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Flight situation position device in an aircraft - or aviator within the stationary position, the cabin chu

机译:飞机上的飞行情况定位装置-或固定位置内的飞行员,机舱

摘要

1,066,282. Aircraft indicators. BRITISH AIRCRAFT CORPORATION (OPERATING) Ltd. April 28, 1965 [May 15, 1964], No. 20359/64. Heading B7W. [Also in Division H3] In navigational equipment for an aircraft or aircraft flight simulator, the outline of an imaginary aircraft is projected on to the windscreen from a cathode-ray tube and the pilot is required to follow the imaginary aircraft to maintain course. The imaginary aircraft is seen in perspective, and is represented by five lines corrsponding to the two leading edges, two trailing edges and the fin of a delta wing. The co-ordinates of the points at the ends of the lines are computed from the aircraft flight data, from preset signals corresponding to the dimensions of the imaginary aircraft, and variable signals corresponding to the roll, pitch and yaw of the imaginary aircraft, i.e. the command signals, relative to the actual aircraft axes. The image is rotated in accordance with the roll angle of the actual aircraft, and may be produced on the cathode-ray tube as a television image, or as described, by deflection of the electron beam to form the five lines (see Division H3), and a horizon line. For landing, the image also contains two lines representing the edges of a runway, the distance from the touchdown point being represented by the arc of a circle centred on the base of the fin of the imaginary aircraft, the length of the arc being a measure of the distance. The image may also contain a speed error indicator, and in digital form the altitude and air-speed (Fig. 7, not shown).
机译:1,066,282。飞机指标。英国飞机公司(运营)有限公司。1965年4月28日(1964年5月15日),编号20359/64。标题B7W。 [也在H3分区中]在飞机或飞机飞行模拟器的导航设备中,假想飞机的轮廓从阴极射线管投射到挡风玻璃上,并且要求飞行员跟随假想飞机保持航向。假想飞机是从透视图中看到的,由与两条前缘,两个后缘和三角翼鳍相对应的五条线表示。根据飞机的飞行数据,对应于假想飞机尺寸的预设信号以及对应于假想飞机的侧倾,俯仰和偏航的可变信号,可以计算出飞机末端的点的坐标相对于实际飞机轴的命令信号。该图像根据实际飞机的侧倾角旋转,并且可以作为电视图像在阴极射线管上生成,或者如上所述,通过电子束的偏转以形成五条线来生成(请参阅H3部分) ,以及一条地平线。对于着陆,图像还包含两条线,它们代表跑道的边缘,距着陆点的距离由以假想飞机的鳍的底部为中心的圆弧表示,圆弧的长度为度量的距离。该图像还可以包含速度误差指示器,并以数字形式显示高度和空速(图7,未显示)。

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