刘凯.某间冷燃气轮机台架试验控制系统总体设计方案研究[J].航空发动机,2017,43(5):48-53
某间冷燃气轮机台架试验控制系统总体设计方案研究
Research on Overall Design Scheme of Control System of Test BedExperimental for a Intercooled Gas Turbine
  
DOI:
中文关键词:  间冷燃气轮机  控制系统  设计方案  航空发动机
英文关键词:intercooled gas turbine  control system  design scheme  aeroengine
基金项目:燃气轮机研究项目资助
作者单位E-mail
刘凯 中国航发沈阳发动机研究所沈阳110015 18642093785@163.com。 
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中文摘要:
      为了研究某间冷燃气轮机的性能,需要研制1 套控制系统完成燃气轮机在台架上的试车验证,并视情对燃气轮机的控 制规律及参数进行修改。介绍了某间冷燃气轮机台架试验控制系统总体设计方案,详细地阐述该系统的组成、功能实现方案及控制 逻辑、对燃气轮机的安全保护及数据监控等方面。描述了此系统的“六性”设计准则、研制风险、关键技术等。研究结果表明:该间冷 燃气轮机控制系统的特点结构简单、原理合理、功能完善、技术成熟、工作安全可靠,证明该系统总体设计方案可行。
英文摘要:
      In order to investigate a intercooled gas turbine performance, a control system was developed to complete experimental validation of gas turbine on the test, and the system control law and main parameters could be modified according to working condition. The overall control design scheme of the test bed was introduced for a intercooled gas turbine, and system components, realization scheme, control logic, safety protect and data controlling of gas turbine control function are expatiated. Moreover, the six performance design, the development risk and the main technology are also expatiated. The results show that the control system of the intercooled gas turbine has the characteristic of simple structure, reasonable principle, general function, mature technology, working safety and feasible system plan.
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