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    • 33. 发明申请
    • SURVEILLANCE SYSTEM FOR AIRCRAFT INTERIOR
    • 飞机内部监视系统
    • WO2004030336A2
    • 2004-04-08
    • PCT/US2003/027629
    • 2003-09-04
    • L-3 COMMUNICATIONS CORPORATION
    • GOMEZ, Oscar
    • H04N
    • G08B13/1965B64D45/0015B64D2045/0035G08B13/19645H04N7/181
    • A surveillance system for monitoring activity within at least the cabin portion of the aircraft in order to alert the flight crew within the cockpit of any emergency activity including, but not limited to, highjacking or terrorist activity. A viewing assembly in the form of one or more cameras is disposed to selectively capture images throughout the aircraft cabin interior and deliver the captured image data to a display assembly observable by the flight crew. Activation of the system is accomplished by controlled operation of one or more portable, wireless transmitters and at least one receiver which is operationally connected to the viewing assembly and the display assembly.
    • 一种监视系统,用于监视飞机至少舱室部分内的活动,以便提醒驾驶舱内的飞行机组人员进行任何紧急活动,包括但不限于高空劫持或恐怖活动。 以一个或多个相机形式的观看组件设置成选择性地捕获整个飞机机舱内部的图像,并将捕获的图像数据传送到由飞行机组人员可观察到的显示组件。 系统的激活是通过一个或多个便携式无线发射器和至少一个操作地连接到观察组件和显示组件的接收器的受控操作实现的。
    • 35. 发明申请
    • DIELECTRICALLY LOADED WIDE BAND FEED
    • 电介质装载宽带饲料
    • WO1998007210A1
    • 1998-02-19
    • PCT/US1997013990
    • 1997-08-08
    • L-3 COMMUNICATIONS CORPORATION
    • L-3 COMMUNICATIONS CORPORATIONANDERSON, Bryant, FordYAMAMOTO, Mark, JohnathonULMER, Douglas, Harry
    • H01Q13/00
    • H01P1/161H01Q5/47H01Q13/02H01Q19/08
    • A feed system for an antenna has a set of inner and outer coaxial waveguides (70, 66) which apply, respectively, both higher and lower frequency radiations to a common radiating aperture provided by a horn (68) and a shroud (62) which envelopes radiating apertures of the individual feed waveguides. Lower frequency radiation to be transmitted by the outer coaxial feed waveguide is applied thereto by a set of four waveguides of a launcher (72). Each of the launch waveguides is initially a rectangular double-ridged waveguide for increase bandwidth. Impedance matching rings (160) are slidable within the space between the inner and outer surfaces of the coaxial waveguide for development of a desired standing wave ratio for accurate generation of a desired beam pattern. A dielectric rod (144) is disposed in a forward end of the tube of the inner feed waveguide and protrudes therefrom into the horn for shaping a beam of the higher frequency radiation.
    • 用于天线的馈送系统具有一组内部和外部同轴波导(70,66),其分别将高频和低频辐射施加到由喇叭(68)和护罩(62)提供的公共辐射孔 信封辐射各个馈电波导的孔。 由外部同轴馈电波导传输的较低频率的辐射由发射器(72)的一组四个波导施加到其上。 每个发射波导最初是一个矩形双脊形波导,用于增加带宽。 阻抗匹配环(160)可以在同轴波导的内表面和外表面之间的空间内滑动,以形成期望的驻波比,从而精确地产生期望的波束图案。 介电棒(144)设置在内馈电波导的管的前端,并从其中突出到喇叭中,以形成较高频辐射的波束。
    • 39. 发明申请
    • FIELD OBSERVABLE LIGHTING FOR AIRPORT SURFACE VEHICLES
    • 机场表面车辆现场可观察照明
    • WO2010099531A2
    • 2010-09-02
    • PCT/US2010/025752
    • 2010-03-01
    • L-3 COMMUNICATIONS CORPORATIONALLEN, John, W.GOELZ, RichardROESLER, Withelm, G.
    • ALLEN, John, W.GOELZ, RichardROESLER, Withelm, G.
    • G08G5/04G08G5/06
    • B60Q1/52B60Q1/2611H04L67/125H04L67/18H04W4/02
    • A warning light system for an airport vehicle has a warning light carried on a movable vehicle and a power controller linking the warning light to an electrical power source, selectively causing the electrical power to flow to the warning light such that the warning light illuminates and to interrupt flow of the electrical power to the warning light such that said warning light is not illuminated. Control circuitry connected with the power controller determines whether or not a geographical position of the vehicle indicated by a GPS receiver on it is within a predefined geographical area. Responsive to a determination that the vehicle is within the predefined geographical area, the control circuitry causes the power controller to illuminate the warning light. Responsive to a determination that the vehicle is not within the predefined geographical area, the control circuitry causes the power controller to interrupt flow of the electrical power to the warning light such that the warning light is off. The warning light as a result illuminates without any action by a user when the vehicle enters the predefined geographical area and is extinguished when the vehicle leaves the predetermined geographical area.
    • 机场车辆的警示灯系统具有携带在可移动车辆上的警告灯和将警告灯与电源连接的电源控制器,选择性地使电力流向警告灯,使得警告灯亮起,并且 中断电力到警告灯的电流,使得所述警告灯不被照亮。 与功率控制器连接的控制电路确定由其上的GPS接收器指示的车辆的地理位置是否在预定义的地理区域内。 响应于车辆在预定义的地理区域内的确定,控制电路使得功率控制器照亮警告灯。 响应于车辆不在预定义的地理区域内的确定,控制电路使得功率控制器中断电力到警告灯的流动,使得警告灯熄灭。 作为结果,当车辆进入预定义的地理区域并且当车辆离开预定的地理区域时熄灭,警告灯因此而不会被用户的任何动作照亮。