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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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12.发明申请公开(公告)号：US20160177828A1
公开(公告)日：2016-06-23
申请号：US14606076
申请日：2015-01-27
Applicant: United Technologies Corporation
Inventor： Ryan K. Snyder , Michael R. Thomas
CPC classification number: F02C6/08 , F02C7/185 , F02K3/075 , F02K3/077 , F02K3/115 , F05D2260/213 , Y02T50/675
Abstract: A gas turbine bypass flow arrangement comprises an outer housing and an inner housing, an outer bypass duct defined between the outer housing and the inner housing and an inner bypass duct defined inwardly of the inner housing. A first heat exchanger is positioned at an upstream location within the outer bypass duct and a second heat exchanger is positioned within the inner bypass duct at an upstream location. A downstream heat exchanger is positioned to be in the path of air downstream of the second heat exchanger in the inner bypass duct. Air flowing across the downstream heat exchanger passes from the inner bypass duct into the outer bypass duct. A gas turbine engine is also disclosed.
Abstract translation: 燃气轮机旁路流动装置包括外壳体和内壳体，限定在外壳体和内壳体之间的外旁通管道以及限定在内壳体内侧的内旁通管道。 第一热交换器定位在外部旁路管道内的上游位置处，并且第二热交换器位于内部旁通管道的上游位置处。 下游热交换器被定位成位于内部旁通管道中的第二热交换器下游的空气路径中。 流过下游热交换器的空气从内部旁通管道进入外部旁路管道。 还公开了一种燃气涡轮发动机。
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公开(公告)号：US20160090190A1
公开(公告)日：2016-03-31
申请号：US14866119
申请日：2015-09-25
Applicant: United Technologies Corporation
Inventor： Ryan K. Snyder , Eric J. Heims
CPC classification number: B64D45/00 , B01D46/10 , B01D2273/10 , B01D2279/60 , B64D33/02 , B64D33/08 , F02C7/05 , F02C7/052 , F02C7/055 , F02C7/14 , F02K3/115 , F05D2260/213 , F05D2260/607 , F05D2260/98 , Y02T50/671 , Y02T50/675
Abstract: Aspects of the disclosure are directed to a screen configured for use in association with a cooler of an aircraft, the screen comprising: a first portion arranged as a grid and located in a line-of-sight of the cooler with respect to a fluid inlet, and a second portion located out of the line-of-sight of the cooler with respect to the fluid inlet, wherein the second portion is grid-free.
Abstract translation: 本公开的方面涉及被配置为与飞机的冷却器相关联使用的屏幕，该屏幕包括：第一部分，布置成格栅并且相对于流体入口位于冷却器的视线内 以及位于冷却器相对于流体入口的视线之外的第二部分，其中第二部分是无栅格的。
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公开(公告)号：US10260426B2
公开(公告)日：2019-04-16
申请号：US14427396
申请日：2013-02-10
Applicant: United Technologies Corporation
Inventor： Marc R. Sauerhoefer , Ryan K. Snyder , James D. Marshall , Kari L. Kisselbrack , Thomas Livingston
Abstract: An adapter for a gas turbine engine has a first portion with a control module mount interface. A second portion with a sensor mount interface defines a sensor mount position relative to a control module. A connecting body connects the first and second portions such that the second portion provides a re-orientated sensor mount position relative to the control module. A lubrication system for a gas turbine engine is also disclosed.
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公开(公告)号：US10041409B2
公开(公告)日：2018-08-07
申请号：US14442547
申请日：2014-01-30
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Ryan K. Snyder , Kari L. Kisselbrack , Jesse Ian Berube , Michael C. O'Brien , Eric J. Heims , Ryan Timothy Matte , Vito Guardi , Bruce Paradise
Abstract: An oil control module for a gas turbine engine is provided comprising a housing on which numerous components of a lubricating system are mounted. The components may include a variable oil reduction valve/shuttle valve, a main oil pressure sensor, a main oil temperature sensor, a main oil filter delta pressure sensor, an oil debris monitor, a lube filter, an active oil damper valve, a cool oil orifice, a knock down orifice and a lube trim orifice. By packing numerous lubricating system components onto or within a housing located adjacent to the gas turbine engine, the oil control module reduces cost and weight and simplifies the maintenance of the lubricating system.
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Patent Agency Ranking
公开(公告)号：US09964037B2
公开(公告)日：2018-05-08
申请号：US14606076
申请日：2015-01-27
Applicant: United Technologies Corporation
Inventor： Ryan K. Snyder , Michael R. Thomas
CPC classification number: F02C6/08 , F02C7/185 , F02K3/075 , F02K3/077 , F02K3/115 , F05D2260/213 , Y02T50/675
Abstract: A gas turbine bypass flow arrangement comprises an outer housing and an inner housing, an outer bypass duct defined between the outer housing and the inner housing and an inner bypass duct defined inwardly of the inner housing. A first heat exchanger is positioned at an upstream location within the outer bypass duct and a second heat exchanger is positioned within the inner bypass duct at an upstream location. A downstream heat exchanger is positioned to be in the path of air downstream of the second heat exchanger in the inner bypass duct. Air flowing across the downstream heat exchanger passes from the inner bypass duct into the outer bypass duct. A gas turbine engine is also disclosed.
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公开(公告)号：US20160222889A1
公开(公告)日：2016-08-04
申请号：US14612755
申请日：2015-02-03
Applicant: United Technologies Corporation
Inventor： Ryan K. Snyder
CPC classification number: F02C9/00 , F02C7/32 , F05D2220/32 , F05D2220/764 , F05D2270/54 , G05B15/02 , Y02T50/671
Abstract: A distributed electrical system includes a plurality of engine components each in electrical communication with one of a plurality of docking stations. An electronic engine control is positioned remote from the engine components and is configured to communicate wirelessly with each of the plurality of engine components.
Abstract translation: 分布式电气系统包括多个与多个对接站中的一个电气通信的发动机部件。 电子发动机控制器位于远离发动机部件的位置，并被配置为与多个发动机部件中的每一个进行无线通信。
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公开(公告)号：US20150247460A1
公开(公告)日：2015-09-03
申请号：US14427396
申请日：2013-02-10
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Marc R. Sauerhoefer , Ryan K. Snyder , James D. Marshall , Kari L. Kisselbrack , Thomas Livingston
Abstract: An adapter for a gas turbine engine has a first portion with a control module mount interface. A second portion with a sensor mount interface defines a sensor mount position relative to a control module. A connecting body connects the first and second portions such that the second portion provides a re-orientated sensor mount position relative to the control module. A lubrication system for a gas turbine engine is also disclosed.
Abstract translation: 用于燃气涡轮发动机的适配器具有带有控制模块安装接口的第一部分。 具有传感器安装接口的第二部分定义相对于控制模块的传感器安装位置。 连接体连接第一和第二部分，使得第二部分相对于控制模块提供重新定向的传感器安装位置。 还公开了一种用于燃气涡轮发动机的润滑系统。
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公开(公告)号：US20140334916A1
公开(公告)日：2014-11-13
申请号：US14273111
申请日：2014-05-08
Applicant: United Technologies Corporation
Inventor： Ryan K. Snyder , Michael Dreher
IPC: F01D25/28
CPC classification number: F01D25/285 , F01D21/003 , G02B23/2492
Abstract: A borescope inspection (BSI) port fitting is provided for a gas turbine engine. The borescope inspection (BSI) port fitting includes a housing with a borescope inspection port.
Abstract translation: 为燃气涡轮发动机提供管道检查（BSI）端口接头。 管道检查（BSI）端口接头包括一个带孔镜检查口的外壳。
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公开(公告)号：US20140231437A1
公开(公告)日：2014-08-21
申请号：US14186435
申请日：2014-02-21
Applicant: United Technologies Corporation
Inventor： Ryan K. Snyder , Kari L. Kisselbrack , Curtis J. Ruckey , Robert Howard
IPC: B60K15/04
CPC classification number: F01D25/18 , F01D25/00 , F01M11/0458 , F01M2011/0491 , F05D2260/98 , F16N19/00 , F16N31/00
Abstract: A cap assembly includes a plunger mounted to a retainer pin and a latch operable to retract the retainer pin.
Abstract translation: 帽组件包括安装到保持销的柱塞和可操作以缩回保持销的闩锁。
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