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航空发动机U形金属密封环的设计与优化
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Design and Optimization of Metallic U-ring in Aero-engine
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    摘要:

    针对某型发动机高压转子连接结构的密封问题,设计一种U形金属密封环,分析研究密封环的密封和强度性能,探究结构参数(包括根部倒圆、壁厚、环高、接触面曲率半径、密封环接触面角度、密封环配合件角度)对密封环最大等效应力、最大接触应力的影响,基于ANSYS Workbench优化设计模块,采用代理模型结合遗传算法的优化技术对密封环结构进行优化。结果表明:安装压缩率范围为3.56%~6.33%时,可保证安装和工作2种工况下密封和强度的要求;最大等效应力与壁厚成正比关系,而与根部倒圆和环高成反比关系;接触面曲率半径对最大等效应力影响较小,但最大接触应力随着接触面曲率半径的增加而增加;选择合适的角度范围时,密封环接触面角度和密封环配合件角度对最大等效应力、最大接触应力影响均较小。密封环结构优化后,最大等效应力在安装和工作2种工况下分别减小了34.3%和30.4%,同时密封环质量减少了6.1%。对设计的U形金属密封环随整机进行了试验,结果表明U形金属密封环密封性能良好,验证了设计的合理性。

    Abstract:

    Aimed at the sealing problem of the connecting structure of a highpressure rotor of an engine,a U-shaped metal seal ring was designed.The sealing and strength performance of the seal ring were analyzed and studied.The influence of structural parameters,such as root circle,wall thickness,ring height,curvature radius of contact surface,contact surface angle of sealing ring and seal ring fitting angle on the maximum equivalent stress and the maximum contact stress of the seal ring was explored.Based on the optimization design module of ANSYS Workbench,the optimization technology of agent model and genetic algorithm was used to optimize the structure of the seal ring.The results show that the sealing and strength requirements can be guaranteed when the installation compression ratio ranges from 3.56% to 6.33% under the installation and operation conditions.The maximum equivalent stress is directly proportional to the wall thickness,but inversely proportional to the root circle and ring height.The curvature radius of the contact surface has little effect on the maximum equivalent stress,while the maximum contact stress is increased with the increase of the curvature radius of the contact surface.When choosing the appropriate angle range,the angle of the contact surface and the angle of the mating part of the sealing ring have little influence on the maximum equivalent stress and the maximum contact stress.After optimization,the equivalent stress of the sealing ring under the installation and operation conditions is reduced by 34.3% and 30.4% respectively.The mass of the sealing ring is reduced by 6.1%.The designed U-shaped metal seal ring was tested with the whole machine.The results show that the sealing performance of the U-shaped metal seal ring is good,which verifies the rationality of the design.

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黄 发,马 健,吴正洪.航空发动机U形金属密封环的设计与优化[J].润滑与密封,2020,45(7):128-135.
HUANG Fa, MA Jian, WU Zhenghong. Design and Optimization of Metallic U-ring in Aero-engine[J]. Lubrication Engineering,2020,45(7):128-135.

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  • 在线发布日期: 2020-10-15
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