| 注册
首页|期刊导航|航空科学技术|一种分布式电推进飞机的多学科参数快速估计方法

一种分布式电推进飞机的多学科参数快速估计方法

于昊亮 雷涛 张星雨 张晓斌

航空科学技术2024,Vol.35Issue(1):65-74,10.
航空科学技术2024,Vol.35Issue(1):65-74,10.DOI:10.19452/j.issn1007-5453.2024.01.007

一种分布式电推进飞机的多学科参数快速估计方法

A Fast Multidisciplinary Parameter Estimation Method for Distributed Electric Propulsion Aircraft

于昊亮 1雷涛 1张星雨 1张晓斌1

作者信息

  • 1. 西北工业大学 飞机电推进技术工业和信息化部重点实验室,陕西 西安 710072
  • 折叠

摘要

Abstract

Due to the significant overall performance and strong interdisciplinary nature of distributed electric propulsion aircraft,it is a trend in the future development of aircraft in the aviation industry.Therefore,establishing a multidisciplinary parameter evaluation method applicable to the conceptual design phase of distributed electric propulsion aircraft is of great fundamental significance for their design.To improve the efficiency of electric aircraft in the initial design phase,this paper proposes a rapid multidisciplinary parameter estimation method for distributed electric propulsion aircraft.This method involves the overall modeling of distributed electric propulsion aircraft and the establishment of an electric power system framework.It utilizes a simplified aerodynamic analysis method based on potential flow theory to analyze the aerodynamic-propulsive coupling characteristics between the propellers and the wings.Through simulation validation,it is demonstrated that the simplified aerodynamic model can effectively simulate the aerodynamic-propulsive coupling characteristics between the propellers and the wings.Using this method,a rapid multidisciplinary parameter estimation is performed on a specific distributed electric propulsion aircraft under a set flight profile,obtaining the variations in the aircraft's aerodynamic performance and the performance of the electric propulsion system throughout the flight profile,providing support for the conceptual design of distributed electric propulsion aircraft.

关键词

分布式电推进/多学科分析/电力推进技术/涡格法/螺旋桨滑流

Key words

distributed electric propulsion/multidisciplinary analysis/electric propulsion technology/vortex lattice method/propeller slipstream

分类

航空航天

引用本文复制引用

于昊亮,雷涛,张星雨,张晓斌..一种分布式电推进飞机的多学科参数快速估计方法[J].航空科学技术,2024,35(1):65-74,10.

基金项目

国家自然科学基金(51877178)National Natural Science Foundation of China(51877178) (51877178)

航空科学技术

1007-5453

访问量0
|
下载量0
段落导航相关论文