The invention discloses a rocket stabilizing device and a hoisting system, and belongs to the technical field of rocket launching, the rocket stabilizing device comprises a fixing frame, a fastening mechanism and a wrapping tape; the fixing frame comprises a fixing frame body with an opening; the fixed frame body is provided with a limiting arc surface matched with the outer diameter of the arrow body; the limiting arc surface is arranged on an inferior arc taking the axis of the rocket body as a circle center; the fastening mechanism is arranged at the end point of the limiting arc surface and is fixedly connected with the fixed frame body; the bag belt is arranged at the opening of the fixing frame; the end part of the wrapping tape is fixedly connected with the fastening mechanism; the fastening mechanism is configured to adjust the length of the bag belt so as to fix the rocket body in an area defined by the bag belt and the fixing frame. A lifting point does not need to be arranged on the rocket body, a hydraulic or pneumatic system does not need to be used, the structure is simple, stability is good, and later maintenance cost is low.
本发明公开了一种火箭稳固装置及吊装系统,属于火箭发射技术领域,包括:固定架、紧固机构和包带;固定架包括具有开口的固定架体;固定架体上具有与箭体外径相适应的限位圆弧面;限位圆弧面设置在以箭体轴心为圆心的劣弧上;紧固机构设置于限位圆弧面的端点处,与固定架体固定连接;包带设置于固定架的开口处;包带端部与紧固机构固定连接;紧固机构配置成调整包带的长度以将箭体固定于包带与固定架围成的区域内。本发明无需在箭体上设置吊点,且无需使用液压或气动系统,结构简单,稳定性好,后期维护成本低。
Rocket stabilizing device and lifting system
一种火箭稳固装置及吊装系统
2024-03-01
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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