CAJ | 학술논문

小型化指令发射机安装于发动机上方的飞机垂尾根部，振动剧烈，安装空间非常有限，飞机能提供的冷却风很少，难以满足发射机的散热需要。文中通过模块化方法对发射机进行了整体结构设计，利用数值仿真对发射机进行了抗振和强度设计，并针对发射机的特点对其进行了热设计和高压绝缘设计。实验结果表明，该发射机具有良好的工作稳定性和可靠性。
소형화지령발사궤안장우발동궤상방적비궤수미근부，진동극렬，안장공간비상유한，비궤능제공적냉각풍흔소，난이만족발사궤적산열수요。문중통과모괴화방법대발사궤진행료정체결구설계，이용수치방진대발사궤진행료항진화강도설계，병침대발사궤적특점대기진행료열설계화고압절연설계。실험결과표명，해발사궤구유량호적공작은정성화가고성。
Small airborne command transmitter is installed above the engine, at the root of the vertical tail. Installation space is very limited and vibration is severe. Cooling air that aircraft can provide is very few. It is difficult to meet the cooling requirements of the transmitter. In this paper, overall structural design is per- formed by modular method. Vibration and strength design and high voltage insulation design are carried are analyzed by means of numerical simulation. Thermal out according to the characteristics of the transmitter. Test results show that the transmitter has good working stability and reliability