一种运载火箭气液连接器平衡气路及其控制方法
By balancing the gas path through the gas-liquid connector of the launch vehicle and using a gas-controlled pressure reducing valve and a pressure-stabilizing gas cylinder to control the filling and releasing of the cylinder, the problem of increased weight of the gas-liquid connector docking is solved, and a stable and adaptable interface balance is achieved.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- SHANGHAI AEROSPACE SYST ENG INST
- Filing Date
- 2022-10-19
- Publication Date
- 2026-07-17
AI Technical Summary
In existing technologies, the weight of gas-liquid connectors increases when docking with launch vehicles, leading to docking difficulties and interface tension. Furthermore, they have poor adaptability and cannot effectively balance the weight of connectors of different specifications and weights.
The launch vehicle gas-liquid connector is used to balance the gas path, including a gas source input end, a balanced gas supply output end, a balanced cylinder, a direct gas supply path, and a balanced gas supply path. The weight of the gas-liquid connector and pipeline is balanced by the cooperation of a pneumatic pressure reducing valve and a pressure stabilizing gas cylinder. The filling and discharging of the cylinder is controlled by a solenoid valve and an adjustable flow valve to maintain a constant output pressure.
It achieves stability of the weight of the gas-liquid connector and pipeline under the condition of rocket body swaying or sinking, avoids interface pulling force, adapts to connectors of different weights, and improves interface reliability and adaptability.
Smart Images
Figure CN115653950B_ABST