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    • 2. 发明授权
    • Aircraft combination engines exhaust thrust recovery
    • 飞机组合发动机排气推力恢复
    • US07762056B2
    • 2010-07-27
    • US11803432
    • 2007-05-15
    • Frederick M. SchwarzBrian M. FentressCharles E Lents
    • Frederick M. SchwarzBrian M. FentressCharles E Lents
    • F02K3/00F02K7/00F02K9/00F02K99/00
    • F02K5/02F02B61/00F02B65/00F02B73/00F02C3/13F02C5/00F02C6/10F02C6/12F05D2220/50F05D2220/76
    • 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.
    • 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。
    • 8. 发明授权
    • Aircraft combination engines thermal management system
    • 飞机组合引擎热管理系统
    • US07836680B2
    • 2010-11-23
    • US11820722
    • 2007-06-20
    • Frederick M. SchwarzJorn A. GlahnBrian M. Fentress
    • Frederick M. SchwarzJorn A. GlahnBrian M. Fentress
    • F02K3/00
    • F01D15/10F01D13/02F01D25/125F02C6/08F02C6/10F02C7/185F02C7/224F02K3/06F02K3/115F05D2220/76F05D2260/213Y02T50/676
    • 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.
    • 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
    • Aircraft combination engines thermal management system
    • 飞机组合引擎热管理系统
    • US20080314573A1
    • 2008-12-25
    • US11820722
    • 2007-06-20
    • Frederick M. SchwarzJorn A. GlahnBrian M. Fentress
    • Frederick M. SchwarzJorn A. GlahnBrian M. Fentress
    • F28F3/02
    • F01D15/10F01D13/02F01D25/125F02C6/08F02C6/10F02C7/185F02C7/224F02K3/06F02K3/115F05D2220/76F05D2260/213Y02T50/676
    • 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.
    • 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。