公开(公告)号：US10280798B2

公开(公告)日：2019-05-07

申请号：US14776719

申请日：2014-02-27

Applicant: United Technologies Corporation

Inventor： Paul K. Sanchez

IPC: F01D25/24 ,  F02C7/20 ,  B64D29/08 ,  F01D5/02 ,  F01D9/04 ,  F02C3/04

Abstract: A turbine engine includes a full ring fairing having at least a first and second keyed feature. The full ring fairing is rotatable so that the second keyed feature is in the first keyed feature position relative to the turbine engine.

公开(公告)号：US09982548B2

公开(公告)日：2018-05-29

申请号：US14890496

申请日：2014-06-25

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： John T. Ols ,  Karl A. Mentz ,  Richard N. Allen ,  Steven D. Porter ,  Renee J. Jurek ,  Paul K. Sanchez ,  Sandra S. Pinero

IPC: F01D9/04 ,  F01D5/14 ,  F01D5/02 ,  F01D25/24

CPC classification number: F01D9/041 ,  F01D5/02 ,  F01D5/143 ,  F01D9/04 ,  F01D25/246 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/303 ,  F05D2240/304 ,  F05D2240/80 ,  F05D2250/71 ,  F05D2250/90 ,  Y02T50/673

Abstract: An airfoil extends between radially inner and radially outer platforms. The airfoil extends between a leading edge and a trailing edge, and merges into facing surfaces of the radially inner and outer platforms. A variable fillet merges a facing surface of one of the radially inner and outer platforms into a wall of the airfoil. The variable fillet has a length extending away from a surface of the airfoil and a height extending away from the facing surface of at least one of the radially inner and outer platforms outwardly on to the airfoil. The variable fillet has a greater length at one of the leading edge and the trailing edge. A spaced portion has a shorter length at locations spaced from at least one of the leading and trailing edges. A mid-turbine frame and a gas turbine engine are also disclosed.

公开(公告)号：US20170044985A1

公开(公告)日：2017-02-16

申请号：US15340353

申请日：2016-11-01

Applicant: United Technologies Corporation

Inventor： Paul K. Sanchez ,  Kalpendu J. Parekh ,  William A. Daniels ,  John S. Tu

IPC: F02C7/20 ,  F02K3/04 ,  F02C7/12

CPC classification number: F01D25/14 ,  F01D25/12 ,  F01D25/16 ,  F01D25/162 ,  F01D25/24 ,  F01D25/246 ,  F02C7/12 ,  F02C7/20 ,  F02K3/04 ,  F05D2220/36 ,  F05D2260/20

Abstract: A turbine engine includes a compressor section, a combustor section in fluid communication with the compressor section, a high pressure turbine in fluid communication with the combustor, a low pressure turbine in fluid communication with the high pressure turbine, and a mid-turbine frame located axially between the high pressure turbine and the low pressure turbine. The mid-turbine frame includes an outer frame case, an inner frame case, and a plurality of hollow spokes that distribute loads from the inner frame case to the outer frame case. The spokes are hollow to allow cooling airflow to be supplied through the spokes to the inner frame case.

Abstract translation: 涡轮发动机包括压缩机部分，与压缩机部分流体连通的燃烧器部分，与燃烧器流体连通的高压涡轮机，与高压涡轮机流体连通的低压涡轮机和位于 轴向在高压涡轮机和低压涡轮机之间。 中间涡轮机框架包括外框架壳体，内框架壳体和多个中空轮辐，其将负载从内框架壳体分配到外框架壳体。 轮辐是中空的，以允许冷却气流通过轮辐供应到内框架壳体。

公开(公告)号：US20160362993A1

公开(公告)日：2016-12-15

申请号：US15245798

申请日：2016-08-24

Applicant: United Technologies Corporation

Inventor： Paul K. Sanchez ,  John S. Tu ,  Kalpendu J. Parekh ,  William A. Daniels

IPC: F01D9/06 ,  F02C3/04 ,  F01D25/12 ,  F01D25/28 ,  F01D25/24

CPC classification number: F01D9/065 ,  F01D25/12 ,  F01D25/162 ,  F01D25/24 ,  F01D25/28 ,  F02C3/04 ,  F02C6/08 ,  F02C7/12 ,  F05D2240/14 ,  F05D2240/55 ,  F05D2260/20 ,  Y02T50/676

Abstract: A mid-turbine frame (MTF) for a gas turbine engine includes an inner manifold directing air to a turbine rotor of the gas turbine engine. The MTF includes an outer MTF case and an inner MTF case. The inner manifold of the MTF is located in the inner case of the MTF.

Abstract translation: 用于燃气涡轮发动机的中涡轮机架（MTF）包括将空气引导到燃气涡轮发动机的涡轮机转子的内部歧管。 MTF包括外部MTF情况和内部MTF情况。 MTF的内部歧管位于MTF的内部情况。

公开(公告)号：US20160230598A1

公开(公告)日：2016-08-11

申请号：US14617506

申请日：2015-02-09

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Anthony P. Cherolis ,  Jeffrey J. Lienau ,  Robert Newman ,  John H. Mosley ,  Joshua Daniel Winn ,  Paul K. Sanchez

IPC: F01D25/14 ,  F01D25/24 ,  F01D25/12

CPC classification number: F01D25/14 ,  F01D9/065 ,  F01D25/12 ,  F01D25/162 ,  F01D25/24 ,  F02C7/12 ,  F05D2220/32 ,  F05D2220/3213 ,  F05D2260/20 ,  F05D2260/31 ,  Y02T50/676

Abstract: A mid-turbine frame assembly includes an inner frame case which includes a first plurality of holes and a second plurality of holes. A plurality of tie rods is circumferentially spaced around the inner frame case and includes an inlet passage that is aligned with the first plurality of holes. A plurality of hollow airfoils is aligned with the second plurality of holes.

Abstract translation: 中间涡轮机框架组件包括内框架壳体，其包括第一多个孔和第二多个孔。 多个拉杆围绕内框架周向隔开并包括与第一多个孔对准的入口通道。 多个中空翼型件与第二多个孔对准。

公开(公告)号：US20160222827A1

公开(公告)日：2016-08-04

申请号：US14612469

申请日：2015-02-03

Applicant: United Technologies Corporation

Inventor： Joshua Daniel Winn ,  Alexander Broulidakis ,  Paul K. Sanchez ,  Anthony P. Cherolis ,  Joseph J. Sedor ,  Christopher Treat

IPC: F01D25/28 ,  F01D25/26 ,  F01D25/12 ,  F01D5/02

CPC classification number: F01D25/28 ,  F01D5/02 ,  F01D9/065 ,  F01D25/12 ,  F01D25/162 ,  F01D25/26 ,  F02C7/12 ,  F05D2220/32 ,  F05D2220/3213 ,  F05D2240/24 ,  F05D2260/20 ,  F05D2260/31 ,  Y02T50/676

Abstract: A fastener assembly includes a first component that includes a bushing opening. A second component includes a fastener opening. A threaded bushing is at least partially located within the bushing opening. A fastener extends through the fastener opening and engages the bushing.

Abstract translation: 紧固件组件包括包括衬套开口的第一部件。 第二部件包括紧固件开口。 螺纹衬套至少部分地位于衬套开口内。 紧固件延伸穿过紧固件开口并接合衬套。