CAJ | 학술논문

为减小重机枪发射过程中的后坐力，提升武器系统发射稳定性，建立安装有浮动装置的机枪系统发射动力学模型。基于多体动力学理论，以 ADAMS 软件为平台，建立某通用机枪的虚拟实验，并对其进行动力学仿真，得到机枪射击过程中机框浮动速度和后坐力曲线。结果表明：重机枪采用合适的浮动发射机构能大幅度降低射击后坐力，可为改进重机枪系统射击性能提供参考。
위감소중궤창발사과정중적후좌력，제승무기계통발사은정성，건립안장유부동장치적궤창계통발사동역학모형。기우다체동역학이론，이 ADAMS 연건위평태，건립모통용궤창적허의실험，병대기진행동역학방진，득도궤창사격과정중궤광부동속도화후좌력곡선。결과표명：중궤창채용합괄적부동발사궤구능대폭도강저사격후좌력，가위개진중궤창계통사격성능제공삼고。
To reduce recoil of heavy machine gun when launching and improve launching stability of weapon system, weapon dynamic model mounted with floating apparatus was built. Established virtual experiment of certain general purpose machine gun based on multi-body dynamic theory, taking ADAMS software as platform, and progress dynamic simulation to obtained machine frame velocity and recoil curve in machine gun launching process. The results are recoil can be reduced significantly with floating apparatus applied to heavy machine gun. Research results can provide guidance for the performance of heavy machine gun improvement.