公开(公告)号：US20100020557A1

公开(公告)日：2010-01-28

申请号：US12509850

申请日：2009-07-27

申请人： Tomoyuki Mukai ,  Makoto Nawa ,  Shigeo Sawada

发明人： Tomoyuki Mukai ,  Makoto Nawa ,  Shigeo Sawada

IPC分类号： B64D47/02

CPC分类号： B64D47/04 ,  B60Q1/0088 ,  B60Q1/0094 ,  F21V3/00 ,  F21V17/12 ,  F21V19/008 ,  F21V23/02 ,  F21V23/06 ,  F21V29/15 ,  F21V29/503 ,  F21V31/005 ,  F21W2107/30 ,  F21Y2103/00

摘要： An aircraft lamp includes a housing capable of being attached to a body of an aircraft; a discharge lamp; a reflector which reflects visible light from the discharge lamp; a light transmissive cover which transmits reflected light from the reflector to a front side of the housing; a lamp socket connected electrically to the discharge lamp and an igniter which activates the discharge lamp; and a high-voltage electrical power line that electrically connects the lamp socket with the igniter. The discharge lamp, the reflector, the light transmissive cover, the lamp socket, and the igniter are provided within the housing. A heat insulating air layer is provided between the lamp socket and the igniter. The high-voltage electrical power line is provided so as to pass through the heat insulating air layer.

摘要翻译： 飞机灯包括能够附接到飞行器主体的壳体; 放电灯; 反射器，其反射来自放电灯的可见光; 透光盖，其将来自反射器的反射光透射到壳体的前侧; 与放电灯电连接的灯座和激活放电灯的点火器; 以及将灯座与点火器电连接的高压电力线。 放电灯，反射器，透光盖，灯插座和点火器设置在壳体内。 在灯座和点火器之间设置隔热空气层。 高压电力线设置成穿过绝热空气层。

公开(公告)号：US08297811B2

公开(公告)日：2012-10-30

申请号：US12509850

申请日：2009-07-27

申请人： Tomoyuki Mukai ,  Makoto Nawa ,  Shigeo Sawada

发明人： Tomoyuki Mukai ,  Makoto Nawa ,  Shigeo Sawada

IPC分类号： B64D47/02

CPC分类号： B64D47/04 ,  B60Q1/0088 ,  B60Q1/0094 ,  F21V3/00 ,  F21V17/12 ,  F21V19/008 ,  F21V23/02 ,  F21V23/06 ,  F21V29/15 ,  F21V29/503 ,  F21V31/005 ,  F21W2107/30 ,  F21Y2103/00

摘要： An aircraft lamp includes a housing capable of being attached to a body of an aircraft; a discharge lamp; a reflector which reflects visible light from the discharge lamp; a light transmissive cover which transmits reflected light from the reflector to a front side of the housing; a lamp socket connected electrically to the discharge lamp and an igniter which activates the discharge lamp; and a high-voltage electrical power line that electrically connects the lamp socket with the igniter. The discharge lamp, the reflector, the light transmissive cover, the lamp socket, and the igniter are provided within the housing. A heat insulating air layer is provided between the lamp socket and the igniter. The high-voltage electrical power line is provided so as to pass through the heat insulating air layer.

摘要翻译： 飞机灯包括能够附接到飞行器主体的壳体; 放电灯; 反射器，其反射来自放电灯的可见光; 透光盖，其将来自反射器的反射光透射到壳体的前侧; 与放电灯电连接的灯座和激活放电灯的点火器; 以及将灯座与点火器电连接的高压电力线。 放电灯，反射器，透光盖，灯插座和点火器设置在壳体内。 在灯座和点火器之间设置隔热空气层。 高压电力线设置成穿过绝热空气层。

公开(公告)号：US06650425B2

公开(公告)日：2003-11-18

申请号：US09814510

申请日：2001-03-22

申请人： Yasushi Kubota ,  Makoto Nawa ,  Toshihiko Kurebayashi

发明人： Yasushi Kubota ,  Makoto Nawa ,  Toshihiko Kurebayashi

IPC分类号： G01B1114

CPC分类号： G01D5/28

摘要： A position measuring laser apparatus includes first and second laser transmitter-receivers and a position measure. The laser transmitter-receiver includes a laser beam emitter for emitting a laser beam, and a laser beam receiver for receiving a laser beam resulting from the emitted laser beam reflected from a reference reflecting mirror. An optical axis of the laser transmitter-receiver is oriented at a required angle toward a moving body. The position of the moving body with respect to the reference reflecting mirror is measured based on a beam receiving signal of the laser beam obtained by the laser transmitter-receiver. The position measure compares a drive signal for driving the laser beam emitter with a beam receiving signal generated by the laser beam receiver to measure the position of the moving body based on the beam receiving signal when the drive signal and the beam receiving signal coincide with each other.

摘要翻译： 位置测量激光装置包括第一和第二激光发射器 - 接收器和位置测量。 激光发射器 - 接收器包括用于发射激光束的激光束发射器和用于接收由从参考反射镜反射的发射激光束产生的激光束的激光束接收器。 激光发射器 - 接收器的光轴朝向移动体以所需的角度定向。 基于由激光发射器 - 接收器获得的激光束的光束接收信号来测量移动体相对于参考反射镜的位置。 位置测量将用于驱动激光束发射器的驱动信号与由激光束接收器产生的波束接收信号进行比较，以便当驱动信号和波束接收信号与每个信号一致时，基于波束接收信号测量移动体的位置 其他。