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1.发明申请Multiple detonation initiator for frequency multiplied pulsed detonation combustion 有权多重爆震引发器用于频率相加脉冲爆震燃烧公开(公告)号：US20050279078A1
公开(公告)日：2005-12-22
申请号：US10870898
申请日：2004-06-18
申请人： Anthony Dean , Keith McManus , Venkat Tangirala
发明人： Anthony Dean , Keith McManus , Venkat Tangirala
摘要： The present invention is a pulse detonation combustion system, having a plurality of detonation initiation devices coupled to a main combustion chamber, where each of the detonation initiation devices is operating out-of-phase with each other. Each of the detonation initiation devices assists in the initiation of a detonation in the main combustion chamber, out-of-phase from each other such that the operational frequency of the pulse detonation combustion system is related to the number of detonation initiation devices multiplied by the operational frequency of a single detonation initiation device.
摘要翻译： 本发明是一种脉冲爆震燃烧系统，其具有耦合到主燃烧室的多个爆震启动装置，其中每个爆震启动装置彼此不同相运行。 每个爆震启动装置有助于在主燃烧室中引起爆震，彼此不相位，使得脉冲爆震燃烧系统的操作频率与爆震开始装置的数量相乘 单个引爆装置的工作频率。
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公开(公告)号：US20050279083A1
公开(公告)日：2005-12-22
申请号：US10870877
申请日：2004-06-18
申请人： Keith McManus , Anthony Dean , Venkat Tangirala
发明人： Keith McManus , Anthony Dean , Venkat Tangirala
IPC分类号： F02K7/02
CPC分类号： F02K7/04 , F23C15/00 , F23L7/007 , F23R7/00 , Y02E20/344
摘要： In the present invention, at least one detonation initiator is positioned downstream of a main combustion chamber, with the initiator oriented such that it projects a detonation initiation wave forward into the main combustion chamber. The main combustion chamber contains a wave reflection surface. The detonation initiation wave is directed into the main combustion chamber and at the wave reflector surface and is used to initiate, or assist in the initiation of, a fuel and gas mixture in the main combustion chamber. The fuel and gas mixture is detonated, creating a high temperature and high pressure wave that is directed out of the main combustion chamber.
摘要翻译： 在本发明中，至少一个引爆引发剂位于主燃烧室的下游，其中起爆器被定向为使得爆炸起始波向前推入主燃烧室。 主燃烧室包含波反射面。 引爆起始波被引导到主燃烧室和波浪反射器表面，并用于启动或协助起动主燃烧室中的燃料和气体混合物。 燃料和气体混合物被引爆，产生高温和高压波，该高压和高压波被引导出主燃烧室。
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公开(公告)号：US20070144179A1
公开(公告)日：2007-06-28
申请号：US11315407
申请日：2005-12-22
申请人： Pierre Pinard , Venkat Tangirala , Adam Rasheed , Anthony Dean , Ronald Bunker , David Chapin
发明人： Pierre Pinard , Venkat Tangirala , Adam Rasheed , Anthony Dean , Ronald Bunker , David Chapin
IPC分类号： F23R7/00
CPC分类号： F23R7/00
摘要： A detonation chamber for a pulse detonation combustor including: a plurality of dimples disposed on at least a portion of an inner surface of the detonation chamber wherein the plurality of dimples enhance a turbulence of a fluid flow through the detonation chamber
摘要翻译： 一种用于脉冲爆震燃烧器的爆轰室，包括：多个凹坑，其设置在所述爆炸室的内表面的至少一部分上，其中所述多个凹坑增强了通过所述爆轰室的流体流动的紊流
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4.发明申请公开(公告)号：US20070137172A1
公开(公告)日：2007-06-21
申请号：US11304889
申请日：2005-12-16
申请人： Adam Rasheed , Anthony Dean , Venkat Tangirala , David Chapin
发明人： Adam Rasheed , Anthony Dean , Venkat Tangirala , David Chapin
IPC分类号： F02C5/00
摘要： A pulse detonation combustor is provided with a fuel-air mixer located upstream from a detonation chamber. A fuel-air mixture exits the fuel-air mixer and enters the detonation chamber, where it is ignited by an ignition source. The flow from the fuel-air mixer passes over the surface of a center body, which extends downstream from the fuel-air mixer. The surface of the center body contains at least one turbulence generator, which imparts additional turbulence in the fuel-air mixture passing through the chamber. The turbulence generator aids in the mixing of the fuel and air of the fuel-air mixture to enhance the deflagration to detonation transition within the pulse detonation combustor.
摘要翻译： 脉冲爆震燃烧器设置有位于爆炸室上游的燃料 - 空气混合器。 燃料 - 空气混合物离开燃料空气混合器并进入爆燃室，在那里它被点火源点燃。 来自燃料空气混合器的流动通过在燃料 - 空气混合器下游延伸的中心体的表面。 中心体的表面包含至少一个湍流发生器，其在通过腔室的燃料 - 空气混合物中施加额外的湍流。 湍流发生器有助于燃料 - 空气混合物的燃料和空气的混合，以增强脉冲爆震燃烧器内爆燃转化的爆燃。
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5.发明申请公开(公告)号：US20070137171A1
公开(公告)日：2007-06-21
申请号：US11304411
申请日：2005-12-15
IPC分类号： F02C5/00
摘要： A swirler having cross-sectional area comparable to the area of a detonation chamber is placed upstream of the detonation chamber to enhance the fuel-air mixing. The swirler has a first region and a second region, each of which induces swirl in the flow through the swirler. Each region induces a different direction of swirl in the flow. The residual net swirl present in the flow downstream of the swirler is controlled by the relative properties of each region of the swirler. The swirler also provides high optical blockage to inhibit the upstream propagation of flow due to the detonation shockwave.
摘要翻译： 具有与爆震室的面积相当的横截面面积的旋流器设置在爆震室的上游，以增强燃料 - 空气混合。 旋流器具有第一区域和第二区域，每个区域在流过旋流器的流中引起漩涡。 每个区域在流动中引起不同的旋流方向。 旋流器下游的流动中存在的残余净涡流由旋流器的每个区域的相对特性控制。 旋流器还提供高的光学阻塞，以抑制由于爆震冲击波引起的上游流动传播。
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公开(公告)号：US20070180810A1
公开(公告)日：2007-08-09
申请号：US11346809
申请日：2006-02-03
申请人： David Chapin , Kevin Hinckley , Venkat Tangirala , Anthony Dean
发明人： David Chapin , Kevin Hinckley , Venkat Tangirala , Anthony Dean
IPC分类号： F02C5/00
摘要： A pulsed detonation combustor (PDC) is described. The PDC includes an outer casing defining a first hollow chamber configured to receive a flow and an inner liner. The inner liner includes at least one portion positioned within the first hollow chamber and configured to receive the flow from a plenum formed between the outer casing and inner liner. The PDC further includes a flow turning device with geometric features configured to direct the flow from the plenum to a second hollow chamber defined within the inner liner. The PDC also includes at least one fuel injection port located downstream of an inlet to the outer casing and an ignition device located downstream of the at least one fuel injection port and configured to periodically ignite fuel.
摘要翻译： 描述了脉冲爆震燃烧器（PDC）。 PDC包括限定被配置为接收流动和内衬的第一中空室的外壳。 内衬层包括位于第一中空室内的至少一个部分，并且构造成接收来自形成在外壳和内衬之间的气室的流。 PDC还包括流动转动装置，其具有几何特征，其被配置为将来自气室的流引导到限定在内衬内的第二中空室。 PDC还包括位于外壳入口下游的至少一个燃料喷射口和位于该至少一个燃料喷射口下游并被配置为周期性点燃燃料的点火装置。
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公开(公告)号：US20060260291A1
公开(公告)日：2006-11-23
申请号：US11135195
申请日：2005-05-20
申请人： Christian Vandervort , Adam Rasheed , Anthony Dean , Venkat Tangirala , Pierre Pinard , James Wiedenhoefer
发明人： Christian Vandervort , Adam Rasheed , Anthony Dean , Venkat Tangirala , Pierre Pinard , James Wiedenhoefer
IPC分类号： F02C5/00
CPC分类号： F02C5/00 , F02K7/02 , F02K7/06 , F05D2260/202 , F23C15/00 , F23R7/00 , Y02T50/675
摘要： A pulse detonation (PD) assembly includes at least one PD chamber having a wall, which defines cooling holes arranged along at least a portion of the PD chamber. A manifold extends around the PD chamber. The manifold and PD chamber are separated by a bypass region. A PD assembly with reverse flow cooling includes at least one PD chamber. A sleeve extends around the PD chamber. The sleeve and PD chamber are separated by a reverse flow cooling passage configured to receive a flow of air and to flow the air in a reverse direction to supply the PD chamber. A PD assembly with bypass flow cooling includes at least one PD chamber and a manifold extending around the PD chamber(s), which are separated by a bypass region. The PD assembly further includes a mixing plenum configured to receive and mix the bypass flow from the bypass region and the detonation by-products from the PD chamber(s).
摘要翻译： 脉冲爆震（PD）组件包括具有壁的至少一个PD室，其限定沿着PD室的至少一部分布置的冷却孔。 歧管围绕PD室延伸。 歧管和PD室由旁路区域分开。 具有逆流冷却的PD组件包括至少一个PD室。 套筒围绕PD室延伸。 套筒和PD室由逆流冷却通道隔开，反流冷却通道构造成接收空气流并使空气沿相反方向流动以供应PD室。 具有旁路流冷却的PD组件包括至少一个PD室和围绕PD室延伸的歧管，其由旁路区域分开。 PD组件还包括配置为接收和混合来自旁路区域的旁路流和来自PD室的爆炸副产物的混合增压室。
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公开(公告)号：US20050120700A1
公开(公告)日：2005-06-09
申请号：US10730219
申请日：2003-12-08
申请人： Venkat Tangirala , Anthony Dean , Ivett Leyva
发明人： Venkat Tangirala , Anthony Dean , Ivett Leyva
摘要： A two-stage pulse detonation system includes a pre-combustor and a geometric resonator connected via a converging-diverging nozzle to the pre-combustor to create a high temperature and high pressure conditions in the resonator in order to create optimal conditions for detonation initiation. A mixture of a fuel and a gas is burned in the pre-combustor and is passed through the nozzle into the geometric resonator, where the burned mixture is detonated. The detonation propagates through the resonator exit nozzle thus generating thrust.
摘要翻译： 两级脉冲爆震系统包括预燃烧器和通过会聚发散喷嘴连接到预燃烧器的几何谐振器，以在谐振器中产生高温和高压条件，以便产生爆炸开始的最佳条件。 燃料和气体的混合物在预燃烧器中燃烧并且通过喷嘴进入几何谐振器，其中燃烧的混合物被引爆。 爆震通过谐振器出口喷嘴传播，从而产生推力。
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9.发明申请COMPACT, LOW PRESSURE-DROP SHOCK-DRIVEN COMBUSTOR AND ROCKET BOOSTER, PULSE DETONATION BASED SUPERSONIC PROPULSION SYSTEM EMPLOYING THE SAME 有权紧凑型，低压降驱动式燃烧器和摇臂增压器，采用脉冲爆震的超声波推进系统公开(公告)号：US20070180815A1
公开(公告)日：2007-08-09
申请号：US11554897
申请日：2006-10-31
申请人： Venkat Tangirala , Jonathan Janssen , Anthony Dean
发明人： Venkat Tangirala , Jonathan Janssen , Anthony Dean
IPC分类号： F02K7/02
CPC分类号： F02K7/02
摘要： A supersonic propulsion system is provided. The supersonic propulsion system includes a plurality of systems for efficiently creating cyclic detonations and at least one rocket booster device. Each of the systems include at least a first initiator chamber configured to generate an initial wave, at least one main chamber coupled to the first initiator chamber. The main chamber is configured to generate a main wave and to output products of supersonic combustion. The products are generated within the main chamber. The main chamber is configured to enable the main wave to travel upstream and downstream within the main chamber when the first initiator chamber is located outside the main chamber. The system further includes an initial connection section located between the first initiator chamber and the main chamber that enhances a combustion process via shock focusing and shock reflection.
摘要翻译： 提供超音速推进系统。 超音速推进系统包括用于有效地产生循环爆炸的多个系统和至少一个火箭增压装置。 每个系统包括至少一个配置成产生初始波的第一启动器室，耦合到第一起动器室的至少一个主室。 主室被配置为产生主波并输出超音速燃烧的产物。 产品在主室内产生。 主室被构造成使得当第一起动器室位于主室外部时，能够使主波浪在主室内的上游和下游行进。 该系统还包括位于第一起动器室和主室之间的初始连接部分，其通过冲击聚焦和冲击反射增强燃烧过程。
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10.发明申请公开(公告)号：US20070157622A1
公开(公告)日：2007-07-12
申请号：US11328394
申请日：2006-01-09
IPC分类号： F23R7/00
CPC分类号： F23R7/00
摘要： A turbine disk assembly including a rotatable cylindrical member rotatably coupled to a shaft and a plurality of turbine blades extend circumferentially outward from said cylindrical member. The turbine blades include at least two different geometrical shapes, a first of the geometrical shapes is configured to facilitate extracting power from a first pulsed detonation combustor product stream. A second of said geometrical shapes is configured to facilitate extracting power from a second pulsed detonation combustor product stream that is different from the first pulsed detonation combustor product stream.
摘要翻译： 包括可旋转地联接到轴的可旋转圆柱形构件和多个涡轮机叶片的涡轮盘组件从所述圆柱形构件周向向外延伸。 涡轮机叶片包括至少两个不同的几何形状，第一几何形状被配置为便于从第一脉冲爆炸燃烧器产物流提取动力。 所述几何形状中的第二个被配置为便于从与第一脉冲爆炸燃烧器产物流不同的第二脉冲爆炸燃烧器产物流提取功率。
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