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Controllable ejection seat catapult

机译:可控制的弹射座椅弹射器

摘要

A catapult seat ejection system for ejecting a pilot and seat from an aircraft is disclosed in which the thrust of the catapult is controlled to prevent injury to the pilot due to acceleration forces. The catapult comprises a main catapult tube; a piston within the tube driven by gas pressure from the burning of two solid propellants cartridges; and four shuttle vent valves powered by gas from a plurality of electrically ignited squibs controlled by an electronic control system. The catapult is initially driven by only one of the two solid propellant cartridges and the electronic controller continuously monitors acceleration. If acceleration is too great the controller fires squibs with a control signal to open the shuttle vent valves to vent the gasses from the catapult and thereby reduce the pressure and acceleration of the seat. If the acceleration is too low and the vent valves are closed, and the sensor fires the second cartridge with a second control signal.
机译:公开了一种用于从飞机上弹出飞行员和座位的弹射器座椅弹出系统,其中控制弹射器的推力以防止由于加速力而伤害飞行员。弹射器包括一个主弹射管。管内的一个活塞,由两个固体推进剂药筒燃烧产生的气压驱动;四个梭形排气阀,由来自电子控制系统控制的多个电爆管的气体驱动。弹射器最初仅由两个固体推进剂弹药筒之一驱动,并且电子控制器连续监控加速度。如果加速度过大,则控制器会通过控制信号向爆管射击,以打开往复阀以从弹射器中排出气体,从而降低座椅的压力和加速度。如果加速度过低并且排气阀已关闭,并且传感器使用第二个控制信号发射第二个弹药筒。

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