The invention discloses a rocket hoisting assembly which comprises a rocket shell provided with a first mounting hole; the hoisting reinforcing piece is arranged on the inner side of the rocket shell, the side, close to the inner wall of the rocket shell, of the hoisting reinforcing piece is a first abutting part, and the area of the first abutting part is larger than the sectional area of the first mounting hole; one end of the connecting piece is a first connecting part, the other end of the connecting piece is a second abutting part, the area of the side, close to the hoisting reinforcing piece, of the second abutting part is also larger than the sectional area of the first mounting hole, the first connecting part is connected with the first abutting part, and the second connecting part is connected with the second abutting part. The fixing device is used for fixing the hoisting reinforcing part to the inner side of the rocket shell. The rocket hoisting assembly can improve the launching efficiency of the rocket.
本申请公开了一种火箭吊装组件,包括:火箭壳体,所述火箭壳体上设有第一安装孔;吊装加固件,所述吊装加固件设于所述火箭壳体内侧,且所述吊装加固件上靠近所述火箭壳体内壁的一侧为第一抵接部,所述第一抵接部的面积大于所述第一安装孔的截面积;连接件,所述连接件的一端为第一连接部,另一端为第二抵接部,所述第二抵接部上靠近所述吊装加固件一侧的面积也大于所述第一安装孔的截面积,所述第一连接部与所述第一抵接部连接,用于将所述吊装加固件固定于所述火箭壳体内侧。该火箭吊装组件可提升火箭的发射效率。
Rocket hoisting assembly
一种火箭吊装组件
2023-07-04
Patent
Electronic Resource
Chinese
IPC: | B66C Krane , CRANES |