公开(公告)号：US09920651B2

公开(公告)日：2018-03-20

申请号：US14598492

申请日：2015-01-16

Applicant: United Technologies Corporation

Inventor： Anthony P. Cherolis ,  John H. Mosley ,  Kalpendu J. Parekh ,  Christopher Treat ,  Alberto A. Mateo

IPC: F01D25/14 ,  F01D25/24 ,  F01D9/06 ,  F02C7/12 ,  F01D25/16 ,  F01D25/12

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

Abstract: A mid-turbine frame for a gas turbine engine includes an inner frame case that includes a fluid passage. At least one spoke includes an inlet passage with at least one branch extending in an axial direction in fluid communication with the fluid passage in the inner frame case. A fitting fluidly connects the at least one branch to the fluid passage in the inner frame case. The fitting also includes a transfer tube connecting the cooling airflow passage to a cup boss. The transfer tube is fixed relative to the cylindrical portion and moveable relative to the cup boss. A swirler tube is in fluid communication with the fluid passage and is configured to direct cooling airflow in a radial inward and downstream direction.

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：US20150233295A1

公开(公告)日：2015-08-20

申请号：US14429167

申请日：2013-03-01

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Jorge I. Farah ,  Kalpendu J. Parekh

IPC: F02C7/18 ,  F02C3/045

CPC classification number: F02C7/18 ,  F01D5/08 ,  F01D5/18 ,  F01D9/065 ,  F01D25/28 ,  F02C3/045 ,  F02C6/08 ,  F02C7/12 ,  F02C7/20 ,  F05D2250/18 ,  Y02T50/675

Abstract: A gas turbine engine includes a core engine that has a compressor section, a combustor section and a turbine section. A thermal management system is configured to receive a cooling stream. The thermal management system includes a metering device that is located near an outer diameter of the core engine. The metering device is configured to divide the cooling stream into multiple segregated passages. The metering device can be configured to divide the cooling stream between a first passage and a second passage that is concentric with the first passage.

Abstract translation: 燃气涡轮发动机包括具有压缩机部分，燃烧器部分和涡轮部分的核心发动机。 热管理系统被配置为接收冷却流。 热管理系统包括位于核心发动机外径附近的计量装置。 计量装置构造成将冷却流分成多个分离的通道。 计量装置可以被配置为在第一通道和与第一通道同心的第二通道之间划分冷却流。