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公开(公告)号：US20110146232A1
公开(公告)日：2011-06-23
申请号：US12645480
申请日：2009-12-23
申请人： Eric Richard Westervelt , Douglas Carl Hofer , Narendra Digamber Joshi , Kit Yan Siu , Ruijie Shi , Adam Rasheed , Venkat Eswarlu Tangirala
发明人： Eric Richard Westervelt , Douglas Carl Hofer , Narendra Digamber Joshi , Kit Yan Siu , Ruijie Shi , Adam Rasheed , Venkat Eswarlu Tangirala
IPC分类号： F02K5/02
CPC分类号： F02C5/11
摘要： A pulse detonation turbine engine (PDTE) includes at least one controllable multi-tube pulse detonation combustor (PDC) configured to initiate firing of one or more pulse detonation tubes in response to operation of a plurality of controllable peripheral PDC components to regulate PDTE output characteristics. A control system including a programmable controller directed by algorithmic software operates to generate control inputs for the plurality of controllable peripheral PDC components in response to PDTE input conditions, such that one or more PD tube controllable inputs can be different for at least one PD tube relative to another PD tube within the multi-tube PDC, and further such that detonation timing can be different for at least one PD tube relative to another PD tube within the multi-tube PDC.
摘要翻译： 脉冲爆震涡轮发动机（PDTE）包括至少一个可控多管脉冲爆震燃烧器（PDC），其被配置为响应于多个可控周边PDC部件的操作而启动一个或多个脉冲爆管的点火，以调节PDTE输出特性 。 包括由算法软件引导的可编程控制器的控制系统操作以响应于PDTE输入条件来生成针对多个可控周边PDC组件的控制输入，使得一个或多个PD管可控输入对于至少一个PD管相对 到多管PDC内的另一个PD管，并且进一步使得至少一个PD管相对于多管PDC内的另一PD管的引爆定时可以不同。
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公开(公告)号：US20120131901A1
公开(公告)日：2012-05-31
申请号：US12956868
申请日：2010-11-30
CPC分类号： F02C9/266 , F02K7/06 , F05D2260/99 , F05D2270/051
摘要： In one embodiment, a pulse detonation engine (PDE) includes a controller configured to receive signals indicative of at least one of a desired operating parameter of the PDE and a measured internal parameter of the PDE, and to adjust at least one of a first fluid flow through the PDE and a second fluid flow through at least one of multiple pulse detonation tubes disposed within the PDE based on the signals. The PDE does not include a turbine or a mechanical compressor.
摘要翻译： 在一个实施例中，脉冲爆震引擎（PDE）包括控制器，其被配置为接收指示PDE的期望操作参数和所测量的PDE的内部参数中的至少一个的信号，并且调整至少一个第一流体 基于该信号，流过PDE和通过设置在PDE内的多个脉冲爆管中的至少一个的第二流体流。 PDE不包括涡轮或机械压缩机。
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3.发明授权Hot gas path component cooling for hybrid pulse detonation combustion systems 有权混合脉冲爆震燃烧系统的热气路径组件冷却公开(公告)号：US08978387B2
公开(公告)日：2015-03-17
申请号：US12974085
申请日：2010-12-21
申请人： Venkat Eswarlu Tangirala , Narendra Digamber Joshi , Adam Rasheed , Brian Gene Brzek , Douglas Carl Hofer , Thomas Michael Lavertu , Fuhua Ma
发明人： Venkat Eswarlu Tangirala , Narendra Digamber Joshi , Adam Rasheed , Brian Gene Brzek , Douglas Carl Hofer , Thomas Michael Lavertu , Fuhua Ma
CPC分类号： F02C5/02 , F02C7/18 , F02C9/18 , F05D2260/205 , F23C15/00
摘要： The flow through the core of a hybrid pulse detonation combustion system is passed through a compressor and then separated into a primary flow, that passes directly to the combustor, and a bypass flow, which is routed to a portion of the system to be used to cool components of the system. The bypass flow is routed to a nozzle of the pulse detonation combustor. The flow is then passed back into the primary flow through the core downstream of where it was extracted.
摘要翻译： 通过混合脉冲爆震燃烧系统的核心的流动通过压缩机，然后分离成直接通向燃烧器的主流，以及旁路流，其被路由到系统的一部分以用于 系统的酷组件。 旁路流被引导到脉冲爆震燃烧器的喷嘴。 然后将流体通过芯被提取的下游的核心传回初级流中。
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4.发明申请HOT GAS PATH COMPONENT COOLING FOR HYBRID PULSE DETONATION COMBUSTION SYSTEMS 审中-公开用于混合脉冲爆震燃烧系统的热气路径组件冷却公开(公告)号：US20120151895A1
公开(公告)日：2012-06-21
申请号：US12974031
申请日：2010-12-21
申请人： Venkat Eswarlu Tangirala , Narendra Digamber Joshi , Adam Rasheed , Brian Gene Brzek , Douglas Carl Hofer , Thomas Michael Lavertu , Fuhua Ma
发明人： Venkat Eswarlu Tangirala , Narendra Digamber Joshi , Adam Rasheed , Brian Gene Brzek , Douglas Carl Hofer , Thomas Michael Lavertu , Fuhua Ma
CPC分类号： F02C5/02
摘要： The flow through the core of a hybrid pulse detonation combustion system is passed through a compressor and then separated into a primary flow, that passes directly to the combustor, and a bypass flow, which is routed to a portion of the system to be used to cool components of the system. The bypass includes a pump that raises the pressure of the bypass flow sufficient to deliver it to downstream stations of the engine that contain combustion products that are at a higher pressure than the compressor exit.
摘要翻译： 通过混合脉冲爆震燃烧系统的核心的流动通过压缩机，然后分离成直接通向燃烧器的主流，以及旁路流，其被路由到系统的一部分以用于 系统的酷组件。 旁路包括一个泵，其提高旁路流的压力，足以将其输送到发动机的下游站，该发动机包含比压缩机出口更高的压力的燃烧产物。
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5.发明申请Control system for a land-based simple cycle hybrid engine for power generation 审中-公开用于发电的陆基简单循环混合动力发动机的控制系统公开(公告)号：US20100154380A1
公开(公告)日：2010-06-24
申请号：US12317350
申请日：2008-12-22
CPC分类号： F02C5/10 , F02C9/28 , F05D2260/16 , F05D2270/05 , F05D2270/304 , F23R7/00
摘要： A pulse detonation combustor (PDC)-based hybrid engine control system includes a programmable controller directed by algorithmic software to control a rotational shaft speed of the PDC-based hybrid engine, an air inlet valve rotational speed for the PDC, and a fuel fill time period for the PDC in response to a corresponding low pressure turbine (LPT) shaft speed signal or a power difference signal based on a difference between desired power and actual power produced by the PDC-based hybrid engine and further in response to a fuel fill time signal for the PDC, such that a desired fuel fill fraction and stoichiometric ratio are maintained and further such that a mass air flowrate from an air compressor matches a mass air flowrate ingested via the PDC while the PDC-based hybrid engine is operating in an acceleration mode or a deceleration mode.
摘要翻译： 基于脉冲爆震燃烧器（PDC）的混合发动机控制系统包括由算法软件引导的可编程控制器，用于控制基于PDC的混合发动机的转轴转速，PDC的进气阀旋转速度和燃料填充时间 响应于相应的低压涡轮机（LPT）轴速度信号或基于由基于PDC的混合动力发动机产生的期望功率和实际功率之间的差异的功率差信号，并且还响应于燃料填充时间 信号，使得保持期望的燃料填充部分和化学计量比，并且进一步使得来自空气压缩机的质量空气流量匹配通过PDC摄入的质量空气流量，而基于PDC的混合动力发动机以加速度运行 模式或减速模式。
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6.发明申请MODULATION OF INLET MASS FLOW AND RESONANCE FOR A MULTI-TUBE PULSE DETONATION ENGINE SYSTEM USING PHASE SHIFTED OPERATION AND DETUNING 审中-公开使用相位转换操作和分离的多管脉冲爆震发动机系统的输入质量流量和谐振的调节公开(公告)号：US20100242436A1
公开(公告)日：2010-09-30
申请号：US12415677
申请日：2009-03-31
IPC分类号： F02K5/02
CPC分类号： F02C5/10
摘要： An engine contains a compressor stage, a plurality of pulse detonation combustors and a plurality of inlet valves, where the inlet valves direct a mass flow into the pulse detonation combustors. A control system controls at least one of a phase shift, firing frequency and a τopen/τcycle ratio of the pulse detonation combustors based on a mass flow and/or a resonance within the engine.
摘要翻译： 发动机包括压缩机级，多个脉冲爆震燃烧器和多个入口阀，其中入口阀将质量流引导到脉冲爆震燃烧器中。 控制系统基于发动机内的质量流和/或谐振来控制脉冲爆震燃烧器的相移，发射频率和τopen/τ循环比中的至少一个。
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公开(公告)号：US20090241507A1
公开(公告)日：2009-10-01
申请号：US12060557
申请日：2008-04-01
CPC分类号： F02C5/00 , F02C7/08 , F02C7/143 , Y02T50/675
摘要： A ground based power generation system contains at least two compressor stages, a combustion stage and a turbine stage. An intercooler is positioned between the two compressor stages and a regenerator is positioned between the compressor stages and the combustion stage. The combustion stage contains at least one of a pulse detonation combustor and constant volume combustor. Downstream of the combustion stage is the turbine stage. Heat for the regenerator is supplied from the turbine stage. Further, a bypass flow device is included which re-directs flow upstream of the combustion stage to downstream of the combustion stage and upstream of the turbine stage.
摘要翻译： 基于地面的发电系统包含至少两个压缩机级，燃烧级和涡轮级。 中间冷却器位于两个压缩机级之间，并且再生器位于压缩机级和燃烧级之间。 燃烧阶段包括脉冲爆震燃烧器和恒定体积燃烧器中的至少一个。 燃烧阶段的下游是涡轮机阶段。 用于再生器的热量由涡轮级供给。 此外，还包括旁路流动装置，其将燃烧阶段上游的流动重新引导到燃烧阶段的下游以及涡轮级的上游。
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8.发明授权Ground-based simple cycle pulse detonation combustor based hybrid engine for power generation 有权用于发电的基于地基的简单循环脉冲爆震燃烧器混合发动机公开(公告)号：US08302377B2
公开(公告)日：2012-11-06
申请号：US12362783
申请日：2009-01-30
IPC分类号： F02K5/02
CPC分类号： F02K7/06 , F02C5/02 , F05D2220/62 , F05D2260/96 , F23R7/00
摘要： An engine contains a compressor stage, a compressor plenum, an inlet valving stage, a PDC stage, a PDC exit nozzle stage, a transition stage, a high pressure turbine stage, a turbine plenum, and a low pressure turbine stage. The PDC stage contains at least one pulse detonation combustor and each of the compressor plenum, PDC exit nozzle stage and turbine plenum contain a volume used to reduce and/or widen pressure peaks generated by the operation of the PDC stage.
摘要翻译： 发动机包括压缩机级，压缩机增压室，入口阀级，PDC级，PDC出口喷嘴级，过渡级，高压涡轮级，涡轮增压室和低压涡轮级。 PDC级包含至少一个脉冲爆震燃烧器，并且压缩机增压室，PDC出口喷嘴级和涡轮增压室中的每一个包含用于减少和/或加宽由PDC级的操作产生的压力峰值的体积。
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9.发明申请GROUND-BASED SIMPLE CYCLE PULSE DETONATION COMBUSTOR BASED HYBRID ENGINE FOR POWER GENERATION 有权基于地基的简单循环脉冲爆轰机组发电机发电机公开(公告)号：US20100192536A1
公开(公告)日：2010-08-05
申请号：US12362783
申请日：2009-01-30
IPC分类号： F02C5/02
CPC分类号： F02K7/06 , F02C5/02 , F05D2220/62 , F05D2260/96 , F23R7/00
摘要： An engine contains a compressor stage, a compressor plenum, an inlet valving stage, a PDC stage, a PDC exit nozzle stage, a transition stage, a high pressure turbine stage, a turbine plenum, and a low pressure turbine stage. The PDC stage contains at least one pulse detonation combustor and each of the compressor plenum, PDC exit nozzle stage and turbine plenum contain a volume used to reduce and/or widen pressure peaks generated by the operation of the PDC stage.
摘要翻译： 发动机包括压缩机级，压缩机增压室，入口阀级，PDC级，PDC出口喷嘴级，过渡级，高压涡轮级，涡轮增压室和低压涡轮级。 PDC级包含至少一个脉冲爆震燃烧器，并且压缩机增压室，PDC出口喷嘴级和涡轮增压室中的每一个包含用于减少和/或加宽由PDC级的操作产生的压力峰值的体积。
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10.发明申请PULSE DETONATION COMBUSTOR VALVE FOR HIGH TEMPERATURE AND HIGH PRESSURE OPERATION 审中-公开用于高温和高压运行的脉冲爆炸式气动阀公开(公告)号：US20090139199A1
公开(公告)日：2009-06-04
申请号：US12271082
申请日：2008-11-14
申请人： Ross Hartley Kenyon , Narendra Digamber Joshi , Venkat Eswarlu Tangirala , Anthony John Dean , Adam Rasheed , Aaron Jerome Glaser , James Fredric Wiedenhoefer , David Chapin , Kevin Hinckley , Pierre Francois Pinard
发明人： Ross Hartley Kenyon , Narendra Digamber Joshi , Venkat Eswarlu Tangirala , Anthony John Dean , Adam Rasheed , Aaron Jerome Glaser , James Fredric Wiedenhoefer , David Chapin , Kevin Hinckley , Pierre Francois Pinard
IPC分类号： F02C5/12
摘要： A pulse detonation combustor valve assembly contains at least one pulse detonation combustor having an inlet portion through which air and/or fuel enters the chamber of the combustor. An annular rotating valve portion is positioned adjacent to an outer surface of the pulse detonation combustor and concentrically with the pulse detonation combustor so that the annular rotating valve portion can be rotated with respect to the combustor. The annular rotating valve portion contains at least one inlet portion through which air and/or fuel passes to enter the inlet portion of the pulse detonation combustor.
摘要翻译： 脉冲爆震燃烧器阀组件包含至少一个具有入口部分的脉冲爆燃燃烧器，空气和/或燃料通过该入口部分进入燃烧室的腔室。 环形旋转阀部分定位成与脉冲爆震燃烧器的外表面相邻并且与脉冲爆震燃烧器同心地定位，使得环形旋转阀部分可相对于燃烧器旋转。 环形旋转阀部分包含至少一个入口部分，空气和/或燃料通过该入口部分进入脉冲爆震燃烧器的入口部分。
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