公开(公告)号：WO2014052007A1

公开(公告)日：2014-04-03

申请号：PCT/US2013/059195

申请日：2013-09-11

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： FARAH, Jorge, I. ,  BURT, Jonathan, P. ,  SANCHEZ, Paul, K. ,  PAREKH, Kalpendu, J. ,  JAKIEL, Jonathan J.

IPC: F02C7/20 ,  F01D25/24 ,  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圈。 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，中空支柱用作转动叶片，用于将从高压涡轮（HPT）通过的气体流转向低压涡轮机（LPT）。 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：WO2014051656A2

公开(公告)日：2014-04-03

申请号：PCT/US2013/020832

申请日：2013-01-09

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： FARAH, Jorge, I. ,  BURT, Jonathan, P. ,  STEWART, Dana, P.

IPC: F02C7/28

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: 提供涡轮发动机叶片装置和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结合到第二叶片装置段的第二配合面。