五相感应电机起动/发电系统起动控制研究

微特电机 ›› 2020, Vol. 48 ›› Issue (9): 34-38.

五相感应电机起动/发电系统起动控制研究

刘路, 卜飞飞, 刘皓喆, 黄文新

南京航空航天大学多电飞机电气系统工信部重点实验室, 南京 211106

收稿日期:2019-08-05 出版日期:2020-09-28 发布日期:2020-09-21
作者简介:刘路(1995—),男,硕士研究生,研究方向为电力电子与电力传动。

Study on Starting Control of Five-Phase Induction Machine Starter/Generator System

LIU Lu, BU Fei-fei, LIU Hao-zhe, HUANG Wen-xin

Center for More-Electric-Aircraft Power System, Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China

Received:2019-08-05 Online:2020-09-28 Published:2020-09-21

摘要/Abstract

摘要： 起动/发电技术是多电飞机中的一项重要技术。以五相感应起动/发电机为起动机,研究了一种适用于多电发动机的五相感应电机起动控制策略。该控制策略根据发动机起动要求,采用定子磁链定向方法,在起动过程中对转速进行控制,从而实现了多电发动机的起动任务。在一台五相感应电机起动/发电系统实验平台上进行了起动控制实验,结果表明,该控制策略能够满足多电飞机发动机起动要求。

关键词: 起动/发电技术, 多电发动机, 五相感应电机, 起动控制

Abstract: Starter/generator technology is an important technology in more-electric-aircraft. Five-phase induction starter/generator was used as the starter, and a starting control strategy of five-phase induction machine was studied.The control strategy adopted the stator flux linkage method according to the engine starting requirement, and it controlled the rotation speed during the starting process,thereby realizing the starting task of more-electric engine. A starting control experiment was carried out on a five-phase induction machine starter/generator system experimental platform, the results showed that the control strategy can meet the starting requirements of more-electric-aircraft engine.

Key words: starter/generator technology, more-electric engine, five-phase induction machine, starting control

中图分类号:

TM346

刘路, 卜飞飞, 刘皓喆, 黄文新. 五相感应电机起动/发电系统起动控制研究[J]. 微特电机, 2020, 48(9): 34-38.

LIU Lu, BU Fei-fei, LIU Hao-zhe, HUANG Wen-xin. Study on Starting Control of Five-Phase Induction Machine Starter/Generator System[J]. Small & Special Electrical Machines, 2020, 48(9): 34-38.

参考文献

[1] 吴志琨,李军,时瑞军.多电航空发动机研究现况及关键技术[J]. 航空工程进展,2012,3(4):463-467.
[2] 顾春雷,胡育文.独立电源起动/发电系统的研究现状及特点[J].电工技术杂志,2004(11):51-54.
[3] 张卓然,杨善水,陈志辉,等.一种新型双凸极起动发电系统电压调节器设计[J].电力电子技术,2004(3):76-78.
[4] 王雨婷. 直升机电源双凸极起动发电机设计方法与效率优化研究[D].南京:南京航空航天大学,2017.
[5] 马鹏, 刘卫国, 骆光照,等.一种三级式航空无刷同步电机起动控制策略[J].电机与控制学报,2012,16(11): 29-32.
[6] 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.
[7] 严加根,吴韬,姚国飞,等.开关磁阻发电机主电路的一种新拓扑[J].南京航空航天大学学报,2003(1):77-80.
[8] 严加根,刘闯,严利,等.开关磁阻起动/发电机系统数字控制器的研究[J]. 电力电子技术,2005(6):98-101.
[9] 严加根.航空高压直流开关磁阻起动/发电机系统的研究[D].南京:南京航空航天大学, 2006.
[10] JIAO N F,LIU W G,PENG J C,et al.Design and control strategy of a two-phase brushless exciter for three-stage starter/generator[C]//IEEE Energy Conversion Congress and Exposition, 2014: 5864-5869.
[11] 周洁敏.飞机电气系统 [M].北京:科学出版社,2010.
[12] 黄文新,胡育文.用于航空高压直流电源系统的笼型异步发电机控制策略的研究[J].航空学报,2002,23(4): 377-380.
[13] 张兰红.异步电机起动/发电系统研究[D].南京:南京航空航天大学,2006.
[14] 胡育文,黄文新,张兰红.异步电机起动/发电系统的研究[J].电工技术学报,2006,21(5):7-13.
[15] LUCACHE D D,HORGA V,ALBU M,et al.Indirect field oriented control of an integrated starter generator[C]//Proceedings of IEEE IECON,2006(1):5107–5112.
[16] MUDANNAYAKE C P,RAHMAN M F.Control design for an inductions machine based 42 V integrated starter alternator[J].IEEE Industry Applications Magazine,2009,15(4):14–25.
[17] SCARCELLA G,SCELBA G,CACCOATP M,et al.Vector control strategy for multidirectional power flow in integrated multidrives starter-alternator applications[J].IEEE Transactions on Industry Applications,2016,52(6):4816–4826.
[18] RIZZOLI G,SERRA G,MAGGIORE P,et al.Optimized design of a multiphase induction machine for an open rotor aero-engine shaft-line- embedded starter/generator[C]// Proceedings of IEEE IECON,2013:5203–5208.
[19] ZHANG Z R,LIU Y,LI J.A HESM-based variable frequency AC starter-generator system for aircraft applications[J].IEEE Transactions on Energy Conversion,2018,33(4):1998-2006.
[20] 屈鲁,谢卫,卢颖娟.六相感应电机的矢量控制研究[J]. 电机与控制应用,2012,39(5):33-36.