CAJ | 학술논문

为了研究击发机构的力学特性，对击发机构零部件进行三维实体建模，考虑拨动子驻栓、发射器推杆和电磁连杆的柔性，利用Hypermesh软件对它们进行模态分析，生成可被动力学分析软件ADAMS调用的模态中性文件，建立击发机构刚柔耦合动力学模型，对击发机构进行了刚柔耦合动力学分析和对击发机构机理分析使用方法与手段，分析结果对于火炮击发机构的设计具有一定的参考价值。
위료연구격발궤구적역학특성，대격발궤구령부건진행삼유실체건모，고필발동자주전、발사기추간화전자련간적유성，이용Hypermesh연건대타문진행모태분석，생성가피동역학분석연건ADAMS조용적모태중성문건，건립격발궤구강유우합동역학모형，대격발궤구진행료강유우합동역학분석화대격발궤구궤리분석사용방법여수단，분석결과대우화포격발궤구적설계구유일정적삼고개치。
In order to study the mechanical properties of the firing mechanism, the modeling of the three Dsolid parts of the firing mechanism is established, considering the flexibility of the cocking lever sear, launcher putter and electromagnetic rod, the modal a-nalysis is done by Hypermesh software, the modal neutral file used by the dynamic analysis software ADAMS is generated, the rigid and flexible coupling dynamics model is established and rigid and flexible coupling dynamics of the firing mechanism is analyzed. The methods and approaches of its analysis and the design of the artil ery are of certain reference value.