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1. 发明授权

US09341080B2 Gas turbine engine with geared turbofan and oil thermal management system 有权
标题翻译：燃气涡轮发动机带有齿轮涡轮风扇和油热管理系统
公开(公告)号：US09341080B2
公开(公告)日：2016-05-17
申请号：US14245317
申请日：2014-04-04
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Kathleen R. Phillips , Thomas G. Phillips , Ethan K. Stearns , Federico Papa
IPC分类号： F01D25/18 , F01D25/20 , F02K9/64 , F02C7/06 , F02C7/14
CPC分类号： F01D25/20 , F01D25/18 , F01M5/002 , F02C7/06 , F02C7/14 , F02K9/64 , F05D2260/213 , F05D2260/40311 , Y02T50/676
摘要： A gas turbine engine includes a fan, a compressor section, a combustion section, and a turbine section. A fan drive gear system is configured for driving the fan at a speed different than the turbine section. A lubricant system includes a lubricant pump delivering lubricant to an outlet line. The outlet line splits into at least a hot line and into a cool line. The hot line is directed primarily to locations in the gas turbine engine that are not intended to receive cooler lubricant. The cool line is directed through one or more heat exchangers at which the lubricant is cooled, and the cool line then is routed to the fan drive gear system. At least one of the one or more heat exchangers is a fuel/oil cooler at which lubricant will be cooled by fuel leading to the combustion section. The fuel/oil cooler is downstream of a point where the outlet line splits into the at least the hot line and the cool line, such that the hot line is not directed through the fuel/oil cooler. A method is also disclosed.
摘要翻译：燃气涡轮发动机包括风扇，压缩机部，燃烧部和涡轮部。风扇驱动齿轮系统构造成以不同于涡轮部分的速度驱动风扇。润滑剂系统包括将润滑剂输送到出口管线的润滑剂泵。出口线分成至少一条热线，并进入冷线。热线主要针对燃气涡轮发动机中不用于接收较冷润滑剂的位置。冷却管线被引导通过一个或多个热交换器，在该热交换器处润滑剂被冷却，然后将冷却管线路由到风扇驱动齿轮系统。一个或多个热交换器中的至少一个是燃料/油冷却器，在该燃料/油冷却器处，通过燃料通向燃烧部分的润滑剂将被冷却。燃料/油冷却器在出口管线分成至少热管线和冷却管线的点的下游，使得热管线不被引导通过燃料/油冷却器。还公开了一种方法。

2. 发明申请

US20140360153A1 GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM 审中-公开
标题翻译：气体涡轮发动机热管理系统
公开(公告)号：US20140360153A1
公开(公告)日：2014-12-11
申请号：US14247575
申请日：2014-04-08
申请人： United Technologies Corporation
发明人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips , Ethan K. Stearns , Justin W. Heiss
IPC分类号： F02C7/12 , F02C7/224 , G05D7/06 , F02C9/48 , F02C7/06 , G05B15/02 , F02C3/08 , F02C7/232
CPC分类号： F02C7/12 , F01D25/12 , F02C3/08 , F02C7/06 , F02C7/08 , F02C7/14 , F02C7/224 , F02C7/232 , F02C9/00 , F02C9/48 , F05D2220/32 , F05D2260/213 , G05B15/02 , G05D7/06 , Y02T50/675
摘要： A gas turbine engine according to an exemplary embodiment of this disclosure, among other possible things includes a fan. A geared architecture is configured for driving the fan. A turbine section is configured for driving the geared architecture. A thermal management system that includes a first fluid circuit and a second fluid circuit that manage heat generated in at least a portion of the gas turbine engine. A first heat exchanger is incorporated into each of the first fluid circuit and the second fluid circuit. A second heat exchanger is incorporated into the first fluid circuit. A valve controls an amount of a first fluid that is communicated to the first heat exchanger and the second heat exchanger. A controller is configured to control a positioning of the valve. The amount of the first fluid communicated to the first heat exchanger is based on a first characteristic of a second fluid and the amount of the first fluid communicated to the second heat exchanger is based on a second characteristic of the second fluid. A method and a system are also disclosed.
摘要翻译：根据本公开的示例性实施例的燃气涡轮发动机以及其它可能的事情包括风扇。齿轮架构配置为驱动风扇。涡轮机部分被配置用于驱动齿轮架构。一种热管理系统，其包括第一流体回路和第二流体回路，其管理在燃气涡轮发动机的至少一部分中产生的热量。第一热交换器被并入到第一流体回路和第二流体回路的每一个中。第二热交换器被并入到第一流体回路中。阀门控制与第一热交换器和第二热交换器连通的第一流体的量。控制器被配置为控制阀的定位。与第一热交换器连通的第一流体的量基于第二流体的第一特性，并且与第二热交换器连通的第一流体的量基于第二流体的第二特性。还公开了一种方法和系统。

3. 发明申请

US20140216003A1 GAS TURBINE ENGINE WITH GEARED TURBOFAN AND OIL THERMAL MANAGEMENT SYSTEM 审中-公开
标题翻译：燃气涡轮发动机与齿轮涡轮和油热管理系统
公开(公告)号：US20140216003A1
公开(公告)日：2014-08-07
申请号：US14245317
申请日：2014-04-04
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Kathleen R. Phillips , Thomas G. Phillips , Ethan K. Stearns , Federico Papa
IPC分类号： F01D25/20 , F02C7/06
CPC分类号： F01D25/20 , F01D25/18 , F01M5/002 , F02C7/06 , F02C7/14 , F02K9/64 , F05D2260/213 , F05D2260/40311 , Y02T50/676
摘要： A gas turbine engine includes a fan, a compressor section, a combustion section, and a turbine section. A fan drive gear system is configured for driving the fan at a speed different than the turbine section. A lubricant system includes a lubricant pump delivering lubricant to an outlet line. The outlet line splits into at least a hot line and into a cool line. The hot line is directed primarily to locations in the gas turbine engine that are not intended to receive cooler lubricant. The cool line is directed through one or more heat exchangers at which the lubricant is cooled, and the cool line then is routed to the fan drive gear system. At least one of the one or more heat exchangers is a fuel/oil cooler at which lubricant will be cooled by fuel leading to the combustion section. The fuel/oil cooler is downstream of a point where the outlet line splits into the at least the hot line and the cool line, such that the hot line is not directed through the fuel/oil cooler. A method is also disclosed.
摘要翻译：燃气涡轮发动机包括风扇，压缩机部，燃烧部和涡轮部。风扇驱动齿轮系统构造成以不同于涡轮部分的速度驱动风扇。润滑剂系统包括将润滑剂输送到出口管线的润滑剂泵。出口线分成至少一条热线，并进入冷线。热线主要针对燃气涡轮发动机中不用于接收较冷润滑剂的位置。冷却管线被引导通过一个或多个热交换器，在该热交换器处润滑剂被冷却，然后将冷却管线路由到风扇驱动齿轮系统。一个或多个热交换器中的至少一个是燃料/油冷却器，在该燃料/油冷却器处，通过燃料通向燃烧部分的润滑剂将被冷却。燃料/油冷却器在出口管线分成至少热管线和冷却管线的点的下游，使得热管线不被引导通过燃料/油冷却器。还公开了一种方法。

4. 发明申请

US20130202406A1 GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM 有权
标题翻译：气体涡轮发动机热管理系统
公开(公告)号：US20130202406A1
公开(公告)日：2013-08-08
申请号：US13799406
申请日：2013-03-13
申请人： United Technologies Corporation
发明人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips , Ethan K. Stearns , Justin W. Heiss
IPC分类号： F01D25/12
CPC分类号： F02C7/12 , F01D25/12 , F02C3/08 , F02C7/06 , F02C7/08 , F02C7/14 , F02C7/224 , F02C7/232 , F02C9/00 , F02C9/48 , F05D2220/32 , F05D2260/213 , G05B15/02 , G05D7/06 , Y02T50/675
摘要： A thermal management system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a heat exchanger and a valve that controls an amount of a first fluid that is communicated through the heat exchanger A first sensor senses a first characteristic of a second fluid that is communicated through the heat exchanger to exchange heat with the first fluid and a second sensor senses a second characteristic of the second fluid. A positioning of the valve is based on at least one of the first characteristic and the second characteristic.
摘要翻译：根据本公开的示例性方面的用于燃气涡轮发动机的热管理系统尤其包括热交换器和阀，其控制通过热交换器A连通的第一流体的量第一传感器感测到第二流体的第一特征，其通过热交换器连通以与第一流体交换热量，第二传感器感测第二流体的第二特性。阀的定位基于第一特征和第二特性中的至少一个。

5. 发明授权

US09879563B2 Gas turbine engine with geared turbofan and oil thermal management system 有权
公开(公告)号：US09879563B2
公开(公告)日：2018-01-30
申请号：US13794976
申请日：2013-03-12
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Kathleen R. Phillips , Thomas G. Phillips , Ethan K. Stearns
IPC分类号： F01D25/20 , F01D25/18 , F02K9/64 , F02C7/06 , F02C7/14 , F01M5/00
CPC分类号： F01D25/20 , F01D25/18 , F01M5/002 , F02C7/06 , F02C7/14 , F02K9/64 , F05D2260/213 , F05D2260/40311 , Y02T50/676
摘要： A lubricant supply system for a gas turbine engine has a lubricant lube pump delivering lubricant to an outlet line. The outlet line is split into at least a hot line and into a cool line, with the hot line directed primarily to locations associated with an engine that are not intended to receive cooler lubricant, and the cool line directed through one or more heat exchangers at which lubricant is cooled. The cool line then is routed to a fan drive gear for an associated gas turbine engine. A method and apparatus are disclosed.

6. 发明授权

US09334802B2 Gas turbine engine thermal management system 有权
标题翻译：燃气轮机发动机热管理系统
公开(公告)号：US09334802B2
公开(公告)日：2016-05-10
申请号：US13799406
申请日：2013-03-13
申请人： United Technologies Corporation
发明人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips , Ethan K. Stearns , Justin W. Heiss
IPC分类号： F02C7/12 , F01D25/12 , F02C7/08 , F02C7/14 , F02C9/00 , F02C3/08 , F02C7/06 , F02C7/224 , F02C7/232 , F02C9/48 , G05B15/02 , G05D7/06
CPC分类号： F02C7/12 , F01D25/12 , F02C3/08 , F02C7/06 , F02C7/08 , F02C7/14 , F02C7/224 , F02C7/232 , F02C9/00 , F02C9/48 , F05D2220/32 , F05D2260/213 , G05B15/02 , G05D7/06 , Y02T50/675
摘要： A thermal management system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a heat exchanger and a valve that controls an amount of a first fluid that is communicated through the heat exchanger A first sensor senses a first characteristic of a second fluid that is communicated through the heat exchanger to exchange heat with the first fluid and a second sensor senses a second characteristic of the second fluid. A positioning of the valve is based on at least one of the first characteristic and the second characteristic.
摘要翻译：根据本公开的示例性方面的用于燃气涡轮发动机的热管理系统尤其包括热交换器和阀，其控制通过热交换器A连通的第一流体的量第一传感器感测到第二流体的第一特征，其通过热交换器连通以与第一流体交换热量，第二传感器感测第二流体的第二特性。阀的定位基于第一特征和第二特性中的至少一个。

7. 发明授权

US09038397B2 Gas turbine engine thermal management system 有权
标题翻译：燃气轮机发动机热管理系统
公开(公告)号：US09038397B2
公开(公告)日：2015-05-26
申请号：US14247575
申请日：2014-04-08
申请人： United Technologies Corporation
发明人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips , Ethan K. Stearns , Justin W. Heiss
IPC分类号： F02C1/00 , F02C7/06 , F02K99/00 , F02C7/12 , F02C3/08 , F02C7/224 , F02C7/232 , F02C9/48 , G05B15/02 , G05D7/06
CPC分类号： F02C7/12 , F01D25/12 , F02C3/08 , F02C7/06 , F02C7/08 , F02C7/14 , F02C7/224 , F02C7/232 , F02C9/00 , F02C9/48 , F05D2220/32 , F05D2260/213 , G05B15/02 , G05D7/06 , Y02T50/675
摘要： A gas turbine engine according to an exemplary embodiment of this disclosure, among other possible things includes a fan. A geared architecture is configured for driving the fan. A turbine section is configured for driving the geared architecture. A thermal management system that includes a first fluid circuit and a second fluid circuit that manage heat generated in at least a portion of the gas turbine engine. A first heat exchanger is incorporated into each of the first fluid circuit and the second fluid circuit. A second heat exchanger is incorporated into the first fluid circuit. A valve controls an amount of a first fluid that is communicated to the first heat exchanger and the second heat exchanger. A controller is configured to control a positioning of the valve. The amount of the first fluid communicated to the first heat exchanger is based on a first characteristic of a second fluid and the amount of the first fluid communicated to the second heat exchanger is based on a second characteristic of the second fluid. A method and a system are also disclosed.
摘要翻译：根据本公开的示例性实施例的燃气涡轮发动机以及其它可能的事情包括风扇。齿轮架构配置为驱动风扇。涡轮机部分被配置用于驱动齿轮架构。一种热管理系统，其包括第一流体回路和第二流体回路，其管理在燃气涡轮发动机的至少一部分中产生的热量。第一热交换器被并入到第一流体回路和第二流体回路的每一个中。第二热交换器被并入到第一流体回路中。阀门控制与第一热交换器和第二热交换器连通的第一流体的量。控制器被配置为控制阀的定位。与第一热交换器连通的第一流体的量基于第二流体的第一特性，并且与第二热交换器连通的第一流体的量基于第二流体的第二特性。还公开了一种方法和系统。

8. 发明授权

US10400671B2 Gas turbine engine thermal management system 有权
公开(公告)号：US10400671B2
公开(公告)日：2019-09-03
申请号：US15076787
申请日：2016-03-22
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips , Ethan K. Stearns , Justin W. Heiss
IPC分类号： F02C7/12 , F01D25/12 , F02C7/08 , F02C7/14 , F02C9/00 , F02C3/08 , F02C7/06 , F02C7/224 , F02C7/232 , F02C9/48 , G05B15/02 , G05D7/06
摘要： A thermal management system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a heat exchanger and a valve that controls an amount of a first fluid that is communicated through the heat exchanger. A first sensor senses a first characteristic of a second fluid that is communicated through the heat exchanger to exchange heat with the first fluid and a second sensor senses a second characteristic of the second fluid. A positioning of the valve is based on at least one of the first characteristic and the second characteristic.

9. 发明申请

US20140083076A1 Gas Turbine Engine With Geared Turbofan and Oil Thermal Management System 审中-公开
标题翻译：燃气轮机发动机带齿轮涡轮风扇和油热管理系统
公开(公告)号：US20140083076A1
公开(公告)日：2014-03-27
申请号：US13794976
申请日：2013-03-12
申请人： United Technologies Corporation
发明人： Kathleen R. Phillips , Thomas G. Phillips , Ethan K. Stearns
IPC分类号： F01D25/20
CPC分类号： F01D25/20 , F01D25/18 , F01M5/002 , F02C7/06 , F02C7/14 , F02K9/64 , F05D2260/213 , F05D2260/40311 , Y02T50/676
摘要： A lubricant supply system for a gas turbine engine has a lubricant lube pump delivering lubricant to an outlet line. The outlet line is split into at least a hot line and into a cool line, with the hot line directed primarily to locations associated with an engine that are not intended to receive cooler lubricant, and the cool line directed through one or more heat exchangers at which lubricant is cooled. The cool line then is routed to a fan drive gear for an associated gas turbine engine. A method and apparatus are disclosed.
摘要翻译：用于燃气涡轮发动机的润滑剂供应系统具有将润滑剂输送到出口管线的润滑剂润滑剂泵。出口管线被分成至少一个热管线并进入冷却管线，热管线主要指向与不用于接收较冷润滑剂的发动机相关联的位置，并且冷管线通过一个或多个热交换器哪种润滑剂被冷却。然后，冷却管线被路由到用于相关联的燃气涡轮发动机的风扇驱动齿轮。公开了一种方法和装置。

10. 发明申请

US20130284398A1 GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM 审中-公开
标题翻译：气体涡轮发动机热管理系统
公开(公告)号：US20130284398A1
公开(公告)日：2013-10-31
申请号：US13926154
申请日：2013-06-25
申请人： United Technologies Corporation
发明人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips
IPC分类号： F02C7/14
CPC分类号： F02C7/14 , F02C7/08 , F02C7/185 , F02C7/224 , F05D2260/4031 , F05D2260/98
摘要： A thermal management system according to an exemplary aspect of the present disclosure includes, among other things, a first fluid circuit that selectively communicates a first portion of a first conditioned fluid having a first temperature to a first gas turbine engine system and a second portion of the first conditioned fluid having a second temperature to a second gas turbine engine system. The second temperature is a greater temperature than the first temperature. A second fluid circuit circulates a second conditioned fluid that is different from the first conditioned fluid to a third gas turbine engine system.
摘要翻译：根据本公开的示例性方面的热管理系统尤其包括第一流体回路，其将具有第一温度的第一调节流体的第一部分选择性地连通到第一燃气涡轮发动机系统，第二部分第一调节流体具有第二温度到第二燃气涡轮发动机系统。第二温度是比第一温度更高的温度。第二流体回路将与第一调节流体不同的第二调节流体循环到第三燃气涡轮发动机系统。

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