首页 | 本学科首页   官方微博 | 高级检索  
     检索      

降低航炮后座力的必要性及可行性
引用本文:李奕,彭会祺.降低航炮后座力的必要性及可行性[J].洪都科技,1998(2):8-13.
作者姓名:李奕  彭会祺
作者单位:洪都航空集团650所
摘    要:航空射击武器的后座力对其载机有诸多不利影响,因此,必须设法减小这些影响。本文就JL8飞机航炮后座力过大对飞机的不利影响进行了分析,阐述了降低航炮后座力的必要性。同时还就如何解决航炮后座力过大问题进行了研究,提出了降低JL8飞机所装23-2航炮后座力的方法。

关 键 词:JL8飞机  23-2航炮  后座力  战斗机

Necessity & Feasibility for Decending Recoil of Gun Pod
Li Yi, Peng Huiqi.Necessity & Feasibility for Decending Recoil of Gun Pod[J].Hongdu Science and Technology,1998(2):8-13.
Authors:Li Yi  Peng Huiqi
Institution:Research Institute 650 of Hongdu Aviation Indusny Group
Abstract:The recoil of aircraf firing weapon has a lot of unfavourable ef fects on the canying aircraft, therefore, the effects must be reduced by means of some ways. This paper analyzes the unfavourable effects on the aircraft from greatly recoil of JL8 aircraf gun pod and demonstrazes the necessity for reducing recoil of gun pod. Meanwhile, the solution for solving great recoil of gun pdod has been studied, making a method for reducing the recoil from 23-2 gun pod fitted on JL8 aircraft.
Keywords:JL8 aircraft 23-2 gun pod recoil of gun pod  
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号