基于模型的多电飞机能源优化特性仿真分析

doi:10.7527/S1000-6893.2021.25801

论文

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

基于模型的多电飞机能源优化特性仿真分析

刘海港, 刘亮, 王鹏, 周维

航空工业沈阳飞机设计研究所, 沈阳 110035

收稿日期:2021-04-15 修回日期:2021-05-08 发布日期:2021-05-31
通讯作者: 刘海港 E-mail:369686575@qq.com

Model based simulation and analysis of energy optimization characteristics of more-electric aircraft

LIU Haigang, LIU Liang, WANG Peng, ZHOU Wei

AVIC Shenyang Aircraft Design and Research Institute, Shenyang 110035, China

Received:2021-04-15 Revised:2021-05-08 Published:2021-05-31

摘要/Abstract

摘要： 多电飞机是一种用电能部分取代原来的液压能和气压能的飞机，其二次能源系统以电能为主。为实现多电飞机能源系统的优化设计，将飞机的发电、配电和用电集成在一个统一的系统内，实行发电、配电和用电的统一规划、统一管理和集中控制。为快速有效地分析多电飞机能源系统优化特性，本文采用基于模型的系统工程方法论，针对多电飞机能源优化仿真分析平台开展研究，提出了一种面向电气设备的多物理域模型建模方法，以实现机载系统的大规模集成仿真。并以飞控系统为对象，建立了多电飞机飞控系统和传统飞机飞控系统的能量利用、能量传送、能量变换设备等仿真模型，仿真分析了两种飞控系统的能源应用特性，为多电飞机能源系统的优化设计提供了有效支撑。

关键词: 多电飞机, 飞控系统, 多物理域建模, 功率损耗, 能源优化

Abstract: More-electric aircraft is an aircraft that uses electric energy to replace the hydraulic energy and air pressure energy, and its secondary energy system is mainly composed of electric energy. To obtain the optimal design of the more-electric aircraft energy system, the generation, distribution and power consumption of aircraft are integrated into a unified system to implement unified planning, unified management, and centralized control of power generation, distribution and consumption. To analyze the optimization characteristics of the more-electric aircraft energy system quickly and effectively, this paper uses the model-based system engineering methodology to study the more-electric aircraft energy optimization simulation platform. A multi physical domain modeling method for electrical equipment is proposed to realize large-scale integrated simulation of the airborne system. The simulation models for energy utilization, energy transmission and energy transformation equipment of the more-electric aircraft flight control system and the traditional aircraft flight control system are established. The energy application characteristics of the two flight control systems are analyzed. Our study can provide effective support for optimization of the energy system of more-electric aircraft.

Key words: more-electric aircraft, flight control system, multi-physical domain modeling, power loss, energy optimization

中图分类号:

V242

刘海港, 刘亮, 王鹏, 周维. 基于模型的多电飞机能源优化特性仿真分析[J]. 航空学报, 2021, 42(8): 525801-525801.

LIU Haigang, LIU Liang, WANG Peng, ZHOU Wei. Model based simulation and analysis of energy optimization characteristics of more-electric aircraft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525801-525801.

参考文献

[1] ROSERO J A, ORTEGA J A, ALDABAS E, et al. Moving towards a more electric aircraft[J].IEEE Aerospace & Electronic Systems Magazine, 2007, 22(3):3-9.
[2] 张卓然, 于立, 李进才, 等. 飞机电气化背景下的先进航空电机系统[J].南京航空航天大学学报, 2017, 49(5):622-634. ZHANG Z R, YU L, LI J C, et al. Key technologies of advanced aircraft electrical machine systems for aviation electrification[J].Journal of Nanjing University of Aeronautics & Astronautics, 2017, 49(5):622-634(in Chinese).
[3] JONES R I. The more electric aircraft assessing the benefits[J].Journal of Aerospace Engineering, 2002, 216(5):259-269.
[4] WHEELER P. Technology for the more and all electric aircraft of the future[C]//2016 IEEE International Conference on Automatica (ICA-ACCA), 2016.
[5] AVERY C R, BURROW S G, MELLOR P H. Electrical generation and distribution for the more electric aircraft[C]//International Universities Power Engineering Conference, 2008.
[6] 张卓然, 李进才, 韩建斌, 等. 多电飞机大功率高压直流起动发电机系统研究与实现[J].航空学报, 2020, 41(2):323537. ZHANG Z R, LI J C, HAN J B, et al. Research and implementation of high-power high-voltage DC brushless starter generator system for more-electric-aircraft[J].Acta Aeronautica et Astronautica Sinica, 2020, 41(2):323537(in Chinese).
[7] HAITAOA Q I, YONGLINGA F U, XIAOYEA Q I. Architecture optimization of more electric aircraft actuation system[J].Chinese Journal of Aeronautics, 2011, 24(4):506-513.
[8] QIAO G, LIU G, SHI Z H, et al. A review of electromechanical actuators for more/all electric aircraft systems[J].Proceedings of the Institution of Mechanical Engineers Part C:Journal of Mechanical Engineering Science, 2017, 232(22):095440621774986.
[9] KARTHIK S P, VIJAY D, JEPPU Y V, et al. Characterization of aircraft electro hydrostatic actuator using virtual instrumentation[C]//2014 IEEE International Conference on Smart Instrumentation, Measurement and Applications (ICSIMA), 2014.
[10] LIANG B, LI Y R, ZHANG Z H. Research on simulation of aircraft electro-hydrostatic actuator anti-skid braking system[C]//2011 Third International Conference on Measuring Technology and Mechatronics Automation, 2011.
[11] 孙晓哲, 杨珍书, 陈棒, 等. 飞控机电作动系统典型故障模式影响分析[J].微特电机, 2019, 47(10):25-30, 35. SUN X Z, YANG Z S, CHEN B, et al. Typical fault modes and effect analysis of flight control electromechanical actuation system[J].Small & Special Electrical Machines, 2019, 47(10):25-30, 35(in Chinese).
[12] 白龙, 孙楚, 周元钧. 航空机电作动器的混合整流全状态反馈控制[J].航空学报, 2016, 37(6):1940-1952. BAI L, SUN C, ZHOU Y J. Full-state feedback control of a novel hybrid rectifier applied to aircraft electric actuator load[J].Acta Aeronautica et Astronautica Sinica, 2016, 37(6):1940-1952(in Chinese).
[13] 付永领, 齐海涛, 王利剑, 等. 混合作动系统的工作模式研究[J].航空学报, 2010, 31(6):1177-1184. FU Y L, QI H T, WANG L J, et al. Research on operating modes in hybrid actuation systems[J].Acta Aeronautica et Astronautica Sinica, 2010, 31(6):1177-1184(in Chinese).
[14] MARE J C, JIAN F U. Review on signal-by-wire and power-by-wire actuation for more electric aircraft[J].Chinese Journal of Aeronautics, 2017, 30(3):857-870.
[15] 关栋, 杨小辉, 刘更, 等. 功率电传作动系统用电机关键技术及其发展趋势[J].微特电机, 2012, 40(5):71-75. GUAN D, YANG X H, LIU G, et al. Development trend and key technologies of the electrical motor for power-by-wire actuator system[J].Small & Special Electrical Machines, 2012, 40(5):71-75(in Chinese).
[16] 黄子林, 刘宏明, 马勇. 多电飞机飞控系统的技术应用[J].航空制造技术, 2014(S1):199-200. HUANG Z L, LIU H M, MA Y. Technical application of multi electric aircraft flight control system[J].Aeronautical Manufacturing Technology, 2014(S1):199-200(in Chinese).
[17] SCHETTINI F, DENTI E, RITO G D, et al. Simulation of an all-electric flight control system for the evaluation of power consumption[C]//29th Congress of the International Council of the Aeronautical Sciences, 2014.
[18] HU W N, ZHOU L, TIAN Y S, et al. Analysis for the power loss of electro hydrostatic actuator and hydraulic actuator[C]//2015 IEEE International Conference on Advanced Intelligent Mechatronics (AIM), 2015.
[19] 许海军, 周扬忠. 直接转矩控制永磁同步高压直流发电系统研究[J].电力电子技术, 2012, 46(1):79-81. XU H J, ZHOU Y Z. Research on high voltage direct current generation system of permanent magnet synchronous generator based on direct torque control[J].Power Electronics, 2012, 46(1):79-81(in Chinese).
[20] 李岩, 苏学军, 李运. 基于航空高压直流电源系统的永磁同步电机起动发电系统设计[J].电机与控制应用, 2017, 44(1):60-64. LI Y, SU X J, LI Y. Design of integrated starter/generator system for permanent magnet synchronous motor based on high voltage DC in aircraft[J].Electric Machines & Control Application, 2017, 44(1):60-64(in Chinese).
[21] CAO Z, ZHOU Y J, LIU H G, et al. Energy optimization characteristic analysis of more electric aircraft flight control system[C]//2017 International Electrical and Energy Conference (CIEEC 2017), 2017.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

基于模型的多电飞机能源优化特性仿真分析

Model based simulation and analysis of energy optimization characteristics of more-electric aircraft

RichHTML

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	荘露, 陆中, 宋海靖, 董力, 吴雨婷, 周伽. 基于故障注入模型的电传飞控系统安全性分析[J]. 航空学报, 2023, 44(9): 327329-327329.
[2]	苏宁, 黄文新. 电推进飞机定子双绕组感应发电机并联系统[J]. 航空学报, 2022, 43(8): 325409-325409.
[3]	张本栋, 江军, 李治, 李世民, 张潮海. 面向未来多电飞机的低气压下局部放电[J]. 航空学报, 2022, 43(7): 325374-325374.
[4]	张卓然, 许彦武, 于立, 李进才, 夏一文. 多电飞机高压直流并联供电系统发展现状与关键技术[J]. 航空学报, 2021, 42(6): 624069-624069.
[5]	江军, 张本栋, 王凯, 李文源, 张潮海. 面向多电飞机的脉冲波形下局部放电规律[J]. 航空学报, 2020, 41(9): 323889-323889.
[6]	张卓然, 李进才, 韩建斌, 陆嘉伟, 石珩. 多电飞机大功率高压直流起动发电机系统研究与实现[J]. 航空学报, 2020, 41(2): 323537-323537.
[7]	雷涛, 闵志豪, 付红杰, 张星雨, 李伟林, 张晓斌. 燃料电池无人机混合电源动态平衡能量管理策略[J]. 航空学报, 2020, 41(12): 324048-324048.
[8]	杨绚, 魏小勇, 崔德龙. 舰载机飞行控制系统总线接口策略[J]. 航空学报, 2019, 40(4): 622283-622283.
[9]	朱德明, 李进才, 韩建斌, 张卓然, 严仰光. 起动发电机在中国大型客机上的应用[J]. 航空学报, 2019, 40(1): 522479-522479.
[10]	程龙, 张方华, 谢敏, 王愈, 邹花蕾. 基于等效时间的混合储能系统高功率密度优化配置[J]. 航空学报, 2018, 39(10): 322129-322129.
[11]	李永锋. 宽体客机飞控电作动系统设计[J]. 航空学报, 2017, 38(S1): 721531-721531.
[12]	葛玉雪, 宋笔锋, 裴扬. 基于可用能的多电飞机能量利用率分析方法[J]. 航空学报, 2014, 35(5): 1276-1283.
[13]	陈云霞;段朝阳. 飞控系统最坏情况分析方法研究[J]. 航空学报, 2005, 26(5): 647-651.
[14]	陈宗基;黄浩东;秦旭东. 飞行控制系统虚拟原型技术[J]. 航空学报, 2002, 23(5): 441-447.
[15]	王少萍;李沛琼;裴英. 飞控系统功能重构技术研究[J]. 航空学报, 1998, 19(S1): 113-115.