首页> 外国专利> Collision sensor for detecting rear contact of an aircraft (or other type of vehicle) with the ground, uses a conical section housing which when deformed past a set value causes electrical contacts inside to be actuated

Collision sensor for detecting rear contact of an aircraft (or other type of vehicle) with the ground, uses a conical section housing which when deformed past a set value causes electrical contacts inside to be actuated

机译:用于检测飞机(或其他类型的飞机)与地面的后部接触的碰撞传感器使用圆锥形外壳,当变形超过设定值时,会触发内部的电接触

摘要

Uses conical section (11) housing (1), for two contacts, with rounded or elliptical surface (14) or elliptical base (13). An admissible non deforming force on the housing is regulated by stability calculation using finite element method. The housing contains rod (4), and in an initial position, a pin (3) is held by its end (31) at the base of the rod. The rod is rigidly fixed to the base or housing surface (13,14) opposite to the pin fixing and has support (41) for glass tube (2) The axes of symmetry of glass tube and rod cut each other at right angles. Aircraft tail strike indicator designed to detect a high inadmissible force on a support structure of vehicles. Uses a conical section housing in which are fitted two electrical contacts which close, when the housing is deformed, so that a deformation signal is transmitted. The device includes: (a) a deformable conical (11) housing (1), a median axis, which connects the centers of the base (13) and the surface envelope 914) of the cone (11). The housing being oriented in the direction of force action; A pin (3) whose end (31) is inside the housing. The pin is rigidly fixed to one of the surfaces envelopes or base (13,14), the electrical contacts inside a glass tube (2) are connected to a contact bridge (21) and maintained closed an electrical circuit. The glass tube is perpendicular to the direction of the pin (3) and transversal to its end (31); and; when the height of the cone is reduced pass a set value by a non-admissible force, the pin end (31) and the glass tube slide towards each other so that the glass tube is broken and the contact bridge (21) is separated.
机译:使用圆锥形部分(11)的外壳(1),用于两个触点,带有圆形或椭圆形的表面(14)或椭圆形的基座(13)。通过使用有限元方法的稳定性计算来调节壳体上允许的非变形力。壳体包含杆(4),在初始位置,销(3)的一端(31)固定在杆的底部。该杆牢固地固定在与销钉固定相反的底部或壳体表面(13,14)上,并具有玻璃管(2)的支撑(41)。玻璃管和杆的对称轴相互垂直切开。飞机尾部打击指示器,用于检测车辆支撑结构上的较大不允许力。使用锥形截面的外壳,该外壳中装有两个电触点,当外壳变形时,两个电触点闭合,从而传输变形信号。该装置包括:(a)可变形的圆锥形(11)壳体(1),正中轴,其连接锥体(11)的底部(13)的中心和表面包络线914)。壳体沿力作用方向定向;销(3),其末端(31)在外壳内。该销牢固地固定在表面外壳或基座(13,14)之一上,玻璃管(2)内的电触点连接到接触桥(21),并保持闭合的电路。玻璃管垂直于销钉(3)的方向并横向于其端部(31);和;当圆锥体的高度减小时,通过不允许的力使其超过设定值时,销端(31)和玻璃管彼此相对滑动,从而玻璃管破裂并且接触桥(21)分离。

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