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1. 发明授权

US07836680B2 Aircraft combination engines thermal management system 有权
标题翻译：飞机组合引擎热管理系统
公开(公告)号：US07836680B2
公开(公告)日：2010-11-23
申请号：US11820722
申请日：2007-06-20
申请人： Frederick M. Schwarz , Jorn A. Glahn , Brian M. Fentress
发明人： Frederick M. Schwarz , Jorn A. Glahn , Brian M. Fentress
IPC分类号： F02K3/00
CPC分类号： F01D15/10 , F01D13/02 , F01D25/125 , F02C6/08 , F02C6/10 , F02C7/185 , F02C7/224 , F02K3/06 , F02K3/115 , F05D2220/76 , F05D2260/213 , Y02T50/676
摘要： An engine combination for generating forces with a gas turbine engine generating force that utilizes an engine lubricant for lubricating moving components in the turbofan engine, and an internal combustion engine provided in the combination as an intermittent combustion engine generating force that utilizes a coolant for transporting heat generated in the intermittent combustion engine away therefrom and having an air intake, there being an air transfer duct connected from a compressor in the gas turbine engine to the air intake to transfer compressed air thereto. A coupling heat exchanger is coupled to both the gas turbine engine and the intermittent combustion engine to have the engine lubricant and the coolant pass therethrough. A further cooling heat exchanger is coupled to both the coupling heat exchanger and the intermittent combustion engine to have a remote fluid from a source thereof and the coolant pass therethrough.
摘要翻译：一种用于产生力的发动机组合，其具有利用用于润滑涡轮风扇发动机中的运动部件的发动机润滑剂的燃气涡轮发动机产生力，以及组合中设置的内燃机作为利用冷却剂传递热量的间歇性内燃机产生力在间歇式内燃机中产生并且具有进气口，存在从燃气涡轮发动机中的压缩机连接到进气口的空气传送管道，以将压缩空气传送到其上。耦合热交换器耦合到燃气涡轮发动机和间歇式内燃机，以使发动机润滑剂和冷却剂通过。另一个冷却热交换器被耦合到耦合热交换器和间歇式内燃机两者以具有来自其源的远程流体并且冷却剂通过其中。

2. 发明授权

US07908840B2 Turbine engine with integrated generator having shared lubrication system 有权
标题翻译：具有集成发电机的涡轮发动机具有共享润滑系统
公开(公告)号：US07908840B2
公开(公告)日：2011-03-22
申请号：US11605671
申请日：2006-11-29
申请人： Frederick M. Schwarz , Jorn A. Glahn
发明人： Frederick M. Schwarz , Jorn A. Glahn
IPC分类号： F02C7/06
CPC分类号： F01D25/18 , F01D15/10 , F01D25/12 , F01D25/125 , F02C7/06 , F05D2220/76 , F05D2260/234 , Y02T50/671 , Y02T50/675
摘要： A heat exchange system for use in operating equipment having a plurality of subsystems in each of which a common working fluid is utilized to provide selected operations in that subsystem with a reservoir containing at least some of the common working fluid and has both a supply system and a return system connected between the reservoir and each of the plurality of subsystems through which any common working fluid in the reservoir can be conveyed. An airstream heat exchanger is provided connected in one of the supply and return systems so as to have the common working fluid conveyed therethrough cooled at selectively variable rates in the airstreams passing thereby during at least some such uses of the operating equipment.
摘要翻译：一种用于操作设备的热交换系统，其具有多个子系统，每个子系统中的共用工作流体用于在该子系统中提供包含至少一些公共工作流体的储存器，并具有供应系统和连接在储存器和多个子系统中的每个子系统之间的返回系统，通过该返回系统可以输送储存器中的任何公共工作流体。提供连接在一个供应和返回系统中的气流热交换器，以便在所述操作设备的至少一些这样的使用期间，通过其中通过的空气中的选择性可变速率使输送的通用工作流体冷却。

3. 发明授权

US07810311B2 Cooling exchanger ducts 有权
标题翻译：冷却换热器管道
公开(公告)号：US07810311B2
公开(公告)日：2010-10-12
申请号：US11650825
申请日：2007-01-08
申请人： Frederick M. Schwarz , Jorn A. Glahn
发明人： Frederick M. Schwarz , Jorn A. Glahn
IPC分类号： F02K99/00
CPC分类号： F02C7/14 , F02K3/115 , Y02T50/675
摘要： A heat exchange system for use in operating equipment in which a working fluid is utilized in providing selected operations thereof, including for use in lubricating systems for aircraft turbofan engine equipment, the heat exchange system for providing air and working fluid heat exchanges to cool the working fluid at selectively variable rates in the operating equipment developed airstreams. A heat exchanger core is provided in a controlled air flow duct system opening at its entrance to those airstreams and having its outlet end opening downstream in those airstreams.
摘要翻译：一种用于操作设备的热交换系统，其中使用工作流体来提供其选择的操作，包括用于飞机涡轮风扇发动机设备的润滑系统，用于提供空气的热交换系统和工作流体热交换以冷却工作在操作设备中选择性变化的流体开发出气流。热交换器芯设置在受控的空气流动管道系统中，在其入口处开口，并且其出口端在这些气流中向下游开口。

4. 发明申请

US20120085528A1 INTERDEPENDENT LUBRICATION SYSTEMS 审中-公开
标题翻译：相互依赖的润滑系统
公开(公告)号：US20120085528A1
公开(公告)日：2012-04-12
申请号：US13313988
申请日：2011-12-07
申请人： Frederick M. Schwarz , Jorn A. Glahn
发明人： Frederick M. Schwarz , Jorn A. Glahn
IPC分类号： F28F27/00
CPC分类号： F01D25/20 , F01D25/08 , F02C7/14 , F05D2220/36 , F05D2220/76 , F05D2260/205 , F05D2270/303 , Y02T50/671 , Y02T50/675
摘要： A heat exchange system for use in operating equipment having a plurality of subsystems in each of which one of a plurality of working fluids is utilized to provide selected operations with there being an air and working fluid heat exchanger providing controlled cooling to cool at least one of the plurality of working fluids in its corresponding subsystem. In addition, a coupling heat exchanger is also provided connected to two of the subsystems to pass there working fluids therethrough, including the subsystem with the air and working fluid heat exchanger, to allow one of the connected subsystems to aid in cooling the other.
摘要翻译：一种用于操作设备的热交换系统，其具有多个子系统，每个子系统中的多个工作流体中的一个用于提供所选择的操作，其中具有空气和工作流体热交换器，其提供受控制的冷却以冷却至少一个其相应子系统中的多个工作流体。此外，还提供连接到两个子系统的耦合热交换器，以将工作流体从其中通过，包括具有空气和工作流体热交换器的子系统，以允许所连接的子系统之一帮助冷却另一个子系统。

5. 发明申请

US20080209911A1 Combination engines for aircraft 有权
标题翻译：飞机组合发动机
公开(公告)号：US20080209911A1
公开(公告)日：2008-09-04
申请号：US11713262
申请日：2007-03-02
申请人： Frederick M. Schwarz , Brian M. Fentress , Andrew P. Berryann , Charles E. Lents , Jorn A. Glahn
发明人： Frederick M. Schwarz , Brian M. Fentress , Andrew P. Berryann , Charles E. Lents , Jorn A. Glahn
IPC分类号： F02C6/08
CPC分类号： F02K5/023 , F01D15/10 , F02C3/10 , F02C6/08 , F02K3/06 , F02K3/075
摘要： An engine combination for generating forces with a gas turbine engine generating force, and an internal combustion engine provided in the combination as an intermittent combustion engine generating force having an air intake, there being an air transfer duct connected from a compressor in the gas turbine engine to the air intake to transfer compressed air thereto.
摘要翻译：一种用于产生具有燃气涡轮发动机产生力的发动机组合，以及组合中设置的内燃机作为具有进气口的间歇式内燃机产生力，存在从燃气涡轮发动机中的压缩机连接的空气传送管道到空气入口以将压缩空气传送到其上。

6. 发明申请

US20080121376A1 Turbine engine with integrated generator having shared lubrication system 有权
标题翻译：具有集成发电机的涡轮发动机具有共享润滑系统
公开(公告)号：US20080121376A1
公开(公告)日：2008-05-29
申请号：US11605671
申请日：2006-11-29
申请人： Frederick M. Schwarz , Jorn A. Glahn
发明人： Frederick M. Schwarz , Jorn A. Glahn
IPC分类号： F28D15/00
CPC分类号： F01D25/18 , F01D15/10 , F01D25/12 , F01D25/125 , F02C7/06 , F05D2220/76 , F05D2260/234 , Y02T50/671 , Y02T50/675
摘要： A heat exchange system for use in operating equipment having a plurality of subsystems in each of which a common working fluid is utilized to provide selected operations in that subsystem with a reservoir containing at least some of the common working fluid and has both a supply system and a return system connected between the reservoir and each of the plurality of subsystems through which any common working fluid in the reservoir can be conveyed. An airstream heat exchanger is provided connected in one of the supply and return systems so as to have the common working fluid conveyed therethrough cooled at selectively variable rates in the airstreams passing thereby during at least some such uses of the operating equipment.
摘要翻译：一种用于操作设备的热交换系统，其具有多个子系统，每个子系统中的共用工作流体用于在该子系统中提供包含至少一些公共工作流体的储存器，并具有供应系统和连接在储存器和多个子系统中的每个子系统之间的返回系统，通过该返回系统可以输送储存器中的任何公共工作流体。提供连接在一个供应和返回系统中的气流热交换器，以便在所述操作设备的至少一些这样的使用期间，通过其中通过的空气中的选择性可变速率使输送的通用工作流体冷却。

7. 发明授权

US07690188B2 Combination engines for aircraft 有权
标题翻译：飞机组合发动机
公开(公告)号：US07690188B2
公开(公告)日：2010-04-06
申请号：US11713262
申请日：2007-03-02
申请人： Frederick M. Schwarz , Brian M. Fentress , Andrew P. Berryann , Charles E. Lents , Jorn A. Glahn
发明人： Frederick M. Schwarz , Brian M. Fentress , Andrew P. Berryann , Charles E. Lents , Jorn A. Glahn
IPC分类号： F02K3/00 , F02K7/00 , F02K9/00 , F02K99/00
CPC分类号： F02K5/023 , F01D15/10 , F02C3/10 , F02C6/08 , F02K3/06 , F02K3/075
摘要： An engine combination for generating forces with a gas turbine engine generating force, and an internal combustion engine provided in the combination as an intermittent combustion engine generating force having an air intake, there being an air transfer duct connected from a compressor in the gas turbine engine to the air intake to transfer compressed air thereto.
摘要翻译：一种用于产生具有燃气涡轮发动机产生力的发动机组合，以及组合中设置的具有进气口的间歇式内燃机产生力的内燃机，存在从燃气涡轮发动机中的压缩机连接的空气输送管道到空气入口以将压缩空气传送到其上。

8. 发明申请

US20080314573A1 Aircraft combination engines thermal management system 有权
标题翻译：飞机组合引擎热管理系统
公开(公告)号：US20080314573A1
公开(公告)日：2008-12-25
申请号：US11820722
申请日：2007-06-20
申请人： Frederick M. Schwarz , Jorn A. Glahn , Brian M. Fentress
发明人： Frederick M. Schwarz , Jorn A. Glahn , Brian M. Fentress
IPC分类号： F28F3/02
CPC分类号： F01D15/10 , F01D13/02 , F01D25/125 , F02C6/08 , F02C6/10 , F02C7/185 , F02C7/224 , F02K3/06 , F02K3/115 , F05D2220/76 , F05D2260/213 , Y02T50/676
摘要： An engine combination for generating forces with a gas turbine engine generating force that utilizes an engine lubricant for lubricating moving components in the turbofan engine, and an internal combustion engine provided in the combination as an intermittent combustion engine generating force that utilizes a coolant for transporting heat generated in the intermittent combustion engine away therefrom and having an air intake, there being an air transfer duct connected from a compressor in the gas turbine engine to the air intake to transfer compressed air thereto. A coupling heat exchanger is coupled to both the gas turbine engine and the intermittent combustion engine to have the engine lubricant and the coolant pass therethrough to thereby permit the coolant to transport heat in the engine lubricant away therefrom. A further cooling heat exchanger is coupled to both the coupling heat exchanger and the intermittent combustion engine to have a remote fluid from a source thereof and the coolant pass therethrough to permit the remote fluid to transport heat in the coolant away therefrom, and with the coolant also circulating through at least one of the coupling heat exchanger and the intermittent combustion engine.
摘要翻译：一种用于产生力的发动机组合，其具有利用用于润滑涡轮风扇发动机中的运动部件的发动机润滑剂的燃气涡轮发动机产生力，以及组合中设置的内燃机作为利用冷却剂传递热量的间歇性内燃机产生力在间歇式内燃机中产生并且具有进气口，存在从燃气涡轮发动机中的压缩机连接到进气口的空气传送管道，以将压缩空气传送到其上。耦合热交换器被耦合到燃气涡轮发动机和间歇式内燃机两者以使发动机润滑剂和冷却剂通过其中，从而允许冷却剂将发动机润滑剂中的热量从其中传出。另一个冷却热交换器被耦合到耦合热交换器和间歇式内燃机两者以具有来自其源的远程流体，并且冷却剂通过其中以允许远程流体将冷却剂中的热量从其中传输，并且与冷却剂还循环通过耦合热交换器和间歇式内燃机中的至少一个。

9. 发明申请

US20080277533A1 Aircraft combination engines inlet airflow control system 有权
标题翻译：飞机组合引擎入口气流控制系统
公开(公告)号：US20080277533A1
公开(公告)日：2008-11-13
申请号：US11801270
申请日：2007-05-09
申请人： Frederick M. Schwarz , Brian M. Fentress , Andrew P. Berryann , Jorn A. Glahn , Charles E. Lents
发明人： Frederick M. Schwarz , Brian M. Fentress , Andrew P. Berryann , Jorn A. Glahn , Charles E. Lents
IPC分类号： F03B15/00
CPC分类号： F02C5/06 , F02C6/06 , F02C6/08 , F02C7/32 , F05D2220/50 , F05D2220/76 , F05D2260/85
摘要： A power generation system for propelling, and generating electrical power in, an aircraft, having a gas turbine engine in an engine compartment in the aircraft with an air inlet in the aircraft that is curved along its extent in leading to an air compressor in the gas turbine engine having a compressor air transfer duct extending therefrom to an internal combustion engine provided as an intermittent combustion engine at an air intake thereof. An inlet duct manifold is positioned against the duct wall of the inlet duct to cover a perforated portion thereof on the air compressor side of a curve therein with the inlet duct manifold having an inlet air transfer duct extending therefrom that is coupled to the intermittent combustion engine air intake.
摘要翻译：一种用于在飞行器中推进和产生电力的发电系统，其具有在飞行器中的发动机舱中的燃气涡轮发动机，其中在飞行器中具有空气入口，其沿着其空间弯曲，导致气体中的空气压缩机涡轮发动机具有从其延伸到在其进气口处作为间歇式内燃机设置的内燃机的压缩机空气输送管道。入口管道歧管定位成抵靠入口管道的管道壁，以覆盖其曲线的空气压缩机侧的穿孔部分，其中入口管道歧管具有从其延伸的入口空气传送管道，其连接到间歇式内燃机进气口。

10. 发明申请

US20080006022A1 Cooling exchanger ducts 有权
标题翻译：冷却换热器管道
公开(公告)号：US20080006022A1
公开(公告)日：2008-01-10
申请号：US11650825
申请日：2007-01-08
申请人： Frederick M. Schwarz , Jorn A. Glahn
发明人： Frederick M. Schwarz , Jorn A. Glahn
IPC分类号： B64G1/40
CPC分类号： F02C7/14 , F02K3/115 , Y02T50/675
摘要： A heat exchange system for use in operating equipment in which a working fluid is utilized in providing selected operations thereof, including for use in lubricating systems for aircraft turbofan engine equipment, the heat exchange system for providing air and working fluid heat exchanges to cool the working fluid at selectively variable rates in the operating equipment developed airstreams. A heat exchanger core is provided in a controlled air flow duct system opening at its entrance to those airstreams and having its outlet end opening downstream in those airstreams.
摘要翻译：一种用于操作设备的热交换系统，其中使用工作流体来提供其选择的操作，包括用于飞机涡轮风扇发动机设备的润滑系统，用于提供空气的热交换系统和工作流体热交换以冷却工作在操作设备中选择性变化的流体开发出气流。热交换器芯设置在受控的空气流动管道系统中，在其入口处开口，并且其出口端在这些气流中向下游开口。

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