METHOD AND APPARATUS FOR INHIBITING FORMATION OF AND/OR REMOVING ICE FROM AIRCRAFT COMPONENTS
    1.
    发明申请
    METHOD AND APPARATUS FOR INHIBITING FORMATION OF AND/OR REMOVING ICE FROM AIRCRAFT COMPONENTS 有权
    用于禁止从飞机组件形成和/或移除冰的方法和装置

    公开(公告)号:US20160280379A1

    公开(公告)日:2016-09-29

    申请号:US15076598

    申请日:2016-03-21

    申请人: General Atomics

    摘要: Methods and systems are generally described that inhibit debris (such as ice) accretions and/or remove debris (such as ice) accretions from the exterior surface of an aircraft. In some embodiments, the invention is a system for an aircraft comprising: a component of the aircraft having a surface; a plurality of piezo-kinetic actuators each positioned proximate to a portion of the surface; and a control unit coupled to the plurality of actuators, the control unit configured to actuate one or more of the actuators at one or more frequencies; wherein the actuators are each configured to introduce a displacement of the surface in three dimensions to inhibit a formation of ice on at least the portion of the surface and to break up existing ice formations on at least the portion of the surface.

    摘要翻译: 通常描述的方法和系统是抑制来自飞行器外表面的碎片(例如冰)的积聚和/或去除碎片(例如冰)的积累。 在一些实施例中,本发明是用于飞行器的系统,其包括:具有表面的飞机的部件; 多个压电动力学致动器,每个定位成靠近所述表面的一部分; 以及耦合到所述多个致动器的控制单元,所述控制单元被配置为以一个或多个频率致动所述致动器中的一个或多个; 其中所述致动器各自被构造成在三维空间中引入所述表面的位移,以阻止在所述表面的至少所述部分上形成冰并在所述表面的至少一部分上分解现有的冰层。

    Electro-Expulsive De-Icing System for Aircraft and Other Applications
    2.
    发明申请
    Electro-Expulsive De-Icing System for Aircraft and Other Applications 审中-公开
    用于飞机和其他应用的电爆炸除冰系统

    公开(公告)号:US20130187006A1

    公开(公告)日:2013-07-25

    申请号:US13790065

    申请日:2013-03-08

    IPC分类号: B64D15/16

    CPC分类号: B64D15/163

    摘要: An apparatus for removing ice from an object (e.g., in-flight ice removal from the skin of an aircraft) includes an actuator assembly that forms an elongated electrically conductive loop. The actuator is mounted in a position enabling it to impact the object to be de-iced in response to movement of the loop that is produced by electric current pulses flowing in opposite directions in two mechanically independent loop subassemblies. The loop subassemblies include multiple electrically conductive elements interconnected at their ends using elongated flexible connectors in order to introduce a physically discontinuity that reduces any restriction of relative movement of the subassembly ends caused by the connectors, thereby achieving enhanced operation and less fatigue failure as compared to a rigid structure having encapsulated element

    摘要翻译: 一种用于从物体(例如从飞行器的皮肤中飞行中除冰)中移除冰的装置包括形成细长导电回路的致动器组件。 致动器安装在使其能够响应于在两个机械独立的回路组件中以相反方向流动的电流脉冲产生的回路的移动而撞击待除冰的物体的位置。 环路组件包括多个导电元件,其端部使用细长的柔性连接器互连,以引入物理不连续性,从而减少由连接器引起的子组件端部的相对运动的任何限制,从而实现增强的操作和较少的疲劳失效,与 具有封装元件的刚性结构

    Anti-icing / de-icing system and method and aircraft structure incorporating this system
    3.
    发明授权
    Anti-icing / de-icing system and method and aircraft structure incorporating this system 有权
    防冰/除冰系统和结合该系统的方法和飞机结构

    公开(公告)号:US08146866B2

    公开(公告)日:2012-04-03

    申请号:US12398515

    申请日:2009-03-05

    IPC分类号: B64D15/16

    摘要: The present invention provides an anti-icing/de-icing system and method using ultrasound waves for an external surface of a structure likely to be iced, such as an aircraft wing or engine nacelle, and such a structure incorporating this system. The system comprises a plurality of piezoelectric transducers with which the structure is fitted, opposite this external surface, and this system is such that it comprises scanning devices at least one matrix of elementary meshes predefined in this surface in relation to an even arrangement of a group of these transducers, these scanning devices being able to focus the waves emitted by all or some of the transducers of the or each group on these meshes one after the other, via signal summing devices coupled to these scanning devices and able to produce, for each mesh, a summation of the signals obtained from the transducers emitting these waves.

    摘要翻译: 本发明提供了一种使用超声波作为可能结冰的结构的外表面的防冰/除冰系统和方法,例如飞行器机翼或发动机机舱,以及这种结合该系统的结构。 该系统包括与该外表面相对配合的多个压电换能器,并且该系统使得其包括相对于组的均匀布置在该表面中预定义的至少一个基本网格的扫描装置 这些扫描装置能够通过耦合到这些扫描装置的信号求和装置将这些或每组的全部或一些换能器发射的波相互集中在这些网格上,并且能够为每个 网格,从发射这些波的换能器获得的信号的总和。

    Vibrating debris remover
    4.
    发明授权
    Vibrating debris remover 有权
    振动碎屑去除剂

    公开(公告)号:US08087297B2

    公开(公告)日:2012-01-03

    申请号:US12336622

    申请日:2008-12-17

    IPC分类号: G01N29/00 H01L41/083

    摘要: A system and a retrofit kit for removing debris from a surface of a material. At least one vibration subunit is provided which is either embedded within or operatively connected to a back surface of the material. The vibration subunits are capable of converting a driving energy to a vibrating mechanical output energy which is coupled to the material. At least one external energy source is provided which is operatively connected to the vibration subunits. The external energy source is capable of providing the driving energy to the vibration subunits. The vibrating mechanical energy is capable of causing debris to be removed from the surface of the material.

    摘要翻译: 用于从材料表面去除碎屑的系统和改进套件。 提供至少一个振动子单元,其被嵌入或可操作地连接到材料的后表面。 振动子单元能够将驱动能量转换成耦合到材料的振动机械输出能量。 提供至少一个外部能源,其可操作地连接到振动子单元。 外部能量源能够为振动子单元提供驱动能量。 振动的机械能能够使碎屑从材料的表面移除。

    Prevention of ice formation by applying electric power to a liquid water layer
    5.
    发明授权
    Prevention of ice formation by applying electric power to a liquid water layer 失效
    通过向液态水层施加电力来防止形成冰

    公开(公告)号:US07227110B2

    公开(公告)日:2007-06-05

    申请号:US10984475

    申请日:2004-11-09

    IPC分类号: H05B6/70

    摘要: A first electrode is separated from a second electrode by an interelectrode space. The interelectrode space does not exceed 3 mm, and preferably does not exceed 100 μm. Liquid water fills the interelectrode space, thereby electrically connecting the first electrode and the second electrode. A power supply, preferably low-frequency AC, is connected to the first and second electrodes, generating a current through the water in the interelectrode space. The applied electric power prevents freezing of a thin liquid water layer in the interelectrode space, thereby preventing ice formation.

    摘要翻译: 第一电极通过电极间空间与第二电极分离。 电极间距离不超过3毫米,优选不超过100毫米。 液体水填充电极间空间,从而电连接第一电极和第二电极。 电源,优选地是低频AC,连接到第一和第二电极,产生电流通过电极间空间中的水。 所施加的电力防止电极间空间中的薄液体水层的冻结,从而防止冰层形成。

    Electro-magnetic expulsion de-icing system
    8.
    发明授权
    Electro-magnetic expulsion de-icing system 失效
    电磁除冰除冰系统

    公开(公告)号:US6102333A

    公开(公告)日:2000-08-15

    申请号:US799277

    申请日:1997-02-13

    摘要: The present invention is a de-icing system that uses electro-magnetic actuators mounted within the airfoil of an aircraft to effect de-icing. Advantageously, the actuators have low-energy requirements. Each actuator includes conductive strips fabricated on a flexible dielectric sheet. The conductive strips are wound into coils with the actuators shaped into a flattened elongated tube. The axis of the winding coils is coincident with the longitudinal axis of the elongated tube. Low adhesive coatings may be used to enhance the efficiency of the electro-magnetic coils in expulsing the ice accretion.

    摘要翻译: 本发明是使用安装在飞行器的翼型内的电磁致动器进行除冰的除冰系统。 有利地,致动器具有低能量要求。 每个致动器包括在柔性电介质片上制造的导电条。 导电条被卷绕成线圈,致动器成形为扁平的细长管。 绕组线圈的轴线与细长管的纵向轴线重合。 可以使用低粘合剂涂层来提高电磁线圈在排除冰层中的效率。

    Hybrid ice-protection system for use on roughness-sensitive airfoils
    9.
    发明授权
    Hybrid ice-protection system for use on roughness-sensitive airfoils 失效
    用于粗糙度敏感翼型的混合冰保护系统

    公开(公告)号:US5921502A

    公开(公告)日:1999-07-13

    申请号:US665914

    申请日:1996-06-19

    IPC分类号: B64D15/00 B64D15/04 B64D15/16

    CPC分类号: B64D15/16 B64D15/163

    摘要: An electro-thermal or hot gas anti-icer of the "running-wet" type is mounted at the leading edge of an airfoil. Mechanical de-icers are mounted on the surfaces aft of the anti-icer. The mechanical de-icers throw off ice without creating runback water, thereby eliminating runback refreeze ridges caused by a known hybrid ice-protection system. Advantageously, the de-icers are of a type in which the airfoil has a semi-rigid skin that forms an aerodynamic surface of the airfoil, and in which there is at least one mechanical actuator for flexing the skin.

    摘要翻译: “跑步湿式”类型的电热或热气体防冰器安装在翼型的前缘。 机械除冰器安装在防冰板后面的表面上。 机械除冰器在不产生回流水的情况下扔冰,从而消除由已知的混合防冰系统引起的回流重冰脊。 有利地,除冰器是其中翼型件具有半刚性皮肤的类型,其形成翼型件的空气动力学表面,并且其中存在至少一个用于使皮肤弯曲的机械致动器。

    Movable sheet for laminar flow and deicing
    10.
    发明授权
    Movable sheet for laminar flow and deicing 失效
    用于层流和除冰的活动板

    公开(公告)号:US5590854A

    公开(公告)日:1997-01-07

    申请号:US333483

    申请日:1994-11-02

    申请人: Solomon Shatz

    发明人: Solomon Shatz

    摘要: A movable sheet overlying a wing is disclosed that creates laminar flow over its exposed surface. The movable sheet serves as an integral, retractable shield for protecting a suction support structure of a wing against contamination, and also serves as a movable, conductive substrate for deicing by means of electrical resistance or hot-gas heating. The invention includes a movable sheet that is mounted scroll-like on two motor-driven rollers. The sheet has a solid area without perforations that protects the suction support structure from contamination, and a porous area with perforations therethrough that allows boundary layer suction. The motor-driven rollers scroll the sheet to cover the suction support structure with either the solid area or the perforations of the sheet. Contact rollers at the edge of the sheet supply electrical current to resistively heat the sheet and melt any accumulated ice. The movable sheet can also be moved back and forth to dislodge the ice.

    摘要翻译: 公开了一种覆盖翼的可动片,其在其暴露的表面上产生层流。 可移动片用作一体的可伸缩护罩,用于防止机翼的吸入支撑结构免受污染,并且还用作通过电阻或热气加热进行除冰的可移动的导电基底。 本发明包括在两个电动辊上滚动地安装的可移动片。 片材具有没有穿孔的固体区域,其保护抽吸支撑结构免受污染,并且具有穿孔的多孔区域允许边界层抽吸。 马达驱动的滚筒滚动片材以覆盖吸力支撑结构,其中固体区域或片材的穿孔。 在片材边缘的接触辊提供电流以电阻加热片材并熔化任何积聚的冰。 可移动片材也可以来回移动以移开冰块。