Article with de-icing/anti-icing function
    2.
    发明授权
    Article with de-icing/anti-icing function 有权
    文章具有除冰/防冰功能

    公开(公告)号:US08662452B2

    公开(公告)日:2014-03-04

    申请号:US13522343

    申请日:2010-01-14

    IPC分类号: B64D15/12

    摘要: A structural article including an outer surface that serves as an aerodynamic surface when the structural article is subjected for an air stream. A resin matrix laminate includes an upper ply and a bottom ply. A heating element is arranged in contact with the bottom ply and coupled to a power supply unit in purpose to deice/anti-ice the outer surface. Each ply includes a thermally conductive filament structure having a filament orientation such that the prolongation of the filaments has an extension essentially perpendicular to the extension of the laminate. The thermally conductive filament structure of the upper ply is embedded in the upper ply in such way that at least a portion of the thermally conductive filament structure is exposed in the outer surface.

    摘要翻译: 包括当结构制品经受气流时用作空气动力学表面的外表面的结构制品。 树脂基质层压体包括上层和底层。 加热元件布置成与底层接触并且耦合到电源单元以用于对外表面进行去冰/防冰。 每个层包括具有长丝取向的导热细丝结构,使得长丝的延伸具有基本上垂直于层压体的延伸部的延伸。 上层的导热丝结构被嵌入上层,使得至少一部分导热丝结构在外表面露出。

    PLASMA-ENHANCED ACTIVE LAMINAR FLOW ACTUATOR SYSTEM
    4.
    发明申请
    PLASMA-ENHANCED ACTIVE LAMINAR FLOW ACTUATOR SYSTEM 有权
    等离子体增强活性层流法致动器系统

    公开(公告)号:US20130291979A1

    公开(公告)日:2013-11-07

    申请号:US13821196

    申请日:2010-09-15

    IPC分类号: B64C23/00

    摘要: The invention regards a plasma-enhanced active laminar flow actuator system (1) adapted to an aerodynamic surface (3) which has a nano-engineered composite material layer(5) comprising a set of electrodes arranged (7′, 7″) in at least an upper (P1) and a lower (P2) plane extending parallel with the aerodynamic surface (3); the electrodes (7′, 7″) comprising nano filaments (9); the electrodes (7′) of the upper plane (P1) are arranged in the aerodynamic surface (3) such that they define a smooth and hard aerodynamic surface (3);conductors (11, 11′) of nano filaments (9″) arranged for electrical communication between a control unit (13) and each of the electrodes (7′, 7″), wherein the control unit (13) is adapted to address current between cooperating electrodes (7′, 7″) of the upper and lower plane (P1, P2) from a current supply depending upon air flow characteristic signals fed from air flow sensor means (19).

    摘要翻译: 本发明涉及一种适用于空气动力学表面(3)的等离子体增强型有源层流致动器系统(1),其具有纳米工程复合材料层(5),其包括一组电极(7',7“) 至少与空气动力学表面(3)平行延伸的上部(P1)和下部(P2)平面; 包括纳米细丝(9)的电极(7',7“); 上平面(P1)的电极(7')布置在空气动力学表面(3)中,使得它们限定平滑且硬的空气动力学表面(3);纳米细丝(9“)的导体(11,11') ),其布置成用于控制单元(13)和每个电极(7',7“)之间的电气通信,其中所述控制单元(13)适于解决所述电极(7',7”)的协作电极 根据从气流传感器装置(19)馈送的气流特性信号,来自电流源的上平面(P1,P2)。

    MULTIFUNCTIONAL DE-ICING/ANTI-ICING SYSTEM OF A WIND TURBINE
    5.
    发明申请
    MULTIFUNCTIONAL DE-ICING/ANTI-ICING SYSTEM OF A WIND TURBINE 审中-公开
    风力涡轮机的多功能防雷系统

    公开(公告)号:US20130028738A1

    公开(公告)日:2013-01-31

    申请号:US13522393

    申请日:2010-01-14

    IPC分类号: F03D11/00

    摘要: A de-icing/anti-icing system including at least two conductive structures embedded in a wind turbine blade. An outer surface is designed as an aerodynamic surface. At least one of the conductive structures is arranged adjacent the outer surface. A control unit adapted to control the energy supply to the conductive structures for generating heat to the outer surface. One conductive structure includes a first conductive nano structure. A conductive property of the conductive structure differs from a conductive property of the other conductive structure including a second conductive nano structure, for achieving different degrees of heat depending on the needed mode of the system.

    摘要翻译: 一种除冰/防冰系统,其包括嵌入在风力涡轮机叶片中的至少两个导电结构。 外表面设计为空气动力学表面。 导电结构中的至少一个布置成与外表面相邻。 控制单元,其适于控制向导电结构的能量供应,以向外表面产生热量。 一个导电结构包括第一导电纳米结构。 导电结构的导电特性与包括第二导电纳米结构的另一导电结构的导电性不同,用于根据系统的所需模式实现不同程度的热。

    AERODYNAMIC SURFACE WITH IMPROVED PROPERTIES
    7.
    发明申请
    AERODYNAMIC SURFACE WITH IMPROVED PROPERTIES 审中-公开
    具有改进性质的空气动力学表面

    公开(公告)号:US20130028744A1

    公开(公告)日:2013-01-31

    申请号:US13522364

    申请日:2010-01-14

    IPC分类号: B64C11/18 B32B5/12

    摘要: An article including an outer surface that serves as an aerodynamic surface when the article is subjected for an air stream. A resin matrix made of a polymeric composite laminate of at least one ply includes the outer surface. The at least one ply includes a nano structure embedded therein such that nano filaments of the nano structure in the ply essentially have the same angular orientation relative the plane of the outer surface. The outer ply is a ply of a laminate including at least two plies. Each ply includes large fibers having an orientation different from or identical to the orientation of large fibers of an adjacent ply.

    摘要翻译: 一种制品,其包括当制品经受空气流时用作空气动力学表面的外表面。 由至少一层的聚合物复合层压材料制成的树脂基体包括外表面。 所述至少一个层包括嵌入其中的纳米结构,使得所述层中的所述纳米结构的纳米长丝相对于所述外表面的平面基本上具有相同的角度取向。 外层是包括至少两层的叠层层。 每个帘布层包括具有与相邻帘布层的大纤维的取向不同或相同的取向的大纤维。

    Plasma-enhanced active laminar flow actuator system
    8.
    发明授权
    Plasma-enhanced active laminar flow actuator system 有权
    等离子增强有源层流致动器系统

    公开(公告)号:US09067674B2

    公开(公告)日:2015-06-30

    申请号:US13821196

    申请日:2010-09-15

    摘要: The invention regards a plasma-enhanced active laminar flow actuator system (1) adapted to an aerodynamic surface (3) which has a nano-engineered composite material layer (5) comprising a set of electrodes arranged (7′, 7″) in at least an upper (P1) and a lower (P2) plane extending parallel with the aerodynamic surface (3); the electrodes (7′, 7″) comprising nano filaments (9); the electrodes (7′) of the upper plane (P1) are arranged in the aerodynamic surface (3) such that they define a smooth and hard aerodynamic surface (3); conductors (11, 11′) of nano filaments (9″) arranged for electrical communication between a control unit (13) and each of the electrodes (7′, 7″), wherein the control unit (13) is adapted to address current between cooperating electrodes (7′, 7″) of the upper and lower plane (P1, P2) from a current supply depending upon air flow characteristic signals fed from air flow sensor means (19).

    摘要翻译: 本发明涉及一种适用于空气动力学表面(3)的等离子体增强型有源层流致动器系统(1),其具有纳米工程复合材料层(5),所述纳米工程复合材料层(5)包括一组电极(7',7“) 至少与空气动力学表面(3)平行延伸的上部(P1)和下部(P2)平面; 包括纳米细丝(9)的电极(7',7“); 上平面(P1)的电极(7')布置在空气动力学表面(3)中,使得它们限定平滑且硬的空气动力学表面(3); 布置成用于在控制单元(13)和每个电极(7',7“)之间电连通的纳米长丝(9”)的导体(11,11'),其中控制单元(13)适于寻址电流 根据从空气流量传感器装置(19)馈送的空气流特性信号,从电流源供应上和下平面(P1,P2)的配合电极(7',7“)。

    Multifunctional de-icing/anti-icing system
    9.
    发明授权
    Multifunctional de-icing/anti-icing system 有权
    多功能除冰/防冰系统

    公开(公告)号:US08931740B2

    公开(公告)日:2015-01-13

    申请号:US13522368

    申请日:2010-01-14

    摘要: A de-icing/anti-icing system including at least two conductive structures embedded in an article that includes an outer surface designed as an aerodynamic surface. At least one of the conductive structures is arranged adjacent the outer surface. A control unit adapted to control the energy supply to the conductive structures for generating heat to the outer surface. A first of the conductive structures includes a first conductive nano structure and a second of the conductive structures includes a second conductive nano structure. A conductive property of the first of the conductive structures differs from a conductive property of the second of the conductive structures. The first conductive nano structure serves as a heating conductor and the second conductive nano structure serves as a heating element. The first and second conductive nano structures are embedded in a common plane of a resin layer forming the outer surface.

    摘要翻译: 一种除冰/防冰系统,其包括嵌入制品中的至少两个导电结构,其包括被设计为空气动力学表面的外表面。 导电结构中的至少一个布置成与外表面相邻。 控制单元,其适于控制向导电结构的能量供应,以向外表面产生热量。 第一导电结构包括第一导电纳米结构,第二导电结构包括第二导电纳米结构。 第一导电结构的导电性与第二导电结构的导电性不同。 第一导电纳米结构用作加热导体,第二导​​电纳米结构用作加热元件。 第一和第二导电纳米结构嵌入到形成外表面的树脂层的共同平面中。