Modelling and simulation of functioning of the GSh-23 aviation autocannon mechanisms

IF 0.2 Q4 ENGINEERING, GEOLOGICAL
M. Jasztal
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引用次数: 0

Abstract

Article presents the simulation model and the study of the basic mechanisms of the GSh-23 aviation autocannon. The research made use of Solid Edge ST9 software and the multibody systems method implemented in it. Simulation of functioning cannon mechanisms was carried out for two variants of forcing a piston mechanism movement by the gunpowder gases. The results obtained are time courses of a bolt and a cartridge belt drive mechanism elements movement. Assumed variants of a piston mechanism movement and elaborated simulation model will be verified in the next (planned) stage of studies basing on the results of the measurements of the experimental kinematic parameters utilising high-speed camera (Phantom) and TEMA software.
GSh-23航空机炮机构功能建模与仿真
本文建立了GSh-23型航空机炮的仿真模型,并对其基本机理进行了研究。本研究利用Solid Edge ST9软件及其实现的多体系统方法。对两种火药气体驱动活塞运动的火炮机构进行了功能仿真。所得结果为螺栓和筒带驱动机构元件运动的时间轨迹。活塞机构运动的假设变量和详细的仿真模型将在下一个(计划的)研究阶段进行验证,该阶段将基于利用高速相机(Phantom)和TEMA软件测量实验运动学参数的结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Archives for Technical Sciences
Archives for Technical Sciences ENGINEERING, GEOLOGICAL-
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