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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：US07055308B2
公开(公告)日：2006-06-06
申请号：US10452422
申请日：2003-05-30
CPC分类号： F02K7/02 , F02C5/00 , F05D2260/96
摘要： An engine includes at least one pulse detonation chamber configured to receive and detonate a fuel and an oxidizer. The pulse detonation chamber has an outlet end and includes a porous liner adapted to fit within an inner surface of the pulse detonation chamber within a vicinity of the outlet end. The engine also includes a casing housing the pulse detonation chamber.
摘要翻译： 发动机包括至少一个脉冲爆震室，其配置成接收和引爆燃料和氧化剂。 脉冲爆震室具有出口端，并且包括适于装配在出口端附近的脉冲爆震室的内表面内的多孔衬里。 发动机还包括容纳脉冲爆震室的壳体。
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公开(公告)号：US08650856B2
公开(公告)日：2014-02-18
申请号：US12964968
申请日：2010-12-10
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 。
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44.发明申请公开(公告)号：US20120047873A1
公开(公告)日：2012-03-01
申请号：US12872693
申请日：2010-08-31
摘要： A detonation chamber for a pulse detonation combustor including: a plurality of duplex tab obstacles disposed on at least a portion of an inner surface of the detonation chamber wherein the plurality of duplex tab obstacles 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炸室，包括：设置在爆炸室内表面的至少一部分上的多个双重突片障碍物，其中多个双重突出物障碍物增强了通过爆震室的流体流动的紊流。
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公开(公告)号：US07837451B2
公开(公告)日：2010-11-23
申请号：US12040189
申请日：2008-02-29
IPC分类号： F01C1/107 , F03C2/08 , F04C2/107 , F04C18/107
CPC分类号： F01C1/107 , F04C2/1071
摘要： A positive displacement capture device contains a rotor portion positioned inside a casing portion to act as a least area rotor which captures a volume and moves the volume along the length of the separator. The rotor portion contains a plurality of lobes which interact with grooves in the casing portion, such that the interaction of the lobes and grooves create barriers which capture the volume. The creation of the volume creates a flow barrier between a downstream end of the separator and an upstream end of the separator. The flow separator is coupled to a combustion portion to provide a flow of material to the combustion portion. There is a non-contact seal between the lobes and the grooves, and the lobes have channels or depressions at their ends.
摘要翻译： 正位移捕获装置包括位于壳体部分内的转子部分，以用作捕获体积并沿着分离器的长度移动体积的最小区域转子。 转子部分包含与壳体部分中的凹槽相互作用的多个凸角，使得凸角和凹槽的相互作用产生捕获体积的障碍物。 卷的创建在分离器的下游端和分离器的上游端之间产生流动阻挡。 流动分离器联接到燃烧部分以向燃烧部分提供材料流。 在凸角和凹槽之间存在非接触式密封，并且凸角在其端部具有通道或凹陷。
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公开(公告)号：US20080310981A1
公开(公告)日：2008-12-18
申请号：US11761527
申请日：2007-06-12
申请人： James Fredric Wiedenhoefer , Adam Rasheed , Pierre Francois Pinard , Anthony John Dean , Charles Max Byrd
发明人： James Fredric Wiedenhoefer , Adam Rasheed , Pierre Francois Pinard , Anthony John Dean , Charles Max Byrd
IPC分类号： F01C1/107
CPC分类号： F01C1/107
摘要： A positive displacement flow separator contains a rotor portion positioned inside a casing portion to act as a least area rotor which captures a volume and moves the volume along the length of the separator. The rotor portion contains a plurality of lobes which interact with grooves in the casing portion, such that the interaction of the lobes and grooves create barriers which capture the volume The creation of the volume creates a flow barrier between a downstream end of the separator and an upstream end of the separator. The flow separator is coupled to a combustion portion to provide a flow of material to the combustion portion.
摘要翻译： 正位移流分离器包含位于壳体部分内部的转子部分，用作捕获体积并沿着分离器的长度移动体积的最小区域转子。 转子部分包含与壳体部分中的凹槽相互作用的多个凸角，使得凸角和凹槽的相互作用产生捕获体积的障碍。容积的产生在分离器的下游端和 分离器的上游端。 流动分离器联接到燃烧部分以向燃烧部分提供材料流。
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公开(公告)号：US20080127728A1
公开(公告)日：2008-06-05
申请号：US11565252
申请日：2006-11-30
IPC分类号： G01H5/00
CPC分类号： G01H5/00
摘要： A pulse detonation device contains a detonation chamber and a propagation portion, and a plurality of mechanical response gauges coupled to an exterior surface of at least one of the detonation chamber and the propagation portion. Signals from the mechanical response gauges are sent to high frequency AC-coupled amplifiers, and the amplified signals are sent to a high frequency data acquisition system. Based on the data from the mechanical response gauges, the velocity of a detonation pressure wave is determined.
摘要翻译： 脉冲爆震装置包括爆轰室和传播部分，以及耦合到爆炸室和传播部分中的至少一个的外表面的多个机械响应计。 来自机械响应量规的信号被发送到高频AC耦合放大器，并且放大的信号被发送到高频数据采集系统。 基于来自机械响应计的数据，确定爆震压力波的速度。
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公开(公告)号：US20080006019A1
公开(公告)日：2008-01-10
申请号：US11262652
申请日：2005-10-31
IPC分类号： F23R7/00
CPC分类号： F23R3/005 , F23C15/00 , F23R7/00 , Y02T50/675
摘要： A pulse detonation engine comprises a primary air inlet; a primary air plenum located in fluid communication with the primary air inlet; a secondary air inlet; a secondary air plenum located in fluid communication with the secondary air inlet, wherein the secondary air plenum is substantially isolated from the primary air plenum; a pulse detonation combustor comprising a pulse detonation chamber, wherein the pulse detonation chamber is located downstream of and in fluid communication with the primary air plenum; a coaxial liner surrounding the pulse detonation combustor defining a cooling plenum, wherein the cooling plenum is in fluid communication with the secondary air plenum; an axial turbine assembly located downstream of and in fluid communication with the pulse detonation combustor and the cooling plenum; and a housing encasing the primary air plenum, the secondary air plenum, the pulse detonation combustor, the coaxial liner, and the axial turbine assembly.
摘要翻译： 脉冲爆震发动机包括一次空气入口; 位于与一次空气入口流体连通的主要空气室; 二次空气入口; 位于与二次空气入口流体连通的二次空气增压室，其中二次空气增压室基本上与一次空气通风室隔离; 脉冲爆震燃烧器，其包括脉冲爆震室，其中所述脉冲爆震室位于所述主要空气通风室的下游并且与所述主要空气通风室流体连通; 环绕所述脉冲爆震燃烧器的同轴衬套限定冷却气室，其中所述冷却气室与所述二次空气通风室流体连通; 轴向涡轮机组件，位于脉冲爆震燃烧器和冷却气室的下游并与流体连通; 以及包围主空气增压室，二次空气增压室，脉冲爆震燃烧器，同轴衬套和轴向涡轮机组件的壳体。
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公开(公告)号：US20070186556A1
公开(公告)日：2007-08-16
申请号：US11352773
申请日：2006-02-13
申请人： Adam Rasheed , Keith McManus , Anthony Dean
发明人： Adam Rasheed , Keith McManus , Anthony Dean
IPC分类号： F23R7/00
CPC分类号： F23R7/00
摘要： A method for operating a pulse detonation engine, wherein the method includes channeling air flow from a pulse detonation combustor into a flow mixer having an inlet portion, an outlet portion, and a body portion extending therebetween. The method also includes channeling ambient air past the flow mixer and mixing the air flow discharged from the pulse detonation combustor with the ambient air flow such that a combined flow is generated from the flow mixer that has less flow variations than the air flow discharged from the pulse detonation combustor.
摘要翻译： 一种用于操作脉冲爆震引擎的方法，其中所述方法包括将来自脉冲爆震燃烧器的空气流引导到具有入口部分，出口部分和在其间延伸的主体部分的流动混合器。 该方法还包括将环境空气引导通过流动混合器并将从脉冲爆震燃烧器排放的空气流与环境空气流混合，使得从流动混合器产生的组合流量具有比从 脉冲爆震燃烧器。
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公开(公告)号：US07200987B2
公开(公告)日：2007-04-10
申请号：US10870876
申请日：2004-06-18
摘要： The present invention is a gas turbine engine system containing a compressor stage, a pulse detonation stage, and a turbine stage. During operation of the engine system, compressed flow from the compressor stage is directed to at least one off-axis pulse detonation tube in the pulse detonation stage. The off-axis pulse detonation tube detonates a mixture containing the compressed flow and a fuel to create a detonation wave, which is routed to an inlet portion of a reverse flow turbine. The exhaust flow from the reverse flow turbine is then directed away from the engine through ducting.
摘要翻译： 本发明是一种包含压缩机级，脉冲爆震级和涡轮级的燃气轮机发动机系统。 在发动机系统运行期间，来自压缩机级的压缩流被引导到脉冲爆震级中的至少一个离轴脉冲爆管。 离轴脉冲爆震管引爆包含压缩流和燃料的混合物以产生爆震波，该爆震波被引导到逆流涡轮机的入口部分。 然后，来自逆流涡轮机的废气流通过管道被引导离开发动机。
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