Electric dual-mode emergency retracting device for movable platform of spaceflight launching site
By using an electric dual-mode emergency retraction device, which combines the power coupling and precise control of DC and AC motors, the problems of long and unstable manual emergency retraction are solved, enabling fast and stable platform retraction and improving equipment reliability and safety.
Patent Information
- Application Number
- CN202521443868.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-07-10
- Publication Date
- 2026-07-07
- Estimated Expiration
- 2035-07-10
AI Technical Summary
In existing technologies, the manual emergency retraction method of space launch site activity platforms is time-consuming, relies on manpower, is prone to fatigue, is difficult to respond quickly, and the unstable operation affects the reliability and safety of the equipment.
It adopts an electric dual-mode emergency retraction device, integrating 220V AC power supply and 48V DC battery dual working modes. The motor speed and torque are precisely controlled through the control panel. Combined with the power coupling of DC geared motor and AC motor, it can achieve fast and stable platform retraction. The structure of fixed block, screw, limit block and other structures ensures the precise installation of transmission components and platform stability.
It enables the platform to be retracted quickly, stably, and safely in emergency situations, avoiding shaft misalignment, extending equipment lifespan, and improving system reliability and ease of operation.