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公开(公告)号:US20160333791A1
公开(公告)日:2016-11-17
申请号:US15111572
申请日:2015-02-04
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Ryan K. Snyder , Eric J. Heims , Mark W. Colebrook
IPC: F02C7/32 , F02C3/04 , F02C7/14 , B64D29/08 , F01D25/20 , F01D25/26 , F01D25/28 , B64D27/10 , F02K3/06 , H02K7/18
CPC classification number: F02C7/32 , B64C7/02 , B64D27/10 , B64D29/06 , B64D29/08 , F01D25/20 , F01D25/265 , F01D25/28 , F02C3/04 , F02C7/14 , F02K3/06 , F05D2220/327 , F05D2230/72 , F05D2250/30 , F05D2250/411 , H02K7/1823 , Y02T50/671
Abstract: A gas turbine engine comprises a compressor, a combustor and a turbine. A housing for the gas turbine engine includes a mount member to define a vertically upper location. Sides of the engine are defined on opposed sides of the mount, with a fuel filter, a fuel pump and a fuel flow meter being positioned on a first side and an oil pump, an oil filter and an oil tank positioned on a second of the sides.
Abstract translation: 燃气涡轮发动机包括压缩机,燃烧器和涡轮机。 用于燃气涡轮发动机的壳体包括用于限定垂直上方位置的安装构件。 发动机的侧面限定在安装座的相对侧上,燃料过滤器,燃料泵和燃料流量计位于第一侧,油泵,油过滤器和油箱位于第二侧 边。
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公开(公告)号:US20150361827A1
公开(公告)日:2015-12-17
申请号:US14760746
申请日:2014-02-12
Applicant: United Technologies Corporation
Inventor: Pellegrino J. Pisacreta , Christopher D. Ramsey , Mark W. Colebrook
IPC: F01D25/14
CPC classification number: F01D25/14 , F01D11/24 , F02C7/12 , F02C7/16 , F02C7/18 , F05D2250/182 , F05D2250/184
Abstract: A cooling manifold has a plurality of pieces. The pieces extend in a circumferential direction to abutting flanges. The flanges are secured together at circumferential ends of each piece. Cooling channels are formed in between inner and outer walls. Air inlets are formed in the pieces with the air inlets delivering air in the interior. There are fingers on an outer periphery. The fingers are aligned within an air outlet. The air can be delivered into the inlet, cool the interior, and leave through the outlet extending to a main conduit. The main conduit is secured directly to an outer periphery of the cooling manifold.
Abstract translation: 冷却歧管具有多个部件。 这些件在圆周方向上延伸到邻接凸缘。 凸缘在每个件的圆周端固定在一起。 冷却通道形成在内壁和外壁之间。 空气入口形成在碎片中,空气入口在内部传送空气。 外周有手指。 手指在空气出口内对齐。 空气可以输送到入口,冷却内部,并通过出口延伸到主管道。 主导管直接固定在冷却歧管的外周。
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公开(公告)号:US20190195077A1
公开(公告)日:2019-06-27
申请号:US15852483
申请日:2017-12-22
Applicant: United Technologies Corporation
Inventor: Edward Guevel , Rebecca R. Dunnigan , Mark W. Colebrook , Austin R. O'Mara
CPC classification number: F01D9/065 , F02C7/18 , F05D2210/40 , F05D2220/32 , F05D2240/12 , F05D2260/20 , F23R3/002 , F23R3/06 , F23R3/16
Abstract: An airflow deflector is provided that includes at least one liner attachment flange, a deflector panel, and at least one deflector leg. The at least one liner attachment flange has a liner side surface and an opposing outer surface. The at least one deflector leg extends between and is attached to the at least one liner attachment flange. The at least one deflector leg extends a distance between the deflector panel and the liner attachment flange to maintain the deflector panel a separation distance from the liner attachment flange. The airflow deflector is configured for insertion of the at least one deflector leg and the deflector panel within a liner aperture.
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公开(公告)号:US20140312611A1
公开(公告)日:2014-10-23
申请号:US14200649
申请日:2014-03-07
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Billie W. Bunting , Robert J. DeRosa , Craig Michael Callaghan , Mark W. Colebrook , Ranganath Santosh
IPC: F16L15/08
CPC classification number: F16L15/006 , F02C7/222 , F16L15/00 , Y10T29/49895
Abstract: A fluid conduit for a gas turbine engine includes a first fluid conduit attachable to a second fluid conduit and securable together with a lockable connector. The connector includes a first portion including external threads and a second portion receiving the first portion and including internal threads mating to the external threads of the first portion. The internal threads include lead threads defining a first thread interface with the external threads for starting attachment of the first portion to the second portion and locking threads defining a second thread interface for locking the first portion to the second portion.
Abstract translation: 用于燃气涡轮发动机的流体导管包括可连接到第二流体导管并与可锁定连接器一起固定的第一流体导管。 连接器包括包括外螺纹的第一部分和接收第一部分并包括与第一部分的外螺纹配合的内螺纹的第二部分。 内螺纹包括限定与外螺纹的第一螺纹接口的引导螺纹,用于开始将第一部分附接到第二部分,并且锁定螺纹限定用于将第一部分锁定到第二部分的第二螺纹接口。
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公开(公告)号:US10738637B2
公开(公告)日:2020-08-11
申请号:US15852483
申请日:2017-12-22
Applicant: United Technologies Corporation
Inventor: Edward Guevel , Rebecca R. Dunnigan , Mark W. Colebrook , Austin R. O'Mara
Abstract: An airflow deflector is provided that includes at least one liner attachment flange, a deflector panel, and at least one deflector leg. The at least one liner attachment flange has a liner side surface and an opposing outer surface. The at least one deflector leg extends between and is attached to the at least one liner attachment flange. The at least one deflector leg extends a distance between the deflector panel and the liner attachment flange to maintain the deflector panel a separation distance from the liner attachment flange. The airflow deflector is configured for insertion of the at least one deflector leg and the deflector panel within a liner aperture.
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公开(公告)号:US10119635B2
公开(公告)日:2018-11-06
申请号:US14200649
申请日:2014-03-07
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Billie W. Bunting , Robert J. DeRosa , Craig Michael Callaghan , Mark W. Colebrook , Ranganath Santosh
Abstract: A fluid conduit for a gas turbine engine includes a first fluid conduit attachable to a second fluid conduit and securable together with a lockable connector. The connector includes a first portion including external threads and a second portion receiving the first portion and including internal threads mating to the external threads of the first portion. The internal threads include lead threads defining a first thread interface with the external threads for starting attachment of the first portion to the second portion and locking threads defining a second thread interface for locking the first portion to the second portion.
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公开(公告)号:US10072520B2
公开(公告)日:2018-09-11
申请号:US14760746
申请日:2014-02-12
Applicant: United Technologies Corporation
Inventor: Pellegrino J. Pisacreta , Christopher D. Ramsey , Mark W. Colebrook
CPC classification number: F01D25/14 , F01D11/24 , F02C7/12 , F02C7/16 , F02C7/18 , F05D2250/182 , F05D2250/184
Abstract: A cooling manifold has a plurality of pieces. The pieces extend in a circumferential direction to abutting flanges. The flanges are secured together at circumferential ends of each piece. Cooling channels are formed in between inner and outer walls. Air inlets are formed in the pieces with the air inlets delivering air in the interior. There are fingers on an outer periphery. The fingers are aligned within an air outlet. The air can be delivered into the inlet, cool the interior, and leave through the outlet extending to a main conduit. The main conduit is secured directly to an outer periphery of the cooling manifold.
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