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。

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）。

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。

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）。

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

IPC分类号： H05K3/30 ,  B60Q1/00 ,  B60Q1/26

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。

公开(公告)号：US20130077332A1

公开(公告)日：2013-03-28

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： B64D47/06

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。