摘要
新型飞机需要连续旋转型伺服作动系统,选用了叶片式马达作为执行部件,但叶片马达式伺服系统在飞机上还没有广泛成熟的经验可以借鉴,所以研发初期需要开展建模仿真研究,为产品研制提供技术支撑。根据设计参数,在AMESim软件平台中对叶片马达式伺服系统进行了正向建模,并进行了模型校验。之后依托建好的系统模型进行了系统功能与性能分析,根据仿真结果,对现有设计方案提出减小间隙、改善密封的优化建议。
The new aircraft need continuous rotary servo system,which chooses the vane motor as the actuation components.But there is no enough service experience in the aircraft for the vane motor servo system,so the preliminary development phase needs modeling and simulation technology to support.According to the preliminary design parameters,the vane motor servo system is modeled in AMESim software,and the model validation is carried out.Then the system function and performance analysis are carried out based on the established system model.According to the simulation results,the existing design scheme is proposed to reduce the manufacture gap and improve the seal design.
引文
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