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涡扇发动机加速过程转速预测模型

雷杰 潘鹏飞 许艳芝 马明明

航空科学技术Issue(6):47-51,5.
航空科学技术Issue(6):47-51,5.

涡扇发动机加速过程转速预测模型

Rotor Speed Prediction Model on Acceleration of Turbofan Engine

雷杰 1潘鹏飞 1许艳芝 1马明明1

作者信息

  • 1. 中国飞行试验研究院,陕西 西安 710089
  • 折叠

摘要

Abstract

Took a certain turbofan engine as the research object, made a delving research on the transient lfight data of the accelerated process under different conditions, through the analysis of rotor speed variation characteristics, established a rotor speed prediction model to the type of engine during a accelerated transient process, and combined with the lfight test data to verify the engine prediction model, result show that the calculated results had a higher goodness of ift with the test data, can be used for rotor speed prediction during the accelerated transient process.

关键词

涡扇发动机/飞行试验/加速过程/转速预测/发动机模型

Key words

turbofan engine/lfight test/acceleration transient/rotor speed/engine model

分类

航空航天

引用本文复制引用

雷杰,潘鹏飞,许艳芝,马明明..涡扇发动机加速过程转速预测模型[J].航空科学技术,2015,(6):47-51,5.

航空科学技术

1007-5453

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