首页> 外国专利> Aircraft control equipment for landing approach - has controller with indicators for altitude-time settings and for starting deceleration procedure

Aircraft control equipment for landing approach - has controller with indicators for altitude-time settings and for starting deceleration procedure

机译:用于着陆进近的飞机控制设备-具有带有高度时间设置和启动减速程序指示器的控制器

摘要

An equipment is used to control the landing approach of an aircraft along its guide path. It controls the deceleration during the deceleration phase of the aircraft. It also indicates to the pilot whether correction is required of the deviation between the total slope and the reference slope. The equipment comprises a display (3) with two indicators (2, 4). When the pilot proceeds with the procedure of glide path capture, he presses the triangle indicator to start the decelerated approach equipment. When the aircraft is at a given first altitude, and first instant in time, the arrow indicator lights-up and informs the pilot to initiate the first deceleration phase and to lower the undercarriage, reset the wing flaps and adjust the engine throttle. When the aircraft is at a given second altitude and instant, the arrow indicator again nforms the pilot to reset the wing flaps.
机译:设备用于控制飞机沿其引导路径着陆。它在飞机减速阶段控制减速。它还向飞行员指示是否需要校正总斜率和参考斜率之间的偏差。该设备包括带有两个指示器(2、4)的显示器(3)。当飞行员继续进行滑行路径捕获程序时,他按下三角形指示器以启动减速的进近设备。当飞机处于给定的第一高度并及时到达第一时刻时,箭头指示器点亮,并通知飞行员开始第一减速阶段并降低起落架,重置机翼襟翼并调节发动机油门。当飞机处于给定的第二高度和瞬间时,箭头指示器再次通知飞行员以重置机翼襟翼。

著录项

  • 公开/公告号FR2344001B2

    专利类型

  • 公开/公告日1980-09-26

    原文格式PDF

  • 申请/专利权人 EQUIPEMENTS NAVIGATION AERIENNE;

    申请/专利号FR19760006592

  • 发明设计人

    申请日1976-03-08

  • 分类号G01C23/00;B64D45/04;

  • 国家 FR

  • 入库时间 2022-08-22 17:25:11

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