首页> 外国专利> FLY-BY WIRE FLIGHT CONTROL SYSTEM FOR AIRCRAFT AND METHOD FOR CONTROL OF A PLURALITY OF POSITIONS OF FLIGHT CONTROL WING FACE ON AIRCRAFT

FLY-BY WIRE FLIGHT CONTROL SYSTEM FOR AIRCRAFT AND METHOD FOR CONTROL OF A PLURALITY OF POSITIONS OF FLIGHT CONTROL WING FACE ON AIRCRAFT

机译:飞机的掠过线飞行控制系统和控制飞机上飞行控制翼面多个位置的方法

摘要

PURPOSE: To select so that an operation of one flight control channel is sufficient to fly an aircraft by receiving a flight control wing face command and incorporating a means for connecting the command to a plurality of servo loops. CONSTITUTION: Before a flight control wing face command is executed, each ACE executes validity inspection for the command to confirm that a main flight computer relative to a flight control channel of the ACE correctly operates. If the inspection indicates that the main computer does not correctly operate, the ACE selects one set of flight control wing face command generated from another main flight computer, and uses it for controlling the set of the flight control wing face of the ACE. Accordingly, a left ACE 62 can control movement of the set 66 of the control wing face even when the computer 64 or a left data bus is faulted.
机译:目的:通过接收飞行控制机翼面指令并结合一种将指令连接到多个伺服回路的装置,来选择一个飞行控制通道的操作足以使飞机飞行。组成:在执行飞行控制翼面命令之前,每个ACE都会对该命令执行有效性检查,以确认相对于ACE的飞行控制通道的主飞行计算机是否正确运行。如果检查表明主计算机无法正常运行,则ACE选择从另一台主飞行计算机生成的一组飞行控制机翼面命令,并将其用于控制​​ACE的飞行控制机翼面的集合。因此,即使计算机64或左数据总线发生故障,左ACE 62也可以控制机翼面的组66的运动。

著录项

  • 公开/公告号JPH0632291A

    专利类型

  • 公开/公告日1994-02-08

    原文格式PDF

  • 申请/专利权人 BOEING CO:THE;

    申请/专利号JP19930128639

  • 发明设计人 HENINGU BUUSU;

    申请日1993-05-31

  • 分类号B64C13/00;

  • 国家 JP

  • 入库时间 2022-08-22 04:48:39

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