The invention discloses a rigid-flexible combined lightweight manned sealed cabin. The rigid-flexible combined lightweight manned sealed cabin comprises a metal shell and a flexible film, the metal shell is of an integrated structure composed of a front ball cone, a column section and a rear cone, and a butt joint cabin door is arranged at the front end of the front ball cone and used for being in butt joint with an airship. The bottom end of the rear cone is sealed through a flexible film, and the flexible film is attached to the surface of the storage box extending into the sealed cabin under the action of internal pressure; the column section is provided with an out-of-cabin door, and meanwhile the column section is further provided with an equipment installation platform used for carrying instruments. According to the invention, the requirements of extreme light weight and conformal design with a storage tank and the like can be met.
本发明公开了一种刚柔结合的轻量化载人密封舱,包括金属壳体和柔性膜;金属壳体为前球锥、柱段和后锥构成的一体化结构,前球锥前端设有对接舱门,用于与飞船对接;后锥底端通过柔性膜密封,柔性膜在内压作用下贴附在伸入密封舱内部的贮箱表面;柱段上设有出舱舱门,同时柱段上还设有设备安装平台,用于搭载仪器。本发明能够满足极致轻量化和与贮箱等共型设计的需求。
Rigid-flexible combined lightweight manned sealed cabin
一种刚柔结合的轻量化载人密封舱
2024-02-20
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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