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    Liquid fueled pulse detonation engine with controller and inlet and exit valves
    1.
    发明授权
    Liquid fueled pulse detonation engine with controller and inlet and exit valves 失效
    具有控制器和进出气阀的液体燃料脉冲爆震发动机

    公开(公告)号：US5901550A

    公开(公告)日：1999-05-11

    申请号：US618001

    申请日：1996-03-18

    申请人： Thomas R. A. Bussing ,  Thomas E. Bratkovich

    发明人： Thomas R. A. Bussing ,  Thomas E. Bratkovich

    IPC分类号： B01J3/08 ,  B05B7/00 ,  C23C4/12 ,  F01D5/28 ,  F02K7/06 ,  F02K7/075 ,  F02K9/97 ,  F02C5/02

    CPC分类号： F02K9/974 ,  B01J3/08 ,  B05B7/0006 ,  C23C4/126 ,  F01D5/288 ,  F02K7/06 ,  F02K7/075 ,  F02K9/972

    摘要： The invention provides a liquid fueled pulsed detonation air breathing engine. The engine has at least one, and preferably a multiplicity of, detonation chambers, each of which has an inlet end for opening and receiving a charge of fuel and air, and an outlet end for discharging combustion product gases. A fast-acting valve is located above the inlet ends of the detonation chambers and cyclically opens the fuel and air receiving openings in the inlet ends of the detonation chambers to allow a fuel/air charge to enter the chambers. In a preferred embodiment, the valve is of a rotary type with a body that has at least one opening through which fuel and air can flow into the inlet end of the detonation chamber. Once the valve has closed, detonation is initiated by an ignitor and impulse force is provided by the resultant shock wave. Thereafter, the valve opens again so that the detonation chamber can be charged with fuel and air to recommence the cycle. The invention also provides an embodiment of an engine that has both inlet and outlet valves. These valves operate out of phase so that when the inlet valve is open to receive fuel and air into the detonation chamber, the outlet valve is closed. When detonation commences, the outlet valve is open and the inlet valve is closed. Optionally, a source of oxygen allows a stratified charge in the engine to enhance detonation. Also provided is a control system (48) for sensing the position of the valves, (58, 80) and using this sensed position to inject fuel, inject oxygen and ignite the fuel and air mixture.

    摘要翻译： 本发明提供一种液体燃料脉冲爆震空气呼吸发动机。 发动机具有至少一个，优选地是多个爆轰室，每个都具有用于打开和接收燃料和空气的进料口的入口端，以及用于排出燃烧产物气体的出口端。 快速作用阀位于引爆室的入口端上方，并循环地打开引爆室入口端的燃料和空气接收孔，以允许燃料/空气进入腔室。 在优选实施例中，阀是具有主体的旋转型，其具有至少一个开口，燃料和空气可以通过该开口流入爆炸室的入口端。 一旦阀门关闭，爆震就由点火器启动，冲击力由所产生的冲击波提供。 此后，阀再次打开，使得引爆室可以充入燃料和空气以重新开始循环。 本发明还提供了具有入口和出口阀的发动机的实施例。 这些阀门异相工作，因此当入口阀打开以接收燃料和空气进入爆轰室时，出口阀关闭。 当爆炸开始时，出口阀打开，进气阀关闭。 可选地，氧源允许发动机中的分层装料增强爆震。 还提供了一种用于感测阀（58,80）的位置并使用该感测位置喷射燃料，注入氧气并点燃燃料和空气混合物的控制系统（48）。

    Pulsed detonation rocket engine
    2.
    发明授权
    Pulsed detonation rocket engine 失效
    脉冲爆震火箭发动机

    公开(公告)号：US5873240A

    公开(公告)日：1999-02-23

    申请号：US662858

    申请日：1996-06-12

    申请人： Thomas R. A. Bussing ,  Thomas E. Bratkovich

    发明人： Thomas R. A. Bussing ,  Thomas E. Bratkovich

    IPC分类号： B01J3/08 ,  C23C4/12 ,  F02K7/06 ,  F02K7/075 ,  F02K9/97 ,  C06D5/00 ,  F02K5/02

    CPC分类号： F02K9/972 ,  B01J3/08 ,  C23C4/126 ,  F02K7/06 ,  F02K7/075 ,  F02K9/974

    摘要： A pulse detonation rocket engine, having at least two detonation chambers. The rocket propelled vehicle includes at least one fuel delivery system in fluid communication with each of the at least two detonation chambers, and at least one oxidant delivery system in fluid communication with the detonation chambers, along with fast-acting valves to inject fuel and oxidant controlledly into the chambers. An ignitor in each of the detonation chambers intermittently initiates detonation of a fuel and oxidant mixture in the chamber, in a controlled cycle, to provide motive force. Also provided is a combined cycle engine, able to operate in air breathing mode, oxidant augmented mode, and as a rocket engine. The combined cycle engine includes at least one detonation chamber, and may include a plurality of such chambers. The invention further provides methods of intermittently detonating sequentially created fuel and oxygen mixtures in these engines, and methods of using these engines.

    摘要翻译： 具有至少两个爆震室的脉冲爆震火箭发动机。 火箭推进车辆包括与至少两个爆炸室中的每一个流体连通的至少一个燃料输送系统，以及与爆震室流体连通的至少一个氧化剂输送系统，以及用于喷射燃料和氧化剂的快速作用阀 受控地进入房间。 每个引爆室中的点火器在受控循环中间歇地启动燃料和氧化剂混合物的爆炸，以提供动力。 还提供了能够在空气呼吸模式，氧化剂增强模式和作为火箭发动机中操作的联合循环发动机。 联合循环发动机包括至少一个爆震室，并且可以包括多个这样的室。 本发明还提供了在这些发动机中间歇地引爆依次产生的燃料和氧气混合物的方法，以及使用这些发动机的方法。

    Exhaust nozzle for multi-tube detonative engines
    3.
    发明授权
    Exhaust nozzle for multi-tube detonative engines 失效
    多管爆炸发动机排气喷嘴

    公开(公告)号：US6003301A

    公开(公告)日：1999-12-21

    申请号：US827278

    申请日：1997-03-27

    申请人： Thomas E. Bratkovich ,  Kevin E. Williams ,  Thomas R. A. Bussing ,  Gary L. Lidstone ,  John B. Hinkey

    发明人： Thomas E. Bratkovich ,  Kevin E. Williams ,  Thomas R. A. Bussing ,  Gary L. Lidstone ,  John B. Hinkey

    IPC分类号： B05B7/00 ,  F02K7/075 ,  F02K9/97 ,  F02C5/02

    CPC分类号： B05B7/0006 ,  F02K7/075 ,  F02K9/972 ,  F02K9/974

    摘要： A nozzle for a detonative combustion engine, the engine having multiple combustor tubes, comprises a common plenum communicating with the combustor tubes. The common plenum combines separate exhaust streams from the combustor tubes into a compound subsonic exhaust stream. A compound flow throat communicates with the common plenum. The compound flow throat converts the compound subsonic exhaust stream into a compound sonic exhaust stream. The common plenum and compound flow throat cooperate to maintain a predetermined upstream combustor pressure regardless of down stream pressure exiting the expansion section. Optionally, an interface section is inserted between the plenum and the engine such that it communicates with the common plenum section and with outlets of the combustor tubes. The interface section is compartmentalized into flow passages with each flow passage having a cross-sectional area that increases from that of a particular nozzle intake port connected to a conductor tube exit. Additionally, an expansion section communicates with the outlet of the compound flow throat and has a diameter greater than the diameter of the compound flow throat. The expansion section converts the compound sonic exhaust stream into a compound supersonic exhaust stream thus expanding the exhaust stream to predetermined lower pressure.

    摘要翻译： 用于爆炸内燃机的喷嘴，具有多个燃烧器管的发动机包括与燃烧器管连通的公共气室。 公共气室将来自燃烧器管的分离的废气流组合成复合亚音速排气流。 复合流通道与公共气室连通。 复合流动喉将化合物亚音速排气流转化为复合声音排气流。 常见的集气室和复合流道喉部协作以保持预定的上游燃烧器压力，而不管离开膨胀段的下游流压。 可选地，接口部分插入在气室和发动机之间，使得其与公共气室部分和燃烧器管的出口连通。 接口部分被分隔成流动通道，每个流动通道的横截面面积从连接到导体管出口的特定喷嘴进口的横截面面积增加。 此外，膨胀部分与复合流动喉部的出口连通并且具有大于化合物流动喉部的直径的直径。 膨胀部分将化合物声音排气流转化为化合物超音速排气流，从而将排气流扩展到预定的较低压力。

    Detonative cleaning apparatus
    5.
    发明授权
    Detonative cleaning apparatus 失效
    爆炸清洗设备

    公开(公告)号：US07104223B2

    公开(公告)日：2006-09-12

    申请号：US10718855

    申请日：2003-11-20

    申请人： Thomas R. A. Bussing

    发明人： Thomas R. A. Bussing

    IPC分类号： F22B37/48

    CPC分类号： F28G7/00 ,  B08B7/0007 ,  B08B9/08 ,  F28G7/005

    摘要： An apparatus and methods are provided for cleaning a surface within a vessel. A vessel wall separates a vessel exterior from a vessel interior and has a wall aperture. An elongate conduit has an upstream first and a downstream second end and is positioned to direct a shock wave from the second end into the vessel interior. A source of fuel and oxidizer is coupled to the conduit to deliver the fuel an oxidizer to the conduit. An initiator is positioned to initiate a reaction of the fuel and oxidizer to produce the shock wave within the conduit for generating the shock wave. A source of purge gas is positioned to introduce the purge gas to the conduit to drive reaction products of the fuel and oxidizer downstream.

    摘要翻译： 提供了用于清洁容器内的表面的装置和方法。 血管壁将容器外部与容器内部分开并具有壁孔。 细长导管具有上游第一和下游第二端，并且定位成将冲击波从第二端引导到血管内部。 燃料和氧化剂源联接到管道以将燃料输送到导管的氧化剂。 定位引发剂以引发燃料和氧化剂的反应，以在管道内产生冲击波，以产生冲击波。 定位吹扫气体源将吹扫气体引入导管，以驱动燃料和氧化剂在下游的反应产物。

    Pulse detonation electrical power generation apparatus with water injection
    7.
    发明授权
    Pulse detonation electrical power generation apparatus with water injection 失效
    脉冲爆震发电装置注水

    公开(公告)号：US6062018A

    公开(公告)日：2000-05-16

    申请号：US646022

    申请日：1996-05-07

    申请人： Thomas R. A. Bussing

    发明人： Thomas R. A. Bussing

    IPC分类号： B01J3/08 ,  C23C4/12 ,  F01D5/28 ,  F02C5/02 ,  F02K7/06 ,  F02K7/075 ,  F02K9/97

    CPC分类号： B01J3/08 ,  C23C4/126 ,  F01D5/288 ,  F02C5/02 ,  F02K7/06 ,  F02K7/075 ,  F02K9/972 ,  F02K9/974 ,  F23R7/00

    摘要： A pulse detonation power generation apparatus is provided. This apparatus is provided with a detonation chamber connected to fuel and air sources which detonate to produce energy which may be converted to electrical energy. The pulse detonation energy generator may have one or more detonation chambers, each having an inlet end and an outlet end; a fuel manifold for supplying fuel from a fuel source to said generator; an air manifold for supplying air to said generator; a pre-mixer operatively connected to said fuel manifold, air manifold, and the inlet end of said one or more detonation chambers; an impingement ring disposed along an internal wall of said pre-mixer; a disk valve positioned between the pre-mixer and the air manifold; a predetonator for initiating detonation in said detonation chambers; a rotary valve for pulse feeding an oxidizer or fuel to the predetonator; means for injecting liquid water or steam into combustion products produced in said detonation chambers; and means for converting the energy generated by a detonation in said detonation chambers into electrical energy.

    摘要翻译： 提供脉冲爆震发电装置。 该装置设置有连接到燃料和空气源的爆炸室，其引爆以产生可转换成电能的能量。 脉冲爆震能量发生器可以具有一个或多个引爆室，每个具有入口端和出口端; 燃料歧管，用于从燃料源向所述发电机提供燃料; 用于向所述发生器供应空气的空气歧管; 可操作地连接到所述燃料歧管，空气歧管和所述一个或多个引爆室的入口端的预混合器; 沿着所述预混合器的内壁设置的冲击环; 位于预混合器和空气歧管之间的盘阀; 用于在所述爆震室中起爆的预引爆器; 旋转阀，用于将氧化剂或燃料脉冲馈送到预灭火器; 用于将液态水或蒸汽注入在所述爆炸室中产生的燃烧产物中的装置; 以及用于将由所述爆震室中的爆震产生的能量转换为电能的装置。

    Pulse detonation synthesis
    8.
    发明授权
    Pulse detonation synthesis 失效
    脉冲爆震综合

    公开(公告)号：US5855827A

    公开(公告)日：1999-01-05

    申请号：US613194

    申请日：1996-03-08

    申请人： Thomas R. A. Bussing ,  Joseph M. Ting

    发明人： Thomas R. A. Bussing ,  Joseph M. Ting

    IPC分类号： B01J3/08 ,  B05B7/00 ,  C23C4/12 ,  F01D5/28 ,  F02K7/06 ,  F02K7/075 ,  F02K9/97 ,  B29B9/00 ,  B05D1/36

    CPC分类号： B01J3/08 ,  B05B7/0006 ,  C23C4/126 ,  F01D5/288 ,  F02K7/06 ,  F02K7/075 ,  F02K9/972 ,  F02K9/974

    摘要： A Pulse Detonation Synthesis (PDS) process for the manufacture and deposition of ceramic powders and coatings is disclosed. PDS may use multiple detonation pulses that are initiated in a reaction chamber to synthesize ceramic materials from reactants introduced into the chamber. The reactants may be provided in the form of divided solids, gases, liquids, gels, and/or mixtures of the foregoing. The synthesized ceramic materials may take the form of micron and/or nano-scale powders or coatings. Non-coating powders may be collected for later use. The coatings produced by the present invention include, but are not limited to, gradient coatings, uniform coatings, thermal barrier coatings, and other commercially useful coatings.

    摘要翻译： 公开了用于制造和沉积陶瓷粉末和涂层的脉冲爆震合成（PDS）方法。 PDS可以使用在反应室中引发的多个引爆脉冲，以从引入室中的反应物合成陶瓷材料。 反应物可以以分开的固体，气体，液体，凝胶和/或前述物质的混合物的形式提供。 合成的陶瓷材料可以采取微米和/或纳米级粉末或涂层的形式。 可以收集非涂层粉末供以后使用。 由本发明生产的涂层包括但不限于梯度涂层，均匀涂层，热障涂层和其它商业上有用的涂层。