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

Applicant: PAUL MARIUS A

Inventor： MARIUS A PAUL

IPC: F02K5/00 ,  F02K20060101 ,  F02K3/02

CPC classification number: 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

Abstract: 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.

Abstract translation: 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。

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

Applicant: PAUL, Marius, A.

Inventor： PAUL, Marius, A.

IPC: F02K9/66

Abstract: 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.

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

Applicant: PAUL, Marius, A.

IPC: F02C07/20

CPC classification number: F23R3/38 ,  F01D5/081 ,  F02C7/16 ,  F02K7/16 ,  F23R3/34 ,  Y02T50/676

Abstract: 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.

Abstract translation: 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。

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

Applicant: PAUL MARIUS A

Inventor： PAUL MARIUS A

IPC: F01K9/00

CPC classification number: F01K25/10 ,  F01K25/08 ,  F02C1/10 ,  F02C7/141 ,  F05D2210/12 ,  F05D2210/13 ,  F05D2240/40

Abstract: 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.

Abstract translation: 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。

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

Applicant: PAUL, Marius, A.

Inventor： PAUL, Marius, A.

IPC: F02C3/067

CPC classification number: F02C3/05 ,  F01D1/28 ,  F01D3/00 ,  F01D13/02 ,  F01D15/10 ,  F02C3/067 ,  F02C3/30 ,  F02C5/02 ,  H02K7/1823

Abstract: 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.

Abstract translation: 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。

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

Applicant: PAUL, Marius, A.

Inventor： PAUL, Marius, A.

IPC: F01K9/00

CPC classification number: F01K25/10 ,  F01K25/08 ,  F02C1/10 ,  F02C7/141 ,  F05D2210/12 ,  F05D2210/13 ,  F05D2240/40

Abstract: 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.

Abstract translation: 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。

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

Applicant: PAUL MARIUS A

Inventor： PAUL MARIUS A

IPC: F02K3/02

CPC classification number: F02C3/073 ,  F02C3/045 ,  F02C3/14 ,  F02C7/08 ,  F02C7/10 ,  F02K3/02 ,  F02K3/06 ,  F02K3/08 ,  F05D2210/42 ,  F05D2220/327 ,  F05D2220/36 ,  Y02T50/671

Abstract: 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.

Abstract translation: 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。

公开(公告)号：WO1984004779A1

公开(公告)日：1984-12-06

申请号：PCT/US1984000754

申请日：1984-05-17

Applicant: PAUL, Marius, A.

IPC: F01B29/04

CPC classification number: F02B47/02 ,  F01B29/04 ,  F02B3/06 ,  F02B69/06 ,  F02B75/02 ,  F02B2075/025 ,  F02B2075/027 ,  Y02T10/121

Abstract: 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.

Abstract translation: 一种内燃机，其与兰金型的热循环相结合，其中水被加热到蒸汽并与燃料一起喷射到发动机中以增加发动机输出。 可以通过接收来自发动机的排气并将进气压缩到发动机的涡轮压缩机（16）来提供增加的功率。 可以设置另外的燃料燃烧器（22）以驱动涡轮以提供更进一步的增加和立即的功率。 发动机可以作为二冲程或四冲程发动机运行。 当与将选择性地将单个阀与空气入口或出口连通的旋转阀（8）结合使用时，单个阀（7）可用于将发动机气缸与进气和排气连通。 具有预燃室（35）的两循环发动机具有接收用于提供增加的性能的活塞轮廓（38）的开口。

公开(公告)号：WO2006001927A3

公开(公告)日：2006-01-05

申请号：PCT/US2005/016881

申请日：2005-05-14

Applicant: PAUL, Marius, A.

Inventor： PAUL, Marius, A.

IPC: F02K9/42

Abstract: Carnot cycle aircraft engines having a housing having a main air intake and a common discharge nozzle, a central rotor shaft with a central compressor unit supported by struts in the main air intake wherein the compressor unit has a fan unit with hollow fan blades and an air intake to the hollow fan blades and an annular ducted combustion chamber in the housing wherein air compressed in the hollow fan blades is ejected into the combustion chamber wherein the combustion chamber includes a cascade combustor with a series of fuel injectors for isothermal combustion with combustion gases discharged in an annular expansion nozzle with a variable geometry control before being discharged into the common discharge nozzle with air that bypasses the compressor unit and flows between the fan blades to the common discharge nozzle.

公开(公告)号：WO1993023667A1

公开(公告)日：1993-11-25

申请号：PCT/US1993004738

申请日：1993-05-17

Applicant: PAUL, Marius, A. ,  PAUL, Ana

IPC: F02M41/00

CPC classification number: F02M63/0017 ,  F02B2075/025 ,  F02M45/08 ,  F02M47/027 ,  F02M59/105 ,  F02M59/243 ,  F02M59/46 ,  F02M61/162 ,  F02M61/1806 ,  F02M63/0007 ,  F02M63/004 ,  F02M63/0047 ,  F02M63/0049 ,  F02M63/0225

Abstract: A high pressure fuel injector system including a high pressure fuel pump (16) useable with a pressure booster, a pressure stabilizer with a high speed tandem actuated distributor and a fuel having a fuel injector (12) with high pressure fuel admission passages and low pressure fuel return passages with a needle valve (32) hydraulically operated by high pressure fuel from the high pressure fuel admission passage by a distributor valve (50) which selectively directs a hydraulic fuel pressure against one side or the other of a piston body (35) forming part of the needle valve whereby the needle valve is urged to a position closing discharge orifices or a position opening discharge orifices, the distributor valve (50) being controlled by an electronic actuator (20) wherein the injector system is designed with unique floating valve pistons in the components, the components being useable separately or together in the integrated systems preferred for high pressure, high speed operation.

Abstract translation: 一种高压燃料喷射器系统，包括可用于增压器的高压燃料泵（16），具有高速串联致动分配器的压力稳定器和具有燃料喷射器（12）的燃料，所述燃料喷射器具有高压燃料入口通道和低压 具有针阀（32）的燃料返回通道，所述针阀（32）通过分配器阀（50）由来自高压燃料进入通道的高压燃料液压操作，分配器阀（50）选择性地引导液压燃料压力抵靠活塞体（35）的一侧或另一侧， 形成针阀的一部分，由此针阀被推动到关闭排出孔或位置打开排出孔的位置，分配阀（50）由电子致动器（20）控制，其中喷射器系统设计有独特的浮阀 组件中的活塞，组件可以单独使用或一起用于高压，高速操作优选的集成系统中。