Based on engine structure and sealing principles,a shaft rotation processing method is proposed to address the issue of excessive leakage of turbine end shaft seal after testing of a type of liquid rocket engine,which leads to the inability to deliver the engine normally.The feasibility of the technique is analyzed,and craft equipment is designed and manufactured to obtain process parameters for improving sealing performance by process testing.The experimental results show that after engine process testing,it can improve the fitting state of the turbine end shaft seal,reduce seal leakage,upgrade the reliability and reusability without decomposing the engine.
关键词
涡轮端轴密封/泄漏量/轴系回转
Key words
turbine end shaft seal/leakage amount/axis rotation
维普
万方数据