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31. 发明申请

WO2006096223A2 DROP-IN HIGH INTENSITY DISCHARGE LAMP ASSEMBLY, AND RETROFIT METHOD OF DEPLOYING SAME 审中-公开
标题翻译：降低高强度放电灯组件及其改进方法
公开(公告)号：WO2006096223A2
公开(公告)日：2006-09-14
申请号：PCT/US2005/044020
申请日：2005-12-07
申请人： LUMINESCENT SYSTEMS, INC. , POWELL, John, Eddie
发明人： POWELL, John, Eddie
IPC分类号： F21S8/00
CPC分类号： B64D47/04 , F21S8/02 , F21V21/04 , F21W2107/30 , F21W2111/06
摘要： A retrofit HID lamp assembly, for use in a non-HID lighting receptacle, to provide HID illumination is disclosed. The lamp assembly includes (i) a housing compatible in size and shape with the receptacle, (ii) a base terminal structure coupled with the housing and adapted to mate with the receptacle, (iii) a ballast unit in the interior of the housing, (iv) a reflector overlying the ballast unit in the interior of the housing, (v) an HID lamp electrically coupled with the ballast unit and mounted in the interior of the housing, and (vi) a lens coupled with the housing. A corresponding fabrication methodology is described. The retrofit HID lamp assembly may be used to retrofit existing lighting installations such as PAR receptacles in exterior aircraft lightning systems, to provide a cost-efficient illumination upgrade.
摘要翻译：公开了一种用于非HID照明插座的改进型HID灯组件，用于提供HID照明。灯组件包括（i）尺寸和形状与壳体兼容的壳体，（ii）与壳体耦合并适于与插座配合的基座端子结构，（iii）壳体内部的压载单元，（iv）覆盖在壳体内部的镇流器单元的反射器，（v）与镇流器单元电耦合并安装在壳体内部的HID灯，以及（vi）与壳体耦合的透镜。描述相应的制造方法。改装的HID灯组件可用于改装现有的照明装置，例如外部飞机闪电系统中的PAR插座，以提供经济高效的照明升级。

32. 发明申请

WO2003050002A1 ELECTRONICALLY CONTROLLED AIRCRAFT RETRACTABLE LANDING LIGHT WITH MANUAL REFRACTION CAPABILITY 审中-公开
标题翻译：电子控制的具有手动折射能力的飞行器可回收的光线
公开(公告)号：WO2003050002A1
公开(公告)日：2003-06-19
申请号：PCT/US2002/037472
申请日：2002-11-21
申请人： HONEYWELL INTERNATIONAL INC.
发明人： BARNHART, Brian, J. , MUBASLAT, Saed, M. , HAMILTON, Scott, E. , GIFFEN, Craig, E.
IPC分类号： B64D47/04
CPC分类号： B64D47/04
摘要： An electronically controlled retractable landing light (100) for use with aircraft. A controller (106) compares the commanded position of a lighthead (108) by means of a contactless absolute position sensor (212).Operation of a brake (111), motor (110), and lamp (112) is controlled by a control unit (210). Electrical power to the brake (111), motor (110), and lamp (112) is slowly applied and removed to reduce electromagnetic emissions and extend the service life of a power stage (208), brake (111), motor (110), and lamp (112). The lighthead (108) may be manually stowed in the event of a fault.
摘要翻译：一种用于飞机的电子控制的可伸缩落地灯（100）。控制器（106）通过无接触绝对位置传感器（212）比较光头（108）的指令位置。制动器（111），电动机（110）和灯（112）的操作由控制器单元（210）。缓慢地施加和去除制动器（111），电动机（110）和灯（112）的电力以减少电磁辐射并延长功率级（208），制动器（111），电动机（110）的使用寿命，和灯（112）。在发生故障的情况下，可以手动收起光头（108）。

33. 发明申请

WO02049916A1 IR LASER DIODE BASED HIGH INTENSITY LIGHT 审中-公开
标题翻译：红外激光二极管基于高强度光
公开(公告)号：WO02049916A1
公开(公告)日：2002-06-27
申请号：PCT/US2001/049730
申请日：2001-12-20
IPC分类号： B64D47/02 , B64D47/04 , F21S2/00 , F21V13/00 , F21V29/00 , F21Y101/02 , G01J3/10 , F21S8/10 , H01S5/40
CPC分类号： G01J3/108 , B64D47/04
摘要： An infrared LASER diode based high intensity light (100) for use as an aircraft landing light or searchlight in conjunction with night vision imaging systems. The high intensity light (100) uses infrared LASER diodes (110) installed into a heat sink (112) for temperature stability. The infrared light emitted from the LASER diodes (110) is transmitted to an optical positioning plate (106) by optical transmission means (108). The optical positioning plate (106) combines the emissions of the individual LASER diodes (110) to a single infrared light beam, which is collimated by an aspheric lens (102).
摘要翻译：一种基于红外线激光二极管的高强度光（100），用作飞机着陆灯或探照灯与夜视成像系统。高强度光（100）使用安装在散热器（112）中的红外线激光二极管（110）来实现温度稳定性。从激光二极管（110）发射的红外光通过光传输装置（108）传输到光学定位板（106）。光学定位板（106）将单个激光二极管（110）的发射与由非球面透镜（102）准直的单个红外光束组合。

34. 发明申请

WO01046011A1 HIGH INTENSITY DISCHARGE AIRCRAFT LIGHTING SYSTEM AND COMPONENTS 审中-公开
标题翻译：高强度放射性飞机照明系统和组件
公开(公告)号：WO01046011A1
公开(公告)日：2001-06-28
申请号：PCT/US2000/034829
申请日：2000-12-20
IPC分类号： B64D47/04 , F21V23/02
CPC分类号： F21V23/02 , B64D47/04 , F21W2107/30
摘要： A method for replacing non-HID landing and taxi lights in an aircraft wing housing that originally was designed to contain the non-HID landing and taxi lights in side-by-side relationship, is accomplished by installing an HID landing light (18), an HID taxi light (20) and an power control device (36) in the space originally designed to accommodate the non-HID landing and taxi lights. A single ballast provides power to both lamps which each comprises a housing (46), an HID bulb (52) supported within the housing, a lens (44) for passage of light from the HID bulb out of the housing, a primary reflector (42) surface disposed behind the HID bulb, and a secondary reflector (68) surface disposed in front of the bulb for reflecting light from the bulb back through the bulb for further forward reflection from the primary reflector surface through the lens. The lens may have a lenticular array (76) including a plurality of cylindrical surface elements (84, 86) for spreading the light beam emitted by the lamp. An HID ignitor (108) may be located within the lamp's housing behind the reflector surface and electrically connected to the HID bulb.
摘要翻译：通过安装HID着陆灯（18）来实现最初被设计成包含非HID着陆和出租车灯并排关系的飞机机翼壳体中的非HID着陆和出租车灯的方法，原始设计成容纳非HID着陆和出租车灯的空间中的HID出租车灯（20）和电力控制装置（36）。单个镇流器为两个灯提供电力，每个灯包括壳体（46），支撑在壳体内的HID灯泡（52），用于将光从HID灯泡通过外壳的透镜（44），主反射器 42）表面，以及设置在灯泡前面的次级反射器（68）表面，用于将来自灯泡的光反射通过灯泡，以从主反射器表面进一步向前反射通过透镜。透镜可以具有透镜阵列（76），其包括多个用于扩散由灯发射的光束的圆柱形表面元件（84,86）。 HID点火器（108）可以位于反射器表面后面的灯壳体内，并电连接到HID灯泡。

35. 发明申请

WO00048904A1 HIGH INTENSITY GAS DISCHARGE AIRCRAFT LIGHTING 审中-公开
标题翻译：高强度气体放电飞机照明
公开(公告)号：WO00048904A1
公开(公告)日：2000-08-24
申请号：PCT/IB2000/000311
申请日：2000-02-18
IPC分类号： B64D47/04 , F21S8/10 , F21V15/04 , F21V19/00 , F21V23/02 , F21V31/00
CPC分类号： F21V23/02 , B64D47/04 , F21S41/17 , F21S41/192 , F21S45/50 , F21V15/04 , F21V31/00
摘要： An HID lamp assembly (10) has a relatively small envelope size enabling use of the lamp assembly in aircraft applications as well as other applications. The lamp assembly comprises a reflector (12), a discharge lamp (16) mounted to the reflector, and a ballast (18) which controls the delivery of power to the discharge lamp. The ballast is mounted to and carried by the reflector, at least partially surrounds a base (24) of the discharge lamp, and is axially aligned with the reflector. The transverse dimensions of the ballast are less than the corresponding dimensions of the reflector at a wide front end thereof.
摘要翻译： HID灯组件（10）具有相对小的信封尺寸，使得能够在飞行器应用中以及其它应用中使用灯组件。灯组件包括反射器（12），安装到反射器的放电灯（16）和控制向放电灯输送功率的镇流器（18）。所述镇流器安装到所述反射器并由所述反射器承载，至少部分地围绕所述放电灯的基座（24）并且与所述反射器轴向对准。镇流器的横向尺寸小于反射器在其宽前端的对应尺寸。

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