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公开(公告)号：US08579479B2
公开(公告)日：2013-11-12
申请号：US12996831
申请日：2009-06-19
申请人： Carsten Kohlmeier-Beckmann , Martin Griesbach , Bernhard Müller , Sonja Ferling , Andre Hessling , Sascha Lüder
发明人： Carsten Kohlmeier-Beckmann , Martin Griesbach , Bernhard Müller , Sonja Ferling , Andre Hessling , Sascha Lüder
IPC分类号： B64D47/02
CPC分类号： B64D47/06 , B64D2203/00 , F21S43/14 , F21S45/43 , F21S45/47 , F21V29/70 , F21V29/74 , F21V29/83 , F21W2107/30 , F21W2111/00 , F21Y2115/10
摘要： The warning lamp for an aircraft is provided with a housing (10) which possesses a light permeable cover (12) that is exposed to the surrounding air when the housing is mounted on the aircraft, with a frontal cover area and a rear cover area, a mounting element (44) to fasten the cover to a lower part (14) of the housing (10), wherein one edge (41) of the cover (12) is covered by an edge of the mounting element (44) and protrudes from it, a lamp with at least one LED (42,46,58,60), which is arranged within an area that is covered by the cover (12), and a cooling body (18) for the at least one LED (42,46,58,60), wherein the cooling body (18) possesses a cooling surface (32) that is exposed to the surrounding air when the housing (10) is mounted on the aircraft. The frontal cover area is formed by a frontal cover element (22) which is made from a light permeable first material. The rear cover area is formed by a rear cover element (28), which is made from a light permeable second material. The cooling body (18), while separating the frontal cover element (22) from the rear cover element (28), is arranged between them, wherein its cooling surface (32) is a part of the external contours of the cover (12) of the housing (10) that is given by the frontal and rear cover elements (22,28) and possesses an upper region (38) as well as adjacent, opposing side areas (40).
摘要翻译： 用于飞行器的警示灯设置有壳体（10），该壳体具有透光罩（12），当壳体安装在飞行器上时，该透光罩暴露于周围的空气，具有正面盖区域和后盖区域， 安装元件（44），用于将盖子紧固到壳体（10）的下部（14），其中盖（12）的一个边缘（41）被安装元件（44）的边缘覆盖并且突出 一种具有至少一个LED（42,46,58,60）的灯，其布置在由所述盖（12）覆盖的区域内，以及用于所述至少一个LED的冷却体（18） 42,46,58,60），其中所述冷却体（18）具有当壳体（10）安装在飞机上时暴露于周围空气的冷却表面（32）。 正面覆盖区域是由可透光的第一材料制成的前盖元件（22）形成的。 后盖区域由可透光的第二材料制成的后盖元件（28）形成。 冷却体（18）在将前盖元件（22）与后盖元件（28）分离的同时被布置在它们之间，其中其冷却表面（32）是盖子（12）的外部轮廓的一部分， 由前侧和后盖元件（22,28）给出并具有上部区域（38）以及相邻的相对的侧部区域（40）的壳体（10）。
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公开(公告)号：US20110261577A1
公开(公告)日：2011-10-27
申请号：US12996831
申请日：2009-06-19
申请人： Carsten Kohlmeier-Beckmann , Martin Griesbach , Bernhard Müller , Sonja Ferling , Andre Hessling , Sascha Lüder
发明人： Carsten Kohlmeier-Beckmann , Martin Griesbach , Bernhard Müller , Sonja Ferling , Andre Hessling , Sascha Lüder
IPC分类号： F21S8/10
CPC分类号： B64D47/06 , B64D2203/00 , F21S43/14 , F21S45/43 , F21S45/47 , F21V29/70 , F21V29/74 , F21V29/83 , F21W2107/30 , F21W2111/00 , F21Y2115/10
摘要： The warning lamp for an aircraft is provided with a housing (10) which possesses a light permeable cover (12) that is exposed to the surrounding air when the housing is mounted on the aircraft, with a frontal cover area and a rear cover area, a mounting element (44) to fasten the cover to a lower part (14) of the housing (10), wherein one edge (41) of the cover (12) is covered by an edge of the mounting element (44) and protrudes from it, a lamp with at least one LED (42,46,58,60), which is arranged within an area that is covered by the cover (12), and a cooling body (18) for the at least one LED (42,46,58,60), wherein the cooling body (18) possesses a cooling surface (32) that is exposed to the surrounding air when the housing (10) is mounted on the aircraft. The frontal cover area is formed by a frontal cover element (22) which is made from a light permeable first material. The rear cover area is formed by a rear cover element (28), which is made from a light permeable second material. The cooling body (18), while separating the frontal cover element (22) from the rear cover element (28), is arranged between them, wherein its cooling surface (32) is a part of the external contours of the cover (12) of the housing (10) that is given by the frontal and rear cover elements (22,28) and possesses an upper region (38) as well as adjacent, opposing side areas (40).
摘要翻译： 用于飞行器的警示灯设置有壳体（10），该壳体具有透光罩（12），当壳体安装在飞行器上时，该透光罩暴露于周围的空气，具有正面盖区域和后盖区域， 安装元件（44），用于将盖子紧固到壳体（10）的下部（14），其中盖（12）的一个边缘（41）被安装元件（44）的边缘覆盖并且突出 一种具有至少一个LED（42,46,58,60）的灯，其布置在由所述盖（12）覆盖的区域内，以及用于所述至少一个LED的冷却体（18） 42,46,58,60），其中所述冷却体（18）具有当壳体（10）安装在飞机上时暴露于周围空气的冷却表面（32）。 正面覆盖区域是由可透光的第一材料制成的前盖元件（22）形成的。 后盖区域由可透光的第二材料制成的后盖元件（28）形成。 冷却体（18）在将前盖元件（22）与后盖元件（28）分离的同时被布置在它们之间，其中其冷却表面（32）是盖子（12）的外部轮廓的一部分， 由前侧和后盖元件（22,28）给出并具有上部区域（38）以及相邻的相对的侧部区域（40）的壳体（10）。
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公开(公告)号：US08006376B2
公开(公告)日：2011-08-30
申请号：US12125645
申请日：2008-05-22
申请人： Sonja Ferling , Sascha Lüder , Martin Griesbach , Andre Hessling
发明人： Sonja Ferling , Sascha Lüder , Martin Griesbach , Andre Hessling
CPC分类号： F21V17/101 , B60Q3/44 , B60Q3/76 , F21K9/00 , F21V7/0066 , F21V29/70 , F21Y2115/10 , G02B27/62 , Y10T29/49004 , Y10T29/4913 , Y10T29/49133
摘要： The method for assembly of an LED lighting device comprising an LED module and a reflective and/or refractive optical unit and provided particularly as a reading or seat light for use in a vehicle such as, e.g., an airplane, a train or a bus, comprises the following steps: providing an LED module (12) comprising at least one LED (22), providing a reflective and/or refractive optical unit (14) for illuminating a measuring plane by use of electromagnetic radiation from the LED module (12) and with the aid of said optical unit, arranging the optical unit (14) and the LED module (12) for later fixation to each other, driving the LED module (12) to cause it to emit electromagnetic radiation for illuminating a measuring plane, detecting at least a part of the electromagnetic radiation of the LED module (12) that is incident on the measuring plane, by use of a detector (18), moving the LED module (12) relative to the optical unit (14) and/or the optical unit (14) relative to the LED module (12) along the optical axis (16), until the detector (18) detects electromagnetic radiation of the LED module (12) of a presettable intensity, and fixing the optical unit (14) and the LED module (12) relative to each other in their current relative positions.
摘要翻译： 一种用于组装LED照明装置的方法，包括LED模块和反射和/或折射光学单元，并且特别地用作用于诸如飞机，火车或公共汽车的车辆的读取或座椅灯， 包括以下步骤：提供包括至少一个LED（22）的LED模块（12），其提供用于通过使用来自所述LED模块（12）的电磁辐射来照亮测量平面的反射和/或折射光学单元（14） 并且借助于所述光学单元，将所述光学单元（14）和所述LED模块（12）布置成用于稍后的固定，驱动所述LED模块（12）使其发射用于照射测量平面的电磁辐射， 通过使用检测器（18）来检测入射在测量平面上的LED模块（12）的至少一部分电磁辐射，使LED模块（12）相对于光学单元（14）移动和/ 或所述光学单元（14）相对于所述LED模块（1） 2）沿着光轴（16），直到检测器（18）检测到LED模块（12）的电磁辐射为可预见的强度，并且相对于彼此固定光学单元（14）和LED模块（12） 在当前的相对位置。
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公开(公告)号：US20090025202A1
公开(公告)日：2009-01-29
申请号：US12125645
申请日：2008-05-22
申请人： Sonja Ferling , Sascha Luder , Martin Griesbach , Andre Hessling
发明人： Sonja Ferling , Sascha Luder , Martin Griesbach , Andre Hessling
IPC分类号： G01R31/28
CPC分类号： F21V17/101 , B60Q3/44 , B60Q3/76 , F21K9/00 , F21V7/0066 , F21V29/70 , F21Y2115/10 , G02B27/62 , Y10T29/49004 , Y10T29/4913 , Y10T29/49133
摘要： The method for assembly of an LED lighting device comprising an LED module and a reflective and/or refractive optical unit and provided particularly as a reading or seat light for use in a vehicle such as, e.g., an airplane, a train or a bus, comprises the following steps: providing an LED module (12) comprising at least one LED (22), providing a reflective and/or refractive optical unit (14) for illuminating a measuring plane by use of electromagnetic radiation from the LED module (12) and with the aid of said optical unit, arranging the optical unit (14) and the LED module (12) for later fixation to each other, driving the LED module (12) to cause it to emit electromagnetic radiation for illuminating a measuring plane, detecting at least a part of the electromagnetic radiation of the LED module (12) that is incident on the measuring plane, by use of a detector (18), moving the LED module (12) relative to the optical unit (14) and/or the optical unit (14) relative to the LED module (12) along the optical axis (16), until the detector (18) detects electromagnetic radiation of the LED module (12) of a presettable intensity, and fixing the optical unit (14) and the LED module (12) relative to each other in their current relative positions.
摘要翻译： 一种用于组装LED照明装置的方法，包括LED模块和反射和/或折射光学单元，并且特别地用作用于诸如飞机，火车或公共汽车的车辆的读取或座椅灯， 包括以下步骤：提供包括至少一个LED（22）的LED模块（12），其提供用于通过使用来自所述LED模块（12）的电磁辐射来照亮测量平面的反射和/或折射光学单元（14） 并且借助于所述光学单元，将所述光学单元（14）和所述LED模块（12）布置成用于稍后的固定，驱动所述LED模块（12）使其发射用于照射测量平面的电磁辐射， 通过使用检测器（18）来检测入射在测量平面上的LED模块（12）的至少一部分电磁辐射，使LED模块（12）相对于光学单元（14）移动和/ 或所述光学单元（14）相对于所述LED模块（1） 2）沿着光轴（16），直到检测器（18）检测到LED模块（12）的电磁辐射为可预见的强度，并且相对于彼此固定光学单元（14）和LED模块（12） 在当前的相对位置。
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公开(公告)号：US09260201B2
公开(公告)日：2016-02-16
申请号：US13629322
申请日：2012-09-27
申请人： Andre Hessling , Martin Griesbach
发明人： Andre Hessling , Martin Griesbach
IPC分类号： H05B33/08 , B64D47/06 , F21V5/04 , F21V7/00 , F21V7/08 , F21V13/02 , F21V13/04 , B64D47/04 , F21Y101/02 , F21Y103/02 , F21Y113/02
CPC分类号： B64D47/06 , B64D47/04 , B64D2203/00 , F21V5/046 , F21V7/0016 , F21V7/0033 , F21V7/0058 , F21V7/08 , F21V13/02 , F21V13/04 , F21Y2103/33 , F21Y2113/20 , F21Y2115/10
摘要： A light for an aircraft comprises a holder for carrying a first group of light emitting diodes arranged along a curvilinear line and a first reflector having an elliptic reflective partial surface defining a plurality of focal points forming a first curvilinear focal line coinciding with the light emitting sites of the first group of light emitting diodes and second focal point or curvilinear focal line. The light further includes a second optical unit comprising a single further focal point or curvilinear focal line that coincides with the second focal point or focal line of the first reflector. The light further includes a second group of light emitting diodes displaced axially with respect to the first light emitting diodes, which emit light that bypasses the second focal point or focal line of the first reflector of the first optical unit.
摘要翻译： 用于飞行器的光包括用于承载沿着曲线布置的第一组发光二极管的保持器和具有椭圆反射部分表面的第一反射器，所述第一反射器限定多个焦点，所述第一反射部分表面形成与发光部位重合的第一曲线焦线 的第一组发光二极管和第二焦点或曲线焦线。 光进一步包括第二光学单元，其包括与第一反射器的第二焦点或焦线重合的单个另外焦点或曲线焦线。 光进一步包括相对于第一发光二极管轴向移动的第二组发光二极管，其发射绕过第一光学单元的第一反射器的第二焦点或焦线的光。
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公开(公告)号：US06572304B1
公开(公告)日：2003-06-03
申请号：US09623566
申请日：2000-11-17
IPC分类号： F16B2100
CPC分类号： B64D11/0696 , B60R11/00 , F16B37/045 , Y10T403/59 , Y10T403/591
摘要： A device is provided for fastening a first part to a stationary second part, in particular to a part of a vehicle, having a fastening element which can be connected to the first part and has at least one locking element arranged so it cannot be lost, such that it can be brought into a locked position where the first part is joined to the second part and it can also be brought into an unlocked position where the first part is released from the second part, where the fastening element has a top part facing the second part and a bottom part facing the first part, where the top part and the bottom part are designed to pivot about a pivot axis, and the locking element is mounted on the top part.
摘要翻译： 提供一种用于将第一部分固定到固定的第二部分，特别是车辆的一部分的装置，其具有可连接到第一部分的紧固元件，并且具有布置成不会丢失的至少一个锁定元件， 使得其可以进入锁定位置，其中第一部分连接到第二部分，并且其也可以进入解锁位置，其中第一部分从第二部分释放，其中紧固元件具有顶部朝向 第二部分和面向第一部分的底部部分，其中顶部部分和底部部分设计成围绕枢转轴线枢转，并且锁定元件安装在顶部部分上。
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公开(公告)号：US20130154476A1
公开(公告)日：2013-06-20
申请号：US13714846
申请日：2012-12-14
申请人： Andre Hessling
发明人： Andre Hessling
CPC分类号： H05B37/02 , B64D47/02 , B64D47/06 , B64D2203/00 , H05B33/0854 , H05B33/0893
摘要： An anti-collision aircraft light comprises at least one LED and a control unit for operating the at least one LED in a pulsed manner. In this anti-collision aircraft light, the control unit comprises an ambient temperature sensor for sensing the ambient temperature and an adjustable current control for setting an LED operating current depending on the sensed ambient temperature. The control unit further includes a light intensity sensor for sensing the intensity of the light emitted from the at least one LED, an integrator connected to the light sensor for integrating the sensed light intensity, and a comparator for comparing the integrated light intensity to a threshold value. The operating current for the at least one LED is interrupted as soon as the integrated light intensity is equal to the threshold value.
摘要翻译： 防撞飞机灯包括至少一个LED和用于以脉冲方式操作至少一个LED的控制单元。 在这种防碰撞飞机灯中，控制单元包括用于感测环境温度的环境温度传感器和用于根据检测到的环境温度来设定LED工作电流的可调电流控制。 所述控制单元还包括用于感测从所述至少一个LED发射的光的强度的光强度传感器，连接到所述光传感器以用于积分所述感测光强度的积分器和用于将所述积分光强度与阈值进行比较的比较器 值。 一旦集成光强度等于阈值，至少一个LED的工作电流就会中断。
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8.发明申请公开(公告)号：US20090010013A1
公开(公告)日：2009-01-08
申请号：US12166717
申请日：2008-07-02
申请人： Andre Hessling
发明人： Andre Hessling
IPC分类号： B64D47/02
CPC分类号： B64D47/06 , B64D2203/00
摘要： The light for a vehicle, particularly a flash warning light for an aircraft, is provided with at least one LED (10) bearing a semiconductor chip (14) emitting electromagnetic radiation. The semiconductor chip (14) emits blue or UV light. A conversion material (18) is arranged in the beam path that is permeable to low-energy radiation portions of the emitted light and is partly permeable to high-energy radiation portions of the emitted light, wherein a part of the high-energy radiation portions of the emitted light can be converted into low-energy radiation portions by the conversion material (18) The part of the high-energy radiation of the emitted light that penetrates the conversion material (18) is limited by means of an optical element and can partly be used again to increase efficiency.
摘要翻译： 用于车辆的光，特别是用于飞机的闪光警告灯，设置有至少一个带有发射电磁辐射的半导体芯片（14）的LED（10）。 半导体芯片（14）发出蓝色或紫外光。 转换材料（18）布置在所述光束路径中，其对所发射的光的低能辐射部分是可透过的，并且对于所发射的光的高能辐射部分是部分透过的，其中一部分高能辐射部分 通过转换材料（18）可以将发射的光转换成低能辐射部分。穿透转换材料（18）的发射光的高能辐射的一部分由光学元件限制，并且可以 部分再次被用来提高效率。
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公开(公告)号：US09132923B2
公开(公告)日：2015-09-15
申请号：US13450259
申请日：2012-04-18
申请人： Andre Hessling
发明人： Andre Hessling
CPC分类号： B64D47/06 , B62D47/02 , B64D2203/00 , F21V29/60 , F21V29/713 , F21W2107/30 , F21Y2115/10
摘要： An aircraft light comprises a housing (24), at least one light source (32) to be cooled, the at least one light source (32) being arranged in the housing (24), a heat sink element (26) thermally coupled to the at least one light source (32) and defining a cooling surface (36) exposable to a cooling airstream (52) for the cooling airstream (52) to flow along the cooling surface (36) in a flow direction. The cooling surface (36) extends between upstream and downstream end portions (40,42) spaced apart in the flow direction and means for generating a pressure difference between the upstream and downstream end portions (40,42) of the cooling surface. Due to the pressure difference, a cooling airstream (52) flowing along the cooling surface (36) is created.
摘要翻译： 飞机灯包括壳体（24），待冷却的至少一个光源（32），所述至少一个光源（32）布置在壳体（24）中;散热元件（26），热耦合到 所述至少一个光源（32）并且限定可暴露于冷却空气流（52）的冷却表面（36），以使冷却空气流（52）沿着流动方向沿着冷却表面（36）流动。 冷却表面（36）在沿流动方向间隔开的上游和下游端部（40,42）之间延伸，以及用于在冷却表面的上游和下游端部（40,42）之间产生压力差的装置。 由于压力差，产生沿着冷却表面（36）流动的冷却气流（52）。
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公开(公告)号：US08956021B2
公开(公告)日：2015-02-17
申请号：US13626510
申请日：2012-09-25
申请人： Andre Hessling
发明人： Andre Hessling
CPC分类号： F21S45/40 , B64D47/06 , B64D2203/00 , F21S43/14 , F21S45/47 , F21S45/48 , F28F2013/008
摘要： An aircraft light consists of a housing containing a light source, a heat sink element forming at least part of the exterior surface of the housing and an auxiliary thermal capacitor that is thermally decoupled from the heat sink element. A thermally expandable medium is coupled to the heat sink element and operates to thermally decouple the light source from the heat sink element and thermally couple the light source to the auxiliary thermal capacitor and vice versa, depending on the actual temperature of the heat sink element.
摘要翻译： 飞机灯由包含光源的壳体，形成壳体的外表面的至少一部分的散热元件和与散热元件热分离的辅助热电容器组成。 热膨胀介质耦合到散热元件，用于根据散热元件的实际温度，将光源与散热元件热分解并将光源热耦合到辅助热电容器，反之亦然。
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