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31. 发明授权

US4843813A Compact turbocompressor unit 失效
标题翻译：紧凑型涡轮压缩机单元
公开(公告)号：US4843813A
公开(公告)日：1989-07-04
申请号：US127804
申请日：1987-12-02
申请人： Marius A. Paul
发明人： Marius A. Paul
IPC分类号： F01D5/14 , F02C3/067 , F02C3/08 , F02C6/12 , F04D17/12 , F04D25/04
CPC分类号： F02C6/12 , F01D5/142 , F02C3/067 , F02C3/085 , F04D17/127 , F04D25/04
摘要： A compact double-stage turbocompressor unit having a compressor section with two-stage, radially aligned rotors that are counter rotated and a turbine section with two-stage, radially aligned rotors that are counter rotated, the rotors of the low pressure compressor and turbine sections being interconnected and the rotors of the high pressure compressor and turbine sections being interconnected.
摘要翻译：紧凑型双级涡轮压缩机单元，其具有压缩机部分，其具有反向旋转的两级径向排列的转子和具有反向旋转的两级径向排列的转子的涡轮部分，低压压缩机和涡轮部分的转子并且高压压缩机和涡轮机部分的转子相互连接。

32. 发明授权

US4791787A Regenerative thermal engine 失效
公开(公告)号：US4791787A
公开(公告)日：1988-12-20
申请号：US805184
申请日：1985-12-05
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F02B77/02 , F02D41/30 , F02F7/00 , F02G3/00 , F02B33/44
CPC分类号： F02B77/02 , F02F7/0087 , F02G3/00 , F02D41/3023 , F05C2203/08
摘要： An internal combustion engine having a cylinder, a piston reciprocally movable in the cylinder, the cylinder and piston defining in part a chamber for combustion, intake means for introducing air into the cylinder at predetermined intervals, exhaust means for removing combustion gases from the cylinder at predetermined intervals, and a regenerator liner in at least a part of the chamber, the liner having a structure with surfaces defining a plurality of regenerative cells constructed to cyclically admit, hold and discharge compressed air from the cylinder for thermally insulating the cylinder from the heat of combustion, the engine including a mechanism to maintain the piston displaced from the cylinder to avoid contact of the piston with the liner and including a positive displacement, rotary compressor-expander to precompress air delivered to the piston cylinder and receive combustion gases from the cylinder to drive the compressor-expander.

33. 发明授权

US07426832B2 Universal thermodynamic gas turbine in a closed Carnot cycle 失效
标题翻译：通用热力学燃气轮机在封闭的卡诺循环
公开(公告)号：US07426832B2
公开(公告)日：2008-09-23
申请号：US11212815
申请日：2005-08-25
申请人： Marius A. Paul
发明人： Marius A. Paul
IPC分类号： F01K7/34
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。

34. 发明申请

US20080148739A1 FLUIDIZED BED HEAVY FUEL COMBUSTOR 审中-公开
标题翻译：流化床重型燃油机
公开(公告)号：US20080148739A1
公开(公告)日：2008-06-26
申请号：US11748728
申请日：2007-05-15
申请人： Marius A. Paul
发明人： Marius A. Paul
IPC分类号： F23C10/00 , F02C3/04
CPC分类号： F23C10/00 , F02C3/24 , F23C2900/99004 , F23G2900/50001 , F23L15/04 , F23L2900/00001 , Y02E20/348
摘要： A method and system for burning a first and second fuel includes injecting a first fuel into a super-heated highly compressed stream at approximately one-fourth of a stoichiometric ratio to the oxygen in the highly compressed stream. Combustion of the first fuel further heats the highly compressed stream. The highly compressed stream is admitted into a combustion vessel to fluidize a bed of a second fuel with the highly compressed stream. The second fuel is combusted to create a compressed effluent which fluidizes an adsorbent bed to remove sulfur from the compressed effluent.
摘要翻译：用于燃烧第一和第二燃料的方法和系统包括将第一燃料以与高压缩流中的氧的化学计量比大约四分之一的超加热高度压缩流注入。第一燃料的燃烧进一步加热高度压缩的流。将高度压缩的流进入燃烧容器中以使高压缩流流化第二燃料的床。第二燃料燃烧以产生压缩流出物，其使吸附剂床流化，以从压缩流出物中除去硫。

35. 发明授权

US06966174B2 Integrated bypass turbojet engines for air craft and other vehicles 失效
标题翻译：飞行器和其他车辆的集成旁路涡轮喷气发动机
公开(公告)号：US06966174B2
公开(公告)日：2005-11-22
申请号：US10383462
申请日：2003-03-06
申请人： Marius A. Paul
发明人： Marius A. Paul
IPC分类号： B64C29/00 , B64D27/16 , F02C3/045 , F02C3/08 , F02K3/02 , F02K3/04 , F02K3/077 , F02C3/14
CPC分类号： F02K3/04 , B64C29/0075 , B64D27/16 , F02C3/045 , F02C3/08 , F02K3/02 , F02K3/077 , Y02T50/44 , Y02T50/671
摘要： Turbojet engines and aircraft configurations for advantageous use of the turbojet engines; the turbojet engines utilizing ram air turbine units that centrifugally compress air isothermally for use in various combustion configurations designed for stoichiometric combustion, wherein a stream of by-pass ram-air jets is mixed with combustion gas jets for discharge in a common discharge nozzle.
摘要翻译： Turbojet发动机和飞机配置，有利于涡轮喷气发动机; 涡轮喷气发动机利用冲压空气涡轮机单元，其等压地空气压缩空气，用于设计用于化学计量燃烧的各种燃烧配置中，其中旁路冲击空气射流流与燃烧气体射流混合，以便在公共排放喷嘴中排放。

36. 发明授权

US06845942B2 Omni-directional air vehicle personal transportation system 失效
标题翻译：全方位空中车辆个人运输系统
公开(公告)号：US06845942B2
公开(公告)日：2005-01-25
申请号：US10371680
申请日：2003-02-20
申请人： Marius A. Paul
发明人： Marius A. Paul
IPC分类号： B64C39/02 , B64C15/00
CPC分类号： B64C39/026
摘要： An omni-directional air vehicle having a pod with a connected turbofan system, the pod has a body that contains a power source for generating electrical power and a ducted fan with spherical articulation mechanism having a projecting arm with counter-rotating propellers and a ducted shroud around the periphery of the counter rotating propellers and containing drive motors for electrically driving the propellers.
摘要翻译：一种具有连接的涡扇风扇系统的荚的全方位空中飞行器，所述荚具有包含用于产生电力的动力源的主体和具有球形关节运动机构的管道风扇，所述风扇具有带反向旋转螺旋桨的突出臂和管道罩围绕反旋转螺旋桨的周边并且包含用于电驱动螺旋桨的驱动马达。

37. 发明授权

US06282897B1 Advanced thermo-electronic systems for hybrid electric vehicles 失效
标题翻译：混合电动汽车先进的热电子系统
公开(公告)号：US06282897B1
公开(公告)日：2001-09-04
申请号：US09583103
申请日：1998-05-18
申请人： Marius A. Paul
发明人： Marius A. Paul
IPC分类号： F02B3910
CPC分类号： B60K6/24 , B60K6/46 , B60W2710/06 , F01D15/10 , F02B39/10 , F02C3/09 , F02C5/06 , F02C6/20 , Y02T10/6217 , Y02T10/6295 , Y10S903/905
摘要： A hybrid propulsion system for vehicles having an electronic storage and drive system for driving a vehicle and a thermal engine for charging and energizing the electrical storage and drive system, the thermal engine having a thermal energy source with a compressor and turbine combination operating in a Brayton cycle with the compressor being driven by an electrical motor and the turbine driving a generator, the compressor compressing the motive gas which is thermally heated by the thermal energy source and the heated gas expanding in the turbine.
摘要翻译：一种用于车辆的混合动力推进系统，具有用于驱动车辆的电子存储和驱动系统以及用于对电气存储和驱动系统进行充电和激励的热引擎，热机具有具有压缩机的热能源和在Brayton中操作的涡轮组合循环，压缩机由电动机驱动，涡轮驱动发电机，压缩机压缩由热能源热加热的动力气体和在涡轮机中膨胀的加热气体。

38. 发明授权

US06227823B1 Compressed gas dispensing station with high pressure compressor with internal cooled compression 失效
标题翻译：具有内部冷却压缩的高压压缩机的压缩气体分配站
公开(公告)号：US06227823B1
公开(公告)日：2001-05-08
申请号：US09095375
申请日：1998-06-10
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F04B2300
CPC分类号： F04B41/02 , F04B39/062
摘要： A compressed gas dispensing station having a high pressure gas compressor with a cyclic control system for selective recirculation of cooled, ultra high pressure gas through the compression chamber after the end of the compression stroke for scavenging hot compressed gas from the compression chamber and providing a residual, partially-expanded replacement gas for the expansion stroke which is mixed with the incoming, new charge of gas for a cryogenic gas at the start of compression and a relatively low temperature gas at the end of compression for a single stage compressor. The cyclic control system times the opening and closing of two delivery valves for separate 4000 psi and a 3600 psi branches, the delivery valve for the 4000 psi branch also regulating recirculation of 4000 psi cooled gas through the compression chamber for the 3600 psi branch after the end of the compression stroke to cool the chamber and replace the hot residual compression gas with a cold expanded gas, which is further expanded in the expansion stroke. Compressed gas is collected and stored in two receiver tanks having different pressures for mixing and dispensing at a customer service station according to customer requirements.
摘要翻译：一种具有高压气体压缩机的压缩气体分配站，具有循环控制系统，用于在压缩冲程结束之后通过压缩室选择性再循环冷却的超高压气体，以从压缩室中清除热压缩气体并提供残余物用于膨胀冲程的部分膨胀的替代气体，其与在压缩开始时用于低温气体的新的气体输入混合，并且在单级压缩机的压缩结束时与相对低温的气体混合。循环控制系统打开和关闭两个输送阀，分开4000 psi和3600 psi分支，4000 psi分支的输送阀也可调节4000 psi冷却气体通过压缩室的再循环，用于3600 psi分支结束压缩行程以冷却腔室，并用冷膨胀气体替换热残余压缩气体，膨胀气体在膨胀冲程中进一步膨胀。根据客户要求，将压缩气体收集并储存在具有不同压力的两个接收罐中，用于在客户服务站进行混合和分配。

39. 发明授权

US5862792A Self-injection system 失效
标题翻译：自动注射系统
公开(公告)号：US5862792A
公开(公告)日：1999-01-26
申请号：US909164
申请日：1997-08-11
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F01L9/02 , F02M45/04 , F02M45/12 , F02M49/02 , F02M57/02 , F02M59/36 , F02M61/08 , F02M61/16 , F02M37/04
CPC分类号： F01L9/02 , F02M45/04 , F02M45/12 , F02M49/02 , F02M57/025 , F02M57/028 , F02M59/366 , F02M61/08 , F02M61/162
摘要： A fuel injection system for an engine having a combustion chamber, the fuel injection system in a preferred embodiment having a hydraulic actuator module with a hydraulic actuating fluid for activating a fuel injection piston with fluid in an actuating chamber of an injector defined in part by a large head, amplifying piston connected to the fuel injection piston the actuating fluid communicating with a hydraulic pulse pump driven by the pressure in the combustion chamber, the injector including a sub-module to provide a multi-pulse discharge to fuel and a discharge nozzle having an orifice with a poppet valve having a structure to provide a pulsed, conical, swirling spray of fuel.
摘要翻译：一种用于具有燃烧室的发动机的燃料喷射系统，在优选实施例中的燃料喷射系统具有液压致动器模块，该液压致动器模块具有液压致动流体，用于在喷射器的致动室中启动具有流体的喷射活塞，连接到燃料喷射活塞的放大活塞，与由燃烧室中的压力驱动的液压脉冲泵连通的致动流体，所述喷射器包括用于向燃料提供多脉冲排放的子模块和具有具有提升阀的孔口具有提供脉冲的，锥形的旋转燃料喷雾的结构。

40. 发明授权

US5341636A Gas turbine engine operating method 失效
标题翻译：燃气轮机发动机运行方式
公开(公告)号：US5341636A
公开(公告)日：1994-08-30
申请号：US3098
申请日：1993-01-11
申请人： Marius A. Paul
发明人： Marius A. Paul
IPC分类号： F01D5/18 , F02C6/00 , F02C7/12 , F02C9/16 , F02K3/075 , F23R3/34 , F23R3/38 , F02C7/16
CPC分类号： F01D5/18 , F01D5/185 , F01D5/189 , F02C3/08 , F02C3/30 , F02C6/003 , F02C7/12 , F02C7/16 , F02C7/224 , F02C9/16 , F02K3/075 , F02K3/10 , F02K3/11 , F23R3/34 , F23R3/38 , F05D2260/201 , F05D2260/232 , Y02E20/14 , Y02T50/671 , Y02T50/676
摘要： A gas turbine engine that can operate at a very high efficiency over a wide range of load conditions. In one important feature of the invention, combustion gases are discharged along two paths, one with constant energy and the other with energy that varies in accordance with the engine load. The constant energy discharge drives a turbine that, in turn, operates a compressor for the engine at a constant, high efficiency. Alternatively, the compressor is driven at a speed that varies inversely with the engine load such that the engine operates at a high efficiency for all loads. In another, independent feature of the invention, the combustion occurs at a stoichiometric ration of fuel and air, with the turbine blades being protected from the vastly increased combustion gas temperatures by an internal array of passageways through which cooling liquid, e.g., liquid fuel, and air are channeled. The fuel and air mix together to from a rich, turbulent pre-mix for ejection directly into the surrounding combustion chamber. This configuration can also be utilized to inject steam into the combustion chamber, to provide a Rankine cycle, with internal cogeneration. In yet another independent aspect of the invention, the compressor that supplied compressed air to the combustion chamber includes two counter-rotating radial impellers, with the second impeller further functioning as a diffuser for the first impeller.
摘要翻译：一种燃气涡轮发动机，可在宽范围的负载条件下以非常高的效率运行。在本发明的一个重要特征中，燃烧气体沿着两个路径排出，一个具有恒定的能量，另一个具有根据发动机负载而变化的能量。恒定能量放电驱动涡轮机，涡轮机又以恒定的高效率操作发动机的压缩机。或者，压缩机以与发动机负载成反比的速度驱动，使得发动机以高效率对所有负载进行操作。在另一个本发明的独立特征中，燃烧以燃料和空气的化学计量比进行发生，通过内部的通道阵列来保护涡轮机叶片免受大大增加的燃烧气体温度的影响，冷却液体例如液体燃料，空气被引导。燃料和空气混合在一起，由丰富的湍流预混合物直接喷射到周围的燃烧室中。这种结构也可用于将蒸气喷入燃烧室，以提供具有内部热电联产的兰金循环。在本发明的另一独立方面，向燃烧室供应压缩空气的压缩机包括两个反向旋转的径向叶轮，第二叶轮还用作第一叶轮的扩散器。

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