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1. 发明授权

EP2322272B1 AIR CURRENT GENERATING APPARATUS AND METHODS FOR MANUFACTURING THE SAME 有权
公开(公告)号：EP2322272B1
公开(公告)日：2018-10-03
申请号：EP09797717.7
申请日：2009-07-16
申请人： Kabushiki Kaisha Toshiba
发明人： TANAKA, Motofumi , HAYASHI, Kazuo , SHIMURA, Naohiko , YASUI, Hiroyuki , ASAYAMA, Masahiro , ISHIWATA, Yutaka , KATAYAMA, Masahiro
IPC分类号： B01J19/08 , H01T23/00 , H05H1/24 , B64C21/08
CPC分类号： H05K13/00 , B64C21/00 , B64C23/005 , H05H1/2406 , Y02T50/166 , Y10T29/49124
摘要： There is provided an air current generating apparatus capable of reducing an accidental discharge and a method for manufacturing the same. An air current generating apparatus includes: a dielectric substrate exposed to gas: a first electrode disposed inside the dielectric substrate; a second electrode disposed near a surface of the dielectric so as to correspond the first electrode and having a sharp shape; and a power source applying a voltage between the first and second electrodes and plasmatizing part of the gas to generate an air current.

2. 发明公开

EP3261923A1 AIRFRAME-INTEGRATED PROPELLER-DRIVEN PROPULSION SYSTEMS 审中-公开
标题翻译：机载飞机一体化螺旋桨驱动推进系统
公开(公告)号：EP3261923A1
公开(公告)日：2018-01-03
申请号：EP16710084.1
申请日：2016-02-19
申请人： Embraer S.A.
发明人： HIRANO, Helio , TRAPP, Luis Gustavo
IPC分类号： B64C5/02 , B64C5/06 , B64D27/04 , B64D27/10
CPC分类号： B64C11/46 , B64C5/02 , B64C5/06 , B64C23/005 , B64D27/04 , B64D27/10
摘要： Propeller-driven craft (e.g., aircraft) are provided with at least one propulsion system having at least one engine and at least one aerial tractor propeller which generates a propeller propwash airflow when driven by the engine. At least one airfoil is disposed in the propeller propwash airflow of the at least one aerial tractor propeller. The airfoil is contoured and oriented relative to a swirl rotation angle (ω) of the propeller propwash airflow in order to induce a forward force component on the craft in response to the propeller propwash airflow over the at least one airfoil, thus improving the craft's performance and/or reducing fuel consumption.

4. 发明授权

EP2321084B1 SYSTEM AND METHOD FOR AERODYNAMIC FLOW CONTROL 有权
标题翻译：系统VERFAHRENFÜRAERODYNAMISCHE FLUSSSTEUERUNG
公开(公告)号：EP2321084B1
公开(公告)日：2017-03-22
申请号：EP09803664.3
申请日：2009-07-31
申请人： Bell Helicopter Textron Inc.
发明人： CORKE, Thomas , THOMAS, Flint , SHATZMAN, David , WOOD, Tommie
IPC分类号： B23K9/00 , B64C23/00 , F15D1/12
CPC分类号： B64C23/005 , B64C2230/12 , F15D1/12 , Y02T50/166

5. 发明公开

EP3050797A1 BOUNDARY LAYER CONTROL ASSEMBLY FOR AN AIRCRAFT AIRFOIL AND METHOD OF CONTROLLING A BOUNDARY LAYER 审中-公开
标题翻译：接口控制组件一种用于控制界面平行的平面轮廓和方法
公开(公告)号：EP3050797A1
公开(公告)日：2016-08-03
申请号：EP16153404.5
申请日：2016-01-29
申请人： Hamilton Sundstrand Corporation
发明人： LIN, Ray-Sing , TILLMAN, Thomas G. , HENZE, Chad M.
IPC分类号： B64C21/00 , B64C23/00 , B64D15/12
CPC分类号： B64C21/00 , B64C23/005 , B64C2230/10 , B64C2230/28 , B64D15/12 , Y02T50/166 , Y02T50/66
摘要： A boundary layer control assembly for an aircraft airfoil includes a leading edge (16) and a trailing edge (18) spaced from the leading edge (16) to form a chord length (20). The boundary layer control assembly also includes a heating element (28) disposed proximate the leading edge (16) to heat a boundary layer formed along the surface of the aircraft airfoil.
摘要翻译：在飞机机翼边界层控制组件包括前缘（16）和从所述前缘（16）隔开的后缘（18），以形成一个弦长（20）。因此，该边界层控制组件包括一个加热元件（28）设置成邻近所述前缘（16）以加热沿飞行器翼面的表面形成的边界层。

6. 发明公开

EP2933188A1 VTOL aircraft with a thrust-to-weight ratio smaller than 0.1 审中-公开
标题翻译： Senkrechtstarterflugzeug mit einemSchubgewichtsverhältniskleiner als 0,1
公开(公告)号：EP2933188A1
公开(公告)日：2015-10-21
申请号：EP14075023.3
申请日：2014-04-17
申请人： Chen, Li Jing
发明人： Chen, Li Jing
IPC分类号： B64C29/00 , B64C21/04
CPC分类号： B64C29/00 , B64C9/00 , B64C15/02 , B64C21/04 , B64C23/005 , B64C29/005 , B64C29/0066 , B64C2009/005 , B64D27/16 , Y02T50/166
摘要： An aircraft includes: ailerons (1,2); a turbofan engine (3) comprising a high-temp duct (4) with an openable/ closable propelling nozzle (5), and a low-temp duct (6) with an openable/closable propelling nozzle (7); a high-temp bypass duct (9) comprising an openable/closable inlet (8) connected to the high-temp duct(4), an outer wall(10) and a rectangle outlet(12) with a height-to-width ratio smaller than 0.1; a low-temp bypass duct (15) comprising an openable/closable inlet (14) connected to the low-temp duct (7), an outer wall (16), an inner wall (17) and a rectangle outlet (19) with a height-to-width ratio smaller than 0.1. During vertical take-off/lading, closing the propelling nozzles (5, 7) of turbofan engine (3), and opening the inlets (8,14) of high-temp and low-temp bypass ducts(9,15), low-temp planar air jet (20) is cause to flow over upper surface of the aircraft, thereby generating lift and no air flow over lower one.
摘要翻译：飞机包括：副翼（1,2）; 涡轮风扇发动机（3）包括具有可打开/关闭的推进喷嘴（5）的高温管道（4）和具有可打开/关闭的推进喷嘴（7）的低温管道（6）; 包括连接到高温管道（4）的可打开/关闭的入口（8）的高温旁通管道（9），外壁（10）和矩形出口（12），高度 - 宽度比小于0.1; 包括连接到低温管道（7）的可打开/关闭的入口（14）的低温旁通管道（15），外壁（16），内壁（17）和矩形出口（19）高度比宽度小于0.1。在垂直起飞期间，关闭涡轮风扇发动机（3）的推进喷嘴（5,7），并打开高温和低温旁通管道（9,15）的入口（8,14），低 - 平面空气喷射（20）导致飞行器的上表面流动，从而产生升力，而不会在较低的空气流中流动。

7. 发明公开

EP2933185A1 WING AERIAL REFUELING SYSTEM 有权转让
标题翻译： Ü。。。。。。。。。
公开(公告)号：EP2933185A1
公开(公告)日：2015-10-21
申请号：EP15163131.4
申请日：2015-04-10
申请人： The Boeing Company
发明人： Ferguson, Stanley D , Fialho, Ian J , Potter, Richard C
IPC分类号： B64C23/00 , B64D29/02 , B64D39/00
CPC分类号： B64C23/005 , B64C9/00 , B64C23/00 , B64D39/00
摘要： An aircraft (110) comprises a wing assembly (130), a pod (176), and a pylon (178) attaching the pod (176) to the wing assembly (130). The pylon (178) has a swept pylon flap (410), which is configured to unload the pylon and pod during flight of the aircraft, and also to create downward flow that counters a vortex trailing the pod.
摘要翻译：飞机（110）包括翼组件（130），吊舱（176）和将吊舱（176）附接到翼组件（130）的塔架（178）。塔架（178）具有扫掠的吊架（410），其构造成在飞行器飞行期间卸载塔架和吊舱，并且还产生向下的流动，其对应于荚顶部的涡流。

8. 发明公开

EP2853486A1 Vortex generators 有权
标题翻译： Wirbelgeneratoren
公开(公告)号：EP2853486A1
公开(公告)日：2015-04-01
申请号：EP14185895.1
申请日：2014-09-23
申请人： The Boeing Company
发明人： Clingman, Dan J. , Zidovetzki, Esther S. , Mallari, Randy Lee M.
IPC分类号： B64C23/06 , B64C23/00
CPC分类号： F15D1/009 , B64C23/005 , B64C23/06 , Y02T50/162 , Y02T50/166 , Y10T137/2087
摘要： Vortex generators are disclosed herein. An example apparatus includes a housing including a surface. The example apparatus also includes a bimorph actuator (300) disposed in the housing. The bimorph actuator includes a first bimorph (302) beam having a first portion fixed relative to the surface. A blade (200) is rotatably coupled to the bimorph actuator (300), and the bimorph actuator (300) is to rotate the blade (200) to extend a portion of the blade (08) through the surface to generate a vortex in a fluid flowing past the surface.
摘要翻译：本文公开了涡街发生器。示例性装置包括包括表面的壳体。示例性装置还包括设置在壳体中的双压电晶片致动器（300）。双压电晶片致动器包括具有相对于表面固定的第一部分的第一双压电晶片（302）。叶片（200）可旋转地联接到双压电晶片致动器（300），并且双压电晶片致动器（300）将使叶片（200）旋转以使叶片（08）的一部分延伸穿过该表面，以在流体流过表面。

9. 发明公开

EP2322272A4 AIR CURRENT GENERATING APPARATUS AND METHOD FOR MANUFACTURING SAME 审中-公开
标题翻译： VERFAHREN ZU IHRER HERSTELLUNG LUFTSTRUM ERZEUGENDE VORRICHTUNG
公开(公告)号：EP2322272A4
公开(公告)日：2014-10-29
申请号：EP09797717
申请日：2009-07-16
申请人： TOSHIBA KK
发明人： TANAKA MOTOFUMI , HAYASHI KAZUO , SHIMURA NAOHIKO , YASUI HIROYUKI , ASAYAMA MASAHIRO , ISHIWATA YUTAKA , KATAYAMA MASAHIRO
IPC分类号： B01J19/08 , B64C21/08 , H01T23/00 , H05H1/24
CPC分类号： H05K13/00 , B64C21/00 , B64C23/005 , H05H1/2406 , Y02T50/166 , Y10T29/49124
摘要： There is provided an air current generating apparatus capable of reducing an accidental discharge and a method for manufacturing the same. An air current generating apparatus includes: a dielectric substrate exposed to gas: a first electrode disposed inside the dielectric substrate; a second electrode disposed near a surface of the dielectric so as to correspond the first electrode and having a sharp shape; and a power source applying a voltage between the first and second electrodes and plasmatizing part of the gas to generate an air current.
摘要翻译：提供了能够减少意外放电的气流发生装置及其制造方法。一种气流发生装置，包括：暴露于气体的电介质基板;设置在电介质基板内部的第一电极; 设置在所述电介质的表面附近以对应于所述第一电极并且具有尖锐形状的第二电极; 以及在所述第一和第二电极之间施加电压并使所述气体的等离子体化部分产生气流的电源。

10. 发明授权

EP2431275B1 Rotor blade with integrated passive surface flap 失效
标题翻译：转子叶片与集成无源表面襟翼
公开(公告)号：EP2431275B1
公开(公告)日：2014-10-22
申请号：EP11182069.2
申请日：2011-09-20
申请人： Deutsches Zentrum für Luft- und Raumfahrt e.V.
发明人： Höfinger, Marc
IPC分类号： B64C27/72 , B64C23/00
CPC分类号： B64C27/72 , B64C23/005 , B64C2027/7261 , B64C2230/28 , Y02T50/166 , Y02T50/34

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