-
公开(公告)号：US20220212802A1
公开(公告)日：2022-07-07
申请号：US17566244
申请日：2021-12-30
发明人： Carsten Pawliczek , Robert Trinschek , Andreas Ueberschaer , Marion Depta , Bjoern Schallenberg
摘要： A method of assigning a passenger to a lavatory within an aircraft passenger cabin, wherein the aircraft passenger cabin comprises at least two lavatories, each having a waiting queue, and wherein the aircraft passenger cabin is divided into at least two spatial zones, includes: receiving a lavatory assignment request from a passenger; based on a seat location of said passenger, determining a particular spatial zone of the aircraft passenger cabin which includes the seat location of said passenger; and based on the particular spatial zone, adding the passenger to the waiting queue of a particular lavatory, associated with the particular spatial zone. The configuration of the at least two spatial zones is variable and it is based on a plurality of zone configuration parameters including a queue length of each of the waiting queues of the at least two lavatories.
-
公开(公告)号：US11851208B2
公开(公告)日：2023-12-26
申请号：US17700772
申请日：2022-03-22
IPC分类号： B64D47/06 , F21V5/00 , F21Y105/18 , F21Y113/10
CPC分类号： B64D47/06 , F21V5/007 , F21Y2105/18 , F21Y2113/10
摘要： An aircraft anti-collision light includes a first group of light sources arranged in a first annular configuration around an axis (A) and a second group of light sources arranged in a second annular configuration. The first group of light sources is surrounded by the second group of light sources. The light also has a first lens structure, which is configured for generating a first light output from light emitted by the first group of light sources, a second lens structure, which is configured for generating a second light output from light emitted by the second group of light sources, and a light transmissive cover, which is arranged over the first lens structure and the second lens structure and which passes the first light output and the second light output for emitting a total light output.
-
公开(公告)号：US11465772B2
公开(公告)日：2022-10-11
申请号：US17075921
申请日：2020-10-21
摘要： An exterior aircraft image projector includes at least one light source, providing a light output in operation; an optical system configured for transforming the light output of the at least one light source into a light beam and projecting said light beam onto the ground below the aircraft and the of the aircraft; a photo detector arranged to detect a brightness level (Iambient) of the ground or the exterior and configured to provide a corresponding brightness signal; and a controller, coupled to the photo detector and the at least one light source configured to control an intensity of the light output of the at least one light source as a function of the brightness level (Iambient), as provided by the photo detector via the brightness signal.
-
4.发明申请Aircraft Interior Light Unit and Method of Operating an Aircraft Interior Light Unit 有权飞机内部灯单元和操作飞机内部灯单元的方法公开(公告)号：US20170015436A1
公开(公告)日：2017-01-19
申请号：US15210167
申请日：2016-07-14
CPC分类号： B64D47/02 , B64D11/00 , B64D2203/00 , F21V3/00 , F21Y2115/10 , G02B6/00 , G02B6/0043 , G02B6/0055 , G09F9/302 , G09F9/33 , G09F13/04 , G09F13/10 , G09F13/16 , G09F13/18 , G09F13/22 , G09F21/10 , G09F2013/049 , G09F2013/1831 , G09F2013/222 , G09F2013/227
摘要： An aircraft interior light unit having a light output over an extended light emission area includes a flat light distribution body having a front surface, through which the light output is coupled out, and a back surface, wherein at least one of the front surface and the back surface of the flat light distribution body has a plurality of surface irregularities.
摘要翻译： 具有在扩展的发光区域上的光输出的飞行器内部照明单元包括平坦的配光体，该平面配光体具有前表面，光输出被耦合出来的前表面和后表面，其中，前表面和 平面配光体的后表面具有多个表面凹凸。
-
公开(公告)号：US11435053B2
公开(公告)日：2022-09-06
申请号：US17169821
申请日：2021-02-08
摘要： A cover for an exterior aircraft light includes a lens cover structure, attachable to an exterior aircraft light housing and configured to close the exterior aircraft light housing, wherein the lens cover structure has an inside and an outside and is at least partially made of transparent material; and a wear indicator, attached to the inside of the lens cover structure, the wear indicator having a contrasted pattern visible from the outside of the lens cover structure through the transparent material.
-
公开(公告)号：US10914446B2
公开(公告)日：2021-02-09
申请号：US16443061
申请日：2019-06-17
摘要： A cover for an exterior aircraft light includes a lens cover structure, attachable to an exterior aircraft light housing and configured to close the exterior aircraft light housing, wherein the lens cover structure has an inside and an outside and is at least partially made of transparent material; and a wear indicator, attached to the inside of the lens cover structure, the wear indicator having a contrasted pattern visible from the outside of the lens cover structure through the transparent material.
-
公开(公告)号：US10793288B2
公开(公告)日：2020-10-06
申请号：US16362893
申请日：2019-03-25
摘要： An aircraft vertical stabilizer illumination light, the light includes a LED group, having a plurality of LEDs; an optical system, having at least one optical element, the optical system being associated with the LED group for shaping a light output from the light emitted by the LED group; an image generator, arranged within the aircraft vertical stabilizer illumination light for being oriented towards the vertical stabilizer, the image generator being configured to provide image data of the vertical stabilizer; and a controller, coupled to the image generator for receiving the image data; wherein the controller is configured to operate the aircraft vertical stabilizer illumination light in a plurality of operating modes.
-
8.发明授权公开(公告)号：US10085323B2
公开(公告)日：2018-09-25
申请号：US15680303
申请日：2017-08-18
CPC分类号： H05B37/0218 , B60Q1/1423 , B60Q1/245 , B64D47/04 , B64D2203/00 , H05B33/0854
摘要： A helicopter search light comprises a lighting arrangement comprising at least one light source and having an adjustable light output; a light detector, which is configured for detecting light reflected by the ground and/or at least one item on the ground and for providing a detection signal which is correlated to an amount of light detected; and a control unit, coupled to the light detector for receiving the detection signal and to the at least on light source for controlling the adjustable light output of the lighting arrangement.
-
公开(公告)号：US09731840B2
公开(公告)日：2017-08-15
申请号：US15210167
申请日：2016-07-14
IPC分类号： F21V8/00 , G06F17/50 , B64D47/02 , G02B6/00 , G09F9/302 , G09F9/33 , G09F13/04 , G09F13/18 , G09F21/10 , B64D11/00 , F21V3/00 , G09F13/10 , G09F13/16 , G09F13/22 , F21Y115/10
CPC分类号： B64D47/02 , B64D11/00 , B64D2203/00 , F21V3/00 , F21Y2115/10 , G02B6/00 , G02B6/0043 , G02B6/0055 , G09F9/302 , G09F9/33 , G09F13/04 , G09F13/10 , G09F13/16 , G09F13/18 , G09F13/22 , G09F21/10 , G09F2013/049 , G09F2013/1831 , G09F2013/222 , G09F2013/227
摘要： An aircraft interior light unit having a light output over an extended light emission area includes a flat light distribution body having a front surface, through which the light output is coupled out, and a back surface, wherein at least one of the front surface and the back surface of the flat light distribution body has a plurality of surface irregularities.
-
-
-
-
-
-
-
-
搜索结果
9 条记录 (耗时 0.018 秒)
