更多电动飞机飞行控制系统的能量优化特性分析

2018 IEEE 2nd International Electrical and Energy Conference (CIEEC) Pub Date : 2018-11-01 DOI:10.1109/CIEEC.2018.8745908

Zheng Cao, Haigang Liu, Yuanjun Zhou, Chen Zhang

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引用次数: 2

摘要

更多电动飞机的二次能源是用电能替代液压能和气动能，以达到节约能源的目的。飞控系统是完成能量转换的机载系统。本文根据飞控系统作动器短时功率特性，从能量损耗、能量传输和能量转化等方面对多用途电动飞机的电动作动器系统与传统液压作动器系统进行了比较。本文还分析了多用途电动飞机飞行控制系统的能量优化特性。在此基础上，模拟了典型飞行状态下的功率特性，并通过模拟数据分析了能量优化。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Energy optimization Charateristic Analysis of More Electric Aircraft Flight Control System

The secondary energy of more electric aircraft uses electrical energy to replace hydraulic energy and pneumatic energy in order to achieve the purpose of saving energy. The flight control system is an airborne system to complete energy transformation. According to the actuator short-time power characteristics of flight control system, this paper compares the electric actuator system of more electric aircraft with the traditional hydraulic actuator system in terms of energy loss, energy transmission and energy transformation. It also analyses energy optimization characteristics of more electric aircraft flight control system. On this basis, the power characteristics are simulated under typical flight status and energy optimization is analyzed by simulation data.

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来源期刊

2018 IEEE 2nd International Electrical and Energy Conference (CIEEC)

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