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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：US20060254252A1
公开(公告)日：2006-11-16
申请号：US11129686
申请日：2005-05-13
申请人： Adam Rasheed , Anthony Dean , Christian Vandervort
发明人： Adam Rasheed , Anthony Dean , Christian Vandervort
IPC分类号： F02C5/02
摘要： A pulse detonation (PD) assembly includes a number of PD chambers adapted to expel respective detonation product streams and a number of barriers disposed between respective pairs of PD chambers. The barriers define, at least in part, a number of sectors that contain at least one PD chamber. A hybrid engine includes a number of PD chambers and barriers. The hybrid engine further includes a turbine assembly having at least one turbine stage, being in flow communication with the PD chambers and being configured to be at least partially driven by the detonation product streams. A segmented hybrid engine includes a number of PD chambers and segments configured to receive and direct the detonation product streams from respective PD chambers. The segmented hybrid engine further includes a turbine assembly configured to be at least partially driven by the detonation product streams.
摘要翻译： 脉冲爆震（PD）组件包括适于排出各个爆震产物流的多个PD室和设置在各对PD室之间的多个障碍物。 这些障碍至少部分地限定了包含至少一个PD室的多个扇区。 混合动力发动机包括多个PD室和障碍物。 混合动力发动机还包括具有至少一个涡轮级的涡轮组件，其与PD室流体连通并被构造成至少部分地被爆轰产物流驱动。 分段混合动力发动机包括多个PD室和构造成接收和引导来自相应PD室的爆轰产物流的段。 分段式混合动力发动机还包括构造成至少部分地被引爆产物流驱动的涡轮组件。
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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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4.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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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：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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7.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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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：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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10.发明申请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：US20070180833A1
公开(公告)日：2007-08-09
申请号：US11348869
申请日：2006-02-07
申请人： Adam Rasheed , Anthony Dean
发明人： Adam Rasheed , Anthony Dean
IPC分类号： F02C5/00
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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