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61. 发明公开

EP1710156A3 Conformal aero-adaptive nozzle / aftbody 失效
标题翻译：空气动力学自适应地调整出口部或后部
公开(公告)号：EP1710156A3
公开(公告)日：2011-08-17
申请号：EP06425228.1
申请日：2006-04-03
申请人： Lockheed Martin Corporation
发明人： Miller, Daniel N. , Young, David D.
IPC分类号： B64C23/04 , F15D1/12 , B64C21/04
CPC分类号： F15D1/12 , B64C21/04 , B64C23/00 , B64C23/04 , B64C2230/18 , Y02T50/166
摘要： The present invention provides flow field control techniques that adapt the aft body region flow field to eliminate or mitigate the development of massive separated flow field zones and associated unsteady vortical flow field structures. Embodiments of the present invention use one or more distributed arrays of flow control devices (submerged in the boundary layer) to create disturbances in the flow field that inhibit the growth of larger vortical structures and/or to energize the aft body shear layer to keep the shear layer attached the aft body surface. These undesirable aerodynamic phenomena produce increased vehicle drag which harms vehicle range, persistence, and loiter capabilities. Additionally, the unsteady nature of the turbulent vortical structures shed in the aft body wake region may produce increased dynamic buffeting and aft body heating by entraining nozzle jet exhaust (a.k.a. jet wash) - requiring additional structural support, shielding, and vehicle weight.

62. 发明公开

EP2316729A2 An element for generating a fluid dynamic force 有权
标题翻译：用于产生流体动力的元素
公开(公告)号：EP2316729A2
公开(公告)日：2011-05-04
申请号：EP10182928.1
申请日：2006-07-13
申请人： City University
发明人： Prince, Simon , Khodagolian, Vahik
IPC分类号： B64C23/06
CPC分类号： B64C23/06 , B64C2230/06 , B64C2230/18 , B64C2230/20 , F03D1/0641 , F05D2240/30 , Y02E10/721 , Y02T50/162 , Y02T50/166
摘要： This invention relates to an element (11) for generating a fluid dynamic force, the element (11) comprising first (13) and second (15) surfaces extending in opposite directions from a leading edge (17) of the element (11) and meeting at a trailing edge (18) thereof to define a three dimensional body that is shaped to generate a fluid dynamic force when immersed at an angle of attack α to a fluid flow over the element (11) in a flow direction U, the first surface (13) comprising an array of fluid inlets (19) and the second surface (15) comprising a corresponding array of fluid outlets (21), each said inlet (19) being fluidly coupled to a said outlet (21) by means of a fluid duct (23) at least part of which is pitched at an angle θ to a tangent plane (Y—Y) to said second surface (15) in the vicinity of said outlet (21) and skewed at an angle ϕ to said fluid flow direction U, the arrangement being such that the element (11) is operable in use to generate a relatively high fluid pressure region downstream of said leading edge (17) proximate said first surface (13) and a relatively low fluid pressure region downstream of said leading edge (17) proximate said second surface (15), and fluid from said relatively high fluid pressure region is enabled to flow into said fluid inlets (19) through said fluid ducts (23) and out of said fluid outlets (21) into said relatively low pressure region to generate fluid vortices which reenergise said low pressure region and delay boundary layer separation from said second surface (15).
摘要翻译：本发明涉及用于产生流体动力的元件（11），元件（11）包括从元件（11）的前缘（17）沿相反方向延伸的第一表面（13）和第二表面（15），以及在其后缘（18）处相遇以限定三维主体，所述三维主体被成形为当以在流动方向U上的元件（11）上的流体流以迎角α浸入时产生流体动力，第一包括流体入口（19）阵列的第一表面（13）和包括流体出口（21）的相应阵列的第二表面（15），每个所述入口（19）通过流体连接到所述出口流体通道（23），其至少一部分相对于在所述出口（21）附近的所述第二表面（15）的切平面（Y-Y）以角度θ倾斜并且以与所述出口流体流动方向U，该布置使得元件（11）在使用中可操作以产生相对较高的流体压力在所述前缘（17）的靠近所述第一表面（13）的下游和在所述前缘（17）的靠近所述第二表面（15）的下游的相对较低的流体压力区域，并且来自所述较高流体压力区域的流体是能够通过所述流体通道（23）流入所述流体入口（19）并流出所述流体出口（21）进入所述较低压力区域，从而产生流体涡流，所述流体涡流重新激励所述低压区域并延迟边界层与所述第二表面（15）。

63. 发明公开

EP2086831A2 DISPOSITIF POUR RETARDER LE DECOLLEMENT D'UNE COUCHE LIMITE 有权
标题翻译：设备多延迟赎回接口作者：
公开(公告)号：EP2086831A2
公开(公告)日：2009-08-12
申请号：EP07866478.6
申请日：2007-10-31
申请人： Centre National de la Recherche Scientifique
发明人： STANISLAS, Michel , FOUCAUT, Jean-Marc , KOSTAS, Dimitrios , DYMENT, Arthur
IPC分类号： B64C21/04
CPC分类号： B64C21/08 , B64C21/04 , B64C2230/04 , B64C2230/06 , B64C2230/18 , F15D1/12 , Y02T50/166
摘要： The invention relates to a device for delaying the separation of a boundary layer in a flow of air (10) on a wall (12), including holes (14) formed in the wall (12) and connected to compressed air supply valves (18) by means of channels (16), the frequency of the valve opening and closing cycles and the valve opening duration being selected so as to generate peak output velocities from the holes (14), which occur in quasi-continuous succession. The invention is particularly suitable for aircraft wings and motor vehicle bodies.

64. 发明公开

EP1931566A2 OSCILLATING VANE ACTUATOR APPARATUS AND METHOD FOR ACTIVE FLOW CONTROL 有权
标题翻译：摆动FOR主动流动控制刀片交换机的设备和方法
公开(公告)号：EP1931566A2
公开(公告)日：2008-06-18
申请号：EP06851665.7
申请日：2006-07-26
申请人： The Boeing Company
发明人： POWELL, Arthur G.
IPC分类号： B64C21/02
CPC分类号： B64C21/025 , B64C2230/04 , B64C2230/06 , B64C2230/18 , Y02T50/166
摘要： An oscillating vane actuator for active control of fluid flow over a surface (24) includes a pivoted vane (16) surrounded by a wedge-shaped chamber (18), and first (20) and second (26) conduits with openings adjacent the surface (24). The actuator also includes a rotating shaft with a connecting rod to actuate the vane (16) in a oscillatory manner.' As the vane (16) travels in one direction, fluid is forced out from the chamber through the first conduit (20) and opening (22) into the fluid stream adjacent the surface, while fluid is simultaneously drawn in through the second opening (28) and conduit (26) into the opposite side of the chamber (18). Similarly, when the vane (16) travels in the opposite direction, fluid is forced out through the second conduit (26) and opening (28) into the fluid stream adjacent the surface (24), while fluid is simultaneously drawn in through the first opening (22) and conduit (24).

65. 发明授权

EP1040736B1 SYNTHETIC JET ACTUATORS FOR COOLING HEATED BODIES AND ENVIRONMENTS 有权
标题翻译：对于一个曼·雷按钮冷却加热型机构和ENVIRONMENTS
公开(公告)号：EP1040736B1
公开(公告)日：2007-02-07
申请号：EP98957870.3
申请日：1998-11-12
申请人： GEORGIA TECH RESEARCH CORPORATION
发明人： GLEZER, Ari , ALLEN, Mark, G.
IPC分类号： H05K1/11 , H05K1/14
CPC分类号： F21V29/70 , B64C21/08 , B64C2230/02 , B64C2230/04 , B64C2230/06 , B64C2230/14 , B64C2230/16 , B64C2230/18 , B64G1/26 , B64G1/40 , B64G1/401 , F01D5/148 , F02K1/28 , F15C1/14 , F15C5/00 , F15D1/009 , F15D1/08 , F15D1/12 , F16K99/0001 , F16K99/0007 , F16K99/0034 , F16K99/0048 , F16K2099/0094 , F16K2099/0098 , F21V29/677 , F21V29/74 , F21V29/83 , F23R3/24 , F28F13/02 , H01L23/4336 , H01L2924/0002 , H01L2924/3011 , H05K7/20172 , Y02T50/166 , H01L2924/00
摘要： Briefly described, the present invention is concerned with cooling heated bodies and/or heated fluid with synthetic jet actuators in either open or closed systems. A first preferred embodiment of a cooling system of the present invention comprises a synthetic jet actuator directed to impinge directly on a heat producing (or heated) body. The synthetic jet actuator generates a synthetic jet stream comprised of cool ambient fluid that impinges on the heated surface thereby cooling this surface. As an example, the heated surface/body could be a microchip array in a microcomputer. After coming into contact with the heated surface, the fluid moves along the surface and is finally rejected to the ambient where it mixes and cools down. The synthetic jet may be incorporated into a modular unit that may be clipped on to a circuit board or other heat producing element to provide added, 'ad hoc' cooling. In another configuration, a synthetic jet actuator may be positioned, relative to the heated surface, to create a synthetic jet stream to flow along the heated surface. In this embodiment, the flow would be approximately tangential to a surface of a heat producing body. This embodiment may further comprise a cyclical flow of the fluid jet, along the heated body and about a heat sink surface.

66. 发明公开

EP1710156A2 Conformal aero-adaptive nozzle / aftbody 失效
标题翻译：适形的空气自适应喷嘴/尾部体
公开(公告)号：EP1710156A2
公开(公告)日：2006-10-11
申请号：EP06425228.1
申请日：2006-04-03
申请人： Lockheed Martin Corporation
发明人： Miller, Daniel N. , Young, David D.
IPC分类号： B64C23/04 , F15D1/12
CPC分类号： F15D1/12 , B64C21/04 , B64C23/00 , B64C23/04 , B64C2230/18 , Y02T50/166
摘要： The present invention provides flow field control techniques that adapt the aft body region flow field to eliminate or mitigate the development of massive separated flow field zones and associated unsteady vortical flow field structures. Embodiments of the present invention use one or more distributed arrays of flow control devices (submerged in the boundary layer) to create disturbances in the flow field that inhibit the growth of larger vortical structures and/or to energize the aft body shear layer to keep the shear layer attached the aft body surface. These undesirable aerodynamic phenomena produce increased vehicle drag which harms vehicle range, persistence, and loiter capabilities. Additionally, the unsteady nature of the turbulent vortical structures shed in the aft body wake region may produce increased dynamic buffeting and aft body heating by entraining nozzle jet exhaust (a.k.a. jet wash) - requiring additional structural support, shielding, and vehicle weight.
摘要翻译：本发明提供流场控制技术，其适应尾部本体区域流场以消除或减轻块状分离流场区域和相关联的不稳定涡流流场结构的发展。本发明的实施例使用流控制装置的一个或多个分布式阵列（浸没在边界层中）以在流场中产生干扰，其抑制较大涡旋结构的生长和/或激励后体剪切层以保持剪切层附接在尾部本体表面上。这些不合要求的空气动力学现象会产生增加的车辆阻力，从而损害车辆的行驶范围，持久性和空闲能力。此外，尾部尾部尾流区域中的湍流旋涡结构的不稳定性质可通过夹带喷嘴喷射排气（也称为喷射清洗）产生增加的动态抖振和尾部本体加热 - 需要额外的结构支撑，屏蔽和车辆重量。

67. 发明公开

EP1544089A1 A motor vehicle with a device for controlling aerodynamic flow using synthetic jets 有权
标题翻译： Kraftfahrzeug mit einer Kontrollanlagefürdie airodynamischeStrömung，mittels synthetischen Jets
公开(公告)号：EP1544089A1
公开(公告)日：2005-06-22
申请号：EP04028097.6
申请日：2004-11-26
申请人： C.R.F. Società Consortile per Azioni
发明人： Casella, Mauro , Tregnago, Roberto
IPC分类号： B62D37/02 , B62D35/00
CPC分类号： B62D35/001 , B62D37/02 , B64C2230/02 , B64C2230/18 , Y02T50/166
摘要： A motor vehicle has: at least one portion of external surface with one or more openings (1); and an internal cavity communicating with said opening or openings, and delimited at least in part by one or more mobile elements. Actuator means displace each mobile element between two operative positions so as to vary cyclically the volume of said internal cavity for the purpose of generating one or more jets of air (J), pulsed at a pre-set or controlled frequency (synthetic jets), which interact with the flow of air that laps the bodywork of the motor vehicle causing it to change its aerodynamic characteristics.
摘要翻译：机动车辆具有：具有一个或多个开口（1）的至少一部分外表面; 以及与所述开口或开口连通并且至少部分地由一个或多个移动元件限定的内部空腔。致动器意味着使每个移动元件在两个操作位置之间移位，以便周期性地改变所述内部空腔的体积，以便产生以预设或受控频率（合成射流）脉冲的一个或多个空气射流（J）这与空气流动相互作用，使得机动车辆的车身导致其改变其空气动力特性。

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