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21. 发明授权

US2627161A Elastic fluid power system utilizing a rotary engine with cooled rotors 失效
标题翻译：使用具有冷却转子的旋转发动机的弹性流体动力系统
公开(公告)号：US2627161A
公开(公告)日：1953-02-03
申请号：US28916152
申请日：1952-05-21
申请人： JARVIS C MARBLE , LESLIE M MERRILL , PERCY H BATTEN
发明人： IMMANUEL LINDHAGEN TEODOR , ROBERT NILSSON HANS
IPC分类号： F01B17/00 , F01B17/02 , F01C1/16 , F01C11/00 , F01C21/06 , F01D5/08 , F02B53/00 , F02C3/055 , F02C7/08
CPC分类号： F01B17/00 , F01B17/02 , F01C1/16 , F01C11/004 , F01C21/06 , F01D5/08 , F02B53/00 , F02C3/055 , F02C7/08 , Y02T50/671 , Y02T50/676

22. 发明授权

US2449022A Fuel system for aircraft power plants for aircraft propulsion and boundary layer aircontrol 失效
标题翻译：用于飞机推进和边界层空调的飞机发电厂的燃料系统
公开(公告)号：US2449022A
公开(公告)日：1948-09-07
申请号：US58239445
申请日：1945-03-12
申请人： STALKER EDWARD A
发明人： STALKER EDWARD A
IPC分类号： B64C21/06 , F02C3/055
CPC分类号： B64C21/06 , B64C2230/04 , B64C2230/06 , F02C3/055 , Y02T50/166 , Y02T50/671

23. 发明授权

US2385366A Power plant for aircraft 失效
标题翻译：飞机发电厂
公开(公告)号：US2385366A
公开(公告)日：1945-09-25
申请号：US26854039
申请日：1939-04-18
申请人： JARVIS C MARBLE , LESLIE M MERRILL , PERCY H BATTEN
发明人： ALF LYSHOLM
IPC分类号： F02C3/055
CPC分类号： F02C3/055

24. 发明授权

US2195025A Gas turbine 失效
公开(公告)号：US2195025A
公开(公告)日：1940-03-26
申请号：US8957136
申请日：1936-07-08
申请人： ARTHUR COUZINET RENE ALEXANDRE
发明人： ARTHUR COUZINET RENE ALEXANDRE
IPC分类号： F02C3/055
CPC分类号： F02C3/055

25. 发明授权

US11802507B2 Dual-pressure jet engine and device for work done by compressed air thereof 有权
公开(公告)号：US11802507B2
公开(公告)日：2023-10-31
申请号：US18066167
申请日：2022-12-14
申请人： Yunfeng Li
发明人： Yunfeng Li
IPC分类号： F02C3/055 , F02C7/22
CPC分类号： F02C3/055 , F02C7/22 , F05D2220/323
摘要： A device for work done by compressed air and a dual-pressure jet engine thereof are provided, a first compressed air storage chamber for cooperating with the air intake compressor is arranged between the air intake compressor and the screw gas compressor so as to pressurize the air. The first compressed air storage chamber is communicated with the screw gas compressor, the air intake end of the screw gas compressor is provided with the fuel injection mechanism for injecting fuel inside the screw gas compressor. The air outlet end of the screw gas compressor is provided with the second compressed air storage chamber for cooperating with the screw gas compressor so as to pressurize the air. The second compressed air storage chamber is communicated with the combustion chamber which is used to be injected with fuel.

26. 发明授权

US5771693A Gas compressor 失效
标题翻译：燃气压缩机
公开(公告)号：US5771693A
公开(公告)日：1998-06-30
申请号：US343499
申请日：1994-11-29
申请人： Michael Coney
发明人： Michael Coney
IPC分类号： F02C3/04 , F02C20060101 , F02C3/055 , F02C6/16 , F02C6/18 , F02C7/08 , F02C7/143 , F02C7/16 , F02G5/02 , F04B20060101 , F04B9/08 , F04B31/00 , F04B35/00 , F04B35/02 , F04B39/00 , F04B39/06 , F16D31/02
CPC分类号： F04B35/00 , F04B31/00 , F04B39/0011 , F04B39/06 , F04B39/062 , Y02E20/16
摘要： A gas compressor is provided comprising a chamber (9) to contain gas to be compressed, a piston (12) and the chamber (9) and an apparatus to drive the piston into the chamber (9) to compress the gas. The compressor also comprises another apparatus (5) to form a spray of liquid in the chamber (9) to cool the gas on compression therein, so that the gas may be compressed approximately isothermally. Valve (17) are provided to allow compressed gas to be drawn from the chamber. The apparatus to drive the piston (12) comprises another apparatus to deliver driving energy stored in the fluid directly to the piston. In one embodiment, the driving energy is provided by a combustible fuel. The heat of compression is rejected at the lowest temperatures and the hot exhaust gas from the combustion process may be used to preheat the isothermally compressed gas.
摘要翻译： PCT No.PCT / GB93 / 01137 Sec。 371日期：1994年11月29日 102（e）日期1994年11月29日PCT提交1993年5月28日PCT公布。出版物WO93 / 24754 日本公报1993年12月12日提供了一种气体压缩机，其包括容纳待压缩气体的腔室（9），活塞（12）和腔室（9），以及将活塞驱动进入腔室（9）加油站。压缩机还包括在腔室（9）中形成液体喷射的另一装置（5），以在其中压缩气体冷却，使得气体可以被近似等压地压缩。提供阀（17）以允许压缩气体从腔室中抽出。用于驱动活塞（12）的装置包括用于将存储在流体中的驱动能量直接传递到活塞的另一装置。在一个实施例中，驱动能量由可燃燃料提供。压缩热在最低温度被排除，来自燃烧过程的热废气可用于预热等温压缩气体。

27. 发明授权

US4873822A Energy producing installation with internal combustion engine and turbine 失效
标题翻译：内燃机和涡轮机的能源生产设备
公开(公告)号：US4873822A
公开(公告)日：1989-10-17
申请号：US171428
申请日：1988-03-04
申请人： Henry Benaroya
发明人： Henry Benaroya
IPC分类号： F02B37/00 , F02B3/06 , F02B71/00 , F02B71/04 , F02B75/02 , F02B75/04 , F02C3/00 , F02C3/055 , F02C5/08 , F02C6/00
CPC分类号： F02C3/00 , F02B71/045 , F02B75/04 , F02B2075/025 , F02B3/06
摘要： The installation comprises a compression unit and a power unit. The compression unit comprises at least one engine operation according to a Diesel cycle and supercharged by a turbine having an expansion turbine supplied with the exhaust gases of the engine and rotary compressor taking air from the atmosphere through a filter. The compressor delivers a primary supercharging flow to the Diesel cylinders via a cooler. The Diesel engine drives two compressors supplied with atmospheric air through the filter. One of the compressors provides a secondary flow to the power unit. The power unit comprises a combustion chamber which is supplied through the exchanger with part at least of the secondary airflow from the compression unit. The combustion chamber feeds a turbine producing on its shaft the whole of the output power. The Diesel type engine may be a conventional crank type engine or a free piston engine.
摘要翻译： PCT No.PCT / FR87 / 00270 Sec。 371日期：1988年3月4日 102（e）1988年3月4日PCT PCT 1987年7月8日PCT公布。公开号WO88 / 00279 日期1988年1月14日。安装包括压缩单元和动力单元。压缩单元包括根据柴油循环的至少一个发动机操作，并且由涡轮机增压，该涡轮机具有供应有发动机和旋转压缩机的废气的膨胀涡轮机，其通过过滤器从大气中吸入空气。压缩机通过冷却器向柴油机提供主要的增压流。柴油发动机通过过滤器驱动两个带有大气空气的压缩机。其中一台压缩机为动力装置提供二次流量。功率单元包括燃烧室，其通过交换器供应至少一部分来自压缩单元的二次气流。燃烧室供给在其轴上产生整个输出功率的涡轮机。柴油发动机可以是传统的曲柄发动机或自由活塞发动机。

28. 发明授权

US4504196A Rotary turboengine and supercharger 失效
标题翻译：旋转涡轮发动机和增压器
公开(公告)号：US4504196A
公开(公告)日：1985-03-12
申请号：US451496
申请日：1982-12-20
申请人： Joachim E. Lay
发明人： Joachim E. Lay
IPC分类号： F01C1/344 , F01D15/08 , F02C3/055 , F02C6/12 , F04D25/04 , F04B17/00 , F04B35/00
CPC分类号： F02C6/12 , F01C1/3441 , F01D15/08 , F02C3/055 , F04D25/045
摘要： A fluid driven turbine having a stator member and a turbine member rotatable on an axis and supporting turbine blades and with a fluid compression section is described. The fluid compression section is provided along the axis of rotation of and inside the turbine member by providing: (1) a tubular extension (13 or 102) of the stator member and (2) a rotor means (30 or 104) and at least one rotor blade means (50, 51, 52) moveable perpendicular to the axis on the turbine member which fits inside the tubular member to provide at least two adjacent first and second chambers which are defined by an inside wall of the tubular extension and the rotor means and blade means. The tubular member has a line of minimum eccentricity (12) parallel to the axis with inlet and outlet openings (15, 16) on either side of the line of minimum eccentricity to and from the chambers so that fluid is drawn into the chamber and compressed and then exits from the chambers. The turbine-compressor is useful for instance as a turbocharger, as a drive means for other apparatus and as a refrigeration compressor.
摘要翻译：描述了具有定子构件和可在轴线上旋转并支撑涡轮叶片和流体压缩部分的涡轮机构件的流体驱动涡轮机。通过提供：（1）定子构件的管状延伸部（13或102）和（2）转子装置（30或104），并且至少在所述涡轮构件的旋转轴线和涡轮机构件的内部设置流体压缩部分一个转子叶片装置（50,51,52）可垂直于涡轮机构件上的轴线移动，该转子叶片装置配合在管状构件内部，以提供至少两个相邻的第一和第二室，其由管状延伸部的内壁和转子手段和刀片手段。管状构件具有平行于轴线的最小偏心线（12），其中入口和出口开口（15,16）在离开和离开室的最小偏心线的任一侧上，使得流体被吸入腔室并压缩然后从室离开。涡轮压缩机例如可用作涡轮增压器，作为其他装置和制冷压缩机的驱动装置是有用的。

29. 发明授权

US3995431A Compound brayton-cycle engine 失效
标题翻译：复合布雷顿循环发动机
公开(公告)号：US3995431A
公开(公告)日：1976-12-07
申请号：US452168
申请日：1974-03-18
申请人： Everett H. Schwartzman
发明人： Everett H. Schwartzman
IPC分类号： F01K3/18 , F02B1/04 , F02C3/055 , F02C5/06 , F01K25/02
CPC分类号： F02C5/06 , F01K3/18 , F02C3/055 , F02B1/04
摘要： A system is disclosed incorporating a positive-displacement compressor-and-engine arrangement for converting heat of a working fluid to attain a pressure increase in a working fluid that is supplied to a turbine system. The system employs a heater interposed to pass exhaust fluid from the drive engine to the turbine system at an elevated temperature. As disclosed, the housing of the compressor-and-drive structure incorporates cooling apparatus, for example so that the reciprocating compressor may approach isothermal operation. Also, the turbine system is divided into one unit which supplies mechanical output power and another to drive a rotary compressor or supercharger, which supplies intake fluid to the positive-displacement compressor, the output of which supplies the positive-displacement engine.
摘要翻译：公开了一种系统，其结合用于转换工作流体的热量的正排量压缩机和发动机装置，以获得供应到涡轮机系统的工作流体的压力增加。该系统采用加热器，以将升高的温度下的来自驱动发动机的排出流体传递到涡轮机系统。如所公开的，压缩机和驱动结构的壳体包括冷却装置，例如使得往复式压缩机可接近等温操作。此外，涡轮机系统被分成一个单元，其提供机械输出功率，另一个单元驱动旋转式压缩机或增压器，该旋转式压缩机或增压器将进气流体供应到正排量压缩机，该排量压缩机的输出供给正排量发动机。

30. 发明授权

US2674089A Gas turbine system with displacement compressor of the multiple outer rotor type 失效
标题翻译：具有多重外转子类型的排量压缩机的燃气轮机系统
公开(公告)号：US2674089A
公开(公告)日：1954-04-06
申请号：US78273247
申请日：1947-10-29
申请人： JARVIS C MARBLE , LESLIE M MERRILL , PERCY H BATTEN
发明人： BOESTAD GUSTAV K W , ROBERT NILSSON HANS
IPC分类号： F02C3/055
CPC分类号： F02C3/055 , Y02T50/671

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