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弹箭与制导学报 >

2013 , Vol. 33 >Issue 5: 115 - 118,122

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2013.05.049

弹药技术

涡扇发动机总体性能虚拟试验平台研究

  • 张世英 ,
  • 罗方正 ,
  • 胡宇 ,
  • 朱杰堂
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  • 第二炮兵工程大学,西安 710025

张世英(1962-),男,山东莘县人,教授,博士,研究方向:航空推进系统控制与故障诊断。

收稿日期: 2013-02-01

  网络出版日期: 2025-05-26

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Virtual Experiment Platform for Turbofan Engine Overall Performance

  • ZHANG Shiying ,
  • LUO Fangzheng ,
  • HU Yu ,
  • ZHU Jietang
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  • The Second Artillery Engineering University, Xi'an 710025, China

Received date: 2013-02-01

  Online published: 2025-05-26

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摘要

针对涡扇发动机研制难度大、周期长和费用高的问题,构建了一个涡扇发动机总体性能虚拟试验平台。试验平台遵循MVC(model-view-controller)设计模式分为模型层、试验控制层和用户界面层;基于Lab-VIEW虚拟仪器开发平台,设计了虚拟试验平台用户界面。通过某型涡扇发动机总体性能虚拟试验,表明了虚拟试验平台具有良好的可视化效果和扩展能力,可以运用于涡扇发动机的设计、研制和试验。

关键词： 虚拟试验平台; 涡扇发动机; 总体性能; MVC设计模式; LabVIEW

本文引用格式

张世英 , 罗方正 , 胡宇 , 朱杰堂 . 涡扇发动机总体性能虚拟试验平台研究[J]. 弹箭与制导学报, 2013 , 33(5) : 115 -118,122 . DOI: 10.15892/j.cnki.djzdxb.2013.05.049

Abstract

Due to difficulty, long cycle and high cost of turbofan engine development, a virtual experiment platform for overall performance of turbofan engine was built up. According to the MVC design pattern, the model layer, the experiment control layer and the user interface layer were designed for the virtual experiment platform. Based on LabVIEW virtual instrument development platform, the user interface of virtual experiment platform was designed. Through overall performance virtual experiments of a certain type of turbofan engine, the good visual effect and good expansibility of the platform were verified. Therefore, the virtual experiment platform can be used for design, development and experiment of turbofan engine.

Key words： virtual experiment platform; turbofan engine; overall performance; MVC design pattern; LabVIEW

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