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    THRUST MODULATION IN A MULTIPLE COMBUSTOR PULSE DETONATION ENGINE USING CROSS-COMBUSTOR DETONATION INITIATION
    3.
    发明申请
    THRUST MODULATION IN A MULTIPLE COMBUSTOR PULSE DETONATION ENGINE USING CROSS-COMBUSTOR DETONATION INITIATION 审中-公开
    使用跨燃烧器爆震启动在多个燃烧器脉冲爆震发动机中进行调速

    公开(公告)号：US20110126511A1

    公开(公告)日：2011-06-02

    申请号：US12627763

    申请日：2009-11-30

    申请人： Aaron Jerome Glaser ,  Adam Rasheed ,  Douglas Carl Hofer ,  Narendra Digamber Joshi

    发明人： Aaron Jerome Glaser ,  Adam Rasheed ,  Douglas Carl Hofer ,  Narendra Digamber Joshi

    IPC分类号： F02K5/02 ,  F02C9/00

    CPC分类号： F02C5/00 ,  F05D2270/051

    摘要： A method and apparatus for modulating the thrust during a flight envelope of a multiple combustor chamber detonation engine using cross-combustor chamber detonation initiation are provided. The detonation combustor chambers are filled with a combustible mixture of fuel and oxidizer. The combustible mixture in one of the detonation combustor chambers is ignited by an ignition source, and the remaining detonation combustor chambers are ignited by detonation cross-firing via connectors. A controller controls the ignition source and the supply of oxidizer and fuel to the detonation combustor chambers to modulate the thrust of the engine during the flight envelope.

    摘要翻译： 提供了一种使用交叉燃烧器室爆震启动来调节多燃烧室室爆震发动机的飞行包络内的推力的方法和装置。 爆炸燃烧室中充满燃料和氧化剂的可燃混合物。 其中一个引爆燃烧室中的可燃混合物被点火源点燃，剩余的爆炸燃烧室通过连接器的爆炸交叉点燃。 控制器控制点火源，并将氧化剂和燃料供应到爆炸燃烧器室，以在飞行包络内调节发动机的推力。

    Side-initiated augmentor for engine applications
    7.
    发明授权
    Side-initiated augmentor for engine applications 有权
    发动机应用的侧面起动增压器

    公开(公告)号：US08991189B2

    公开(公告)日：2015-03-31

    申请号：US12914776

    申请日：2010-10-28

    申请人： Narendra Digamber Joshi ,  Adam Rasheed ,  Matthew Patrick Boespflug ,  Seyed Gholamali Saddoughi

    发明人： Narendra Digamber Joshi ,  Adam Rasheed ,  Matthew Patrick Boespflug ,  Seyed Gholamali Saddoughi

    IPC分类号： F02K3/10 ,  F23R3/20

    CPC分类号： F02K3/10 ,  F23R3/20

    摘要： A gas turbine engine augmentor includes at least one fluid based augmentor initiator defining a chamber in flow communication with a source of air and a source of fuel. The chamber includes a plurality of ejection openings in flow communication with an exhaust flowpath. The at least one fluid based augmentor initiator is devoid of any exhaust flowpath protrusions thereby minimizing any pressure drops and loss of thrust during dry work phase of operation. The source of fuel is operable for injecting fuel into the chamber such that at least a portion of the fuel flow is ignited at the plurality of ejection openings to produce a plurality of fuel-rich hot jets radially into the exhaust flowpath.

    摘要翻译： 燃气涡轮发动机增压器包括至少一个基于流体的增压器起动器，其限定与空气源和燃料源流动连通的室。 该腔室包括与排气流路流动连通的多个喷射口。 所述至少一个基于流体的增压器引发器没有任何排气流路突起，从而使在操作的干燥工作阶段期间的任何压力下降和推力损失最小化。 燃料源可操作以将燃料喷射到室中，使得燃料流的至少一部分在多个喷射口处被点燃以产生多个富燃料的热喷射流体径向地进入排气流路。

    Rotating valve assembly for high temperature and high pressure operation
    8.
    发明授权
    Rotating valve assembly for high temperature and high pressure operation 有权
    旋转阀组件，用于高温高压运行

    公开(公告)号：US08661782B2

    公开(公告)日：2014-03-04

    申请号：US12627640

    申请日：2009-11-30

    申请人： Ross Hartley Kenyon ,  Narendra Digamber Joshi ,  Adam Rasheed ,  Mark Joseph Pombles

    发明人： Ross Hartley Kenyon ,  Narendra Digamber Joshi ,  Adam Rasheed ,  Mark Joseph Pombles

    IPC分类号： F02C5/02 ,  F02C5/10

    CPC分类号： F02K7/06 ,  F02C5/10

    摘要： A rotating valve assembly includes an inner cup having at least one inlet port; an outer cup having at least one inlet port, the outer cup rotatably mounted concentric with the inner cup by a bearing arrangement; and a cooling system located between the inner cup and the bearing arrangement for providing a thermal barrier between the inner cup and the bearing arrangement. The valve assembly also includes a labyrinth sealing arrangement located around the at least one inlet port of one of the inner and outer cups for preventing leakage of pressure waves generated by detonations or quasi-detonations within a combustion chamber of the inner cup.

    摘要翻译： 旋转阀组件包括具有至少一个入口的内杯; 具有至少一个入口的外杯，所述外杯通过轴承装置与所述内杯同心地安装; 以及位于内杯和轴承装置之间的冷却系统，用于在内杯和轴承装置之间提供热障。 阀组件还包括迷宫式密封装置，其位于内杯和外杯之一的至少一个入口周围，用于防止在内杯的燃烧室内的爆炸或准爆炸产生的压力波的泄漏。

    FLUIDIC DEFLAGRATION-TO-DETONATION INITIATION OBSTACLES
    10.
    发明申请
    FLUIDIC DEFLAGRATION-TO-DETONATION INITIATION OBSTACLES 有权
    流体定向到爆炸启动障碍物

    公开(公告)号：US20120144798A1

    公开(公告)日：2012-06-14

    申请号：US12964968

    申请日：2010-12-10

    申请人： Justin Thomas Brumberg ,  Adam Rasheed

    发明人： Justin Thomas Brumberg ,  Adam Rasheed

    IPC分类号： F02K7/02

    CPC分类号： F02K7/02 ,  F02C5/11

    摘要： A detonation chamber and a pulse detonation combustor including a detonation chamber, wherein the detonation chamber includes a plurality of aerodynamic jets disposed adjacent an exterior of a sidewall of the detonation chamber. The detonation chamber further includes a plurality of openings formed in the sidewall of the detonation chamber, wherein each of the plurality of openings is in fluidic communication with one of the plurality of aerodynamic jets. The plurality of aerodynamic jets are adapted to create a plurality of jet flows of a fluid within the detonation chamber during a combustion cycle defining a plurality of initiation obstacles within the detonation chamber to enhance a turbulence of a fluid flow and flame acceleration through the detonation chamber.

    摘要翻译： 一个引爆室和一个包括爆震室的脉冲爆炸燃烧室，其中爆炸室包括邻近爆炸室侧壁外部设置的多个空气动力射流。 引爆室还包括形成在爆炸室的侧壁中的多个开口，其中多个开口中的每一个开口与多个空气动力学射流中的一个流体连通。 多个空气动力学射流适于在燃烧循环期间在引爆室内产生流体的多个喷射流，该循环在爆震室内限定多个起始障碍物，以增强流体流动的紊流和通过爆轰室的火焰加速 。