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1. 发明公开

EP3290333A1 FLUIDAKTUATOR MIT STRAHLVEKTORKONTROLLE UND STRÖMUNGSKÖRPER 审中-公开
标题翻译：带有横梁矢量控制和流体的流体致动器
公开(公告)号：EP3290333A1
公开(公告)日：2018-03-07
申请号：EP16187248.6
申请日：2016-09-05
申请人： Airbus Defence and Space GmbH
发明人： Meyer, Michael , Bauer, Matthias
IPC分类号： B64C21/02 , B64C21/08
CPC分类号： B64C21/025 , B64C5/02 , B64C9/16 , B64C21/08 , B64C2230/04 , B64C2230/06 , B64C2230/20 , Y02T50/166
摘要： Die vorliegende Erfindung beschreibt einen Fluidaktuator (1) zur Beeinflussung einer Strömung eines Umgebungsfluids entlang einer Strömungsoberfläche (100a), mit einem Ausblaskanal (10) zur Verbindung mit einer Druckfluidquelle (240) und mit einer in der Strömungsoberfläche (100a) ausgebildeten Oberflächenausblasöffnung (110) und einem Ansaugkanal (20) zum Anschluss an eine in der Strömungsoberfläche (100a) ausgebildete Oberflächenansaugöffnung (120), wobei der Ansaugkanal (20) an einer Entrainmentöffnung (22A) in den Ausblaskanal (10) einmündet. Ferner ist ein Strömungskörper (100) mit einem Fluidaktuator (1) beschrieben.
摘要翻译：本发明描述了一种流体致动器（1）用于影响周围的流体的流动沿着流动表面（100A），具有用于连接到加压流体（240）的源极的吹出通道（10），并用一个在流动表面（100A）形成Oberflächenausblasöffnung（110）并形成有用于在所述流动表面（100A）连接到进气通道（20）Oberflächenansaugöffnung（120），其中，所述进气导管（20）在所述吹出通道一个Entrainmentöffnung（22A）（10）打开。此外，描述了具有流体致动器（1）的流动体（100）。

2. 发明授权

EP2516264B1 OSCILLATORY VORTICITY GENERATOR AND APPLICATIONS THEREOF 有权
标题翻译：摆动涡发生器及其应用
公开(公告)号：EP2516264B1
公开(公告)日：2016-11-02
申请号：EP10796151.8
申请日：2010-11-23
申请人： Ramot at Tel Aviv University, Ltd.
发明人： SEIFERT, Avraham , STALNOV, Oksana , FONO, Ilan , DAYAN, Isaac , TROSHIN, Victor , AVNAIM, Maor Hai , PALEI, Vitali
IPC分类号： B64C21/02 , F03D1/06
CPC分类号： B64C21/025 , B64C2230/02 , B64C2230/28 , F01D5/145 , F03D1/06 , F05B2240/122 , F05D2240/127 , Y02E10/721 , Y02T50/166 , Y02T50/671 , Y02T50/673

3. 发明授权

EP2893361B1 PANEL FOR CONTROLLING THE AERODYNAMIC PHENOMENA ON A BODY 有权转让
标题翻译： TAFEL ZUR STEUERUNG AERODYNAMISCHERPHÄNOMENENAN EINEMKÖRPER
公开(公告)号：EP2893361B1
公开(公告)日：2016-10-12
申请号：EP13803219.8
申请日：2013-08-30
申请人： LEONARDO S.P.A.
发明人： MARCHETTI, Danilo
IPC分类号： G01P13/02 , G01P5/165 , B64C21/02 , B64C1/00 , B64C1/40 , F15D1/12 , F15D1/00
CPC分类号： B64C1/0009 , B64C1/40 , B64C21/02 , B64C21/025 , B64C2230/22 , F15D1/0055 , F15D1/12 , G01P5/165 , G01P13/025 , Y02T50/166
摘要： A panel (3) for controlling the aerodynamic phenomena generated by a body (0) to be positioned on a surface of an aircraft (V). The panel (3) can be associated with the base of the body (0) and includes at least one inlet aperture (322) and at least one outlet aperture (322′) placed in communication with each other, through which a portion of a fluid flow (W) in which the body (0) is immersed can selectively pass. The inlet aperture (322) is located upstream of the body (0) and the outlet aperture (322′) is located downstream of the body (0), with respect to the direction of the fluid flow (W).
摘要翻译：一种用于控制由身体（0）产生以定位在飞行器（V）的表面上的空气动力学现象的面板（3）。面板（3）可以与主体（0）的底部相关联，并且包括至少一个入口孔（322）和至少一个彼此连通的出口孔（322'），通过该孔主体（0）浸入其中的流体流（W）可以选择性地通过。进口孔（322）位于主体（0）的上游，并且出口孔（322'）相对于流体流（W）的方向位于主体（0）的下游。

4. 发明公开

EP3020631A1 Aerodynamic component and method for producing an aerodynamic component 有权
标题翻译：空气动力学Bauteil und Verfahren zur Herstellung eines aerodynamisches Bauteils
公开(公告)号：EP3020631A1
公开(公告)日：2016-05-18
申请号：EP14192676.6
申请日：2014-11-11
申请人： Airbus Operations GmbH
发明人： Teich, Benjamin
IPC分类号： B64C21/02
CPC分类号： B64C21/025 , B32B1/00 , B32B3/266 , B32B3/28 , B32B3/30 , B32B5/02 , B32B5/18 , B32B5/22 , B32B5/245 , B32B5/26 , B32B7/045 , B32B7/12 , B32B15/14 , B32B15/18 , B32B15/20 , B32B2250/44 , B32B2260/021 , B32B2260/046 , B32B2262/101 , B32B2262/106 , B32B2307/558 , B32B2307/714 , B32B2307/724 , B32B2605/18 , Y02T50/166
摘要： An aerodynamic component (10) which in particular is suitable for use in an aircraft comprises an outer skin sheet (12) having an inner surface and an outer surface and being provided with a plurality of perforation openings (14) allowing a flow of air therethrough. The outer surface of the outer skin sheet (12) forms an aerodynamic surface of the aerodynamic component (10). The aerodynamic component (10) further comprises a sandwich panel (18) which includes an outer layer (20) facing the inner surface of the outer skin sheet (12), an inner layer (22) facing away from the inner surface of the outer skin sheet (12) and a foam core (24) sandwiched between the outer layer (20) and the inner layer (22). The sandwich panel (18) is provided with a plurality of connection openings (26) extending through the sandwich panel (18) between the outer layer (20) and the inner layer (22) and allowing a flow of air therethrough.
摘要翻译：特别适用于飞行器的空气动力学部件（10）包括具有内表面和外表面的外表皮片（12），并且设置有多个穿孔（14），允许空气流过其中。外皮片（12）的外表面形成空气动力学部件（10）的空气动力学表面。空气动力学组件（10）还包括夹层板（18），其包括面向外表层（12）的内表面的外层（20），内层（22）背向外表面表层片（12）和夹在外层（20）和内层（22）之间的泡沫芯（24）。夹层板（18）设置有多个连接开口（26），其延伸穿过位于外层（20）和内层（22）之间的夹层板（18）并允许空气流过其中。

5. 发明公开

EP2843244A3 Suppression of shock-induced airflow separation 有权
标题翻译：由冲击引起的抑制气流分离
公开(公告)号：EP2843244A3
公开(公告)日：2015-07-29
申请号：EP14178046.0
申请日：2014-07-22
申请人： Lockheed Martin Corporation
发明人： Baruzzini, Dan J. , Miller, Daniel N. , Domel, Neal D. , Hakes, Jeff G.
IPC分类号： F15D1/00 , B64C21/02
CPC分类号： F02C7/04 , B64C21/025 , B64D2033/0226 , B64D2033/026 , F15D1/0095 , Y02T50/166 , Y10T137/0318 , Y10T137/0536
摘要： An apparatus for suppressing shock-induced separation of high speed airflow from a relatively low-energy boundary layer. The apparatus may include an actuator or array of actuators configured to alternately inhale and exhale fluid and positioned to alternately inhale fluid from and exhale fluid into a boundary layer of a fluid mass flowing along the wall. The actuator may be positioned to inhale fluid from a boundary layer separation bubble induced by a supersonic shock wave propagated in the fluid mass.

6. 发明授权

EP2160324B1 WING ARRANGEMENT AND METHOD FOR INCREASING THE LIFT OF AERODYNAMIC SURFACES 有权
标题翻译：旋翼装置和方法加固气动表面浮力
公开(公告)号：EP2160324B1
公开(公告)日：2014-07-16
申请号：EP08719628.3
申请日：2008-03-10
申请人： Alenia Aermacchi S.p.A.
发明人： CATINO, Nicola Italo
IPC分类号： B64C21/02
CPC分类号： B64C21/025 , B64C2230/04 , Y02T50/166

7. 发明公开

EP2516264A1 OSCILLATORY VORTICITY GENERATOR AND APPLICATIONS THEREOF 有权
标题翻译：摆动涡发生器及其应用
公开(公告)号：EP2516264A1
公开(公告)日：2012-10-31
申请号：EP10796151.8
申请日：2010-11-23
申请人： Ramot at Tel Aviv University, Ltd.
发明人： SEIFERT, Avraham , STALNOV, Oksana , FONO, Ilan , DAYAN, Isaac , TROSHIN, Victor , AVNAIM, Maor Hai , PALEI, Vitali
IPC分类号： B64C21/02 , F03D1/06
CPC分类号： B64C21/025 , B64C2230/02 , B64C2230/28 , F01D5/145 , F03D1/06 , F05B2240/122 , F05D2240/127 , Y02E10/721 , Y02T50/166 , Y02T50/671 , Y02T50/673
摘要： An oscillatory vorticity generator device for controlling the flow on an aero- or hydrodynamic surface (104) of an element (110), the oscillatory vorticity generator device (130) comprising: two main walls, positioned opposite to each other, forming a first pair of walls and two other walls, the four walls each having proximal and distal ends, the distal ends connected to an aero- or hydrodynamic surface; a connection connecting the walls at their proximal ends; and an opening in the aero- or hydrodynamic surface, the opening being substantially contiguous with the two main walls and the two other walls.

8. 发明公开

EP2389313A2 HOCHAUFTRIEBSKLAPPE, ANORDNUNG EINER HOCHAUFTRIEBSKLAPPE MIT EINER VORRICHTUNG ZUR STRÖMUNGSBEEINFLUSSUNG AN DERSELBEN SOWIE FLUGZEUG MIT EINER DERARTIGEN ANORDNUNG 有权
标题翻译：与主翼的飞行器和电极的翼设置在该阻尼器
公开(公告)号：EP2389313A2
公开(公告)日：2011-11-30
申请号：EP10701627.1
申请日：2010-01-26
申请人： Airbus Operations GmbH
发明人： GÖLLING, Burkhard , HANSEN, Heinz , RADESPIEL, Rolf , JENSCH, Christoph , PFINGSTEN, Kai-Christoph , NEITZKE, Klaus-Peter
IPC分类号： B64C21/08
CPC分类号： B64C21/025 , B64C9/18 , B64C21/08 , B64C2230/04 , B64C2230/06 , Y02T50/166
摘要： The invention relates to an aerodynamic body (K) of an aircraft, which has a first lateral face and a second lateral face, both extending along the flap depth direction (KT) and a flow flowing around them in a direction of flow (S). The first lateral face on the regulating flap has a top surface (11) extending along the intake side and the second side is a lower surface (12) extending along the pressure side (B) of the regulating flap (K), at least one air outlet opening and at least one air inlet opening being arranged on the regulating flap (K), the air inlet opening communicating with the air outlet opening via at least one air conduit (30, 31, 32, 33, 34, 35, 36). A flow delivery drive (40, 41, 42) for influencing the flow within the air conduit (30, 31, 32, 33, 34, 35, 36) is integrated with the air conduit (30, 31, 32, 33, 34, 35, 36) and following openings are provided at the lateral faces of the regulating flap (K) in the flap depth direction (KT): at least one air outlet opening which is arranged in the front area (10a) of the regulating flap (K), when seen in the direction of flow, said area extending across up to 15% of the flap depth (KT), and at least one air inlet opening (23) which is arranged on the top surface of the regulating flap and in the rear area (10b) of the regulating flap (K), when seen in the direction of flow, extending across 30% to 90% of the flap depth (KT), and/or on the top surface of the regulating flap in the rear edge area (10c) extending across 90% to 100% of the flap depth (KT), and/or on the lower surface of the regulating flap in the rear edge area (10c) of the regulating flap (K) extending across 90% to 100% of the flap depth (KT). The invention further relates to arrangements of a main wing and a regulating flap (K) and to an aircraft having said aerodynamic body.

9. 发明公开

EP1755947A1 AIRCRAFT COMPONENT, IN PARTICULAR A WING 有权
标题翻译：飞机部件，特别是翼
公开(公告)号：EP1755947A1
公开(公告)日：2007-02-28
申请号：EP05739393.6
申请日：2005-05-11
申请人： Airbus Deutschland GmbH
发明人： MEISTER, Jürgen
IPC分类号： B64C21/06 , B64D15/04 , F15D1/12
CPC分类号： B64D15/04 , B64C21/025 , B64C21/08 , B64C2230/06 , B64C2230/22 , Y02T50/166
摘要： Aircraft component, in particular a wing (1) with perforations (3) for boundary layer suction. In the space (5) between the double-walled wing (1), partition walls form pressure channels (21) and suction channels (22) that are adjacent to each other and alternate, which channels (21, 22) communicate with the perforations (3). By means of a control device, the pressure channels (21) can be connected to a hot-air reservoir, and the suction channels (22) can be connected to a vacuum reservoir, and by way of a short-circuit valve (16) they can be connected to the respective other region.
摘要翻译：飞机部件，特别是具有用于边界层抽吸的穿孔（3）的机翼（1）。在双壁翼（1）之间的空间（5）中，分隔壁形成彼此相邻且交替的压力通道（21）和抽吸通道（22），所述通道（21,22）与穿孔（3）。通过控制装置，压力通道（21）可以连接到热空气储存器，并且抽吸通道（22）可以连接到真空储存器，并且通过短路阀（16）连接到真空储存器，他们可以连接到相应的其他地区。

10. 发明公开

EP0679572A3 Laminar flow skin 失效
标题翻译：层流皮肤
公开(公告)号：EP0679572A3
公开(公告)日：1996-04-17
申请号：EP95302749.7
申请日：1995-04-26
申请人： BRITISH AEROSPACE PUBLIC LIMITED COMPANY
发明人： Seyfang, George R., Brit. Aerospace Def. Ltd.
IPC分类号： B64C21/06 , B63B1/34 , F15D1/06 , F15D1/12
CPC分类号： B64C21/06 , B64C21/025 , B64C21/08 , B64C23/00 , B64C2230/20 , B64C2230/22 , Y02T50/166
摘要： Apparatus for the control of boundary layer fluids by a suction technique, the said apparatus being adapted to form part of or attach to a fluid dynamic surface and comprising; a sandwich skin material (2) consisting of at least two layers, an outer layer of which is in use positioned adjacent to the boundary layer fluid, the said layers of material bounding internal intercommunicating passageways to allow in use the movement of fluid to substantially all areas within the material, the outer layer being provided with a plurality of holes (4) communicating with the internal passageways (6) of the said sandwich skin material and a plurality of hoods (8) or steps being fixedly attached to the outer layer of the material located such that in use said hoods (8) or steps are downstream of said plurality of holes (4) and each upstream of and shielding an opening in said outer layer and communicating with at least one of said internal intercommunicating passageways (6).
摘要翻译：用于通过抽吸技术控制边界层流体的设备，所述设备适于形成流体动态表面的一部分或附着于流体动态表面并包括：由至少两层构成的夹层蒙皮材料（2），其外层在使用中与边界层流体相邻定位，所述材料层界定内部连通通道以允许在使用中流体移动到基本上全部所述外层设置有与所述夹层蒙皮材料的内部通道（6）连通的多个孔（4），并且多个罩（8）或台阶固定地连接到所述材料的外层所述材料被定位成使得在使用中所述罩（8）或台阶位于所述多个孔（4）的下游并且在所述外层中的每个上游和屏蔽开口并且与至少一个所述内部连通通道（6）。

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