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    • 1. 发明授权
    • Flush-mounted flashing light
    • 嵌入式闪光灯
    • US08128254B2
    • 2012-03-06
    • US12083251
    • 2006-10-09
    • Guy LaenenMichel VanderenJean-Claude VandevoordeLouis Willems
    • Guy LaenenMichel VanderenJean-Claude VandevoordeLouis Willems
    • E01F9/04
    • B64F1/20B64F1/205F21V5/00F21V5/02F21V5/04F21V15/01F21W2111/00F21W2111/06F21Y2103/00
    • The invention relates to a flush-mounted flashing light for approach guidance of aircraft, having a housing which has a housing pot (10) which can be inserted below ground level (F) and a housing cover (12) which covers this approximately at ground level (F) and having an optical system, which is arranged in the housing for controlled production and directed emission of light flashes, which comprises a light source (20) for production of light flashes and a prism (40) for varying the direction of the beam direction of the light flashes, with at least one light outlet opening (13) being provided in the housing cover (12) for light flashes to emerge from in a predetermined emission direction. The external dimensions as well as the total weight of the flashing light can be reduced considerably because the light source (20) is elongated and designed to emit a light over a length (L) of less than 100 mm, and because a lens (42) for focusing the light which is emitted from the light source (20) is arranged on a light inlet surface (41) of the prism (40).
    • 本发明涉及一种用于飞行器接近引导的嵌入式闪光灯,其具有壳体,壳体具有可插入地平面(F)下方的壳体(10)和大致在地面上覆盖的壳体盖(12) (F)并且具有光学系统,其布置在壳体中用于受控制造和定向发射的闪光灯,其包括用于产生闪光的光源(20)和用于改变方向的棱镜(40) 光束的光束方向闪烁,其中至少一个光出口开口(13)设置在壳体盖(12)中,用于闪光,以从预定的发射方向露出。 由于光源(20)被拉长并设计成在小于100mm的长度(L)上发光,并且由于透镜(42)的透镜(42),所以可以显着地减小外部尺寸以及闪光的总重量 ),用于将从光源(20)发射的光聚焦在棱镜(40)的光入射表面(41)上。
    • 2. 发明申请
    • Flush-Mounted Flashing Light
    • 嵌入式闪光灯
    • US20100053946A1
    • 2010-03-04
    • US12083251
    • 2006-10-09
    • Guy LaenenMichel VanderenJean-Claude VandevoordeLouis Villems
    • Guy LaenenMichel VanderenJean-Claude VandevoordeLouis Villems
    • F21V21/00F21V23/00F21V29/00F21V13/02
    • B64F1/20B64F1/205F21V5/00F21V5/02F21V5/04F21V15/01F21W2111/00F21W2111/06F21Y2103/00
    • The invention relates to a flush-mounted flashing light for approach guidance of aircraft, having a housing which has a housing pot (10) which can be inserted below ground level (F) and a housing cover (12) which covers this approximately at ground level (F) and having an optical system, which is arranged in the housing for controlled production and directed emission of light flashes, which comprises a light source (20) for production of light flashes and a prism (40) for varying the direction of the beam direction of the light flashes, with at least one light outlet opening (13) being provided in the housing cover (12) for light flashes to emerge from in a predetermined emission direction. The external dimensions as well as the total weight of the flashing light can be reduced considerably because the light source (20) is elongated and designed to emit a light over a length (L) of less than 100 mm, and because a lens (42) for focusing the light which is emitted from the light source (20) is arranged on a light inlet surface (41) of the prism (40).
    • 本发明涉及一种用于飞行器接近引导的嵌入式闪光灯,其具有壳体,壳体具有可插入地平面(F)下方的壳体(10)和大致在地面上覆盖的壳体盖(12) (F)并且具有光学系统,其布置在壳体中用于受控制造和定向发射的闪光灯,其包括用于产生闪光的光源(20)和用于改变方向的棱镜(40) 光束的光束方向闪烁,其中至少一个光出口开口(13)设置在壳体盖(12)中,用于闪光,以从预定的发射方向露出。 由于光源(20)被拉长并设计成在小于100mm的长度(L)上发光,并且由于透镜(42)的透镜(42),所以可以显着地减小外部尺寸以及闪光的总重量 ),用于将从光源(20)发射的光聚焦在棱镜(40)的光入射表面(41)上。
    • 6. 发明申请
    • DEVICE FOR DETECTING A VEHICLE ON AN AIRPORT RUNWAY
    • 在机场运行中检测车辆的装置
    • US20110187580A1
    • 2011-08-04
    • US12682503
    • 2008-10-09
    • Guy LaenenJean-Claude VandevoordeGeert Bollens
    • Guy LaenenJean-Claude VandevoordeGeert Bollens
    • G01S13/93
    • G01S13/87G01S7/003G01S7/411G01S13/04G01S13/91G01S2013/916
    • The invention relates to a device (10) for detecting a vehicle, especially an aircraft (A), on an airport runway (R), especially a take-off or landing strip, a taxi strip or in the ramp region, said device comprising at least one radar sensor (11) which is arranged in the region of the runway (R) and used to scan a spatial detection region (E) by means of a radar beam. The fact that the detection region (E) comprises two lobe-shaped partial regions (E1, E2) extending horizontally over the runway (R) and transversally to the direction of travel (V) of the vehicle (A), and the radar sensor (11) is designed to scan the detection region (E) by means of microwaves, enables vehicles moving on runways to be detected with higher measuring precision, higher sensor reliability and using a robust measuring principle.
    • 本发明涉及一种用于在机场跑道(R)上特别是起飞或着陆带,滑行带或在斜坡区域中检测车辆,特别是飞行器(A)的装置(10),所述装置包括 至少一个雷达传感器(11),其布置在跑道(R)的区域中,并用于通过雷达波束扫描空间检测区域(E)。 检测区域(E)包括在跑道(R)上水平延伸并且横向于车辆(A)的行进方向(V)的两个叶状部分区域(E1,E2)以及雷达传感器 (11)设计为通过微波扫描检测区域(E),使得能够以更高的测量精度,更高的传感器可靠性和使用鲁棒的测量原理检测跑道上行驶的车辆。