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弹道与气动力技术

基于 ATR 动力的飞行器性能分析

  • 李平 ,
  • 柳长安 ,
  • 何国强 ,
  • 南向谊
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  • 1 西北工业大学航天学院,西安 710072
    2 西安航天动力研究所,西安 710100

李平(1968-),男,湖北石首人,研究员,研究方向:液体火箭发动机和组合推进。

收稿日期: 2011-04-07

  网络出版日期: 2025-05-30

Performance Analysis of an Aircraft with ATR Engine

  • LI Ping ,
  • LIU Chang'an ,
  • HE Guoqiang ,
  • NAN Xiangyi
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  • 1 School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China
    2 Xi'an Aerospace Propulsion Institute, Xi'an 710100, China

Received date: 2011-04-07

  Online published: 2025-05-30

摘要

空气涡轮冲压发动机(ATR)是一种具有大空域、宽速域特点的新型吸气式组合动力。为了分析这种动力的应用特点,文中首先进行了ATR发动机和某型涡扇发动机性能的对比,然后按相同飞行器平台进行了加速和爬升等基本飞行性能的分析,获得了切向过载和经济爬升性等指标的比较结果。结果表明ATR动力可以提升飞行器机动性,扩展飞行包线。

本文引用格式

李平 , 柳长安 , 何国强 , 南向谊 . 基于 ATR 动力的飞行器性能分析[J]. 弹箭与制导学报, 2011 , 31(6) : 173 -175 . DOI: 10.15892/j.cnki.djzdxb.2011.06.031

Abstract

The air-turbo-ramjet engine (ATR) is a kind of combined air-breathing engine with the characters of broad velocity and altitude envelope. the application characters of ATR engine, the ATR engine with the turbofan engine their propulsion characters and basic flight performances of a certain aircraft platform. The results axial-overload and economic-climb-rate etc obtained. The results show that ATR engine can upgrade the aircraft maneuverabilit and flight envelope.

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参考文献

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