公开(公告)号：EP2872683A4

公开(公告)日：2015-07-29

申请号：EP13815972

申请日：2013-06-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HASKO GREGORY H ,  MCCAFFREY MICHAEL G

IPC: D03D13/00 ,  D03D23/00 ,  D03D41/00 ,  D03D47/12

CPC classification number: D03D23/00 ,  D03D41/004 ,  D03D47/12

Abstract: An exemplary weaving method includes placing a first section of a fill fiber between warp fibers, forming a pick, moving a base to reposition the warp fibers, and placing a second section of the fill fiber between the warp fibers.

公开(公告)号：EP2872763A4

公开(公告)日：2015-07-15

申请号：EP13819631

申请日：2013-07-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MCCAFFREY MICHAEL G

IPC: F02C7/00 ,  F01D11/00 ,  F01D11/12 ,  F01D11/24 ,  F01D25/12 ,  F02C7/12 ,  F02C7/28

CPC classification number: F01D11/127 ,  F01D11/12 ,  F01D11/24 ,  F01D25/12 ,  F05D2260/22141 ,  Y10T29/49245

Abstract: A blade outer air seal (BOAS) for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a seal body having a radially inner face and a radially outer face that axially extend between a leading edge portion and a trailing edge portion. At least one cooling fin is disposed on the radially outer face between the leading edge portion and the trailing edge portion.

公开(公告)号：EP3102794A4

公开(公告)日：2017-12-06

申请号：EP15740665

申请日：2015-01-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MCCAFFREY MICHAEL G

IPC: F01D11/14 ,  F01D11/08

CPC classification number: F01D11/12 ,  F01D5/02 ,  F01D11/08 ,  F01D11/16 ,  F01D25/246 ,  F02C3/04 ,  F04D29/164 ,  F04D29/321 ,  F05D2220/32 ,  F05D2240/11 ,  F05D2260/30 ,  F05D2260/38 ,  F05D2260/52 ,  Y02T50/672

Abstract: The present disclosure relates generally to blade outer air seal section mount including a resilient spring element that acts to provide re-centering forces to the blade outer air seal section when non-uniform forces applied to the blade outer air seal section causing it to move away from its nominal position.

公开(公告)号：EP3102793A4

公开(公告)日：2017-12-06

申请号：EP14879923

申请日：2014-11-14

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MCCAFFREY MICHAEL G

IPC: F01D5/30 ,  F01D11/00

CPC classification number: F01D11/006 ,  F01D5/02 ,  F01D5/12 ,  F01D5/3015 ,  F01D11/003 ,  F01D11/005 ,  F02C3/04 ,  F04D29/083 ,  F04D29/324 ,  F05D2220/32 ,  F05D2240/35 ,  F05D2240/55 ,  F05D2250/71 ,  Y02T50/672

Abstract: A toggle seal, for use with a rim seal, including: a seal body, a proximal end and a distal end, a first end seal extending in a first axial direction from the proximal end of the seal body, a second end seal extending in the first axial direction from the distal end of the seal body, a first protruding portion extending in a second axial direction from the proximal end, opposite of the first end seal, and a second protruding portion extending in the second axial direction from the distal end, opposite of the second end seal, wherein the first end seal is configured to operatively engage the wheel disk and the second end seal is configured to operatively engage the at least one blade.

公开(公告)号：EP3055273A4

公开(公告)日：2017-06-28

申请号：EP14876992

申请日：2014-09-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： AMINI SHAHRAM ,  SCHMIDT WAYDE R ,  KASHYAP TANIA BHATIA ,  HERMANN MARK A ,  SHEEDY PAUL ,  LIMARGA ANDI M ,  MCCAFFREY MICHAEL G

IPC: C04B35/64 ,  C04B35/645

CPC classification number: B28B1/24 ,  B28B1/52 ,  B28B11/243 ,  C04B35/524 ,  C04B35/532 ,  C04B35/806 ,  C04B38/0022 ,  C04B2235/48 ,  C04B2235/5252 ,  C04B2235/602 ,  C04B2235/616

公开(公告)号：EP3049626A4

公开(公告)日：2017-06-21

申请号：EP14846447

申请日：2014-09-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DUELM SHELTON O ,  MCCAFFREY MICHAEL G

IPC: F01D5/28 ,  F01D9/04

CPC classification number: F01D5/282 ,  F01D5/147 ,  F01D5/284 ,  F01D9/041 ,  F05D2240/122 ,  F05D2300/6033

Abstract: An airfoil component includes an insert that has angled faces joined at an edge that provides an airfoil trailing edge. An outer CMC fiber layer overlaps the angled faces to provide a trailing edge portion of an airfoil.

Abstract translation: 翼型构件包括插入件，该插入件具有在提供翼型后缘的边缘处连接的成角度的面。 外CMC纤维层与倾斜面重叠以提供翼型的后缘部分。

公开(公告)号：EP3046892A4

公开(公告)日：2017-05-10

申请号：EP14854030

申请日：2014-09-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MCCAFFREY MICHAEL G ,  BERCZIK DOUGLAS M

IPC: C04B35/52 ,  C04B35/626 ,  C04B35/64 ,  C04B35/80 ,  F02C7/00

CPC classification number: C04B38/0615 ,  B05D3/007 ,  C04B35/573 ,  C04B35/6267 ,  C04B35/806 ,  C04B41/89 ,  C04B2235/3821 ,  C04B2235/3826 ,  C04B2235/3873 ,  C04B2235/428 ,  C04B2235/5248 ,  C04B2235/5252 ,  C04B2235/5256 ,  C04B2235/614 ,  C04B2235/616 ,  C04B35/52 ,  C04B38/0096

Abstract: A method of densifying a CMC article includes the steps of pyrolyzing a CMC article until a desired initial porosity is achieved, coating CMC pores within the CMC article with carbon, pyrolyzing the carbon to form carbon pores, coating the carbon pores with silicon, and heat treating the CMC article to create a silicon carbide filled pore integrated with silicon carbide of the CMC article to densify the CMC article.

Abstract translation: 使CMC制品致密化的方法包括以下步骤：热解CMC制品直到获得所需的初始孔隙率;用CMC涂覆CMC制品内的CMC孔;热解碳形成碳孔;用硅涂覆碳孔;加热 处理CMC制品以产生与CMC制品的碳化硅整合的碳化硅填充的孔隙以使CMC制品致密化。

公开(公告)号：EP3097273A4

公开(公告)日：2017-01-25

申请号：EP15737519

申请日：2015-01-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MCCAFFREY MICHAEL G

IPC: F01D11/08 ,  F01D25/24

CPC classification number: F01D11/08 ,  F01D5/02 ,  F01D25/24 ,  F01D25/246 ,  F02C3/04 ,  F04D29/164 ,  F04D29/321 ,  F04D29/526 ,  F05D2220/32 ,  F05D2240/11 ,  F05D2240/35 ,  F05D2260/30 ,  F05D2300/6033 ,  Y02T50/672

Abstract: One exemplary embodiment of this disclosure relates to a system having a static segment with a circumferentially extending slot. The system further includes a retention clip partially received in the slot, and partially contacting a circumferential end of the static segment.

公开(公告)号：EP2964903A4

公开(公告)日：2016-12-21

申请号：EP14801010

申请日：2014-03-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MCCAFFREY MICHAEL G ,  BORJA MARK ,  ROUSE BRANDON T ,  FARRIS JOHN R ,  PELLETIER BRIAN R ,  ALMY THOMAS ,  GARCIA IGOR S

IPC: F01D11/14 ,  F01D5/02 ,  F01D11/18 ,  F01D11/20 ,  F01D11/22 ,  F01D11/24 ,  F01D25/24

CPC classification number: F01D11/18 ,  F01D5/02 ,  F01D11/22 ,  F01D11/24 ,  F01D25/24 ,  F05D2220/32 ,  F05D2240/55 ,  F05D2270/52 ,  F05D2270/62

Abstract: A control ring extends circumferentially about a central axis. A plurality of circumferentially spaced carrier portions have a cavity receiving the control ring. There are circumferential gaps between the carrier portions. A blade outer air seal is mounted on the carrier portions radially inwardly of the control ring. The control ring maintains the carrier portions at a radially outwardly expanded position when heated by an electric heater.

公开(公告)号：EP3022406A4

公开(公告)日：2016-08-31

申请号：EP14825748

申请日：2014-06-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： COOK GRANT O III ,  ABBOTT MICHAEL G ,  MCCAFFREY MICHAEL G

IPC: F01D25/28 ,  F01D5/02 ,  F01D5/28 ,  F01D9/04

CPC classification number: F01D5/284 ,  F01D5/282 ,  F01D9/042 ,  F01D9/044 ,  F05D2230/23 ,  F05D2230/236 ,  F05D2300/6033 ,  Y02T50/672

Abstract: A gas turbine engine component assembly includes first and second portions, wherein at least one of the first and second portions is a ceramic material. The first portion includes an aperture having a first angled surface. The second portion is disposed within the aperture and includes a second angled surface adjacent to the first angled surface. The first and second angled surfaces lock the first and second portions to one another under a pulling load. A bonding material operatively secures the first and second angled surfaces to one another.

Abstract translation: 燃气涡轮发动机部件组件包括第一和第二部分，其中第一部分和第二部分中的至少一个是陶瓷材料。 第一部分包括具有第一倾斜表面的孔。 第二部分设置在孔内并且包括与第一倾斜表面相邻的第二倾斜表面。 第一和第二倾斜表面在牵引载荷下将第一和第二部分彼此锁定。 接合材料将第一和第二倾斜表面相互操作地固定。