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公开(公告)号：US08539752B2
公开(公告)日：2013-09-24
申请号：US12957047
申请日：2010-11-30
CPC分类号： F23R7/00
摘要： A detonation chamber and a pulse detonation combustor including a detonation chamber, wherein the detonation chamber includes a plurality of initiation obstacles and at least one injector in fluid flow communication with each of the plurality of initiation obstacles. The plurality of initiation obstacles are disposed on at least a portion of an inner surface of the detonation chamber with each of the plurality of initiation obstacles defining a low pressure region at a trailing edge. The plurality of initiation obstacles are configured to enhance a turbulence of a fluid flow and flame acceleration through the detonation chamber. The at least one injector in provides a cooling fluid flow to each of the plurality of initiation obstacles, wherein the cooling fluid flow is one of a fuel, a combination of fuels, air, or a fuel/air mixture.
摘要翻译： 爆震室和包括爆震室的脉冲爆炸燃烧室，其中所述爆轰室包括多个起爆障碍物和至少一个与所述多个引发障碍物中的每一个流体流动连通的喷射器。 多个起始障碍物设置在爆震室的内表面的至少一部分上，多个起始障碍物中的每一个在后缘限定低压区域。 多个起始障碍物构造成增强流体流动的紊流和通过爆轰室的火焰加速。 至少一个喷射器提供冷却流体流向多个起始障碍物中的每一个，其中冷却流体流是燃料，燃料，空气或燃料/空气混合物的组合之一。
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公开(公告)号：US20120122039A1
公开(公告)日：2012-05-17
申请号：US12948181
申请日：2010-11-17
IPC分类号： F23C15/00
CPC分类号： F23R7/00 , F02C5/02 , F05D2260/16 , F23D2211/00
摘要： A pulse detonation combustor including a plurality of nozzles engaged with one another via mating surfaces to support a gas discharge annulus in a circumferential direction. The pulse detonation combustor also including multiple pulse detonation tubes extending for the nozzles and a plurality of thermal expansion control joints coupled to the plurality of pulse detonation tubes. Each of the plurality of thermal expansion control joints is configured to facilitate independent thermal growth of each of the plurality of pulse detonation tubes. The thermal expansion control joints may be configured as a bellows expansion joint or a sliding expansion joint.
摘要翻译： 一种脉冲爆震燃烧器，包括通过配合表面彼此接合的多个喷嘴，以在圆周方向上支撑排气环。 脉冲爆震燃烧器还包括为喷嘴延伸的多个脉冲爆管和连接到多个脉冲爆管的多个热膨胀控制接头。 多个热膨胀控制接头中的每一个构造成促进多个脉冲爆管中的每一个独立的热生长。 热膨胀控制接头可以构造为波纹管膨胀接头或滑动膨胀接头。
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53.发明授权Methods and apparatus for controlling air flow within a pulse detonation engine 有权用于控制脉冲爆震发动机内气流的方法和装置公开(公告)号：US07980056B2
公开(公告)日：2011-07-19
申请号：US11348869
申请日：2006-02-07
申请人： Adam Rasheed , Anthony John Dean
发明人： Adam Rasheed , Anthony John Dean
IPC分类号： F02C7/04
摘要： A flow control device for use with a pulse detonation chamber including an inlet coupled in flow communication with a source of compressed air. The inlet extends at least partially into the chamber to facilitate controlling air flow into the chamber. The device also includes a body portion extending downstream from and circumferentially around the inlet, wherein the body portion is positioned in flow communication with the inlet.
摘要翻译： 一种用于脉冲爆震室的流量控制装置，包括与压缩空气源流动连通的入口。 入口至少部分地延伸到室中以便于控制进入室的空气流。 该装置还包括从入口的下游和周向延伸的主体部分，其中主体部分定位成与入口流动连通。
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公开(公告)号：US20110146285A1
公开(公告)日：2011-06-23
申请号：US12641013
申请日：2009-12-17
申请人： Aaron Glaser , Adam Rasheed , Ross Hartley Kenyon
发明人： Aaron Glaser , Adam Rasheed , Ross Hartley Kenyon
CPC分类号： F02K7/02 , F02C5/12 , F02K7/06 , Y02T50/671
摘要： In one embodiment, a pulse detonation system includes a pulse detonation tube and an air valve disposed at an upstream end of the pulse detonation tube. The air valve is configured to provide an air flow into the pulse detonation tube. The pulse detonation system also includes a fuel injector configured to inject fuel into the air flow to establish a fuel-air mixture configured to support detonation, and to establish a region in the fuel-air mixture having a fuel to air ratio insufficient to support a detonation wave. The pulse detonation system further includes an ignition source configured to detonate the fuel-air mixture when the region is disposed adjacent to the air valve.
摘要翻译： 在一个实施例中，脉冲爆震系统包括设置在脉冲爆管的上游端的脉冲爆管和空气阀。 空气阀构造成将空气流提供到脉冲爆管中。 脉冲爆震系统还包括燃料喷射器，燃料喷射器构造成将燃料喷射到空气流中以建立配置成支持爆炸的燃料 - 空气混合物，并且建立燃料 - 空气混合物中具有不足以支持燃料 - 空气混合物的区域 爆震波。 脉冲爆震系统还包括点火源，其构造成当该区域邻近空气阀设置时引爆燃料 - 空气混合物。
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公开(公告)号：US07836682B2
公开(公告)日：2010-11-23
申请号：US11352773
申请日：2006-02-13
IPC分类号： F02K5/02
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：US20100236214A1
公开(公告)日：2010-09-23
申请号：US12407309
申请日：2009-03-19
IPC分类号： F02C5/12
CPC分类号： F23R7/00 , F23R2900/00013
摘要： An engine contains a compressor stage, a plurality of pulse detonation combustors and a rotary inlet valve structure having a plurality of inlet ports through which at least air flows to enter the pulse detonation combustors during operation of the engine. Downstream of the pulse detonation combustors is a turbine stage. Further, the ratio of the pulse detonation combustors to the inlet ports is a non-integer.
摘要翻译： 发动机包括压缩机级，多个脉冲爆震燃烧器和具有多个入口的旋转入口阀结构，所述多个入口端口在发动机操作期间至少经过空气流动以进入脉冲爆震燃烧器。 脉冲爆震燃烧器的下游是涡轮级。 此外，脉冲爆震燃烧器与入口端口的比率是非整数。
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57.发明申请METHOD AND APPARATUS FOR TAILORING THE EQUIVALENCE RATIO IN A VALVED PULSE DETONATION COMBUSTOR 审中-公开在阀门脉冲爆炸装置中定量等效比的方法和装置公开(公告)号：US20090139203A1
公开(公告)日：2009-06-04
申请号：US12271091
申请日：2008-11-14
IPC分类号： F02K7/02
摘要： A pulse detonation combustor assembly contains at least one PDC tube, a mechanical air flow valve which directs an air flow into the PDC tube, where the mechanical air flow assembly changes a rate of the air flow into the PDC tube during a fill stage of the PDC tube. The assembly also contains a fuel flow control valve which directs fuel to the PDC tube and changes the rate of the fuel flow into PDC tube. By controlling the flow of the fuel and air into the PDC tube the equivalence ratio profile of the PDC tube can be tailored and controlled.
摘要翻译： 脉冲爆震燃烧器组件包含至少一个PDC管，机械气流阀，其将空气流引导到PDC管中，其中机械空气流组件在填充阶段期间改变进入PDC管的空气流的速率 PDC管。 组件还包含燃料流量控制阀，其将燃料引导到PDC管并且将燃料流量改变为PDC管。 通过控制燃料和空气流入PDC管中，可以调节和控制PDC管的等效比分布。
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58.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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公开(公告)号：US20070015099A1
公开(公告)日：2007-01-18
申请号：US11172304
申请日：2005-06-30
申请人： James Wiedenhoefer , Adam Rasheed , Anthony Dean , Pierre Pinard
发明人： James Wiedenhoefer , Adam Rasheed , Anthony Dean , Pierre Pinard
IPC分类号： F23D14/82
CPC分类号： F02K7/02
摘要： A pulse detonation device for dividing a pulse detonation shock wave into an primary and control portion to reduce the strength of a propagating shock wave and/or change its direction. The device contains a flow separator which directs a portion of the shock wave into itself, thus reducing the shock wave's strength. In one configuration, the control region converges in cross-sectional area so as to accelerate the flow in the control region, while the primary region diverges to slow the flow in the primary region. The flow in the control region is directed, at an angle, into the flow of the primary region to impede and/or redirect the flow of the primary region.
摘要翻译： 一种脉冲爆震装置，用于将脉冲爆震冲击波分解成初级和控制部分，以减小传播冲击波的强度和/或改变其方向。 该装置包含一个流动分离器，其将冲击波的一部分引导到其中，从而降低冲击波的强度。 在一种构造中，控制区域以横截面积收敛，以便加速控制区域中的流动，而主区域发散以减缓主区域中的流动。 控制区域中的流动以一定角度被引导到主区域的流动中，以阻止和/或重定向主区域的流动。
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公开(公告)号：US08899010B2
公开(公告)日：2014-12-02
申请号：US12948181
申请日：2010-11-17
CPC分类号： F23R7/00 , F02C5/02 , F05D2260/16 , F23D2211/00
摘要： A pulse detonation combustor including a plurality of nozzles engaged with one another via mating surfaces to support a gas discharge annulus in a circumferential direction. The pulse detonation combustor also including multiple pulse detonation tubes extending for the nozzles and a plurality of thermal expansion control joints coupled to the plurality of pulse detonation tubes. Each of the plurality of thermal expansion control joints is configured to facilitate independent thermal growth of each of the plurality of pulse detonation tubes. The thermal expansion control joints may be configured as a bellows expansion joint or a sliding expansion joint.
摘要翻译： 一种脉冲爆震燃烧器，包括通过配合表面彼此接合的多个喷嘴，以在圆周方向上支撑排气环。 脉冲爆震燃烧器还包括为喷嘴延伸的多个脉冲爆管和连接到多个脉冲爆管的多个热膨胀控制接头。 多个热膨胀控制接头中的每一个构造成促进多个脉冲爆管中的每一个独立的热生长。 热膨胀控制接头可以构造为波纹管膨胀接头或滑动膨胀接头。
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