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    Strain amplification structure and synthetic jet actuator
    1.
    发明公开
    Strain amplification structure and synthetic jet actuator 审中-公开
    应变放大结构和合成射流执行器

    公开(公告)号：EP2674721A3

    公开(公告)日：2017-11-01

    申请号：EP13171193.9

    申请日：2013-06-10

    申请人： The Boeing Company

    发明人： Griffin, Steven F. ,  Haar, Shawn

    IPC分类号： G01C19/00 ,  G01P15/00 ,  G01L1/00

    CPC分类号： H01L41/09 ,  B64C21/04 ,  B64C21/08 ,  B64C2230/04 ,  B64C2230/06 ,  B64C2230/18 ,  H01L41/053 ,  H01L41/25 ,  H02N2/043 ,  Y02T50/166 ,  Y10T29/42

    摘要： A strain amplification structure has a frame with a hexagonal structure incorporating a plurality of rigid beams (16a) that are connected to opposing end beams by a plurality of flexible joints (24). A piezoceramic actuator assembly (26) is connected to the opposing end beams having a collar (32)including an opening. A shaft (18) providing an output is connected to the plurality of rigid beams with flexible joints and passes through the opening in the collar (32) for non-interfering motion orthogonal to the actuator assembly.

    摘要翻译： 应变放大结构具有六边形结构的框架，所述六边形结构包括多个刚性梁（16a），多个刚性梁通过多个柔性接头（24）连接到相对的端梁。 压电陶瓷致动器组件（26）连接到具有包括开口的轴环（32）的相对端梁。 提供输出的轴（18）通过柔性接头连接到多个刚性梁并且穿过轴环（32）中的开口，用于与致动器组件正交的非干涉运动。

    Externally driven flow control actuator
    5.
    发明公开
    Externally driven flow control actuator 审中-公开
    外部驱动流量控制执行器

    公开(公告)号：EP2722275A2

    公开(公告)日：2014-04-23

    申请号：EP13188983.4

    申请日：2013-10-16

    申请人： The Boeing Company

    发明人： Raghu, Surya

    IPC分类号： B64C21/04

    CPC分类号： B64C21/04 ,  B64C21/08 ,  B64C2230/04 ,  B64C2230/06 ,  B64C2230/18 ,  F15D1/008 ,  F15D1/12 ,  Y02T50/166

    摘要： A method and apparatus for managing a flow of a fluid. The fluid is received at an input port (206) of a structure (204). The fluid is sent through a chamber (210) in communication with the input port (206). The fluid is caused to flow from the chamber (210) and out of an output (208) port in a direction that changes with a frequency based on an application of pressure pulses in the chamber (210).

    摘要翻译： 一种用于管理流体流动的方法和设备。 流体在结构（204）的输入端口（206）处被接收。 流体通过与输入端口（206）连通的腔室（210）被发送。 使流体从腔室（210）流出并且以基于腔室（210）中的压力脉冲的施加的频率而改变的方向流出输出（208）端口。

    An element for generating a fluid dynamic force
    6.
    发明公开
    An element for generating a fluid dynamic force 有权
    元素zum Erzeugen einer dynamischenFlüssigkeitskraft

    公开(公告)号：EP2316729A3

    公开(公告)日：2011-11-02

    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（13）和第二（15）表面，以及 在其后缘（18）处会合以限定三维体，其被成形为当以冲击角度向流体方向U上的元件（11）上的流体流动浸入时产生流体动力，第一 表面（13）包括一组流体入口（19），第二表面（15）包括相应的流体出口（21）阵列，每个所述入口（19）通过以下方式流体连接到所述出口（21） 流体管道（23），其至少一部分在所述出口（21）附近与所述第二表面（15）成角度θ相对于切平面（Y“Y”）倾斜并以Õ至 所述流体流动方向U，所述布置使得所述元件（11）在使用中可操作以产生相对较高的流体流量 靠近所述第一表面（13）的所述前缘（17）下游的基部区域和靠近所述第二表面（15）的所述前缘（17）下游的相对低的流体压力区域，并且来自所述相对高的流体压力区域的流体是 能够通过所述流体管道（23）流入所述流体入口（19）并且从所述流体出口（21）流入所述相对低压区域以产生流体涡流，其使所述低压区域重新通电并延迟边界层与所述第二 表面（15）。

    STRÖMUNGSKÖRPER UND HOCHAUFTRIEBSSYSTEM MIT EINEM SOLCHEN STRÖMUNGSKÖRPER
    7.
    发明公开
    STRÖMUNGSKÖRPER UND HOCHAUFTRIEBSSYSTEM MIT EINEM SOLCHEN STRÖMUNGSKÖRPER 有权
    流动体和这样的车身流大升力系统

    公开(公告)号：EP2268541A2

    公开(公告)日：2011-01-05

    申请号：EP09731423.1

    申请日：2009-04-07

    申请人： Airbus Operations GmbH

    发明人： LORKOWSKI, Thomas

    IPC分类号： B64C21/02 ,  B64C21/08

    CPC分类号： B64C21/04 ,  B64C21/08 ,  B64C2230/04 ,  B64C2230/06 ,  B64C2230/18 ,  B64C2230/22 ,  Y02T50/166

    摘要： Disclosed is a flow element (1) comprising an external side (3) that has a top face (3a) and a bottom face (3b) in relation to the direction of flow, and lateral end sections (5a, 5b) that form the lateral ends of the flow element (1) transversal to the theoretical direction of flow (S). A duct (10) is arranged inside the flow element (1). Said duct (10) encompasses a flow drive with a driving motor and a compressor means which is driven by the driving motor and is disposed in the duct (10). The duct (10) has at least one inlet (11) on the bottom face (3b) and/or on at least one of the lateral end sections (5a, 5b) of the flow element (1) as well as an outlet (12) on the top face (3a) of the flow element (1) in order to influence the flow on the flow element (1). A sleeve (30) that can be rotated by means of the driving motor is located inside the duct (10). Said sleeve (30) has at least one cavity (33) which can be made to at least partially overlap with the outlet (12) on the top face (3a) of the flow element (1) in a specific rotational position of the sleeve (30) such that the air that is compressed by the compressor flows through the cavity (33) of the sleeve (30) and the outlet (12). A high-lift system comprising such a flow element is also disclosed.

    SYNTHETIC JET ACTUATORS FOR COOLING HEATED BODIES AND ENVIRONMENTS
    10.
    发明公开
    SYNTHETIC JET ACTUATORS FOR COOLING HEATED BODIES AND ENVIRONMENTS 有权
    对于一个曼·雷按钮冷却加热型机构和ENVIRONMENTS

    公开(公告)号：EP1040736A1

    公开(公告)日：2000-10-04

    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.

    摘要翻译： 简单地说，本发明涉及冷却加热体和/或加热的流体在开放或封闭系统中的合成射流致动器。 本发明的冷却系统的第一优选实施方案包括定向到上的产热（或加热）的身体直接撞击的合成射流致动器。 合成射流致动器基因率的合成射流流由冷的环境流体的加热表面，从而冷却该表面上没有撞击。 如在实施例中，加热的表面/体可能是在微型计算机的微型芯片阵列。 进入与加热的表面接触后，沿所述表面和所述流体移动最终拒绝到其混合并冷却周围环境。 合成射流可以被合并到一个模块单元并可以被夹到一个电路板或其它热产生元件以提供附加的，“特定”的冷却。 在另一配置中，合成射流致动器可以被定位，相对于加热表面，以创建一个合成射流流沿着加热表面流动。 在此，流动将是实施例大约相切于产热体的表面。 这可能实施例还包括将流体射流的一个周期性流，沿被加热体和有关的散热器表面。