The invention relates to a flight equipment acceleration device and method, and belongs to the technical field of aircrafts. The flight equipment acceleration device comprises a sliding rail structure and an acceleration structure, and the acceleration structure comprises a mounting base, an elastic reset mechanism, an unlocking mechanism and a supporting arm; the mounting base is arranged on the sliding rail structure in a sliding mode and accelerates or decelerates under the control of the sliding rail structure, the unlocking mechanism and the elastic reset mechanism are both arranged on the mounting base, the supporting arm is hinged to the mounting base, the elastic reset mechanism is connected with the supporting arm, and the supporting arm is used for supporting flight equipment and providing propelling force for the flight equipment. The acceleration structure achieves lifting and falling of the supporting arm through the elastic reset mechanism and the unlocking mechanism in the acceleration stage and the deceleration stage correspondingly. According to the flight equipment acceleration device, power is provided by completely utilizing the inertia of the device in the dumping process of the supporting arm, extra power sources such as a hydraulic oil cylinder and a motor are not needed, and the energy consumption of the device is small.
本申请涉及一种飞行设备加速装置及方法,属于飞行器技术领域。其中飞行设备加速装置包括滑轨结构和加速结构,加速结构包括安装座、弹性复位机构、解锁机构和支撑臂;安装座滑动设置在滑轨结构上并在滑轨结构的控制下加速或减速,解锁机构和弹性复位机构均设置在安装座上,支撑臂与安装座铰接,弹性复位机构与支撑臂连接,支撑臂用于支撑飞行设备并为飞行设备提供推进力。加速结构在加速阶段和减速阶段分别通过弹性复位机构和解锁机构实现支撑臂的抬起和落下。本申请提出的飞行设备加速装置中支撑臂的倾倒过程完全利用装置的自身惯性提供动力,无需液压油缸、电机等额外动力源,装置能耗小。
Flight equipment acceleration device and method
飞行设备加速装置及方法
2024-07-30
Patent
Electronic Resource
Chinese
Flight investigation of acceleration restrictor
Engineering Index Backfile | 1960
|Relativistic rocket flight with constant acceleration.
AIAA | 1969
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