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航炮的后座力问题,在××飞机因后座力等问题换炮之后,引起了特别关注,随着武装直升飞机的发展,减小航炮后座力已是一个迫在眉睫的问题。现有的航炮减小后座力后,将会改善飞机的安全、操枞和作战性能,提高飞机的寿命,并为现有航炮开辟新的使用方向。本文以23——2航炮为对象,说明我们对航炮后座力计算的基本观点,是将航炮作为两个自由度(基本构件扣炮箱),同时考虑射击装置,飞机的刚性、重量、阻尼对后座力的影
The recoil problem of the artillery gun attracted special attention after the replacement of ×× aircraft due to recoil problems. With the development of armed helicopters, reducing the recoil force of the artillery gun has become an urgent issue. The reduction of the recoil force of existing aerial guns will improve the safety, firming and combat performance of the aircraft, enhance the life of the aircraft and open up new directions of use for the existing aircraft guns. In this paper, 23-2 cannon as an object to illustrate our calculation of recoil recoil from the basic point of view, is the artillery as two degrees of freedom (basic components buckle box), taking into account the shooting device, the aircraft’s rigidity, Weight, damping shadow of the recoil