适用于金星表面硬着陆的探测器
By combining the support leg structure, the spherical main body structure, and the aerodynamic deceleration disc, the problem of hard landing of the Venus probe under high temperature and high pressure environment was solved, ensuring the stability of the probe and the normal operation of the internal equipment, and realizing scientific exploration of the surface of Venus.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- DEEP SPACE EXPLORATION LABORATORY
- Filing Date
- 2024-08-02
- Publication Date
- 2026-07-17
AI Technical Summary
Existing Venus landers are unable to achieve a hard landing in high-temperature and high-pressure environments, and their internal instruments and equipment are difficult to isolate from the high-temperature and high-pressure external atmosphere, leading to equipment damage or low-pressure discharge.
It adopts a support leg structure, a spherical main body structure, a pneumatic speed reducer and a modular instrument system, combined with an external sealed connection structure. The support legs provide cushioning, the spherical main body is filled with gas for heat insulation, the pneumatic speed reducer provides deceleration, and the external sealed connection structure isolates the high temperature and high pressure atmosphere to ensure the normal operation of the internal equipment.
The probe achieved stability and normal operation of the equipment under high temperature and high pressure environment during its hard landing on the surface of Venus, avoiding equipment damage and low pressure discharge, and ensuring the success of the exploration mission.
Smart Images
Figure CN118833421B_ABST