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Aircraft training apparatus for visual landing approach

机译:用于视觉着陆进近的飞机训练装置

摘要

961,794. Training aircrew. CURTISS-WRIGHT CORPORATION. Oct. 5, 1962 [Oct. 19, 1961], No. 37858/62. Heading B7W. Apparatus for simulating an aircraft night landing approach comprises a simulated landing field having apertures representing an array of approach and landing lights and illuminated from a light source, and optical pick-up and projecting means presenting the display to a trainee, the landing field and pick-up being relatively movable in accordance with simulated aircraft attitude. Fig. 1 shows a simulated landing strip L having landing lights 1 and approach lights 2, which may shine steadily or flash in sequence to give the impression of a light moving towards the runway. A television camera 3 is moved relative to L by servos controlled by a flight computer responsive to movements of the dummy controls in a mock cockpit T. A television projector 3b is focused on a screen 5 in front of the trainee. A fluorescent tube (not shown) extends the length of the strip L on its underside, and simulated landing lights 1 are provided by transparent plastic inserts extending through the strip. Each insert has a conical recess in its top, so that light passing up through the insert is reflected at a low angle to the plane of the strip. Each approach light 2 is simulated by an aperture 12 in a cover strip 16, overlying an opening 17 in panel 4, Fig. 2. Each aperture 12 is normally covered by a shutter 11 mounted on a lever 10 pivoted on axis 10a. The other end of each lever forms a cam co-operating with a roller 9b on a cam arm 9 secured to shaft 7, the set of rollers 9b lying on a helix coaxial with shaft 7. Each shutter has a row of small apertures, so that rows of approach lights are simulated. To simulate the flashing light sequence, shaft 7 is rotated by motor 5, the cam arms 9 displacing the levers 10 in sequence going towards the runway, to uncover apertures 12 in sequence. When the flashing light sequence is to be stopped, a cam on shaft 7 operates a microswitch to ensure that motor 5 is de-energized and a solenoidcontrolled brake is applied to the shaft, only when the angular position of the shaft is such as to leave all apertures 12 shuttered. A mirror is mounted above each aperture 12 to direct the light towards the camera. Light baffles prevent light from each aperture from reaching the camera other than by such reflection.
机译:961794。训练机组人员。 CURTISS-WRIGHT CORPORATION。 1962年10月5日[十月19,1961],第37858/62号。标题B7W。用于模拟飞机夜间着陆进场的设备包括:模拟的着陆场,其具有表示进近和着陆灯阵列并由光源照明的孔;以及光学拾取和投影装置,其将显示呈现给学员,着陆场和拾取器-up可以根据模拟的飞机姿态相对移动。图1示出了具有着陆灯1和进场灯2的模拟着陆带L,它们可以稳定地发光或依次闪烁以给人以朝向跑道​​移动的光的印象。响应于模拟驾驶舱T中的虚拟控件的运动,通过飞行计算机控制的伺服器使电视摄像机3相对于L移动。电视投影仪3b聚焦在学员前面的屏幕5上。荧光灯管(未示出)在条带L的下侧上延伸其长度,并且模拟的着陆灯1由延伸穿过条带的透明塑料插入物提供。每个插入件的顶部都有一个圆锥形凹槽,因此向上穿过插入件的光线以相对于条带平面的低角度反射。每个进场灯2由覆盖板16中的孔12覆盖在面板4上的开口17(图2)上模拟。每个孔12通常由安装在绕轴10a枢转的杠杆10上的百叶窗11覆盖。每个杠杆的另一端形成一个凸轮,该​​凸轮与固定在轴7上的凸轮臂9上的滚子9b配合,这组滚子9b位于与轴7同轴的螺旋上。每个百叶窗都有一排小孔,因此那行进近灯是模拟的。为了模拟闪光序列,轴7由电动机5旋转,凸轮臂9依次向着跑道移动杠杆10,以依次露出孔12。当要停止闪烁序列时,仅当轴的角度位置离开时,轴7上的凸轮才会操作微动开关,以确保电动机5断电并向轴施加电磁制动器所有的光圈都关闭了12在每个孔12上方安装有镜子,以将光引向相机。遮光板可以防止来自每个光圈的光到达相机,而不是通过这种反射。

著录项

  • 公开/公告号GB961794A

    专利类型

  • 公开/公告日1964-06-24

    原文格式PDF

  • 申请/专利权人 CURTISS-WRIGHT CORPORATION;

    申请/专利号GB19620037858

  • 发明设计人

    申请日1962-10-05

  • 分类号G09B9/30;

  • 国家 GB

  • 入库时间 2022-08-23 16:17:14

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