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2. 发明公开

EP0516265A1 Improvements in or relating to aircraft landing systems 失效
标题翻译： VerbesserungenfürFlugzeug-Landesysteme。
公开(公告)号：EP0516265A1
公开(公告)日：1992-12-02
申请号：EP92301906.1
申请日：1992-03-05
申请人： Siemens Plessey Electronic Systems Limited
发明人： Smart, Peter Britton , Spencer, Timothy James , Sole, John David , Barton, Peter William , Peckham, Richard , Graham, William Morris , Whitehurst, Jonathan
IPC分类号： G01S1/56 , G01S1/02
CPC分类号： G01S1/56 , G01S1/024
摘要： An aircraft landing system (10) is disclosed which produces electromagnetic guidance signals to an incoming aircraft (14) and which allow the incoming aircraft (14) to safely land upon the runway (16). This system (10) includes various antenna arrays (12, 18), and (20) which are orientated so as to provide signals in several directions. Each of these arrays has a separate controller (22, 24), and (26) having a separate transmitter controller (74) uniquely coupled to each of the antennas (80, 88). Each of the transmitter controllers (74) separately amplifies the incoming electromagnetic energy from transmitters (52, 54). System 10 further includes several fault monitors (92, 94, 96) which monitor the operation of system (10) and which further provide self test features. System (10) further includes voting circuitry (98, 118) to allow for continued system operation even upon the failure of one or more of the transmitter controllers (74) and/or the monitors (92, 94, 96) and a dual inclined travelling wave manifold (90) and (566) to provide a monitored beam output which is used by monitors (92, 94, 96) to ensure continued system operation. Further, system 10 includes a connectorless coupling of electromagnetic energy between each of the transmitter controllers (74) and the combiners (82, 84). This connectorless coupling allows for a more efficient energy transfer while obviating the need for separate physical connections which are inherently unreliable; inefficient; and costly.
摘要翻译：公开了一种飞机着陆系统（10），其向进入的飞行器（14）产生电磁引导信号，并允许进入的飞机（14）安全地着陆在跑道（16）上。该系统（10）包括各种天线阵列（12,18）和（20），其被定向成在多个方向上提供信号。这些阵列中的每一个具有单独的控制器（22,24）和（26），其具有唯一地耦合到每个天线（80,88）的单独的发射器控制器（74）。每个发射机控制器（74）分别放大来自发射器（52,54）的输入电磁能量。系统10还包括几个故障监视器（92,94,96），其监视系统（10）的操作并进一步提供自检特征。系统（10）还包括投票电路（98,118），以允许即使在一个或多个发射器控制器（74）和/或监视器（92,94,96）的故障和连续的系统操作行波管道（90）和（566），以提供由监视器（92,94,96）使用的监视的光束输出，以确保持续的系统操作。此外，系统10包括在每个发射机控制器（74）和组合器（82,84）之间的无连接器的电磁能耦合。这种无连接器耦合允许更有效的能量传递，同时避免对本来不可靠的单独的物理连接的需要; 效率低下; 并且成本高昂。

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