EP13863826

申请日：2013-12-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DUBE DAVID P ,  FEIGLESON STEVEN J ,  HAYFORD RICHARD K

IPC: F02C9/22 ,  F01D17/16 ,  F01D25/16 ,  F01D25/28

CPC classification number: F01D5/147 ,  F01D17/16 ,  F01D17/162 ,  F01D25/16 ,  F01D25/28 ,  Y02T50/672 ,  Y10T29/49826 ,  Y10T156/10

Abstract: A variable vane includes a variable vane body that has an airfoil portion. The variable vane body is formed of a first material. A trunnion is attached at one end of the variable vane body. The trunnion includes a pivot formed of a second, different material.

公开(公告)号：EP2880278A4

公开(公告)日：2015-09-09

申请号：EP13825230

申请日：2013-07-10

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TATMAN NEIL L ,  HAYFORD RICHARD K

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

CPC classification number: F01D9/042 ,  F01D11/08 ,  F01D25/246 ,  F05D2240/11 ,  F05D2260/30 ,  Y10T29/49245 ,  Y10T74/20636

公开(公告)号：EP3102792A4

公开(公告)日：2017-11-22

申请号：EP14879341

申请日：2014-12-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HAYFORD RICHARD K ,  MORRIS ROBERT J ,  WARNER CHARLES H ,  GENDRICH CHARLES P

IPC: F01D5/26 ,  F01D9/02 ,  F01D9/04 ,  F01D25/06 ,  F04D29/54 ,  F04D29/66

CPC classification number: F04D29/668 ,  F01D5/26 ,  F01D9/041 ,  F01D9/042 ,  F01D25/06 ,  F04D29/542 ,  F04D29/544 ,  F04D29/666 ,  F05D2220/32 ,  F05D2260/961 ,  Y02T50/671 ,  Y02T50/673

Abstract: A gas turbine engine includes a circumferential array of stator vanes that have first and second vanes with different vibrational frequencies than one another. The first vanes are arranged in circumferentially alternating relationship with the second vanes.