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公开(公告)号：US3809341A
公开(公告)日：1974-05-07
申请号：US30655472
申请日：1972-11-14
申请人： LEVIN I , LEVIN A , ROGOV I , FEDOROV N , TURYANSKY E , AFANASOV E
发明人： ROGOV I , AFANASOV E , TURYANSKY E , LEVIN A , FEDOROV N , LEVIN I
IPC分类号： B64D15/16
CPC分类号： B64D15/163
摘要： Electric current pulses separated by time intervals are transformed into mechanical power pulses acting on a surface to be de-iced. A converter of electric current pulses is constituted by a pair of electrically connected conductors one of which mates intimately with the surface to be de-iced. The conductors are arranged in the area to be de-iced and disposed one beneath the other. The electric current flowing through the conductors cause their mutual repulsion or attraction whereby electric current pulses are transformed into mechanical power pulses thus causing an elastic deformation of the surface being de-iced and effecting the removal of ice from this surface.
摘要翻译： 由时间间隔分开的电流脉冲被转换为作用在要除冰的表面上的机械功率脉冲。 电流脉冲转换器由一对电连接的导体构成，其中一个导体与要除冰的表面紧密配合。 导体布置在要除冰的区域中并且一个放置在另一个之下。 流过导体的电流引起它们的相互排斥或吸引，由此电流脉冲被转换成机械功率脉冲，从而导致被除冰的表面的弹性变形并且从该表面去除冰。
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72.发明授权
公开(公告)号：US3779488A
公开(公告)日：1973-12-18
申请号：US3779488D
申请日：1972-02-15
申请人： LEVIN I
发明人： LEVIN I
CPC分类号： B06B1/023 , B06B2201/58 , B06B2201/70 , B63B59/04 , B64D15/163 , H01Q1/02
摘要： A system is disclosed for deicing the skin surface of aircraft and comprises a power supply unit to which are connected an electrical power accumulator and a program switch. Low inertia converters such as magnetostrictive vibrators are provided in close proximity to the skin surface and are fed from the power supply unit via key switches each having one input connected to the electrical power accumulator while its second input is connected to the program selector switch such that the switch will produce successive single or bundles of electrical pulses separated by pauses at the converters.
摘要翻译： 公开了一种用于除冰飞机的皮肤表面的系统，并且包括连接有蓄电池和程序开关的电源单元。 低惯性转换器（例如磁致伸缩振动器）被设置在皮肤表面附近，并且通过各自具有连接到电力蓄电器的一个输入的键开关从电源单元馈送，同时其第二输入连接到程序选择器开关，使得 该开关将产生在转换器处由暂停分开的连续的单个或一束电脉冲。
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73.发明授权
公开(公告)号：US3672610A
公开(公告)日：1972-06-27
申请号：US3672610D
申请日：1969-05-20
申请人： LEVIN IGOR A
CPC分类号： B06B1/023 , B06B2201/58 , B06B2201/70 , B63B59/04 , B64D15/163 , H01Q1/02
摘要： A system is disclosed for deicing the skin surface of aircraft and comprises a power supply unit to which are connected an electrical power accumulator and a program switch. Low inertia converters such as magnetostrictive vibrators are provided in close proximity to the skin surface and are fed from the power supply unit via key switches each having one input connected to the electrical power accumulator while its second input is connected to the program selector switch such that the switch will produce successive single or bundles of electrical pules separated by pauses at the converters.
摘要翻译： 公开了一种用于除冰飞机的皮肤表面的系统，并且包括与蓄电池和程序开关连接的电源单元。 低惯性转换器（例如磁致伸缩振动器）被设置在皮肤表面附近，并且通过各自具有连接到电力蓄电器的一个输入的键开关从电源单元馈送，同时其第二输入连接到程序选择器开关，使得 该开关将在转换器处产生由暂停分开的连续的单个或多个电。。
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公开(公告)号：US12030648B2
公开(公告)日：2024-07-09
申请号：US17041663
申请日：2019-03-29
CPC分类号： B64D15/12 , B32B27/08 , B32B27/288 , B64D15/163 , H05B3/36 , B32B2250/05 , B32B2250/24 , B32B2307/206 , B32B2307/30 , B32B2605/18 , H05B2203/005 , H05B2203/016
摘要： An ice removal apparatus for an aircraft is provided comprising a laminate structure encapsulating an electrically operable heater. The laminate structure comprises a plurality of layers and at least two layers are configured to be selectively movable relative to each other to increase the separation of the two layers, thereby removing ice.
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公开(公告)号：US11794907B2
公开(公告)日：2023-10-24
申请号：US17286158
申请日：2019-09-30
申请人： LEONARDO S.P.A.
IPC分类号： B64D15/16 , B64C27/473 , B64D15/12
CPC分类号： B64D15/163 , B64C27/473 , B64D15/12
摘要： A blade for a rotor of a hover-capable aircraft is described comprising: a main body with a first outer surface; and a de-icing system for removing ice; the de-icing system, in turn, comprises: a first layer formed by a shape-memory material activatable so as to alter its shape according to a temperature-associable quantity, which is arranged on at least one outer surface of the main body; the de-icing system is characterized in that it comprises a second covering layer, which defines at least a portion of a second outer surface of the blade on which ice deposits; the second layer laid on top of the first layer on the opposite side of the main body is selectively movable under the action of the first layer so as to exert a mechanical action on the ice and remove it from the blade, and is adapted to protect the first layer from external agents.
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公开(公告)号：US20180237145A1
公开(公告)日：2018-08-23
申请号：US15959778
申请日：2018-04-23
申请人： Peter Lenkey
发明人： Peter Lenkey
CPC分类号： B64D15/163 , B64D15/16 , B64D33/02 , B64D2033/0233
摘要： Apparatuses for and methods of deicing aircraft surfaces, engine inlets, windmill blades and other structures are disclosed. Deicing apparatuses comprising at least one standoff coupled with an actuator and a first region of an inner surface of a skin are disclosed. A standoff can act as a moment arm and can create efficient, tailorable skin bending and acceleration, breaking an ice to skin bond. Integral as well as modular leading edges comprising deicing apparatuses are disclosed.
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公开(公告)号：US10000290B2
公开(公告)日：2018-06-19
申请号：US15789854
申请日：2017-10-20
申请人： Peter Lenkey
发明人： Peter Lenkey
CPC分类号： B64D15/163 , B64D15/16 , B64D33/02 , B64D2033/0233
摘要： Apparatuses for and methods of deicing aircraft surfaces, engine inlets, windmill blades and other structures. Deicing apparatuses can comprise at least one standoff coupled with an actuator and a first region of an inner surface of a skin. A standoff can act as a moment arm and can create efficient, tailorable skin bending and acceleration, breaking an ice to skin bond. Integral as well as modular leading edges can comprise deicing apparatuses.
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公开(公告)号：US09878795B2
公开(公告)日：2018-01-30
申请号：US14650012
申请日：2012-12-06
申请人： SAAB AB
发明人： Bertil Hådén , Mats Bäckström
CPC分类号： B64D15/163 , B64D15/12
摘要： A de-icing arrangement and method for de-icing a structural element. The arrangement includes at least one electromagnetic actuator, a capacitive storage bank, a control unit arranged to provide an excitation pulse to the at least one electromagnetic actuator, and a charging circuit arranged to charge the capacitive storage bank. The at least one electromagnetic actuator is arranged to expand in at least one direction when fed with the excitation pulse. The at least one electromagnetic actuator is placed in relation to the structural element so as to apply a mechanical force caused by the expansion on the structural element. The capacitive storage bank includes a plurality of selectable capacitors of different size. The control unit is arranged to select at least one capacitor for charging having a size such that current discharge of the capacitive storage bank into the at least one electromagnetic actuator generates a desired distribution between heat and mechanical power.
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公开(公告)号：US09873517B2
公开(公告)日：2018-01-23
申请号：US14427505
申请日：2013-08-15
申请人： Leonardo MW Ltd
CPC分类号： B64D15/16 , B64D15/163
摘要： A de-icing system for a hemispherical protective housing mounted on an aircraft structure is described. The system can include a series of piezo-electric devices mounted at the boundary of the housing. The piezo-electric devices generate ultrasonic frequencies and resonance of the protective housing is induced. One of the piezo-electric devices senses the frequency generated in the protective housing and acts as part of a feedback loop to maintain structural resonance of the protective housing. The structural resonance of the protective housing prevents the build-up of ice. Additionally, higher power resonances can be generated to remove ice already built up on the protective housing. The system also enables detection of ice build-up on the protective housing by monitoring any change in the frequency required to maintain structural resonance of the protective housing.
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公开(公告)号：US09580181B2
公开(公告)日：2017-02-28
申请号：US13876800
申请日：2010-09-28
CPC分类号： B64D15/163 , F03D80/40 , H02N1/002 , Y02E10/721 , Y02E10/722
摘要： The present invention relates to a de-icing arrangement for de-icing a structural element {170; 270; 370). The structural element could be made of a whole polymeric or metallic material. The arrangement comprises a power source (250) being electrically connected to an electrode configuration (200), said power source is arranged to, when applicable, electrically charge said electrode configuration (200). The electrode configuration (200) is arranged to generate an impulsive force (Fn) for removal of ice adhered on said structural element (170; 270; 370). The invention relates to a method for de-icing a structural element. The invention also relates to a computer program and a computer program product. The invention also relates to a platform carrying the arrangement.
摘要翻译： 本发明涉及一种除冰结构，用于除冰结构元件（170; 270; 370）。 结构元件可以由整个聚合物或金属材料制成。 该装置包括电连接到电极配置（200）的电源（250），所述电源设置成在适用时对所述电极配置（200）充电。 电极配置（200）被布置成产生用于去除附着在所述结构元件（170; 270; 370）上的冰的冲击力（Fn）。 本发明涉及一种用于除冰结构元件的方法。 本发明还涉及计算机程序和计算机程序产品。 本发明还涉及一种承载该装置的平台。
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