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Improved method and means for controlling the fire of guns on aircraft

机译:控制飞机上枪支射击的改进方法和装置

摘要

461,824. Controlling fire of guns on aircraft. NORTH, J. D. Sept. 10, 1935, No. 25119. [Classes 92 (i) and 92 (ii)] Relates to means for controlling the fire of an aircraft gun 1, Fig. 1, movable in elevation and azimuth, as for example on a ring mounting 4, so that firing is prevented when a part of the structure of the aircraft is in the line of fire, said means including as part of the firing circuit a screen member 11, Fig. 2, bearing on its surface a representation of the danger field 17 and a contact member 16 moving in elevation and training with the gun to be controlled, the firing being prevented when the contact member bears on the danger surface. According to the invention, the screen member is of cylindrical form and one of the gun movements, for example the training movement, is represented by a rotation of the contact member relatively to the screen, the other movement, for example the elevating movement, being represented by a linear movement of the contact member parallel to the axis of its rotation. In the form shown in Figs. 1 and 2, the contact 16 is carried by a cross-bar 14 which rotates in training with the ring 4, and is connected by links 12 with the elevating arm 2 to produce the required linear movement. In the form shown in Fig. 3, the contact member 27 is carried by the rotary ring 4 of the gun mounting, and has a linear movement in the slot 26 effected by a spring-controlled bell-crank lever 21 and a cable 18 connected with the elevating arm 2 supporting the gun. The contact member bears against a fixed cylindrical ring not shown, which bears the shaped danger field. The screen is generally formed of conducting material, the danger areas being represented by insulated insets, but the invention includes the use of raised or depressed danger areas when mechanical firing systems are used. Fig. 7 shows a pneumatic servomotor 58 for pulling the trigger 55 under the control of a rotary valve 61. The valve is shown in the firing position with a pressure port 60 and an exhaust port 64. To preclude firing under danger conditions, the screen 11 has a conducting surface corresponding to the danger area and the contact 16 is included in the circuit of a solenoid 53 which acts to open a release valve 65 and enable a spring 59 to move the trigger to inoperative position irrespective of the position of the firing valve 61.
机译:461,824。控制飞机上的枪支火力。北方,JD,1935年9月10日,第25119号。[类别92(i)和92(ii)]与用于控制图1中可在仰角和方位角移动的机枪1的射击的装置有关。例如,在环架4上,以便当飞机的一部分结构处于着火线时防止着火,所述装置包括作为图2的着火电路的一部分的,支承在其表面上的屏蔽构件11。图中示出了危险区域17和接触构件16,该接触构件16在仰角上移动并受控制地进行训练,当接触构件压在危险表面上时,可以防止射击。根据本发明,筛网构件是圆柱形的,并且枪支运动之一,例如训练运动,由接触构件相对于筛网的旋转来表示,另一种运动,例如举升运动,是由接触构件平行于其旋转轴线的线性运动表示。以图1和图2所示的形式。如图1和2所示,触头16由横杆14支撑,该横杆在环4的作用下旋转,并通过连杆12与升降臂2连接,以产生所需的线性运动。在图3所示的形式中,接触构件27由枪支座的旋转环4承载,并在由弹簧控制的曲柄杆21和连接的电缆18的作用下在槽26中具有线性运动。升降臂2支撑喷枪。接触构件靠在未示出的固定圆柱环上,该圆柱环带有成形的危险区域。筛网通常由导电材料形成,危险区域由绝缘嵌体表示,但是当使用机械点火系统时,本发明包括使用升高或降低的危险区域。图7示出了用于在旋转阀61的控制下拉动扳机55的气动伺服电动机58。所示的阀处于点火位置,具有压力口60和排气口64。为了防止在危险情况下点火,屏幕图11所示的电磁阀具有与危险区域相对应的导电表面,并且螺线管53的电路中包括触头16,螺线管53的作用是打开释放阀65,并使弹簧59能够将扳机移动到无效位置,而与击发位置无关。阀61。

著录项

  • 公开/公告号GB461824A

    专利类型

  • 公开/公告日1937-02-25

    原文格式PDF

  • 申请/专利权人 JOHN DUDLEY NORTH;

    申请/专利号GB19350025119

  • 发明设计人

    申请日1935-09-10

  • 分类号F41A17/08;

  • 国家 GB

  • 入库时间 2022-08-24 05:43:03

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