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公开(公告)号:US09920689B2
公开(公告)日:2018-03-20
申请号:US14211140
申请日:2014-03-14
Inventor: M. Razi Nalim
CPC classification number: F02C5/11 , F02C3/02 , F02C3/16 , F02C5/04 , Y02T50/671 , Y10S903/93
Abstract: A hybrid propulsion system includes a wave rotor combustion engine operating in parallel with an electrical motor-generator element. The motor-generator element is coupled to the turbine shaft to selectively drive or be driven by the turbine shaft. In one mode of operation, the motor of the motor generator element is powered by a battery to provide rotational energy to the turbine shaft. In another mode of operation, the wave rotor combustion engine drives the generator to recharge the battery. The wave rotor combustion engine may be further directly coupled to auxiliary components without a gearbox to drive the components at substantially the same speed as the turbine shaft. The turbine rotor of the combustion engine includes a plurality of chambers defined by circumferentially spaced curved vanes that improves specific fuel consumption for the engine.
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公开(公告)号:US09856791B2
公开(公告)日:2018-01-02
申请号:US13969900
申请日:2013-08-19
Inventor: Norbert Müller , Janusz Piechna , Guangwei Sun , Pablo-Francisco Parraga
CPC classification number: F02C3/14 , F01D1/32 , F02C3/165 , F02C5/04 , F02C5/10 , F02K7/04 , F05D2240/302 , F05D2250/82 , Y02T50/673
Abstract: A wave disc engine apparatus is provided. A further aspect employs a constricted nozzle in a wave rotor channel. A further aspect provides a sharp bend between an inlet and an outlet in a fluid pathway of a wave rotor, with the bend being spaced away from a peripheral edge of the wave rotor. A radial wave rotor for generating electricity in an automotive vehicle is disclosed in yet another aspect.
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公开(公告)号:US09212626B2
公开(公告)日:2015-12-15
申请号:US14300043
申请日:2014-06-09
Applicant: Derrick T. Miller, Jr.
Inventor: Derrick T. Miller, Jr.
CPC classification number: F02K9/95 , F02C3/14 , F02C3/165 , F02C5/02 , F02C5/04 , F02C5/12 , F02K9/00 , F05D2220/32 , F41A19/13 , H02K7/1823
Abstract: An engine propulsion system is configured to utilize bursts of pressurized media in order to transmit mechanical energy. The engine propulsion system includes at least one cannon, wherein each cannon is configured to displace the pressurized media and further includes a casing configured to accommodate a rotational firing pin. The rotational firing pin is configured to transmit the mechanical energy.
Abstract translation: 发动机推进系统被配置为利用爆破的加压介质来传递机械能。 发动机推进系统包括至少一个炮,其中每个炮构造成移动加压介质,并且还包括构造成容纳旋转击发销的壳体。 旋转击打销构造成传递机械能。
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公开(公告)号:US20130327010A1
公开(公告)日:2013-12-12
申请号:US13969900
申请日:2013-08-19
Inventor: Norbert Müller , Janusz Piechna , Guangwei Sun , Pablo-Francisco Parraga
IPC: F02C3/14
CPC classification number: F02C3/14 , F01D1/32 , F02C3/165 , F02C5/04 , F02C5/10 , F02K7/04 , F05D2240/302 , F05D2250/82 , Y02T50/673
Abstract: A wave disc engine apparatus is provided. A further aspect employs a constricted nozzle in a wave rotor channel. A further aspect provides a sharp bend between an inlet and an outlet in a fluid pathway of a wave rotor, with the bend being spaced away from a peripheral edge of the wave rotor. A radial wave rotor for generating electricity in an automotive vehicle is disclosed in yet another aspect.
Abstract translation: 提供了一种波盘发动机装置。 另一方面在波转子通道中使用收缩的喷嘴。 另一方面提供在波形转子的流体路径中的入口和出口之间的尖锐弯曲,其中弯曲部与波浪转子的周边边缘间隔开。 在另一方面,公开了一种用于在机动车辆中发电的径向波转子。
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公开(公告)号:US08443583B2
公开(公告)日:2013-05-21
申请号:US12304923
申请日:2007-06-14
Applicant: Razi Nalim , Pezhman Akbari
Inventor: Razi Nalim , Pezhman Akbari
IPC: F02C3/02
Abstract: Apparatus and methods for combustion of fuel. Some embodiments of the inventions include a fuel nozzle which injects fuel into a combustion channel of a wave rotor combustor or a pulse detonation combustor In some embodiments the combustion process includes a backward-propagating detonation wave within a substantially closed channel which compresses discrete quantities of combustible and noncombustible mixture. Yet other embodiments include a precombustion chamber integrated into the wave rotor, the outlet stator or both.
Abstract translation: 用于燃料燃烧的装置和方法。 本发明的一些实施例包括将燃料喷射到波浪转子燃烧器或脉冲爆震燃烧器的燃烧通道中的燃料喷嘴。在一些实施例中,燃烧过程包括在基本封闭的通道内的向后传播的爆震波,其压缩离散量的可燃 和不燃混合物。 其他实施例包括集成到波形转子,出口定子或两者中的预燃室。
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公开(公告)号:US08438834B2
公开(公告)日:2013-05-14
申请号:US12414281
申请日:2009-03-30
Applicant: Daniel P. Guinan , Christopher D. Gettinger
Inventor: Daniel P. Guinan , Christopher D. Gettinger
Abstract: A helical cross flow pulse detonation engine.
Abstract translation: 螺旋交叉流脉冲爆震引擎。
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公开(公告)号:US20100263622A1
公开(公告)日:2010-10-21
申请号:US12827121
申请日:2010-06-30
Applicant: JUNG-KUANG CHOU
Inventor: JUNG-KUANG CHOU
IPC: F02B53/00
CPC classification number: F01D1/34 , F02B53/00 , F02C5/02 , F02C5/04 , Y02T50/671
Abstract: A rotary engine includes one or more combustion chambers around a turbine, and a movable plate at an opening of the combustion chamber and rotated 90 degrees and protruded from the turbine. Both sides of the movable plate and the diameter of the turbine form an align straight line. The turbine comprises a slide member, a U-shape groove, a ditch with an open end coupled to the movable plate to form the explosion chamber. During explosion, the movable plate drives the turbine to rotate while eliminating the waste gases. The air current and pressure of the explosion apply forces to rotate the bottom of the combustion chamber. The volume of the explosion chamber can be extended to provide a relatively large open space since the movable plate can be moved and a higher pressure gases will be reduced rapidly so that the high-pressure gases can produce a greater force.
Abstract translation: 旋转发动机包括围绕涡轮机的一个或多个燃烧室,以及位于燃烧室的开口处并且旋转90度并从涡轮机突出的可动板。 可移动板的两侧和涡轮的直径形成对准的直线。 涡轮机包括滑动构件,U形槽,具有与可动板联接以形成爆炸室的开口端的沟槽。 在爆炸期间,可移动板驱动涡轮机旋转,同时消除废气。 爆炸的气流和压力施加力以使燃烧室的底部旋转。 爆炸室的体积可以延伸以提供相对大的开放空间,因为可移动板可以移动并且较高压力的气体将被快速地减小,使得高压气体可以产生更大的力。
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公开(公告)号:US20090126681A1
公开(公告)日:2009-05-21
申请号:US11997299
申请日:2005-07-29
Applicant: Thomas Cobb
Inventor: Thomas Cobb
IPC: F02B53/04
CPC classification number: F02C5/04 , Y02T50/671
Abstract: The present invention provides an improved rotary internal combustion engine having: a housing structure (19) with an internal stationary cavity, an intake air aperture (23), an exhaust aperture (30), an ignition aperture (21) and a fuel aperture (22) located on the surface of the stationary cavity, a rotational body (15) which contains combustion chambers (17, 18) that form internal cavities within the rotational body.
Abstract translation: 本发明提供一种改进的旋转内燃机,其具有:具有内部固定腔的壳体结构(19),进气孔(23),排气孔(30),点火开孔(21)和燃料孔 22),其位于所述静止空腔的表面上,所述旋转体(15)包含在所述旋转体内形成内部空腔的燃烧室(17,18)。
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公开(公告)号:US20080155957A1
公开(公告)日:2008-07-03
申请号:US11648747
申请日:2007-01-03
Applicant: Hugh Joseph Gallagher
Inventor: Hugh Joseph Gallagher
IPC: F02C3/00
CPC classification number: F02C5/04 , F02C3/165 , F05D2230/211 , F05D2230/52 , F05D2240/35 , F05D2250/15 , F05D2250/82 , F05D2300/211
Abstract: A three or any number of sided combustion chamber with a central entrance hole through which enters air-fuel which is expoded and is exhausted through periferal exhaust ports. It causes rotation of the combustion chamber between 1,000 and 100,000 rpm. It runs a generator which can run any electrical part. The combustion chamber rotates and therefore it is the important part of the machine.
Abstract translation: 三个或任何数量的具有中心入口孔的侧面燃烧室,通过该中心入口进入空气燃料,其被排出并通过周边排气口排出。 它使燃烧室的旋转速度在1,000和100,000rpm之间。 它运行一个可以运行任何电气部件的发电机。 燃烧室旋转,因此是机器的重要部分。
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公开(公告)号:US20060213201A1
公开(公告)日:2006-09-28
申请号:US11090754
申请日:2005-03-24
Applicant: Kirk Lupkes , Gary Lidstone , Mark Parish
Inventor: Kirk Lupkes , Gary Lidstone , Mark Parish
IPC: F02C5/00
CPC classification number: F23R7/00 , F02C3/16 , F02C3/165 , F02C5/02 , F02C5/04 , F02C5/12 , F02K3/075 , F02K7/02 , F02K7/04 , F02K7/06 , F02K7/075 , F02K7/08 , F23C15/00
Abstract: A pulse combustion device has a number of combustors with upstream bodies and downstream nozzles. Coupling conduits provide communication between the combustors. For each given combustor this includes a first communication between a first location upstream of the nozzle thereof and a first location along the nozzle of another. There is second communication between a second location upstream of the nozzle and a second communication between a second location upstream of the nozzle of a second other combustor and a second nozzle location along the nozzle of the given combustor.
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