公开(公告)号：US09327843B2

公开(公告)日：2016-05-03

申请号：US14249934

申请日：2014-04-10

Applicant: Goodrich Lighting Systems GmbH

Inventor： Anil Kumar Jha ,  Christian Schoen ,  Andre Hessling

IPC: B64D47/06

CPC classification number: B64D47/06 ,  B64D2203/00

Abstract: A strobe light unit, particularly wing anti-collision strobe light unit for an aircraft, comprises at least one light source, particularly at least one LED; a reflector element, the at least one light source and the reflector element being configured for projecting light into a desired range of directions; and a stray light blocking element for blocking stray light from being projected into undesired directions, the stray light blocking element attached to the reflector element or to a base portion of the strobe light unit.

Abstract translation: 闪光灯单元，特别是用于飞行器的机翼防冲击频闪灯单元，包括至少一个光源，特别是至少一个LED; 反射器元件，所述至少一个光源和反射器元件被配置为将光投射到期望的方向范围; 以及用于阻止杂散光投射到不想要的方向的杂散光阻挡元件，杂散光阻挡元件附接到反射器元件或闪光灯单元的基部。

公开(公告)号：US08851718B2

公开(公告)日：2014-10-07

申请号：US13712133

申请日：2012-12-12

Applicant: Goodrich Lighting Systems GmbH

Inventor： Anil Kumar Jha ,  Andre Hessling ,  Christian Schön

IPC: B64D47/06 ,  B64D47/04

CPC classification number: B64D47/06 ,  B64D47/04 ,  B64D2203/00

Abstract: An integrated aircraft landing and taxi light includes upper and lower reflector regions in the shape of substantially circular segments and a central longitudinal third reflector region extending between the upper and lower reflector regions. Landing light LEDs are arranged within the upper and lower reflector regions and the outer portions of the central longitudinal reflector region with the diagonals of the LED dies oriented substantially along radial lines extending outward from the center of the light. Taxi light LEDs are arranged within the central and outer portions of the central longitudinal reflector region such that the sides of the LED dies are oriented substantially horizontally and vertically with respect to the aircraft.

Abstract translation: 集成的飞机着陆和出租车灯包括大致圆形段的形式的上反射器区域和下反射器区域以及在上反射器区域和下反射器区域之间延伸的中心纵向第三反射器区域。 着陆光LED布置在上反射器区域和下反射器区域内，并且具有LED的对角线的中心纵向反射器区域的外部部分基本上沿着从光的中心向外延伸的径向线定向。 出租车灯LED布置在中央纵向反射器区域的中心部分和外部部分内，使得LED管芯的侧面相对于飞机基本水平和垂直地定向。

公开(公告)号：US08974097B2

公开(公告)日：2015-03-10

申请号：US13644380

申请日：2012-10-04

Applicant: Goodrich Lighting Systems GmbH

Inventor： Andre Hessling ,  Robert Trinscheck ,  Siegfried Schmees ,  Mike Herberhold ,  Stefan Thomassin

IPC: H05B33/08

CPC classification number: H05B33/0854 ,  B64D47/06 ,  B64D2203/00

Abstract: A method for controlling an aircraft having a plurality of LEDs, light so as to emit a desired light intensity includes the steps of providing a reference LED located within or outside of the aircraft light, providing thermal conditions resulting in a thermal stress for the reference LED similar to the maximum thermal stress, and observing the reference LED by means of an optical sensor for monitoring the optical aging behavior of the reference LED throughout its lifetime. The desired light intensity of the aircraft light is achieved by controlling the plurality of LEDs in accordance with the monitored aging behavior of the reference LED.

Abstract translation: 一种用于控制具有多个LED的飞行器的方法，用于发射所需光强度的光包括以下步骤：提供位于飞行器内部或外部的参考LED，提供导致参考LED的热应力的热条件 类似于最大热应力，并通过光学传感器观察参考LED，用于在整个寿命期间监测参考LED的光老化行为。 通过根据监视的参考LED的老化行为控制多个LED来实现飞行器光的期望的光强度。

公开(公告)号：US20130155706A1

公开(公告)日：2013-06-20

申请号：US13712133

申请日：2012-12-12

Applicant: Goodrich Lighting Systems GmbH

Inventor： Anil Kumar Jha ,  Andre Hessling ,  Christian Schön

IPC: B64D47/06

CPC classification number: B64D47/06 ,  B64D47/04 ,  B64D2203/00

Abstract: An integrated aircraft landing and taxi light includes upper and lower reflector regions in the shape of substantially circular segments and a central longitudinal third reflector region extending between the upper and lower reflector regions. Landing light LEDs are arranged within the upper and lower reflector regions and the outer portions of the central longitudinal reflector region with the diagonals of the LED dies oriented substantially along radial lines extending outward from the center of the light. Taxi light LEDs are arranged within the central and outer portions of the central longitudinal reflector region such that the sides of the LED dies are oriented substantially horizontally and vertically with respect to the aircraft.

Abstract translation: 集成的飞机着陆和出租车灯包括大致圆形段的形式的上反射器区域和下反射器区域以及在上反射器区域和下反射器区域之间延伸的中心纵向第三反射器区域。 着陆光LED布置在上反射器区域和下反射器区域内，并且具有LED的对角线的中心纵向反射器区域的外部部分基本上沿着从光的中心向外延伸的径向线定向。 出租车灯LED布置在中央纵向反射器区域的中心部分和外部部分内，使得LED管芯的侧面相对于飞机基本水平和垂直地定向。

公开(公告)号：US09771168B2

公开(公告)日：2017-09-26

申请号：US14707207

申请日：2015-05-08

Applicant: GOODRICH LIGHTING SYSTEMS GMBH

Inventor： Andre Hessling

IPC: B64D47/02 ,  B64F1/20 ,  F21V1/20 ,  F21V21/00 ,  B64D47/06 ,  B62D47/02 ,  F21V29/02 ,  F21V29/60 ,  F21V29/71 ,  F21W101/06 ,  F21Y115/10

CPC classification number: B64D47/06 ,  B62D47/02 ,  B64D2203/00 ,  F21V29/60 ,  F21V29/713 ,  F21W2107/30 ,  F21Y2115/10

Abstract: An aircraft light comprises a housing, at least one light source to be cooled, the at least one light source being arranged in the housing, a heat sink element thermally coupled to the at least one light source and defining a cooling surface exposable to a cooling airstream for the cooling airstream to flow along the cooling surface in a flow direction. The cooling surface extends between upstream and downstream end portions spaced apart in the flow direction and means for generating a pressure difference between the upstream and downstream end portions of the cooling surface. Due to the pressure difference, a cooling airstream flowing along the cooling surface is created.

公开(公告)号：US08985819B2

公开(公告)日：2015-03-24

申请号：US13626085

申请日：2012-09-25

Applicant: Goodrich Lighting Systems GmbH

Inventor： Andre Hessling

IPC: B64D47/06 ,  F21V29/00

CPC classification number: B64D47/06 ,  B64D2203/00 ,  F21V29/00

Abstract: An aircraft light for emitting light in a desired spatial angular region and with a desired light distribution, comprises a reflector having an upper reflector portion and a lower reflector portion both being symmetrical to a plane. A first row of LEDs are face away from the reflector. A second row of LEDs face towards the reflector. Each of the upper and lower portions of the reflector comprises first, second, and third reflective surfaces with the first reflective surface being convexly shaped, the second reflective surface being substantially flat, and the third reflective surface being partially parabolically shaped.

Abstract translation: 用于在期望的空间角度区域中发射光并具有期望的光分布的飞行器光包括具有上反射器部分和下反射器部分的反射器，两者都与平面对称。 第一排LED背离反射器。 第二排LED朝向反射器。 反射器的上部和下部中的每一个包括第一，第二和第三反射表面，其中第一反射表面是凸形的，第二反射表面基本上是平的，并且第三反射表面是部分抛物线形的。

公开(公告)号：US20140328074A1

公开(公告)日：2014-11-06

申请号：US14249934

申请日：2014-04-10

Applicant: Goodrich Lighting Systems GmbH

Inventor： Anil Kumar Jha ,  Christian Schoen ,  Andre Hessling

IPC: B64D47/06

CPC classification number: B64D47/06 ,  B64D2203/00

Abstract: A strobe light unit, particularly wing anti-collision strobe light unit for an aircraft, comprises at least one light source, particularly at least one LED; a reflector element, the at least one light source and the reflector element being configured for projecting light into a desired range of directions; and a stray light blocking element for blocking stray light from being projected into undesired directions, the stray light blocking element attached to the reflector element or to a base portion of the strobe light unit.

Abstract translation: 闪光灯单元，特别是用于飞行器的机翼防冲击频闪灯单元，包括至少一个光源，特别是至少一个LED; 反射器元件，所述至少一个光源和反射器元件被配置为将光投射到期望的方向范围; 以及用于阻止杂散光投射到不想要的方向的杂散光阻挡元件，杂散光阻挡元件附接到反射器元件或闪光灯单元的基部。

公开(公告)号：US20130314256A1

公开(公告)日：2013-11-28

申请号：US13901754

申请日：2013-05-24

Applicant: Goodrich Lighting Systems GmbH

Inventor： Andre Hessling ,  Alexander Wernicke ,  Anil Kumar Jha ,  Christian Schoen

IPC: B64F1/00 ,  F21K99/00 ,  B64F1/18

CPC classification number: F21V29/60 ,  B60Q1/2696 ,  B64D2203/00 ,  B64F1/002 ,  B64F1/18 ,  B64F1/205 ,  F21K9/60 ,  F21V3/061 ,  F21V3/062 ,  F21V7/0008 ,  F21V7/0025 ,  F21V7/048 ,  F21V7/09 ,  F21V29/54 ,  F21V29/70 ,  F21W2111/06 ,  F21Y2115/10 ,  G08B5/36

Abstract: Aerospace ground maneuver light, comprises a reflector (14), the reflector (14) defining a light exit plane (18), an LED light source (26) arranged outside of the area defined by the reflector (14) and its light exit plane (18), and a mounting bar (22) which has a longitudinal extension and at which the LED light source (26) is mounted. The mounting bar (22) extends across the reflector (14) and is spaced apart from the light exit plane (18) of the reflector (14) and comprises a mounting side (24) facing towards the reflector (14) and its light exit plane (18), with the LED light source (26) arranged on the mounting side (24) for emitting light towards the reflector (14).

Abstract translation: 航空地面机动灯包括反射器（14），反射器（14）限定光出射平面（18），布置在由反射器（14）限定的区域的外部的LED光源（26）和其光出射平面 （18），以及安装杆（22），其具有纵向延伸并且安装有所述LED光源（26）。 安装杆（22）延伸穿过反射器（14）并且与反射器（14）的光出射平面（18）间隔开并且包括面向反射器（14）的安装侧（24）和其光出口 平面（18），其中LED光源（26）布置在安装侧（24）上，用于向反射器（14）发射光。