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Simulation Analysis and Experiment of Herringbone Groove Liquid Film Seal Based on Multi-Physics Coupling
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    Abstract:

    Aiming at the lubrication failure of the contacting mechanical seal of the fuel booster pump,the feasibility of the herringbone groove liquid film seal used in the fuel booster pump was analyzed through multi-physics coupling simulation and experiment.Based on the Reynolds equation considering roughness,energy equation and heat conduction equation,a multi-physics model of liquid film seal was established,and the key performances parameters such as temperature characteristics and leakage characteristics of the seal were analyzed.The sealing performance test was carried out for the herringbone groove liquid film seal.The results show that the average temperature of the herringbone groove seal end face is about 50 ℃ lower than that of the contacting mechanical seal,which is beneficial to the improvement of the seal operation stability.During the test operation,the temperature of the seal is stable,and the leakage is zero,which meets the requirements of the sealing performance for fuel booster pump.

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任宝杰,郝木明,胡广阳,王铭章,苏志善,李勇凡.基于多物理场耦合的航空发动机燃油泵液膜密封仿真分析与试验*[J].润滑与密封英文版,2022,47(12):75-82.

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  • Online: January 12,2023
  • Published: December 15,2022