根据用户的技术需求和航空发动机附件试验台的特性,设计完成了满足对航空发动机多种阀类附件进行试验的多功能试验台,并着重论述了试验台的油品供给系统及温度控制系统的参数选择,通过试验测试表明,理论分析结果与试验测试结果吻合良好,可为同类试验台的研究提供参考。 According to the user’s technical requirements and the characteristics of aeroengine attachment test bed, a multi-functional test bench that meets the requirements of testing a variety of valve attachments of aeroengine has been designed. The oil supply system and temperature control system Parameter selection, through the test test shows that the theoretical analysis and test results agree well with the test bench for the same kind of research provide a reference.