公开(公告)号：JP2013040608A

公开(公告)日：2013-02-28

申请号：JP2012179160

申请日：2012-08-13

Applicant: United Technologies Corp ,  ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation

Inventor： FEINDEL DAVID T ,  PALMER PAUL W ,  BURT JONATHAN P ,  FRICK RAYMOND N

IPC: F01D25/16 ,  F01D25/28 ,  F02C7/00 ,  F02C7/06 ,  F02C7/20

CPC classification number: F01D25/164 ,  Y10T29/49323

Abstract: PROBLEM TO BE SOLVED: To provide a support arrangement that can manage a load within a turbomachine.SOLUTION: An example turbomachine load management assembly includes a support rod extending from a first rod end to a second rod end that is moveable radially relative to a fan duct, a bearing housing, or both, when the support rod couples the fan duct and the bearing housing.

Abstract translation: 要解决的问题：提供可以管理涡轮机内的负载的支撑装置。 解决方案：一个例子涡轮机负载管理组件包括从第一杆端延伸到第二杆端的支撑杆，当支撑杆联接风扇时，第二杆端可相对于风扇管道，轴承壳体或两者径向移动 管道和轴承箱。 版权所有（C）2013，JPO＆INPIT

公开(公告)号：WO2014031205A2

公开(公告)日：2014-02-27

申请号：PCT/US2013042966

申请日：2013-05-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PORTER STEVEN D ,  BURT JONATHAN P ,  JAKIEL JONATHAN J ,  GORDON AMY M ,  DUELM SHELTON O

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

CPC classification number: F16J15/0887 ,  F01D9/02 ,  F01D11/005 ,  F01D11/08 ,  F02C7/28

Abstract: A seal land for a gas turbine engine can include a seal body circumferentially extending about a longitudinal centerline axis. The seal body includes at least one sealing surface that extends in a plane that is transverse to the longitudinal centerline axis.

Abstract translation: 用于燃气涡轮发动机的密封面可以包括围绕纵向中心线轴线周向延伸的密封体。 密封体包括至少一个密封表面，该密封表面在横向于纵向中心线轴线的平面中延伸。

公开(公告)号：WO2014051656A3

公开(公告)日：2015-06-18

申请号：PCT/US2013020832

申请日：2013-01-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FARAH JORGE I ,  BURT JONATHAN P ,  STEWART DANA P

IPC: F04D29/34

CPC classification number: F01D9/042 ,  B23P15/04 ,  F01D9/044 ,  F04D29/544

Abstract: A turbine engine vane arrangement and a method for manufacturing a turbine engine vane arrangement are provided. The vane arrangement includes a plurality of vane arrangement segments arranged circumferentially around an axial centerline. Each of the vane arrangement segments includes an airfoil that extends radially between a first platform segment and a second platform segment. The first platform segment extends circumferentially between a first mate face and a second mate face. The first mate face of a first of the vane arrangement segments is bonded to the second mate face of a second of the vane arrangement segments.

Abstract translation: 提供了一种涡轮发动机叶片装置和用于制造涡轮发动机叶片装置的方法。 叶片装置包括沿轴向中心线周向布置的多个叶片装置段。 每个叶片装置段包括在第一平台段和第二平台段之间径向延伸的翼型件。 第一平台段在第一配合面和第二配合面之间周向延伸。 第一叶片装置段的第一配合面接合到第二叶片装置段的第二配合面。

公开(公告)号：EP2855889A4

公开(公告)日：2016-01-13

申请号：EP13801167

申请日：2013-05-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GORDON AMY M ,  JAKIEL JONATHAN J ,  BURT JONATHAN P ,  PORTER STEVEN D

IPC: F02C7/28 ,  F01D11/00 ,  F01D25/16 ,  F02C3/00

CPC classification number: F04D29/083 ,  F01D11/005 ,  F01D25/162 ,  F02C7/28 ,  F04D29/542

Abstract: A seal land for a gas turbine engine can include a seal body that can extend between a leading edge portion, a trailing edge portion, a radially outer surface and a radially inner surface. A notch can extend at least partially through the seal body between the radially outer surface and the radially inner surface.

公开(公告)号：EP2900973A4

公开(公告)日：2016-11-23

申请号：EP13842236

申请日：2013-09-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FARAH JORGE I ,  BURT JONATHAN P ,  SANCHEZ PAUL K ,  PAREKH KALPENDU J ,  JAKIEL JONATHAN J

IPC: F02C7/20 ,  F01D25/24 ,  F01D25/26 ,  F02C3/073 ,  F02C3/13

CPC classification number: F01D25/28 ,  F01D25/162 ,  F01D25/24 ,  F01D25/26 ,  F02C7/20 ,  F05D2240/91

Abstract: A mid-turbine frame (MTF) system for a gas turbine engine is disclosed. The MTF includes an inner case, an outer case and a fairing sandwiched between the inner and outer cases. The fairing includes an inner ring spaced apart from and coupled to an outer ring by a plurality of hollow struts. The hollow struts accommodate support rods that connect the inner case to the outer case. Further, the hollow struts act as turning vanes for turning the flow of gases passing from a high pressure turbine (HPT) to a low pressure turbine (LPT) for purposes of providing the correct incidence angle to the first vane of the LPT. The outer ring of the fairing includes a plurality of bosses which receive attachment pins that pass through the outer case for correctly locating the fairing with respect to the outer case and for permitting radial expansion in contraction of the fairing.

Abstract translation: 公开了一种用于燃气涡轮发动机的中涡轮机架（MTF）系统。 MTF包括夹在内壳和外壳之间的内壳，外壳和整流罩。 整流罩包括通过多个中空支柱间隔开并与外环连接的内环。 中空支柱适应将内壳连接到外壳的支撑杆。 此外，为了向LPT的第一叶片提供正确的入射角，中空支柱用作用于将从高压涡轮机（HPT）流过的气体流转向低压涡轮（LPT）的转向叶片。 整流罩的外圈包括多个凸台，其接收穿过外壳的连接销，以便正确地将整流罩相对于外壳定位并允许整流罩收缩的径向膨胀。

公开(公告)号：EP2901022A4

公开(公告)日：2016-05-04

申请号：EP13841332

申请日：2013-01-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FARAH JORGE I ,  BURT JONATHAN P ,  STEWART DANA P

IPC: F04D29/34 ,  B23P15/04 ,  F01D9/04 ,  F04D29/54

CPC classification number: F01D9/042 ,  B23P15/04 ,  F01D9/044 ,  F04D29/544

Abstract: A turbine engine vane arrangement and a method for manufacturing a turbine engine vane arrangement are provided. The vane arrangement includes a plurality of vane arrangement segments arranged circumferentially around an axial centerline. Each of the vane arrangement segments includes an airfoil that extends radially between a first platform segment and a second platform segment. The first platform segment extends circumferentially between a first mate face and a second mate face. The first mate face of a first of the vane arrangement segments is bonded to the second mate face of a second of the vane arrangement segments.

公开(公告)号：EP2817496A4

公开(公告)日：2015-12-23

申请号：EP13751563

申请日：2013-02-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FARAH JORGE I ,  KAPUSTKA THEODORE W ,  BURT JONATHAN P ,  JAKIEL JONATHAN J ,  STEWART DANA P

IPC: F02C7/00 ,  B23K1/00 ,  B23K101/00 ,  F01D9/02 ,  F01D9/04 ,  F01D9/06 ,  F01D25/16 ,  F01D25/24

CPC classification number: F01D25/162 ,  B23K1/0018 ,  B23K2201/001 ,  F01D9/04 ,  F01D9/044 ,  F01D9/065 ,  F01D25/246 ,  F05D2230/237

公开(公告)号：EP2855892A4

公开(公告)日：2016-03-09

申请号：EP13830737

申请日：2013-05-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PORTER STEVEN D ,  BURT JONATHAN P ,  JAKIEL JONATHAN J ,  GORDON AMY M ,  DUELM SHELTON O

IPC: F02C7/28 ,  F01D9/02 ,  F01D11/00 ,  F01D11/08 ,  F01D25/24 ,  F16J15/08

CPC classification number: F16J15/0887 ,  F01D9/02 ,  F01D11/005 ,  F01D11/08 ,  F02C7/28

Abstract: A seal land for a gas turbine engine can include a seal body circumferentially extending about a longitudinal centerline axis. The seal body includes at least one sealing surface that extends in a plane that is transverse to the longitudinal centerline axis.

公开(公告)号：EP2875226A4

公开(公告)日：2016-02-24

申请号：EP13819314

申请日：2013-07-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BURT JONATHAN P ,  SANDOVAL JONATHAN PERRY

IPC: F02C7/28 ,  F01D11/00 ,  F02C7/32

CPC classification number: F01D5/3015 ,  F01D5/066 ,  F05D2260/30 ,  F05D2260/33 ,  Y10T29/4932

Abstract: An assembly for connecting a coverplate and a rotor includes a first rotor for use in a rotating engine; a first cover mounted to the first rotor, wherein the rotor and the cover create a space there between, the space for having cooling air therein; and a lock assembly for preventing the cover from rotating circumferentially or moving axially away from the rotor if mounted to the to the rotor wherein the cover is sealed against the rotor.