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1. 发明申请

US20090183491A1 Internal continuous combustion engine system 有权
标题翻译：内燃机系统
公开(公告)号：US20090183491A1
公开(公告)日：2009-07-23
申请号：US12321163
申请日：2009-01-16
申请人： Peter Hofbauer
发明人： Peter Hofbauer
IPC分类号： F02C7/08 , F02C3/00
CPC分类号： F02C7/224 , F02C3/34 , F02C7/08 , F02K5/023 , Y10T137/87217
摘要： A continuous combustion system for an internal combustion engine includes a reaction vessel external to the engine cylinders. The reaction vessel contains a combustion chamber for sustaining continuous combustion of an air fuel mixture during the operation of the associated engine. The reaction vessel contains an incoming air chamber and an exhaust gas chamber that are each in communication with the combustion chamber. Injected fuel vapor is mixed with scavenged exhaust gas for pre-heating and with compressed air from each cylinder provided during the compression stroke of each piston. The compressed air and fuel vapor mixture sustains the ignited combustion continuously, while exhaust gas is fed to the cylinders to provide working fluid to the engine during the power stroke of each piston. A valve mechanism is provided to control the flow of air from and working fluid to the cylinders at the appropriate times in order to sustain operation of the engine.
摘要翻译：用于内燃机的连续燃烧系统包括在发动机气缸外部的反应容器。反应容器包含用于在相关联的发动机操作期间维持空气燃料混合物的连续燃烧的燃烧室。反应容器包含与燃烧室连通的进入空气室和废气室。将注入的燃料蒸气与用于预热的清除的废气和每个活塞的压缩冲程期间提供的来自每个气缸的压缩空气混合。压缩空气和燃料蒸气混合物持续点燃燃烧，同时在每个活塞的动力冲程期间将废气送入气缸以向发动机提供工作流体。提供阀机构以在适当的时间控制来自气缸和工作流体的气流，以维持发动机的运转。

2. 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。

3. 发明授权

US3188805A Internal combustion engine 失效
公开(公告)号：US3188805A
公开(公告)日：1965-06-15
申请号：US25839363
申请日：1963-02-14
申请人： GAHAGAN CHARLES L
发明人： GAHAGAN CHARLES L
IPC分类号： F02B71/06 , F02K5/02
CPC分类号： F02B71/06 , F02K5/023 , Y02T50/671

4. 发明授权

US3112613A Positive power jet engine 失效
标题翻译：正功率喷气发动机
公开(公告)号：US3112613A
公开(公告)日：1963-12-03
申请号：US1671860
申请日：1960-03-22
申请人： NELSON DANIEL E
发明人： NELSON DANIEL E
IPC分类号： F02K5/02
CPC分类号： F02K5/023

5. 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。

6. 再颁专利

USRE35172E Pulsed piston-compressor jet engine 失效
标题翻译：脉冲活塞式压缩机喷气发动机
公开(公告)号：USRE35172E
公开(公告)日：1996-03-12
申请号：US375381
申请日：1995-01-17
申请人： Barre A. M. Clark
发明人： Barre A. M. Clark
IPC分类号： F02B1/04 , F02B75/02 , F02K5/02 , F02K7/06
CPC分类号： F02K5/023 , F02K7/06 , F02B1/04 , F02B2075/025 , Y02T50/671
摘要： An air-breathing pulsed jet engine for aircraft propulsion which employs a piston compressor rather than much more expensive axial or centrifugal compressors and turbines employed by conventional turbojet engines. The engine is similar to the common two-cycle gasoline engine, except its cylinder head comprises a jet nozzle with an internal pressure-activated nozzle-blocking valve. A spring keeps this valve closed during the engine's compression stroke when the piston, connected to a crankshaft and flywheels by a connecting rod, is forced by the moment-of-inertia of the flywheels toward the cylinder head. When ignition and combustion of the compressed air and fuel occurs slightly before the piston reaches the top of its stroke, the much greater pressures within the engine's combustion chamber force the valve to pivot open. This allows a jet of combustion gases to be released through the jet nozzle into the atmosphere. The reactive forces of the gas jet work against the piston to produce linear thrust (due to the moment-of-inertia of the flywheels) and to store up energy in the flywheels to motivate the piston through the next compression stroke. The jet pulse continues until the pressure inside the combustion chamber drops to a predetermined level, when the spring is able to close the valve. Since the pressure inside the combustion chamber of a gasoline engine are on the order of those inside many rocket motors, the thrusts imparted to the engine during each jet pulse is substantial.
摘要翻译：一种用于飞行器推进的呼吸脉冲喷气发动机，其使用活塞式压缩机，而不是由常规涡轮喷气发动机采用的更昂贵的轴向或离心压缩机和涡轮机。发动机类似于普通的双循环汽油发动机，除了其气缸盖包括具有内部压力激活喷嘴截止阀的喷嘴。当发动机的压缩冲程中，当通过连接杆连接到曲轴和飞轮的活塞被飞轮的惯性矩向气缸盖强制时，弹簧保持该阀关闭。当压缩空气和燃料的点燃和燃烧在活塞到达其行程的顶部之前稍微发生时，发动机的燃烧室内的更大的压力迫使阀枢转打开。这使得燃烧气体的喷射通过喷嘴释放到大气中。气体射流的反作用力对活塞产生线性推力（由于飞轮的惯性矩），并且在飞轮中储存能量以通过下一个压缩冲程来激励活塞。当弹簧能够关闭阀时，喷射脉冲持续直到燃烧室内的压力下降到预定水平。由于汽油发动机的燃烧室内的压力是许多火箭发动机内部的压力，因此在每个喷射脉冲期间赋予发动机的推力是显着的。

7. 发明授权

US2512254A Jet engine, including reciprocating pressure gas generator 失效
标题翻译：喷气发动机，包括往复式压气发生器
公开(公告)号：US2512254A
公开(公告)日：1950-06-20
申请号：US56804644
申请日：1944-12-13
申请人： MARION MALLORY
发明人： MARION MALLORY
IPC分类号： F02K5/02
CPC分类号： F02K5/023

8. 发明授权

US08490380B2 Internal continuous combustion engine system 有权
公开(公告)号：US08490380B2
公开(公告)日：2013-07-23
申请号：US12321163
申请日：2009-01-16
申请人： Peter Hofbauer
发明人： Peter Hofbauer
IPC分类号： F02G3/02 , F02D41/32 , F15B13/044
CPC分类号： F02C7/224 , F02C3/34 , F02C7/08 , F02K5/023 , Y10T137/87217
摘要： A continuous combustion system for an internal combustion engine includes a reaction vessel external to the engine cylinders. The reaction vessel contains a combustion chamber for sustaining continuous combustion of an air fuel mixture during the operation of the associated engine. The reaction vessel contains an incoming air chamber and an exhaust gas chamber that are each in communication with the combustion chamber. Injected fuel vapor is mixed with scavenged exhaust gas for pre-heating and with compressed air from each cylinder provided during the compression stroke of each piston. The compressed air and fuel vapor mixture sustains the ignited combustion continuously, while exhaust gas is fed to the cylinders to provide working fluid to the engine during the power stroke of each piston. A valve mechanism is provided to control the flow of air from and working fluid to the cylinders at the appropriate times in order to sustain operation of the engine.

9. 发明授权

US5361581A Pulsed piston-compressor jet engine 失效
标题翻译：脉冲活塞式压缩机喷气发动机
公开(公告)号：US5361581A
公开(公告)日：1994-11-08
申请号：US51026
申请日：1993-04-21
申请人： Barre A. M. Clark
发明人： Barre A. M. Clark
IPC分类号： F02B1/04 , F02B75/02 , F02K5/02 , F02K7/06
CPC分类号： F02K5/023 , F02K7/06 , F02B1/04 , F02B2075/025 , Y02T50/671
摘要： An air-breathing pulsed jet engine for aircraft propulsion which employs a piston compressor rather than much more expensive axial or centrifugal compressors and turbines employed by conventional turbojet engines. The engine is similar to the common two-cycle gasoline engine, except its cylinder head comprises a jet nozzle with an internal pressure-activated nozzle-blocking valve. A spring keeps this valve closed during the engine's compression stroke when the piston, connected to a crankshaft and flywheels by a connecting rod, is forced by the moment-of-inertia of the flywheels toward the cylinder head. When ignition and combustion of the compressed air and fuel occurs slightly before the piston reaches the top of its stroke, the much greater pressures within the engine's combustion chamber force the valve to pivot open. This allows a jet of combustion gases to be released through the jet nozzle into the atmosphere. The reactive forces of the gas jet work against the piston to produce linear thrust (due to the moment-of-inertia of the flywheels) and to store up energy in the flywheels to motivate the piston through the next compression stroke. The jet pulse continues until the pressure inside the combustion chamber drops to a predetermined level, when the spring is able to close the valve. Since the pressures inside the combustion chamber of a gasoline engine are on the order of those inside many rocket motors, the thrusts imparted to the engine during each jet pulse is substantial.
摘要翻译：一种用于飞行器推进的呼吸脉冲喷气发动机，其使用活塞式压缩机，而不是由常规涡轮喷气发动机采用的更昂贵的轴向或离心压缩机和涡轮机。发动机类似于普通的双循环汽油发动机，除了其气缸盖包括具有内部压力激活喷嘴截止阀的喷嘴。当发动机的压缩冲程中，当通过连接杆连接到曲轴和飞轮的活塞被飞轮的惯性矩向气缸盖强制时，弹簧保持该阀关闭。当压缩空气和燃料的点燃和燃烧在活塞到达其行程的顶部之前稍微发生时，发动机的燃烧室内的更大的压力迫使阀枢转打开。这使得燃烧气体的喷射通过喷嘴释放到大气中。气体射流的反作用力对活塞产生线性推力（由于飞轮的惯性矩），并且在飞轮中储存能量以通过下一个压缩冲程来激励活塞。当弹簧能够关闭阀时，喷射脉冲持续直到燃烧室内的压力下降到预定水平。由于汽油发动机的燃烧室内的压力是许多火箭发动机内的压力，因此在每个喷射脉冲期间赋予发动机的推力是显着的。

10. 发明授权

US2587073A Compound reciprocating-pulse jet aircraft power plant 失效
标题翻译：复合往复脉冲喷气飞机发电厂
公开(公告)号：US2587073A
公开(公告)日：1952-02-26
申请号：US11204449
申请日：1949-08-24
申请人： SWARTZ ROBERT H
发明人： SWARTZ ROBERT H
IPC分类号： F02K5/02
CPC分类号： F02K5/023

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