边杰1,王四季2,刘飞春3
收稿日期:2024-11-25
修回日期:2025-06-02
出版日期:2025-06-05
发布日期:2025-06-05
通讯作者:
边杰
基金资助:
Received:2024-11-25
Revised:2025-06-02
Online:2025-06-05
Published:2025-06-05
摘要: 鼠笼弹支是航空发动机转子系统重要的减振支承结构,可支撑转子,有效调节转子系统临界转速、降低转子系统振动,同时还可用于转子振动和轴向载荷监测,在航空发动机转子系统中应用十分广泛。从鼠笼弹支的功能作用、优化设计、刚度强度、测试监测、发展趋势等方面对鼠笼弹支的结构设计和实验技术进行了总结和展望。鼠笼弹支结构设计时需要考虑刚度、强度及测试监测等问题,涉及单个目标、多个目标之间的结构参数优化。重点介绍了鼠笼弹支刚度、强度计算与试验的解析法、有限元法和实验法,阐述了鼠笼弹支的振动监测与轴向力测量技术,对折返式鼠笼弹支、轴承外环集成式鼠笼弹支、变刚度、变阻尼及主控式鼠笼弹支等其它异型鼠笼弹支进行了研究分析,对应用场景不同、功能各异的鼠笼弹支设计和实验研究有重要的参考作用和借鉴意义。
中图分类号:
边杰 王四季 刘飞春. 航空发动机鼠笼弹支设计与实验研究进展[J]. 航空学报.
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