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1. 发明授权

US5716197A High pressure compressor with internal, inter-stage cooled compression having multiple inlets 失效
标题翻译：具有内部，阶段间冷却压缩的高压压缩机具有多个入口
公开(公告)号：US5716197A
公开(公告)日：1998-02-10
申请号：US643057
申请日：1996-05-02
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F02B63/06 , F02B75/06 , F04B25/02 , F04B39/06 , F04B23/00
CPC分类号： F04B39/062 , F02B63/06 , F02B75/065 , F04B25/02 , F04B2205/11
摘要： A high pressure gas compressor having an internal two staged compression with a compression chamber formed in part by a positive displacement, stepped piston and cylinder configuration, providing a first stage compression by an enlarged diameter segment of the piston and a second stage compression provided by a smaller diameter segment of the piston. Temperature is maintained within design limits by the admission to the compression chamber of an expanded gas from a high pressure storage, which on adiabatic expansion of the admission gas reduces the temperature of the mixed charge for final compression at a resultant temperature that is within the design limits of the compressor unit.
摘要翻译：一种具有内部两级压缩的高压气体压缩机，压缩室部分地由正排量，阶梯式活塞和气缸构造形成，通过活塞的扩大直径段提供第一级压缩，以及第二级压缩较小直径的活塞段。通过从高压储存器进入膨胀气体的压缩室，温度保持在设计限度内，在绝热膨胀的入口气体中，在设计内的合成温度下降低混合料的最终压缩温度压缩机单元的极限。

2. 发明授权

US5685272A Self injection system 失效
标题翻译：自动注射系统
公开(公告)号：US5685272A
公开(公告)日：1997-11-11
申请号：US607945
申请日：1996-02-28
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 , F02M7/00
CPC分类号： F02M45/04 , F01L9/02 , 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 injection system having at least one fuel injector with a hydraulically operated actuator for amplifying the pressure of fuel injected from the injector into the combustion chamber, the hydraulic actuator communicating with a hydraulic pulse pump having a slide piston displaced by the pressure of compression and combustion gases within the combustion chamber, the fuel pressure having an amplified pressure profile paralleling the developed pressure profile of gases compressed and combusted in the combustion chamber.
摘要翻译：一种用于具有燃烧室的发动机的燃料喷射系统，所述喷射系统具有至少一个燃料喷射器，其具有用于将从喷射器喷射到燃烧室中的燃料的压力放大的液压操作致动器，液压致动器与液压脉冲泵具有通过燃烧室内的压缩和燃烧气体的压力而移动的滑动活塞，燃料压力具有与在燃烧室中压缩和燃烧的气体的显影压力分布平行的放大压力分布。

3. 发明授权

US5674053A High pressure compressor with controlled cooling during the compression phase 失效
标题翻译：在压缩阶段控制冷却的高压压缩机
公开(公告)号：US5674053A
公开(公告)日：1997-10-07
申请号：US664796
申请日：1996-06-17
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F02B63/06 , F02B75/06 , F04B25/02 , F04B39/06 , F04B39/04
CPC分类号： F02B75/065 , F02B63/06 , F04B25/02 , F04B39/062 , F04B2205/11
摘要： A high pressure gas compressor in one embodiment having an internal two staged compression with a compression chamber formed in part by a positive displacement, stepped piston and cylinder configuration, providing a first stage compression by an enlarged diameter segment of the piston and a second stage compression provided by a smaller diameter segment of the piston, and in another embodiment having an internal, single stage compression with a high compression ratio. Temperature is maintained within design limits by the admission to the compression chamber of an expanded gas from a high pressure storage, which on adiabatic expansion of the admission gas reduces the temperature of the mixed charge for final compression at a resultant temperature that is within the design limits of the compressor unit in one embodiment and by the initial expansion of a residual gas mixed with a compression charge initially, followed by an injection of liquified gas during compression to achieve substantially isothermal compression with the finally compressed gas having an ambient temperature.
摘要翻译：在一个实施例中的高压气体压缩机具有内部两级压缩，其中压缩室部分地由正排量，阶梯式活塞和气缸构造形成，通过活塞的扩大直径段提供第一级压缩和第二级压缩由活塞的较小直径段提供，并且在另一实施例中具有具有高压缩比的内部单级压缩。通过从高压储存器进入膨胀气体的压缩室，温度保持在设计限度内，在绝热膨胀的入口气体中，在设计内的合成温度下降低混合料的最终压缩温度在一个实施方案中压缩机单元的极限值，以及最初膨胀的混合有压缩电荷的残余气体，随后在压缩期间注入液化气体，以实现最终压缩气体具有环境温度的基本等温压缩。

4. 发明授权

US5517951A Two stroke/four stroke engine 失效
标题翻译：两冲程/四冲程发动机
公开(公告)号：US5517951A
公开(公告)日：1996-05-21
申请号：US349732
申请日：1994-12-02
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F01L9/02 , F02B3/06 , F02B69/06 , F02B75/02
CPC分类号： F01L9/02 , F02B69/06 , F02B2075/025 , F02B2075/027 , F02B3/06
摘要： A universal internal combustion engine that is electronically and reversibly convertible from four stroke operation to two stroke operation, the engine having intake and exhaust valves with an electro-hydraulic actuator system for actuating the valves in accordance with electronic control signals from an electronic control module, the electro-hydraulic actuator system having an electronic actuator for each valve coupled to a slide valve for discrete supply of a pressurized hydraulic fluid to a hydraulic piston for each valve, the electronic control module having a program for independent activation of each electronic actuator for select operation of each intake and exhaust valve at any time during the operating cycle.
摘要翻译：一种能够从四冲程操作到两冲程操作的电子和可逆地转换的通用内燃机，该发动机具有进气和排气阀，其具有电液驱动器系统，用于根据来自电子控制模块的电子控制信号致动阀，电动液压致动器系统具有用于每个阀的电子致动器，其连接到滑阀，用于将加压液压流体分离供应到每个阀的液压活塞，该电子控制模块具有用于独立激活每个电子致动器以供选择的程序每个进气门和排气阀在运行循环中的任何时间运行。

5. 发明授权

US5410998A Continuous external heat engine 失效
标题翻译：连续外热机
公开(公告)号：US5410998A
公开(公告)日：1995-05-02
申请号：US7504
申请日：1993-01-22
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F01C19/04 , F02B1/04 , F02B53/00 , F02G3/00 , F04C18/22 , F02G1/02 , F02G1/04
CPC分类号： F01L1/46 , F01C19/04 , F02B53/00 , F02G3/00 , F01L3/205 , F02B1/04 , F02B2053/005 , Y02T10/17
摘要： A thermal engine utilizing a positive displacement rotary expander and preferably a positive displacement rotary compressor in conjunction with an external substantially steady-state thermal source, such as a continuous fuel combustor, the external source heating a high pressure gas that is directed from the thermal source to the rotary expander wherein the gases expand driving a rotor in the positive displacement rotary engine before discharge. An additional embodiment of the thermal engine includes a modified epitrochoidal chamber configuration for the compression cycle and the expansion cycle to utilize the total internal volume for each compression pulse and expansion pulse for obtaining improved thermal efficiency in a manner similar to super long stroke reciprocal piston engines.
摘要翻译：利用正位移旋转膨胀机，优选与正位移旋转式压缩机结合外部基本稳定的热源（例如连续燃料燃烧器）的热发动机，外部源加热从热源引导的高压气体涉及旋转式膨胀机，其中气体在放电之前在正排量旋转发动机中膨胀驱动转子。热引擎的另外的实施例包括用于压缩循环和膨胀循环的改进的外旋腔室构造，以利用每个压缩脉冲和膨胀脉冲的总内部体积，以类似于超长冲程往复式活塞发动机的方式获得改进的热效率。

6. 发明授权

US5355856A High pressure differential fuel injector 失效
标题翻译：高压差动燃油喷射器
公开(公告)号：US5355856A
公开(公告)日：1994-10-18
申请号：US191769
申请日：1994-02-02
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F02M45/10 , F02M47/02 , F02M57/02 , F02M59/10 , F02M63/02 , F02M39/00
CPC分类号： F02M59/105 , F02M45/10 , F02M47/02 , F02M57/025 , F02M63/0225
摘要： A fuel injector system designed to generate an ultra-high, injection pulse with an instant cut-off, the injector system including a distributor component for distributing high pressure fluid from a fuel supply to a fuel injector component and a connected booster component in which the high pressure fuel is increased in pressure to an ultra high fluid pressure by a piston mechanism having large diameter and small diameter pistons. The high pressure fuel hydraulically lifts a needle valve and is ejected through discharge nozzles at the end of the injector component. High pressure fuel in the injector component forces the reseating of the needle valve after fuel discharge.
摘要翻译：一种燃料喷射器系统，其被设计成产生具有瞬时切断的超高喷射脉冲，所述喷射器系统包括用于将高压流体从燃料供应分配到燃料喷射器部件的分配器部件以及连接的升压部件，其中，高压燃料通过具有大直径和小直径的活塞的活塞机构将压力增加到超高流体压力。高压燃料液压提升针阀，并通过喷射器组件末端的排放喷嘴喷射。喷油器部件中的高压燃料迫使排气后针阀停止。

7. 发明授权

US5263645A Fuel injector system 失效
标题翻译：燃油喷射器系统
公开(公告)号：US5263645A
公开(公告)日：1993-11-23
申请号：US786286
申请日：1991-11-01
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F02B75/02 , F02M47/02 , F02M61/16 , F02M61/18 , F02M63/00 , F02M51/06
CPC分类号： F02M63/0007 , F02M47/027 , F02M61/162 , F02M61/1806 , F02B2075/025
摘要： A high pressure fuel injector having high pressure fuel admission passages and low pressure fuel return passages with a needle valve hydraulically operated by high pressure fuel from the high pressure fuel admission passage by a distributor valve which selectively directs a hydraulic pressure fuel against one side or the other of a piston body forming part of the needle valve whereby the needle valve is urged to a position closing discharge orifices or position opening discharge orifices the distributor valve being controlled by an electronic actuator.
摘要翻译：一种高压燃料喷射器，其具有高压燃料进入通道和低压燃料返回通道，其具有通过高压燃料进入通道的高压燃料液压操作的针阀，所述分配器阀选择性地引导液压燃料抵靠一侧或形成针阀的一部分的活塞体的另一个，由此针阀被推动到关闭排出孔或位置打开排出口的位置，分配阀由电子致动器控制。

8. 发明授权

US5224450A Multi-fuel precombustor unit 失效
标题翻译：多燃料预燃机组
公开(公告)号：US5224450A
公开(公告)日：1993-07-06
申请号：US927174
申请日：1992-08-07
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F02B1/04 , F02B19/02
CPC分类号： F02B19/02 , F02B1/04 , Y02T10/125
摘要： A multi-fuel precombustor unit having a housing with an internal precombustion chamber and a passage communicating between the precombustion chamber and the main combustion chamber of the engine on which the precombustor unit is installed, the unit having a valve member blocking the communicating passage with an actuator allowing controlled retraction of the valve member upon activation of a valve actuation mechanism. A compressed air delivery passage regulated by a valve communicates between the main combustion chamber the precombustion chamber for delivery of compressed air to the precombustion chamber, the air delivery providing a carrier for fuel metered into the passage for delivery to the precombustion chamber for initial combustion before release to the main combustion chamber.
摘要翻译：一种多燃料预燃机组件，具有具有内部预燃室的壳体和在其上安装有预燃室单元的发动机的预燃室和主燃烧室之间连通的通道，该单元具有阀构件，其阻塞连通通道致动器允许在启动阀致动机构时阀构件受到控制的缩回。由阀调节的压缩空气输送通道在主燃烧室之间连通预燃室，用于将压缩空气输送到预燃室，空气输送提供用于计量到通道中的燃料的载体，用于输送到预燃室以进行初始燃烧，释放到主燃烧室。

9. 发明授权

US5177954A Gas turbine engine with cooled turbine blades 失效
标题翻译：带涡轮叶片的燃气轮机
公开(公告)号：US5177954A
公开(公告)日：1993-01-12
申请号：US543557
申请日：1990-06-26
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
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 ratio 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 form 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 supplies 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发生，涡轮叶片通过内部通道阵列来保护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形成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。在本发明的另一个独立方面，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，其中第二叶轮进一步用作第一叶轮的扩散器。

10. 发明授权

US5165238A Continuous external heat engine 失效
标题翻译：连续外热机
公开(公告)号：US5165238A
公开(公告)日：1992-11-24
申请号：US704293
申请日：1991-05-21
申请人： Marius A. Paul , Ana Paul
发明人： Marius A. Paul , Ana Paul
IPC分类号： F01C19/04 , F02B1/04 , F02B53/00 , F02G3/00
CPC分类号： F02B53/00 , F01C19/04 , F02G3/00 , F02B1/04 , F02B2053/005 , Y02T10/17
摘要： A thermal engine utilizing a positive displacement rotary expander and preferably a positive displacement rotary compressor in conjunction with an external substantially steady-state thermal source, such as a continuous fuel combustor, the external source heating a high pressure gas that is directed from the thermal source to the rotary expander wherein the gases expand driving a rotor in the positive displacement rotary engine before discharge.
摘要翻译：利用正位移旋转膨胀机，优选与正位移旋转式压缩机结合外部基本稳定的热源（例如连续燃料燃烧器）的热发动机，外部源加热从热源引导的高压气体涉及旋转式膨胀机，其中气体在放电之前在正排量旋转发动机中膨胀驱动转子。

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