民用飞机飞行中推力确定研究
作者:
作者单位:

1.上海交通大学,上海 200240 ;2.中国商飞民用飞机试飞中心,上海 200232 ;3.中国商飞公司,上海 200126

作者简介:

王涛,男,硕士,试飞工程师,正高级工程师。主要研究方向:民用飞机飞行试验与验证。E-mail:wangtao1@comac.cc

通讯作者:

王涛,E-mail:wangtao1@comac.cc

中图分类号:

V235

基金项目:


Research on in-flight thrust determination of commercial aircraft
Author:
Affiliation:

1.Shanghai Jiao Tong University, Shanghai, 200240 ,China ;2.Commercial Aircraft Corporation of China Ltd Flight Test Center, Shanghai 200232 , China ;3.Commercial Aircraft Corporation of China Ltd, Shanghai 200126 , China

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    摘要:

    确定飞行中发动机安装推力对飞机性能计算、发动机推力管理、经济性评价等具有重要意义。飞行中推力无法直接测量,需要在动力装置内部适当位置安装传感器测量性能参数,计算得出飞行中推力。研究了民用飞机动力装置飞行中推力确定方法,给出发动机安装净推力公式。介绍了推力计算的流程,利用某大涵道比涡扇发动机性能试飞数据,计算了该动力装置的安装净推力,并与参考值进行了对比分析,可为民用飞机型号设计提供参考。

    Abstract:

    The net thrust of engine is of great significance for aircraft performance calculation, engine power management and engine performance evaluation etc. Due to the impossibility to measure in-flight thrust of propulsion system directly, sensors must be installed into the engine interior flow paths to collect performance data, then the in-flight thrust can be calculated. The method of determining in flight thrust of civil aircraft powerplant is studied, and a formula for the net thrust of installed engine is provided. The process of thrust calculation was introduced, and the installed net thrust of a new high bypass ratio turbofan engine is calculated by using the data of engine performance flight test,and the comparison and analysis are made with the reference value. This study can provide reference for commercial aircraft design.

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引用本文

王涛,刘燚,米毅,等.民用飞机飞行中推力确定研究[J].民用飞机设计与研 究,2024(2):27-32WANG Tao, LIU Yi, MI Yi, et al. Research on in-flight thrust determination of commercial aircraft[J]. Civil Aircraft Design and Research,2024,(2):27-32. ( in Chinese)

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  • 在线发布日期: 2024-07-01
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