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11. 发明公开

EP0142559A4 INTERNAL COMBUSTION ENGINE. 失效
标题翻译：内燃机。
公开(公告)号：EP0142559A4
公开(公告)日：1985-09-26
申请号：EP84902269
申请日：1984-05-17
申请人： PAUL MARIUS A
发明人： PAUL MARIUS A
IPC分类号： F01B29/04 , F02B3/06 , F02B47/02 , F02B69/06 , F02B75/02 , F02D21/06 , F02M25/032 , F01K21/00 , F02M25/02
CPC分类号： F02B47/02 , F01B29/04 , F02B3/06 , F02B69/06 , F02B75/02 , F02B2075/025 , F02B2075/027 , Y02T10/121
摘要： An internal combustion engine which is combined with a thermal cycle of the Rankine type in which water is heated to steam and injected into the engine along with the fuel for increasing the engine output. Increased power can be provided with a turbine compressor (16) receiving the exhaust from the engine and compressing the air intake to the engine. An additional fuel burner (22) may be provided to drive the turbine to provide still further increased and immediate power. The engine may be run either as a two stroke or four stroke engine. A single valve (7) may be used to communicate the engine cylinder with the air intake and exhaust when used in conjunction with a rotating valve (8) which selectively communicates the single valve with the air inlet or outlet. A two cycle engine having a precombustion chamber (35) has an opening which receives a piston profile (38) for providing increased performance.

12. 发明公开

EP0142559A1 INTERNAL COMBUSTION ENGINE 失效
标题翻译：内燃机
公开(公告)号：EP0142559A1
公开(公告)日：1985-05-29
申请号：EP84902269.0
申请日：1984-05-17
申请人： PAUL, Marius A.
发明人： PAUL, Marius A.
IPC分类号： F01B29 , F02B47 , F02B69 , F02B75 , F02D21 , F02M25 , F02B3
CPC分类号： F02B47/02 , F01B29/04 , F02B3/06 , F02B69/06 , F02B75/02 , F02B2075/025 , F02B2075/027 , Y02T10/121
摘要： Moteur à combustion interne combiné avec un cycle thermique de type Rankine où l'eau est chauffée pour devenir de la vapeur et injectée dans le moteur avec le carburant pour accroître le rendement du moteur. La puissance peut être accrue au moyen d'un compresseur à turbine (16) recevant l'échappement du moteur et comprimant l'admission d'air du moteur. Un brûleur de carburant supplémentaire (22) peut être prévu pour entraîner la turbine afin de fournir une puissance instantanée encore accrue. Le moteur peut être utilisé comme moteur deux temps ou moteur quatre temps. Une soupape unique (7) peut être utilisée pour faire communiquer le cylindre du moteur avec l'admission d'air et l'échappement lorsqu'elle est utilisée de concert avec une soupape rotative (8) faisant communiquer de manière sélective la soupape unique avec l'entrée ou la sortie d'air. Un moteur deux temps possèdant une chambre de précombustion (35) comporte une ouverture accueillant un profil de piston (38) afin d'améliorer le rendement.
摘要翻译：内燃机结合兰金式热循环，水被加热变成蒸汽，并通过燃油喷入发动机，提高发动机效率。通过接收发动机排气并压缩发动机进气的涡轮压缩机（16）可增加功率。可以提供额外的燃料燃烧器（22）以驱动涡轮机以提供增加的瞬时功率。电机可以用作二冲程发动机或四冲程发动机。可以使用单个阀（7）将发动机气缸与进气口和排气口连通，当与旋转阀（8）一起使用时，该旋转阀（8）选择性地将单个阀与进气口或出气口。具有预燃室（35）的两冲程发动机具有容纳活塞轮廓（38）的开口以提高效率。

13. 发明授权

EP0211076B1 COMPOUND ROTARY-RECIPROCAL ENGINE 失效转让
标题翻译：复合式旋转发动机
公开(公告)号：EP0211076B1
公开(公告)日：1991-03-27
申请号：EP86902085.9
申请日：1986-01-27
申请人： PAUL, Marius A. , PAUL, Ana
发明人： PAUL, Marius A. , PAUL, Ana
IPC分类号： F02B77/02 , F02B33/44
CPC分类号： F02G3/00 , F02B77/02 , F02D41/3023 , F02F7/0087 , F05C2203/08
摘要： The regenerative thermal engine relates to the field of reciprocating internal combustion engines and in particular to thermal engines that approach adiabatic conditions through effective integration of novel components and operations. Suggested reliance on ceramic components for adiabatic operation has created problems inherent in the materials and in the compatibility of the components with other metallic components. To solve problems encountered in increasing engine efficiency a novel regenerative cylinder (2) has been devised to operate with a piston (6) arranged to avoid contact with the cylinder wall. The regenerative wall or liner has a structure with surface cells (4) designed to admit, hold and release compressed air during the combustion cycle to thermally insulate the cylinder from the heat of combustion. Other components and arrangements combine to enable effective generation and use of higher operating pressures and temperatures to achieve overall engine efficiencies surpassing conventional systems for use in transportation and stationary generation of electrical and mechanical energy.

14. 发明申请

WO2005012714A3 TURBO ROCKET WITH REAL CARNOT CYCLE 审中-公开
标题翻译： TURBO ROCKET与真正的卡车周期
公开(公告)号：WO2005012714A3
公开(公告)日：2007-07-19
申请号：PCT/US2004013234
申请日：2004-04-28
申请人： PAUL MARIUS A
发明人： MARIUS A PAUL
IPC分类号： F02K5/00 , F02K20060101 , F02K3/02
CPC分类号： F01D5/187 , F02C3/067 , F02C3/073 , F02C3/08 , F02C3/36 , F02C7/042 , F02C7/143 , F02K1/1207 , F02K3/10 , F02K3/105 , F02K7/16 , F02K7/18 , F02K9/78 , F05D2260/202 , F05D2260/40311
摘要： Engine embodiments primarily designed for aircraft propulsion and power generation incorporating the Carnot cycle for efficient combustion with typical embodiments including air compressors having one or more stages with isothermal compression and including combustion and expansion chambers having in part isothermal expansion before final adiabatic expansion.
摘要翻译：发动机实施例主要设计用于结合卡诺循环以用于有效燃烧的飞行器推进和发电，其典型实施例包括具有一个或多个等级压缩级的空气压缩机，并且包括在最终绝热膨胀之前具有部分等温膨胀的燃烧和膨胀室。

15. 发明申请

WO2007001427A3 UNIVERSAL CARNOT PROPULSION SYSTEMS FOR TURBO ROCKETRY 审中-公开
公开(公告)号：WO2007001427A3
公开(公告)日：2007-01-04
申请号：PCT/US2005/038008
申请日：2005-10-21
申请人： PAUL, Marius, A.
发明人： PAUL, Marius, A.
IPC分类号： F02K9/66
摘要： Turbofan jet engines utilizing the Carnot cycle for improved performance with isothermal compression of combustion air and, in part, isothermal expansion of thermally heated air, the engines having a turbofan compressor rotor with hollow fan blades in a core bypass passage through the engine and an annular, peripheral thermal chamber with staged turbine blades in an expansion chamber where heated gases are supplied to multiple stages to maintain peak temperatures.

16. 发明申请

WO1985000199A1 PROCESS OF INTENSIFICATION OF THE THERMOENERGETICAL CYCLE AND AIR JET PROPULSION ENGINES 审中-公开
标题翻译：强化循环和空气喷射推进发动机的过程
公开(公告)号：WO1985000199A1
公开(公告)日：1985-01-17
申请号：PCT/US1984000935
申请日：1984-06-20
申请人： PAUL, Marius, A.
IPC分类号： F02C07/20
CPC分类号： F23R3/38 , F01D5/081 , F02C7/16 , F02K7/16 , F23R3/34 , Y02T50/676
摘要： The process of increasing the efficiency and output of a gas-turbine having blades in a combustion chamber (7) which includes cooling the gas-turbine blades (10) with a liquid-fuel and mixing the fuel used for cooling with air in the combustion chamber (7) and burning the mixture and driving the turbine (15) by the exhaust from the combustion chamber (7). This allows the fuel and air to be in stoichiometric mixture. Preferably the fuel is a liquid-gas such as hydrogen. The turbine (15) may be cooled by injecting liquid-fuel onto its disk (11) to provide a film coating which is centrifuged around the blades whereby the liquid will cool both the interior and exterior of the blades and the absorbed heat is introduced into the combustion chamber (7). The combustion chamber (7) includes a plurality of air inlets (8). The turbine (15) drives a compressor, and the compressor and the air inlet may be cooled with the liquid-fuel, which may be cryogenically cooled. An improved jet engine which is convertible from a turbo to a ram-jet is provided.
摘要翻译：在燃烧室（7）中增加具有叶片的燃气轮机的效率和输出的过程，其包括用液体燃料冷却燃气涡轮叶片（10）并将用于冷却的燃料与燃烧中的空气混合燃烧混合物并通过来自燃烧室（7）的排气驱动涡轮机（15）。这允许燃料和空气在化学计量混合物中。优选地，燃料是诸如氢的液体气体。涡轮机（15）可以通过将液体燃料喷射到其盘（11）上来冷却，以提供薄膜涂层，其在叶片周围离心，由此液体将冷却叶片的内部和外部，吸收的热量被引入燃烧室（7）。燃烧室（7）包括多个空气入口（8）。涡轮（15）驱动压缩机，并且压缩机和空气入口可以用可能被低温冷却的液体燃料冷却。提供了一种从涡轮转换成冲压射流的改进的喷气发动机。

17. 发明申请

WO2007025217A3 UNIVERSAL THERMODYNAMIC GAS TURBINE IN A CLOSED CARNOT CYCLE 审中-公开
标题翻译：通用热循环中的通用热力气体涡轮机
公开(公告)号：WO2007025217A3
公开(公告)日：2009-04-30
申请号：PCT/US2006033367
申请日：2006-08-25
申请人： PAUL MARIUS A
发明人： PAUL MARIUS A
IPC分类号： F01K9/00
CPC分类号： F01K25/10 , F01K25/08 , F02C1/10 , F02C7/141 , F05D2210/12 , F05D2210/13 , F05D2240/40
摘要： A closed-cycle gas turbine power generator system with a combined cycle system with a neutral gaseous primary motive medium and a secondary phase change medium with a lower pressure sub-system having a counter-rotating compressor module in combination with a counter-rotating gas turbine module, and with a higher pressure sub-system having a counter-rotating compressor module and a counter-rotating gas turbine module wherein the phase change medium in liquid form is injected into the compressor modules during compression of the primary motive medium with the phase change medium changing to a gas to form a compressed gaseous mixture that is heated by the heat source and supplied to the gas turbine module of the higher pressure sub-system for partial expansion and combining with a heated portion of the compressed gaseous mixture from the compressor module for final expansion in the lower pressure gas turbine modules.
摘要翻译：一种封闭循环燃气轮机发电机系统，其具有具有中性气体主动力介质的组合循环系统和具有低压子系统的次级相变介质，该低压子系统具有反向旋转压缩机模块与反向旋转燃气轮机模块，并具有具有反向旋转压缩机模块和反向旋转燃气轮机模块的更高压力的子系统，其中在相变的主动力介质的压缩期间将液体形式的相变介质注入到压缩机模块中介质改变为气体以形成被热源加热并被供应到高压子系统的燃气轮机模块的压缩气体混合物，用于部分膨胀并与来自压缩机模块的压缩气体混合物的加热部分组合用于在低压燃气轮机模块中的最终膨胀。

18. 发明申请

WO2003095814A1 HIGH EFFICIENCY GAS TURBINE POWER GENERATOR SYSTEMS 审中-公开
标题翻译：高效气体发电机系统
公开(公告)号：WO2003095814A1
公开(公告)日：2003-11-20
申请号：PCT/US2003/014110
申请日：2003-05-07
申请人： PAUL, Marius, A.
发明人： PAUL, Marius, A.
IPC分类号： F02C3/067
CPC分类号： F02C3/05 , F01D1/28 , F01D3/00 , F01D13/02 , F01D15/10 , F02C3/067 , F02C3/30 , F02C5/02 , H02K7/1823
摘要： A gas turbine power generator with ultra high efficiency, the generator being an assembly of electric motor-generator machines (171, 172, 173) and turbine configurations (110, 140) used in combination with combustor systems (180) for operation of select integrated turbine configurations.
摘要翻译：一种具有超高效率的燃气轮机发电机，该发电机是与燃烧器系统（180）组合使用的电动发电机组（171,172,173）和涡轮机结构（110,140）的组合，用于选择集成涡轮机配置。

19. 发明申请

WO2007025217A2 UNIVERSAL THERMODYNAMIC GAS TURBINE IN A CLOSED CARNOT CYCLE 审中-公开
标题翻译：通用热循环中的通用热力气体涡轮机
公开(公告)号：WO2007025217A2
公开(公告)日：2007-03-01
申请号：PCT/US2006/033367
申请日：2006-08-25
申请人： PAUL, Marius, A.
发明人： PAUL, Marius, A.
IPC分类号： F01K9/00
CPC分类号： F01K25/10 , F01K25/08 , F02C1/10 , F02C7/141 , F05D2210/12 , F05D2210/13 , F05D2240/40
摘要： A closed-cycle gas turbine power generator system with a combined cycle system with a neutral gaseous primary motive medium and a secondary phase change medium with a lower pressure sub-system having a counter-rotating compressor module in combination with a counter-rotating gas turbine module, and with a higher pressure sub-system having a counter-rotating compressor module and a counter-rotating gas turbine module wherein the phase change medium in liquid form is injected into the compressor modules during compression of the primary motive medium with the phase change medium changing to a gas to form a compressed gaseous mixture that is heated by the heat source and supplied to the gas turbine module of the higher pressure sub-system for partial expansion and combining with a heated portion of the compressed gaseous mixture from the compressor module for final expansion in the lower pressure gas turbine modules.
摘要翻译：一种封闭循环燃气轮机发电机系统，其具有具有中性气体主动力介质的组合循环系统和具有低压子系统的次级相变介质，该低压子系统具有反向旋转压缩机模块与反向旋转燃气轮机模块，并具有具有反向旋转压缩机模块和反向旋转燃气轮机模块的更高压力的子系统，其中在相变的主动力介质的压缩期间将液体形式的相变介质注入到压缩机模块中介质改变为气体以形成被热源加热并被供应到高压子系统的燃气轮机模块的压缩气体混合物，用于部分膨胀并与来自压缩机模块的压缩气体混合物的加热部分组合用于在低压燃气轮机模块中的最终膨胀。

20. 发明申请

WO2007001427A2 UNIVERSAL CARNOT PROPULSION SYSTEMS FOR TURBO ROCKETRY 审中-公开
标题翻译：用于涡轮轴承的通用卡车推进系统
公开(公告)号：WO2007001427A2
公开(公告)日：2007-01-04
申请号：PCT/US2005038008
申请日：2005-10-21
申请人： PAUL MARIUS A
发明人： PAUL MARIUS A
IPC分类号： F02K3/02
CPC分类号： F02C3/073 , F02C3/045 , F02C3/14 , F02C7/08 , F02C7/10 , F02K3/02 , F02K3/06 , F02K3/08 , F05D2210/42 , F05D2220/327 , F05D2220/36 , Y02T50/671
摘要： Turbofan jet engines utilizing the Carnot cycle for improved performance with isothermal compression of combustion air and, in part, isothermal expansion of thermally heated air, the engines having a turbofan compressor rotor with hollow fan blades in a core bypass passage through the engine and an annular, peripheral thermal chamber with staged turbine blades in an expansion chamber where heated gases are supplied to multiple stages to maintain peak temperatures.
摘要翻译： Turbofan喷气发动机利用卡诺循环来改善燃烧空气的等温压缩性能，并且部分地是热加热空气的等温膨胀，发动机具有涡轮风扇压缩机转子，其具有穿过发动机的铁芯旁通通道中的中空风扇叶片，，具有分级涡轮机叶片的外围热室，在膨胀室中，其中加热的气体被供应到多个级以保持峰值温度。

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