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公开(公告)号:US2548804A
公开(公告)日:1951-04-10
申请号:US58436245
申请日:1945-03-23
申请人: STEWART WARNER CORP
发明人: THELMA MCCOLLUM
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公开(公告)号:US2490623A
公开(公告)日:1949-12-06
申请号:US55712944
申请日:1944-10-04
申请人: ELSBY SAMUEL J
发明人: ELSBY SAMUEL J
CPC分类号: F02K7/005
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公开(公告)号:US2486990A
公开(公告)日:1949-11-01
申请号:US57132445
申请日:1945-01-04
发明人: SHARPE CATHERINE D
IPC分类号: F02K7/00
CPC分类号: F02K7/005
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公开(公告)号:US2481235A
公开(公告)日:1949-09-06
申请号:US67744246
申请日:1946-06-18
申请人: PARR RALPH G , PARR SAMUEL D
发明人: PARR RALPH G , PARR SAMUEL D
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公开(公告)号:US2438151A
公开(公告)日:1948-03-23
申请号:US56159044
申请日:1944-11-02
申请人: DAVIS RALPH B
发明人: DAVIS RALPH B
IPC分类号: F02K7/00
CPC分类号: F02K7/005
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86.
公开(公告)号:US20180023472A1
公开(公告)日:2018-01-25
申请号:US15641760
申请日:2017-07-05
申请人: Brent Wei-Teh LEE
发明人: Brent Wei-Teh LEE
CPC分类号: F02C3/165 , F01D1/32 , F01D5/02 , F01D13/02 , F02C5/04 , F02C7/16 , F02C7/22 , F02C7/36 , F02K7/005 , F05D2220/32 , F05D2220/76 , F05D2240/242 , F05D2240/35 , F05D2260/207 , F05D2260/40 , Y02T50/671 , Y02T50/675
摘要: An engine, a rotary device, a power generation system, and methods of manufacturing and using the same are disclosed. The engine includes a detonation and/or combustion chamber configured to detonate a fuel and rotate around a central rotary shaft extending from the detonation and/or combustion chamber, a fuel supply inlet configured to provide the fuel to the detonation and/or combustion chamber, at least two rotating arms extending radially from the detonation and/or combustion chamber and configured to exhaust detonation gases from detonating the fuel in the detonation and/or combustion chamber and provide a rotational thrust and/or force, the rotating arms having inner and outer walls and a nozzle at a distal end thereof, the nozzle being at or having an angle configured to provide the rotational thrust and/or force, and a plurality of cooling coils between the inner and outer walls. Alternatively, the rotary device may include a rotary disc.
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公开(公告)号:US09255478B2
公开(公告)日:2016-02-09
申请号:US13659492
申请日:2012-10-24
申请人: HYBRID TURBINE GROUP
发明人: Howard Purdum , William Downs , L. Vann Downs
摘要: A reaction turbine has channels formed in the top surface of a disc to create nozzles. The channels can be covered by a membrane sealed to the disc or by the housing extended from a combustor. Each channel may have a first section extending radially outwardly from an inlet of the reaction turbine and a second curved section extending from the first section to a periphery of the disc. A reaction turbine may also receive input from an impulse turbine. Fluid flows through the impulse turbine and fluid from the impulse turbine enters an inlet of the reaction turbine. The reaction turbine may have cooling channels and cooling fins to lower the temperature of the disc during operation. In addition, magnets may provide bearing support and electricity generation. In addition, the reaction turbine may have a dual shaft construction, with each shaft connected to a reaction turbine. One reaction turbine powers a compressor, while the second reaction turbine powers a load through the second shaft.
摘要翻译: 反应涡轮机具有形成在盘的顶表面中的通道,以形成喷嘴。 通道可以被密封到盘上的膜或从燃烧器延伸的壳体覆盖。 每个通道可以具有从反应涡轮机的入口径向向外延伸的第一部分和从第一部分延伸到盘的周边的第二弯曲部分。 反应涡轮机还可以接收来自脉冲涡轮机的输入。 流体流过脉冲涡轮机,并且来自脉冲涡轮机的流体进入反应涡轮机的入口。 反应涡轮机可以具有冷却通道和冷却翅片,以在操作期间降低盘的温度。 此外,磁体可以提供轴承支撑和发电。 此外,反应涡轮机可以具有双轴结构,每个轴连接到反应涡轮机。 一个反应涡轮机为压缩机供电,而第二反应涡轮机通过第二轴来驱动负载。
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公开(公告)号:US09052116B2
公开(公告)日:2015-06-09
申请号:US14466360
申请日:2014-08-22
发明人: Ernst Bergen
摘要: A toroidal combustion chamber and a plurality of plates are disposed with respect to one another such that their labyrinthine walls are juxtaposed and form labyrinthine conduits leading from an exhaust outlet of the toroidal combustion chamber to an exit perpendicular to the exhaust outlet.
摘要翻译: 环形燃烧室和多个板相对于彼此设置,使得它们的迷宫壁并置并且形成从环形燃烧室的排气出口引导到垂直于排气出口的出口的迷路管路。
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公开(公告)号:US08839599B1
公开(公告)日:2014-09-23
申请号:US14047693
申请日:2013-10-07
申请人: Juan Pedro Mesa, Jr.
发明人: Juan Pedro Mesa, Jr.
IPC分类号: F02C3/14 , F02C5/12 , F02C3/04 , F02K7/00 , F01D1/28 , F01D1/32 , F02C3/16 , F01D5/04 , F01D5/06
摘要: An axially aligned combustion engine with a rotationally fixed housing and rotationally disposed rotor is presented. Particularly, the rotor includes an engine assembly and one or more air compressor assemblies axially aligned about an axis within the housing. The engine assembly includes a plurality of radially disposed combustion chambers extending from a closed interior edge outward toward an at least partially open access port disposed at an outer peripheral edge of the engine assembly. As the engine assembly rotates within the housing, the radially disposed combustion chambers are successively aligned with or communicatively disposed with an air manifold to receive compressed air, actuator(s) to receive fuel and ignite the fuel, and an exhaust manifold to expel the combusted gases.
摘要翻译: 提出了具有旋转固定壳体和旋转地设置的转子的轴向对准的内燃机。 特别地,转子包括发动机组件和围绕壳体内的轴线轴向对齐的一个或多个空气压缩机组件。 发动机组件包括从封闭的内部边缘向外延伸到设置在发动机组件的外周边缘处的至少部分开放的进入端口的多个径向设置的燃烧室。 当发动机组件在壳体内旋转时,径向设置的燃烧室依次与空气歧管对准或通信地设置以接收压缩空气,致动器以接收燃料并点燃燃料,以及排气歧管以排出燃烧的 气体。
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公开(公告)号:US20110268581A1
公开(公告)日:2011-11-03
申请号:US12799878
申请日:2010-05-03
申请人: Thuan Huu Khong
发明人: Thuan Huu Khong
IPC分类号: F01D25/00
摘要: A rotating engine produces a torque created by exhaust products routed through angled nozzles exiting the nacelle. In one instance, a hollow drive shaft includes a plurality of fuel injector nozzles through which pressurized fuel is fed into an ignition chamber and ignited. Exiting exhaust is directed to cause the nacelle to spin. This spinning motion of the nacelle is harnessed to perform electrical or mechanical work.
摘要翻译: 旋转发动机产生由通过离开机舱的倾斜喷嘴引导的排气产物产生的扭矩。 在一种情况下,空心驱动轴包括多个燃料喷射器喷嘴,加压燃料通过该喷嘴喷嘴进入点火室并点燃。 排气排气导致机舱旋转。 机舱的这种旋转运动被利用来执行电气或机械工作。
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