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1. 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。

2. 发明申请

US20090065652A1 Aircraft combination engines exhaust thrust recovery 有权
标题翻译：飞机组合发动机排气推力恢复
公开(公告)号：US20090065652A1
公开(公告)日：2009-03-12
申请号：US11803432
申请日：2007-05-15
申请人： Frederick M. Schwarz , Brian M. Fentress , Charles E. Lents
发明人： Frederick M. Schwarz , Brian M. Fentress , Charles E. Lents
IPC分类号： B64D27/02 , F02C6/06 , F02G3/00 , F02B65/00 , F02B63/04
CPC分类号： F02K5/02 , F02B61/00 , F02B65/00 , F02B73/00 , F02C3/13 , F02C5/00 , F02C6/10 , F02C6/12 , F05D2220/50 , F05D2220/76
摘要： A gas turbine engine with a turbine with an exhaust manifold thereabout from which fluids can be transferred to the turbine and an air compressor having an air transfer duct extending therefrom so as to be capable to provide compressed air in that air transfer duct at one end thereof to the air intake of an internal combustion engine provided as an intermittent combustion engine. The air intake and an exhaust outlet are each coupled to combustion chambers therein and a rotatable output shaft is also coupled to those combustion chambers for generating force. The exhaust outlet has an exhaust transfer duct extending therefrom so as to have the intermittent combustion engine be capable to provide exhaust therefrom in that exhaust transfer duct at one end thereof, and the exhaust transfer duct being connected at an opposite end thereof to the exhaust manifold to be capable of transferring intermittent combustion engine exhaust thereto.
摘要翻译：一种具有涡轮机的燃气涡轮发动机，具有排气歧管，流体可从该排气歧管传递到涡轮机，以及具有从其延伸的空气传输管道的空气压缩机，以便能够在该空气传输管道的一端处提供压缩空气到作为间歇式内燃机设置的内燃机的进气口。进气口和排气出口各自连接到其中的燃烧室，并且可旋转输出轴也联接到那些燃烧室以产生力。排气出口具有从其延伸的排气传送管道，以便使间歇式内燃机能够在其一端处于该排气传送管道中提供排气，并且排气传送管道在其相对端连接到排气歧管能够将间歇的内燃机排气转移到其上。

3. 发明授权

US07762056B2 Aircraft combination engines exhaust thrust recovery 有权
标题翻译：飞机组合发动机排气推力恢复
公开(公告)号：US07762056B2
公开(公告)日：2010-07-27
申请号：US11803432
申请日：2007-05-15
申请人： Frederick M. Schwarz , Brian M. Fentress , Charles E Lents
发明人： Frederick M. Schwarz , Brian M. Fentress , Charles E Lents
IPC分类号： F02K3/00 , F02K7/00 , F02K9/00 , F02K99/00
CPC分类号： F02K5/02 , F02B61/00 , F02B65/00 , F02B73/00 , F02C3/13 , F02C5/00 , F02C6/10 , F02C6/12 , F05D2220/50 , F05D2220/76
摘要： A gas turbine engine with a turbine with an exhaust manifold thereabout from which fluids can be transferred to the turbine and an air compressor having an air transfer duct extending therefrom so as to be capable to provide compressed air in that air transfer duct at one end thereof to the air intake of an internal combustion engine provided as an intermittent combustion engine. The air intake and an exhaust outlet are each coupled to combustion chambers therein and a rotatable output shaft is also coupled to those combustion chambers for generating force. The exhaust outlet has an exhaust transfer duct extending therefrom so as to have the intermittent combustion engine be capable to provide exhaust therefrom in that exhaust transfer duct at one end thereof, and the exhaust transfer duct being connected at an opposite end thereof to the exhaust manifold to be capable of transferring intermittent combustion engine exhaust thereto.
摘要翻译：一种具有涡轮机的燃气涡轮发动机，具有排气歧管，流体可从该排气歧管传递到涡轮机;以及空气压缩机，其具有从其延伸的空气传送管道，以便能够在该空气传输管道的一端处提供压缩空气到作为间歇式内燃机设置的内燃机的进气口。进气口和排气出口各自连接到其中的燃烧室，并且可旋转输出轴也联接到那些燃烧室以产生力。排气出口具有从其延伸的排气传送管道，以便使间歇式内燃机能够在其一端处于该排气传送管道中提供排气，并且排气传送管道在其相对端连接到排气歧管能够将间歇的内燃机排气转移到其上。

4. 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。

5. 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。

6. 发明授权

US07690189B2 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：US07690189B2
公开(公告)日：2010-04-06
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： F02K3/00 , F02K7/00 , F02K9/00 , F02K99/00
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。

7. 发明授权

US08015795B2 Aircraft combination engines plural airflow conveyances system 失效
标题翻译：飞机组合引擎多重气流运输系统
公开(公告)号：US08015795B2
公开(公告)日：2011-09-13
申请号：US11804429
申请日：2007-05-18
申请人： Frederick M. Schwarz , Brian M. Fentress
发明人： Frederick M. Schwarz , Brian M. Fentress
IPC分类号： F02K3/00 , F02K7/00 , F02K9/00 , F02K99/00
CPC分类号： F01D13/02 , F02C5/06 , F02C6/08 , F05D2220/76
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 a plurality of air transfer ducts each extending from a different location in the gas turbine engine so as to be capable to provide air in each of those air transfer ducts at one end thereof at pressures differing from one another and connected at the other end of each to the air intake to transfer air thereto.
摘要翻译：用于产生具有燃气涡轮发动机产生力的力的发动机组合和设置在该组合中的内燃机作为具有进气口的间歇式内燃机产生力，存在多个空气传送管道，每个空气传送管道从不同位置延伸燃气涡轮发动机，以便能够在其一端处在彼此不同的压力下在这些空气输送管道的每一个中提供空气，并且在每个空气传输管道的另一端连接到进气口以将空气输送到其上。

8. 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。

9. 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。

10. 发明申请

US20100013242A1 Aircraft combination engines plural airflow conveyances system 失效
标题翻译：飞机组合引擎多重气流运输系统
公开(公告)号：US20100013242A1
公开(公告)日：2010-01-21
申请号：US11804429
申请日：2007-05-18
申请人： Frederick M. Schwarz , Brian M. Fentress
发明人： Frederick M. Schwarz , Brian M. Fentress
IPC分类号： F01B21/04 , H02K23/52 , F01D15/10
CPC分类号： F01D13/02 , F02C5/06 , F02C6/08 , F05D2220/76
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 a plurality of air transfer ducts each extending from a different location in the gas turbine engine so as to be capable to provide air in each of those air transfer ducts at one end thereof at pressures differing from one another and connected at the other end of each to the air intake to transfer air thereto.
摘要翻译：用于产生具有燃气涡轮发动机产生力的力的发动机组合和设置在该组合中的内燃机作为具有进气口的间歇式内燃机产生力，存在多个空气传送管道，每个空气传送管道从不同位置延伸燃气涡轮发动机，以便能够在其一端处在彼此不同的压力下在这些空气输送管道的每一个中提供空气，并且在每个空气传输管道的另一端连接到进气口以将空气输送到其上。

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