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    • 1. 发明公开
    • ELECTROTHERMAL HEATER MAT
    • 电热加热垫
    • EP2528813A1
    • 2012-12-05
    • EP11702860.5
    • 2011-01-31
    • GKN Aerospace Services Limited
    • LEWIS, Stuart, MartinWINTER, Nicholas, JohnENGLISH, Peter
    • B64D15/12H05B3/36
    • B64D15/12B64D2033/0233H05B3/36H05B2203/013H05B2203/017H05B2203/033H05B2214/02
    • An electrothermal heater mat (3) is provided for an ice protection system for an aircraft (1) or the like. The heater mat (3) is a laminated heater mat and comprises dielectric layers (50-58), a heater element (501) and a temperature sensor (507). Each dielectric layer (50-58) comprises thermoplastic material, and the temperature sensor (507) comprises a sprayed metal track (5010, 5012) deposited on a substrate (50, 5019) comprising thermoplastic material. The substrate may be one of the dielectric layers (50) or a separate carrier (5019) which is smaller than the dielectric layers (50-58). The substrate (50, 5019) is laminated to at least a first one of the dielectric layers (53, 58) and the thermoplastic material of the substrate is (i) the same as the thermoplastic material of the first dielectric layer such that the thermoplastic material of the substrate is dispersed or merged into the thermoplastic material of the first dielectric layer or (ii) compatible with the thermoplastic material of the first dielectric layer such that the thermoplastic material of the substrate is fused to the thermoplastic material of the first dielectric layer. Thus, the formation of an undesirable discontinuity at the interface between the substrate (50, 5019) and the first dielectric layer (53, 58) is substantially prevented or minimised.
    • 电热加热垫(3)被设置用于飞机(1)等的防冰系统。 加热垫(3)是层压加热垫,并且包括介电层(50-58),加热元件(501)和温度传感器(507)。 每个介电层(50-58)包括热塑性材料,并且温度传感器(507)包括沉积在包括热塑性材料的基底(50,5019)上的喷射金属轨道(5010,5012)。 衬底可以是介电层(50)之一或者小于介电层(50-58)的单独的载体(5019)。 衬底(50,5019)被层压到介电层(53,58)中的至少第一个,并且衬底的热塑性材料(i)与第一介电层的热塑性材料相同,使得热塑性材料 基板的材料分散或合并到第一电介质层的热塑性材料中或(ii)与第一电介质层的热塑性材料相容,使得基板的热塑性材料熔合到第一电介质层的热塑性材料 。 因此,在衬底(50,5019)与第一介电层(53,58)之间的界面处形成不希望的不连续性基本上被阻止或最小化。
    • 6. 发明公开
    • DIELECTRIC COMPONENT WITH ELECTRICAL CONNECTION
    • HEIZMATTE AUFWEISEND EIN DIELEKTRISCHES BAUTEIL MIT ELEKTRISCHEM ANSCHLUSS
    • EP2528816A2
    • 2012-12-05
    • EP11704822.3
    • 2011-01-31
    • GKN Aerospace Services Limited
    • WINTER, Nicholas, JohnLEWIS, Stuart, MartinENGLISH, Peter
    • B64D15/12H05B3/36
    • B64D15/12H05B3/36H05B2203/013H05B2203/017H05B2203/033H05B2214/02Y10T29/49082
    • A dielectric component with electrical connection is provided for a laminated heater mat (3) for an ice protection system for an aircraft (1). The dielectric component with electrical connection comprises at least one dielectric layer (50, 55) comprising thermoplastic material, and the dielectric layer (50) or a stack of the dielectric layers (50, 55) has first and second main surfaces and a hole (505) extending between the first and second main surfaces. A first sprayed metal coating (501) comprises a first portion (503) deposited on the first main surface (502) adjacent to the hole (505) and a second portion (5014) which projects into the hole. A second sprayed metal coating (5013, 5513) comprises a third portion deposited on the second main surface (506, 552) adjacent to the hole (505) and a fourth portion (5015) which projects into the hole (505). The second portion (5014) overlaps the fourth portion (5015) to form a continuous conductive path between the first main surface and the second main surface. This provides a cheap, neat and thin connection through the dielectric layer or the stack of dielectric layers.
    • 为用于飞机(1)的防冰系统的层叠加热器垫(3)提供具有电连接的电介质部件。 具有电连接的电介质部件包括至少一个包括热塑性材料的电介质层(50,55),介电层(50)或电介质层(50,55)的叠层具有第一和第二主表面和孔 505)在第一和第二主表面之间延伸。 第一喷涂金属涂层(501)包括沉积在与孔(505)相邻的第一主表面(502)上的第一部分(503)和突出到孔中的第二部分(5014)。 第二喷涂金属涂层(5013,5513)包括沉积在与孔(505)相邻的第二主表面(506,552)上的第三部分和突出到孔(505)中的第四部分(5015)。 第二部分(5014)与第四部分(5015)重叠以在第一主表面和第二主表面之间形成连续的导电路径。 这提供了通过电介质层或电介质层的叠层的便宜,整齐和薄的连接。