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公开(公告)号：US20160208647A1
公开(公告)日：2016-07-21
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
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. 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.
Abstract translation: 用于燃气涡轮发动机的中涡轮机框架包括内框架，其包括流体通道。 旋流管与流体通道流体连通，并且构造成在径向向内和向下流动的方向引导冷却气流。
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公开(公告)号：US20150260057A1
公开(公告)日：2015-09-17
申请号：US14438562
申请日：2013-09-11
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Jorge I. Farah , Jonathan P. Burt , Paul K. Sanchez , Kalpendu J. Parekh , Jonathan J. Jakiel
IPC: F01D25/28
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。
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公开(公告)号：US20130192268A1
公开(公告)日：2013-08-01
申请号：US13753821
申请日：2013-01-30
Applicant: United Technologies Corporation
Inventor： Paul K. Sanchez , Kalpendu J. Parekh , William A. Daniels , John S. Tu
IPC: F01D25/24
CPC classification number: F02C7/20 , F01D25/12 , F01D25/14 , F01D25/16 , F01D25/162 , F01D25/24 , F01D25/246 , F02C7/12 , 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.
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公开(公告)号：US09863319B2
公开(公告)日：2018-01-09
申请号：US14429167
申请日：2013-03-01
Applicant: United Technologies Corporation
Inventor： Jorge I. Farah , Kalpendu J. Parekh
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.
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公开(公告)号：US09512738B2
公开(公告)日：2016-12-06
申请号：US13753821
申请日：2013-01-30
Applicant: United Technologies Corporation
Inventor： Paul K. Sanchez , Kalpendu J. Parekh , William A. Daniels , John S. Tu
CPC classification number: F02C7/20 , F01D25/12 , F01D25/14 , F01D25/16 , F01D25/162 , F01D25/24 , F01D25/246 , F02C7/12 , 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，以及位于轴向 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。
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Patent Agency Ranking
公开(公告)号：US20160230602A1
公开(公告)日：2016-08-11
申请号：US14617323
申请日：2015-02-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Alexander Broulidakis , Anthony P. Cherolis , Jonathan Lemoine , Kalpendu J. Parekh , Steven W. Trinks , Christopher Treat , Kevin Zacchera , Alberto A. Mateo
CPC classification number: F01D25/28 , F01D9/065 , F01D25/162 , F01D25/26 , F02C7/12 , F05D2220/32 , F05D2220/3213 , F05D2230/20 , F05D2230/64 , F05D2260/20 , F05D2260/30 , F05D2260/31 , Y02T50/671 , Y02T50/676
Abstract: A tie rod assembly for a mid-turbine frame includes at least one tie rod for connecting an outer frame case to an inner frame case. At least one tie rod includes an inlet passage that branches into a first branch and a second branch. A plug is located in the first branch to block flow through a portion of the first branch.
Abstract translation: 用于中涡轮机架的拉杆组件包括用于将外框壳体连接到内框架壳体的至少一个拉杆。 至少一个拉杆包括分支到第一分支和第二分支中的入口通道。 插头位于第一分支中以阻止流过第一分支的一部分。
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公开(公告)号：US10107120B2
公开(公告)日：2018-10-23
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
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.
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公开(公告)号：US10087785B2
公开(公告)日：2018-10-02
申请号：US14617323
申请日：2015-02-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Alexander Broulidakis , Anthony P. Cherolis , Jonathan Lemoine , Kalpendu J. Parekh , Steven W. Trinks , Christopher Treat , Kevin Zacchera , Alberto A. Mateo
Abstract: A tie rod assembly for a mid-turbine frame includes at least one tie rod for connecting an outer frame case to an inner frame case. At least one tie rod includes an inlet passage that branches into a first branch and a second branch. A plug is located in the first branch to block flow through a portion of the first branch.
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公开(公告)号：US10006308B2
公开(公告)日：2018-06-26
申请号：US14438562
申请日：2013-09-11
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Jorge I. Farah , Jonathan P. Burt , Paul K. Sanchez , Kalpendu J. Parekh , Jonathan J. Jakiel
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.
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公开(公告)号：US20140137534A1
公开(公告)日：2014-05-22
申请号：US14166320
申请日：2014-01-28
Applicant: United Technologies Corporation
Inventor： Paul K. Sanchez , Kalpendu J. Parekh , William A. Daniels , John S. Tu
IPC: F01D25/14
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，以及位于轴向 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。
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