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1.发明授权Nozzle plasma flow control utilizing dielectric barrier discharge plasma actuators 失效使用介质阻挡放电等离子体致动器的喷嘴等离子体流量控制公开(公告)号：US08453457B2
公开(公告)日：2013-06-04
申请号：US12547635
申请日：2009-08-26
IPC分类号： F02K1/46
CPC分类号： F02K1/386 , F02K1/46 , F02K9/80 , F05D2250/323 , F05D2250/324 , F05D2260/962 , F05D2270/172
摘要： Dielectric barrier discharge plasma actuators are used to manipulate exhaust flow within and behind a jet engine nozzle. The dielectric barrier discharge plasma actuators may be used to direct cooling airflow near the surface of the nozzle to reduce heating of the nozzle, create thrust vectoring, and reduce noise associated with the exhaust flow exiting the nozzle.
摘要翻译： 介质阻挡放电等离子体致动器用于操纵喷气发动机喷嘴内部和之后的排气流。 电介质阻挡放电等离子体致动器可以用于引导喷嘴表面附近的冷却气流，以减少喷嘴的加热，产生推力矢量化，并减少与离开喷嘴的排气流相关的噪声。
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2.发明申请NOZZLE PLASMA FLOW CONTROL UTILIZING DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATORS 失效喷嘴等离子体流量控制器采用电磁障碍物放电等离子体激光器公开(公告)号：US20110048025A1
公开(公告)日：2011-03-03
申请号：US12547635
申请日：2009-08-26
CPC分类号： F02K1/386 , F02K1/46 , F02K9/80 , F05D2250/323 , F05D2250/324 , F05D2260/962 , F05D2270/172
摘要： Dielectric barrier discharge plasma actuators are used to manipulate exhaust flow within and behind a jet engine nozzle. The dielectric barrier discharge plasma actuators may be used to direct cooling airflow near the surface of the nozzle to reduce heating of the nozzle, create thrust vectoring, and reduce noise associated with the exhaust flow exiting the nozzle.
摘要翻译： 介质阻挡放电等离子体致动器用于操纵喷气发动机喷嘴内部和之后的排气流。 电介质阻挡放电等离子体致动器可以用于引导喷嘴表面附近的冷却气流，以减少喷嘴的加热，产生推力矢量化，并减少与离开喷嘴的排气流相关的噪声。
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3.发明申请SYSTEM, METHOD AND APPARATUS FOR VECTORING NOZZLE EXHAUST PLUME WITH EXTERNAL ACTUATION 有权用于外部执行喷嘴喷嘴的系统，方法和装置公开(公告)号：US20100089031A1
公开(公告)日：2010-04-15
申请号：US12249059
申请日：2008-10-10
CPC分类号： F02K1/28 , F02K1/08 , F02K1/10 , F02K1/1207 , F02K1/30 , Y02T50/671
摘要： A vectoring nozzle with external actuation generates thrust vectoring by applying mechanical or fluidic actuation, or both, on the nozzle deck, external sidewalls, and/or air vehicle aft body to produce changes in the aft body flowfield and/or exhaust plume. An external mechanical sidewall may be integrated into a nozzle deck or side walls without the need for engine bleed to supply fluid injectors. An external fluidic vectoring system uses injectors or plasma devices located aft of the nozzle exit to vector the exhaust plume with no external moving parts. Elements of both mechanical and fluidic systems may be combined for a given application.
摘要翻译： 具有外部致动的矢量喷嘴通过在喷嘴甲板，外侧壁和/或空气车身后部施加机械或流体致动或两者来产生推力矢量，从而产生尾部身体流场和/或排气羽流的变化。 外部机械侧壁可以集成到喷嘴面板或侧壁中，而不需要发动机排出以供应流体喷射器。 外部流体矢量化系统使用位于喷嘴出口后部的喷射器或等离子体装置，以便在没有外部移动部件的情况下对排气羽流进行矢量化。 机械和流体系统的元件可以针对给定的应用进行组合。
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4.发明授权公开(公告)号：US08408281B2
公开(公告)日：2013-04-02
申请号：US11872165
申请日：2007-10-15
CPC分类号： B64D13/00 , B64D2013/0674 , Y02T50/44 , Y02T50/56
摘要： A pulsed-jet active flowfield control actuation system enhances the rate of heat transfer and heat removal in a heat exchanger for better management of thermal loads. The pulsed jet actuators impart an unsteady component of velocity to the working fluid of the heat exchanger. This design increases the convective heat transfer, and avoids increases in heat exchanger volume and weight for a given performance value.
摘要翻译： 脉冲喷射主动流场控制致动系统提高热交换器中的传热速率和散热速率，从而更好地管理热负荷。 脉冲喷射致动器对热交换器的工作流体施加不稳定的速度分量。 这种设计增加了对流传热，并避免了给定性能值的热交换器体积和重量的增加。
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5.发明授权System, method, and apparatus for control input prediction and state verification of fluidic vectoring exhaust in high performance aircraft 有权用于控制输入预测和高性能飞机中流体矢量排气状态验证的系统，方法和装置公开(公告)号：US08065868B2
公开(公告)日：2011-11-29
申请号：US11615050
申请日：2006-12-22
申请人： Rob S. Burgun , Kerry B. Ginn , Daniel N. Miller
发明人： Rob S. Burgun , Kerry B. Ginn , Daniel N. Miller
CPC分类号： F02K1/15 , B64C15/02 , F02K1/008 , F02K1/28 , F05D2270/051 , F05D2270/301
摘要： A non-invasive system, method, and apparatus for control input prediction and state verification of an aircraft's fluidic vectoring exhaust is disclosed. The control system derives a desired vector state, then predicts and sets the fluidic injection input required to produce the desired vector state. A vectored state verification routine is used to determine the resulting vector state for feedback to the control system.
摘要翻译： 公开了一种用于控制输入预测和飞机的流体矢量化排气的状态验证的非侵入性系统，方法和装置。 控制系统导出所需的矢量状态，然后预测并设定产生所需矢量状态所需的流体注入输入。 矢量状态验证程序用于确定所得矢量状态以反馈给控制系统。
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6.发明授权公开(公告)号：US08371104B2
公开(公告)日：2013-02-12
申请号：US12249059
申请日：2008-10-10
IPC分类号： F02K1/28
CPC分类号： F02K1/28 , F02K1/08 , F02K1/10 , F02K1/1207 , F02K1/30 , Y02T50/671
摘要： A vectoring nozzle with external actuation generates thrust vectoring by applying mechanical or fluidic actuation, or both, on the nozzle deck, external sidewalls, and/or air vehicle aft body to produce changes in the aft body flowfield and/or exhaust plume. An external mechanical sidewall may be integrated into a nozzle deck or side walls without the need for engine bleed to supply fluid injectors. An external fluidic vectoring system uses injectors or plasma devices located aft of the nozzle exit to vector the exhaust plume with no external moving parts. Elements of both mechanical and fluidic systems may be combined for a given application.
摘要翻译： 具有外部致动的矢量喷嘴通过在喷嘴甲板，外侧壁和/或空气车身后部施加机械或流体致动或两者来产生推力矢量，从而产生尾部身体流场和/或排气羽流的变化。 外部机械侧壁可以集成到喷嘴面板或侧壁中，而不需要发动机排出以供应流体喷射器。 外部流体矢量化系统使用位于喷嘴出口后部的喷射器或等离子体装置，以便在没有外部移动部件的情况下对排气羽流进行矢量化。 机械和流体系统的元件可以针对给定的应用进行组合。
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公开(公告)号：US20090095446A1
公开(公告)日：2009-04-16
申请号：US11872165
申请日：2007-10-15
IPC分类号： F28D15/00
CPC分类号： B64D13/00 , B64D2013/0674 , Y02T50/44 , Y02T50/56
摘要： A pulsed-jet active flowfield control actuation system enhances the rate of heat transfer and heat removal in a heat exchanger for better management of thermal loads. The pulsed jet actuators impart an unsteady component of velocity to the working fluid of the heat exchanger. This design increases the convective heat transfer, and avoids increases in heat exchanger volume and weight for a given performance value.
摘要翻译： 脉冲喷射主动流场控制致动系统提高热交换器中的传热速率和散热速率，从而更好地管理热负荷。 脉冲喷射致动器对热交换器的工作流体施加不稳定的速度分量。 这种设计增加了对流传热，并避免了给定性能值的热交换器体积和重量的增加。
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8.发明授权Method and apparatus of asymmetric injection into subsonic flow of a high aspect ratio/complex geometry nozzle 有权不对称注入到高纵横比/复数几何喷嘴的亚音速流中的方法和装置公开(公告)号：US06962044B1
公开(公告)日：2005-11-08
申请号：US09621795
申请日：2000-07-21
摘要： The present invention reveals a method and apparatus for controlling the effective area and thrust vector angle of a fluid flow. In one embodiment, the fluid flow is controlled in an advanced, high aspect ratio, complex aperture geometry nozzle using asymmetric injection into the subsonic portion of the fluid flow. The present invention vectors the primary flow by partially blocking the flow with an opposed flow across the flow field. A fluidic flow field is defined in a flow container that directs a pressurized, primary fluidic flow from the container towards an exit of the container. A nozzle may cooperate with the exit of the flow container to control the fluidic flow as it exits the flow container. One or more injectors associated with the container are proximate to the effect throat of the primary flow while other are located downstream of to introduce an opposing fluidic flow that interacts with the primary fluidic flow. A controller associated with the injectors directs the injectors to provide the opposing flow as needed to achieve a desired partial blockage of the primary flow, thereby vectoring the primary flow.
摘要翻译： 本发明揭示了一种用于控制流体流动的有效面积和推力矢量角的方法和装置。 在一个实施例中，使用对流体流的亚音速部分的不对称注入，将流体流控制在先进的高纵横比的复合孔径几何喷嘴中。 本发明通过跨过流场的相对流部分地阻断流动来对主流进行矢量化。 在流动容器中限定流体流场，其将来自容器的加压的初级流体流引导到容器的出口。 喷嘴可以与流动容器的出口配合，以在流体流动离开流动容器时控制流体流动。 与容器相关联的一个或多个注射器靠近主流的效应，而另一个位于下游，以引入与主流体流相互作用的相反的流体流。 与注射器相关联的控制器引导喷射器以根据需要提供相对的流动，以实现初级流的期望的部分阻塞，从而对主流进行矢量化。
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9.发明申请SYSTEM, METHOD, AND APPARATUS FOR CONTROL INPUT PREDICTION AND STATE VERIFICATION OF FLUIDIC VECTORING EXHAUST IN HIGH PERFORMANCE AIRCRAFT 有权用于控制输入预测的系统，方法和装置以及高性能飞机中的流体检测排气的状态验证公开(公告)号：US20080149742A1
公开(公告)日：2008-06-26
申请号：US11615050
申请日：2006-12-22
申请人： Rob S. Burgun , Kerry B. Ginn , Daniel N. Miller
发明人： Rob S. Burgun , Kerry B. Ginn , Daniel N. Miller
IPC分类号： F02K1/15
CPC分类号： F02K1/15 , B64C15/02 , F02K1/008 , F02K1/28 , F05D2270/051 , F05D2270/301
摘要： A non-invasive system, method, and apparatus for control input prediction and state verification of an aircraft's fluidic vectoring exhaust is disclosed. The control system derives a desired vector state, then predicts and sets the fluidic injection input required to produce the desired vector state. A vectored state verification routine is used to determine the resulting vector state for feedback to the control system.
摘要翻译： 公开了一种用于控制输入预测和飞机的流体矢量化排气的状态验证的非侵入性系统，方法和装置。 控制系统导出所需的矢量状态，然后预测并设定产生所需矢量状态所需的流体注入输入。 矢量状态验证程序用于确定所得矢量状态以反馈给控制系统。
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公开(公告)号：US06308740B1
公开(公告)日：2001-10-30
申请号：US09639187
申请日：2000-08-15
IPC分类号： E03B500
CPC分类号： F02C9/50 , F02C7/04 , F04B45/04 , F04F5/16 , F04F5/54 , Y10T137/87619 , Y10T137/87652
摘要： The present invention reveals a method and apparatus for more efficiently injecting a primary fluid flow in a fluid ejector used to pump lower velocity fluid from a secondary source. In one embodiment, the primary fluid flow is a pulsed or unsteady fluid flow contained within an inner nozzle situated within a secondary flow field. This secondary fluid flow is bounded within the walls of an ejector or shroud. The secondary and primary fluid flows meet within the ejector shroud section wherein the secondary fluid flow is entrained by the primary fluid flow. The geometry of the ejector shroud section where the primary and secondary fluids mix is such as to allow the beginning of primary injector pulse to be synchronized with an acoustic wave moving upstream through the ejector initiated by the exiting of the previous pulse from the ejector shroud. The ejector's geometric properties are determined by the acoustic properties, frequency, duty cycle, and amplitude, of the pulsed primary fluid flow. Furthermore, the frequency, duty cycle and amplitude of the primary fluid flow may be varied in order to vary the efficiency of the injector.
摘要翻译： 本发明揭示了一种用于在用于从次级源泵送较低速度流体的流体喷射器中更有效地喷射主流体流的方法和装置。 在一个实施例中，主流体流是包含在位于二次流场内的内部喷嘴内的脉冲或不稳定流体流。 该次级流体流动在喷射器或护罩的壁内。 次级和初级流体流动在喷射器护罩部分内相交，其中次流体流被主流体流动夹带。 初级和次级流体混合的喷射器护罩部分的几何形状允许初级喷射器脉冲的开始与通过喷射器的上游移动的声波同步，该喷射器由从喷射器护罩的先前脉冲的离开开始。 喷射器的几何特性由脉冲初级流体流的声学特性，频率，占空比和幅度决定。 此外，可以改变初级流体流的频率，占空比和幅度，以改变喷射器的效率。
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