The utility model discloses a portable missile launch missile sitting type supporting device, fixture is composed of two parallel clamping plates connected by a curved end which is arranged on the lower end of the knob hole and the shaft clamping hole; the through holes are connected at the upper end of the frame is provided with a rotating shaft hole and the splint at the lower end of the corresponding; between the lower part of the two splints connected at the upper end of the frame insert missile fixture through hole, the shaft passes through the shaft holes and connected at the upper end of the frame; a fastening knob knob hole through the two splints on the fixed seat is installed on the top of the tripod; three through the support rod; the support frame comprises a horizontal bar and a vertical frame, a bolt pin hole vertical frame is arranged on the upper end of the connecting frame and at the lower end of the corresponding the lower end of the connecting frame; the bolt is inserted into the pin hole support frame, thereby connecting the above frame is fixed on the support frame. The utility model has the advantages that the utility model has the advantages of relieving fatigue and being suitable for long time operation, and the portable missile can be carried on the launching support device in the launching process, and has the advantages of simple structure, light weight and portability.
【技术实现步骤摘要】
【技术保护点】
一种便携导弹单发坐式发射支撑装置，其特征在于，包括夹持便携导弹（1）的导弹夹具（2）、转轴（3）、紧固旋钮（4）、连接架（5）、支撑架（6）、座（7）和三角支架（8）；其中，所述导弹夹具（2）由通过弧形端（2?1）连接的两块平行的夹板（2?2）组成，两块所述夹板（2?2）的下端的相对应位置均设有旋钮孔（2?3）和转轴孔（2?4）；连接架（5）为条状支架，连接架（5）上端设有与夹板（2?2）下端的转轴孔（2?4）相对应的通孔，下端设有至少两个竖直方向的插销（5?1）；连接架（5）上端插入导弹夹具（2）的两块夹板（2?2）下端之间，转轴（3）穿过转轴孔（2?4）和连接架（5）上端的通孔，从而将导弹夹具（2）固定在连接架（5）上端，且导弹夹具（2）能够绕转轴（3）相对于连接架（5）转动；紧固旋钮（4）穿过两块夹板（2?2）上的旋钮孔（2?3）后固定，通过紧固旋钮（4）的旋转能够控制两块夹板（2?2）的夹紧程度；座（7）通过支撑杆（9）安装在三脚架（8）顶端；支撑架（6）包括水平横杆（6?2）和竖架（6?3），所述竖架（6?3）下端固定在水平横杆（6?2）一端上，水平横杆（6?2）另一端通过轴...
【技术特征摘要】
【专利技术属性】
技术研发人员：李世龙，
申请(专利权)人：西安天伟电子系统工程有限公司，
类型：实用新型
国别省市：
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