专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明公开

EP4353591A1 ADAPTABLE LIGHTING SYSTEMS AND METHODS FOR AN INTERNAL CABIN OF A VEHICLE 审中-公开
公开(公告)号：EP4353591A1
公开(公告)日：2024-04-17
申请号：EP23189931.1
申请日：2023-08-07
申请人： The Boeing Company
发明人： BECKMAN, John Christiaan , CHANG, Julian K
IPC分类号： B64D11/00 , B64D9/00 , B64D47/02
CPC分类号： B64D2011/003820130101 , B64D11/00 , B64D9/00 , B64D2203/0020130101 , B64D47/02 , B60Q3/30 , B60Q3/43 , B60Q3/68 , B60Q3/70 , B60Q3/47 , A61L9/00
摘要： A system and a method include a lighting sub-system including one or more light fixtures (106) configured to be disposed within a cargo area of an internal cabin (102) of a vehicle (104). A control unit (112) is in communication with the one or more light fixtures (106). The control unit (112) is configured to control the one or more light fixtures (106). The control unit (112) is configured to selectively adjust light emitted from the one or more light fixtures (106) based on the cargo within the cargo area. The system and the method can also include one or more temperature control devices configured to one or both of adjust or maintain a temperature within the cargo area of the internal cabin (102) of the vehicle (104). The control unit (112) can be configured to control the one or more temperature control devices (122) based on the cargo within the cargo area.

2. 发明公开

EP3403934A1 DRAIN VALVE, EXTERIOR AIRCRAFT LIGHT UNIT AND POWER SUPPLY BOX 有权
公开(公告)号：EP3403934A1
公开(公告)日：2018-11-21
申请号：EP17171905.7
申请日：2017-05-19
申请人： Goodrich Lighting Systems GmbH
发明人： HESSLING-von HEIMENDAHL, Andre , JHA, Anil Kumar , LUEDER, Sascha , SRINIVASAMURTHY, Ramesh
IPC分类号： B64D47/02 , H05K5/02 , F21V31/03
CPC分类号： F16K1/32 , B64D47/02 , B64D2221/00 , F16K15/023 , F16K24/00 , F21S45/30 , F21V31/03
摘要： A drain valve (20) for draining liquid from an enclosed space (14) comprises a movable plunger (42), which is movable between a closed position in which the plunger (42) does not allow liquid to flow through the drain valve (20), and at least one open position, in which the plunger (42) allows liquid to flow through the drain valve (20); and an elastic element (40; 54), which is configured to urge the movable plunger (42) into its closed position. The plunger (42) is provided with at least one duct (44) extending through the plunger (42) and allowing fluid to flow through the drain valve (20) when the plunger (42) is positioned in its closed position, wherein said at least one duct (44) is closed by a semi-permeable medium (48), which is permeable for air and water vapor and impermeable for liquid water.

3. 发明公开

EP3342717A1 ILLUMINATION DEVICE FOR ILLUMINATING THE VERTICAL TAIL PLANE OF AN AIRCRAFT AND AIRCRAFT WITH EXTERIOR ILLUMINATION ON ITS VERTICAL TAIL PLANE 审中-公开
公开(公告)号：EP3342717A1
公开(公告)日：2018-07-04
申请号：EP16382665.4
申请日：2016-12-28
申请人： Airbus Operations, S.L.
发明人： DE BROUWER, Gabrielle Joséphine Christiane , GONZÁLEZ FERNÁNDEZ, Sergio , ROBLEDO BUENO, Jesús
IPC分类号： B64D47/06
CPC分类号： G09F21/10 , B64C5/02 , B64D47/02 , B64D47/06 , B64D2203/00 , F21S43/13 , F21S43/14 , F21S45/47 , F21V5/007 , F21V14/02 , F21V23/003 , F21V23/023 , F21Y2113/13 , F21Y2115/10 , F21Y2115/30 , H05B33/0845
摘要： Illumination device (1) for illuminating the vertical tail plane (9) of an aircraft (2), comprising:
- a matrix of LEDs (3) or lasers,
- a laser diode (4) with a diffractive optical element (5),
- an electronic board (6) with a microcontroller (16),
- a power supply unit (7), and
- a housing (8) that encloses one or all of the matrix of LEDs (3), the laser diode (4), the electronic board (6) and the power supply unit (7),
wherein the LEDs (3) or lasers and the laser diode (4) are individually and electronically controlled by the microcontroller (16), in such a way that the LEDs (3) or lasers can be individually dimmed to create a dynamic illumination pattern (14) on the side surfaces of the vertical tail plane (9), the illumination pattern (14) being transmitted by the microcontroller (16), and the laser diode (4) with the diffractive optical element (15) can create a fixed figure on the side surfaces of the vertical tail plane (9). The invention also refers to an aircraft (2) with exterior illumination on its vertical tail plane (9), comprising such illumination devices (1).

4. 发明授权

EP2579060B1 Laser light reflection method and device for aircraft-installed laser apparatus 有权
公开(公告)号：EP2579060B1
公开(公告)日：2018-06-06
申请号：EP12186362.5
申请日：2012-09-27
申请人： Japan Aerospace Exploration Agency
发明人： Inokuchi, Hamaki
IPC分类号： G01S17/93 , G01S7/497
CPC分类号： B64D47/02 , G01S7/4972 , G01S17/933
摘要： The present invention provides a laser light reflection device for an aircraft-installed laser apparatus with which, when a function check is performed on the aircraft-installed laser apparatus by emitting laser light from a parked aircraft to a body exterior, the emitted laser light can be reflected in a desired direction safely and efficiently. A reflection mirror is capable of autorotation about at least an in-plane horizontal axis thereof, and a support ring is attached to the reflection mirror so as to be capable of rotating about an in-plane vertical axis and the in-plane horizontal axis of the reflection mirror. Further, a laser pointer unit formed by inserting a laser pointer into a sleeve pipe is attached to the support ring so as to be oriented toward an in-plane of the reflection mirror. Furthermore, a guide scope is attached to the support ring such that an optical axis thereof matches an optical axis of the laser pointer unit.

5. 发明公开

EP3299298A1 DUAL MODE AIRCRAFT LIGHT ASSEMBLY 审中-公开
标题翻译：双模式飞机灯组件
公开(公告)号：EP3299298A1
公开(公告)日：2018-03-28
申请号：EP17164362.0
申请日：2017-03-31
申请人： Goodrich Lighting Systems, Inc.
发明人： FRANICH, David , LAPUJADE, Philippe
IPC分类号： B64D47/06 , F21V7/00
CPC分类号： B64D47/06 , B64D47/02 , B64D47/04 , B64D2203/00 , F21V7/00 , F21V11/16 , F21W2107/30 , F21Y2115/10
摘要： A dual mode light assembly (100) for a forward position light of an aircraft includes a base (110), a visible light source (120) mounted to the base that is configured to emit visible light, a covert light source (130) mounted to the base (110) that is configured to emit covert light, and a light shield (140) mounted to the base (110). The light shield (140) is configured to restrict transmission of the visible light to a visible light pattern and to restrict transmission of the covert light to a covert light pattern.
摘要翻译：一种用于飞行器的前向位置灯的双模式灯组件（100）包括基座（110），安装到基座的可见光源（120），该可见光源被配置为发射可见光，安装的隐蔽光源（130）到被配置成发射隐蔽光的基座（110），以及安装到基座（110）的遮光罩（140）。遮光板（140）被配置为限制可见光透射到可见光图案并且限制隐蔽光透射到隐形光图案。

6. 发明公开

EP3184432A1 TRANSLUCENT ILLUMINATED EVACUATION SLIDE 有权
标题翻译：半透明照明疏散幻灯片
公开(公告)号：EP3184432A1
公开(公告)日：2017-06-28
申请号：EP16184624.1
申请日：2016-08-17
申请人： Goodrich Corporation
发明人： HARTMAN, Drew , VOLNY, Jaro S.
IPC分类号： B64D25/14
CPC分类号： B64D25/14 , B64D47/02
摘要： An inflatable evacuation slide (200, 300) is provided. The slide (200, 300) may comprise a slide surface with a tubular member (202, 302) coupled to the slide surface. The tubular member (202, 302) may comprise a translucent material defining a chamber (206, 306) internal to the tubular member. A light source (208, 308) may be directed into the chamber (206, 306) and configured to illuminate the tubular member (202, 302) from within the chamber (206, 306).
摘要翻译：提供可充气的撤离滑梯（200,300）。滑块（200,300）可以包括滑动表面，该滑动表面具有联接到滑动表面的管状构件（202,302）。管状构件（202,302）可以包括限定管状构件内部的腔室（206,306）的半透明材料。光源（208,308）可以被引导到腔室（206,306）中并且被配置成从腔室（206,306）内照亮管状构件（202,302）。

7. 发明公开

EP3179591A1 SOLID STATE POWER CONTROLLER 审中-公开
标题翻译：固态功率控制器
公开(公告)号：EP3179591A1
公开(公告)日：2017-06-14
申请号：EP15199559.4
申请日：2015-12-11
申请人： HS Elektronik Systeme GmbH
发明人： Greither, Markus
IPC分类号： H02J3/00 , H03K17/081 , H03K17/13 , H03K17/687 , H03K17/689 , H03K17/725
CPC分类号： H02J3/00 , B64D47/02 , H02M1/08 , H02M3/04 , H02M5/293 , H03K17/08122 , H03K17/133 , H03K17/6874 , H03K2217/0009
摘要： Disclosed is a solid state power controller (10) configured to supply electric power from an AC power supply (14) to at least one load (16A, 16B) via at least one power distribution channel (12A, 12B), the at least one power distribution channel (12A, 12B) comprising a primary solid state switching device (22A, 22B) and a secondary solid state solid state switching device (24A, 24B) connected in series;
each of the primary and secondary solid state switching devices (22A, 24A, 22B, 24B) having a first terminal (D), a second terminal (S), and a control terminal (G), the solid state switching device (22A, 24A, 22B, 24B) configured to switch between an OFF operation mode in which the second terminal (S) is electrically disconnected from the first terminal (D), and an ON operation mode in which the second terminal (S) is electrically connected to the first terminal (D), according to a control voltage applied to the control terminal (G);
wherein the solid state power controller (10) comprises:
- a primary control terminal driver (30) configured to supply a primary control voltage to the control terminal (G) of the primary solid state switching device (22A, 22B) with respect to a reference potential (R); and
- a secondary control terminal driver (40A, 40B) configured to supply a secondary control voltage to the control terminal (G) of the secondary solid state switching device (24A, 24B).
摘要翻译：公开了一种固态功率控制器（10），其被配置为经由至少一个功率分配通道（12A，12B）从交流电源（14）向至少一个负载（16A，16B）供应电力，所述至少一个包括串联连接的主固态开关器件（22A，22B）和次级固态固态开关器件（24A，24B）的功率分配通道（12A，12B）每个具有第一端子（D），第二端子（S）和控制端子（G）的初级和次级固态开关器件（22A，24A，22B，24B），固态开关器件（22A，（S）与所述第一端子（D）电断开的断开动作模式和所述第二端子（S）与所述第二端子（S）电连接的导通动作模式之间进行切换的电路（图24A，图22B，根据施加到所述控制端子（G）的控制电压，所述第一端子（D）; 其中，所述固态功率控制器（10）包括：主控制端子驱动器（30），其被配置为向主固态开关器件（22A，22B）的控制端子（G）提供关于参考电位（R）; 以及 - 次级控制终端驱动器（40A，40B），其被配置为将次级控制电压提供给次级固态开关装置（24A，24B）的控制终端（G）。

8. 发明公开

EP3152111A4 DUST COVER ASSEMBLY WITH EDGE LIGHT 有权
标题翻译： STAUBSCHUTZABDECKUNGSANORDNUNG MIT KANTENLICHT
公开(公告)号：EP3152111A4
公开(公告)日：2017-05-24
申请号：EP15803977
申请日：2015-06-03
申请人： GENTEX CORP
发明人： ASH KEVIN L , VEENMAN STEVEN J
IPC分类号： B64C1/14 , G02F1/15
CPC分类号： F21V14/08 , B64C1/1492 , B64D47/02 , F21V11/00
摘要： A window assembly includes a pressure pane and a bezel proximate a periphery of the pressure pane and defining an inner opening. The bezel includes an inner wall with a channel. An electro-optic element is disposed in the inner opening and is received in the channel of the inner wall. The electro-optic element operates between a transmissive condition and a dimmed condition. A surface of the electro-optic element exhibits a first level of spectral reflectivity at least when in the dimmed condition. The assembly further includes a dust cover assembly proximate the bezel. The dust cover assembly including a light transmitting sheet and a plurality of light sources disposed at edges of the light transmitting sheet and to emit light into the light transmitting sheet to illuminate the light transmitting sheet with a diffuse light.
摘要翻译：窗户组件包括压力板和靠近压力板的周边并限定内部开口的挡板。表圈包括带通道的内壁。电光元件设置在内部开口中并容纳在内壁的通道中。电光元件在透射状态和暗淡状态之间工作。至少当处于调光状态时，电光元件的表面呈现第一水平的光谱反射率。该组件还包括靠近边框的防尘罩组件。防尘罩组件包括透光片和设置在透光片的边缘处的多个光源，并且将光发射到透光片中以利用漫射光来照射透光片。

9. 发明公开

EP3040282A1 Exterior aircraft light 审中-公开
标题翻译： Flugzeugaußenlicht
公开(公告)号：EP3040282A1
公开(公告)日：2016-07-06
申请号：EP15150020.4
申请日：2015-01-02
申请人： Goodrich Lighting Systems GmbH
发明人： Jha, Anil Kumar , Hessling von Heimendahl, Andre
IPC分类号： B64D47/04
CPC分类号： F21V5/048 , B64D47/02 , B64D47/04 , B64D2203/00 , F21S41/143 , F21V7/06 , F21W2107/30 , F21Y2115/10
摘要： An exterior aircraft light (20) includes a base plate (4) and a plurality of lighting units (2) arranged on the base plate, wherein each of the plurality of lighting units (2) includes an elongated LED light source (10) for emitting light, the elongated LED light source (10) having a light emitting surface with a longitudinal extension and a transverse extension, with the longitudinal extension being greater than the transverse extension and with a projection of the longitudinal extension onto the base plate (4) defining an orientation direction of the elongated LED light source, and a collimating optical system (12) for collimating the light emitted by the elongated LED light source (10) towards a main output direction, wherein the plurality of lighting units (2) has at least a first lighting unit (2-1) and a second lighting unit (2-2), with the orientation direction of the elongated LED light source (10-1) of the first lighting unit (2-1) and the orientation direction of the elongated LED light source (10-2) of the second lighting unit (2-2) being angled with respect to each other and with the main output direction of the first lighting unit (2-1) and the main output direction of the second lighting unit (2-2) being substantially parallel.
摘要翻译：外部飞机灯（20）包括基板（4）和布置在基板上的多个照明单元（2），其中多个照明单元（2）中的每一个包括细长LED光源（10），用于所述细长LED光源（10）具有具有纵向延伸部和横向延伸部的发光表面，所述纵向延伸部分大于所述横向延伸部，并且所述纵向延伸部分突出于所述基板（4）上，限定细长LED光源的取向方向;以及准直光学系统（12），用于将由细长LED光源（10）发射的光朝向主输出方向准直，其中多个照明单元（2）具有至少第一照明单元（2-1）和第二照明单元（2-2），其中第一照明单元（2-1）的细长LED光源（10-1）的取向方向和取向方向的细长第二照明单元（2-2）的LED光源（10-2）相对于彼此成角度并且与第一照明单元（2-1）的主输出方向和第二照明单元的主输出方向照明单元（2-2）基本上平行。

10. 发明公开

EP2993130A1 FEU LUMINEUX ET PROCÉDÉ DE FABRICATION D'UN TEL FEU 审中-公开
标题翻译：信号光与方法
公开(公告)号：EP2993130A1
公开(公告)日：2016-03-09
申请号：EP15182284.8
申请日：2015-08-25
申请人： NSE Industries
发明人： LAURIN, Guillaume , DISDIER, Patrick
IPC分类号： B64D25/00 , B64D47/02 , B64D45/00
CPC分类号： B64D47/02 , B64D2045/0045
摘要： Ce feu lumineux (10) comprend un socle (12), un capot de protection (14) et au moins une source lumineuse (16A, 16B) adaptée pour émettre un faisceau lumineux (52A, 52B) à travers le capot de protection (14), le socle (12) et le capot de protection (14) étant solidaires l'un de l'autre et formant un boitier de protection (20). Chaque source lumineuse (16A, 16B) est disposée à l'intérieur du boitier de protection.
Le feu lumineux (10) comprend en outre une antenne radioélectrique (18) solidaire du boitier de protection (20), l'antenne radioélectrique (18) étant adaptée pour émettre et/ou recevoir des ondes radioélectriques vers et/ou depuis l'extérieur du boitier de protection (20).

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式