ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Modeling and analysis of aero DC generation system based on excitation current feedforward regulation
Received date: 2014-05-23
Revised date: 2014-10-13
Online published: 2014-10-21
Supported by
Funding of Jiangsu Innovation Program for Graduate Education (CXZZ13_0161); Fundamental Research Funds for the Central Universities
High-voltage direct-current (HVDC) power system has been the preferred aviation power supply because of its high efficiency, light weight and high reliability. The large capacitor in the system leads to the fact that the traditional regulating plan using PI cannot meet the requirements of the dynamic performance. For this, the excitation current feedforward (ECF) technology has been proposed in the regulators in the aircraft generation system. The mathematical model of the generation system with and without the ECF is built respectively to compare the dynamic characteristics of the system. Experimental results show that with ECF the system can respond quickly and remain stable, and the dynamic performance improves significantly in sudden change of the load in the system. This technology could be applied to other voltage regulators in the aircraft generation system.
ZHAO Yao , WANG Huizhen , ZHANG Haibo , CHEN Chen , XIAO Lan . Modeling and analysis of aero DC generation system based on excitation current feedforward regulation[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015 , 36(4) : 1230 -1239 . DOI: 10.7527/S1000-6893.2014.0287
[1] Du X F, Hou Y Z, Sun C, et al. Optimization analysis of rectangular rotor slot of cage induction motor operating with aero variable frequency power[J]. Acta Aeronautica et Astronautica Sinica, 2015: 36(2): 614-624 (in Chinese). 杜肖飞, 侯砚泽, 孙楚, 等. 航空变频电源下笼型感应电机矩形转子槽结构优化分析[J]. 航空学报, 2015: 36(2): 614-624.
[2] Zhuang S L, Huang W X, Bu F F, et al. Asymmetric operation performance for variable frequency AC generation system based on dual stator-winding induction generator[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(12): 3415-3424 (in Chinese). 庄圣伦, 黄文新, 卜飞飞, 等. 定子双绕组异步发电机航空变频交流发电系统不对称运行性能分析[J]. 航空学报, 2014, 35(12): 3415-3424.
[3] Hao Z Y, Hu Y W, Huang W X, et al. Analysis and prediction of high accuracy nonlinear inductance analytical formulation of fault tolerant permanent magnet machines[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(11): 2156-2164 (in Chinese). 郝振洋, 胡育文, 黄文新, 等. 具有高精度的永磁容错电机非线性电感分析及其解析式求取[J]. 航空学报, 2009, 30(11): 2156-2164.
[4] Yu W T, Hu Y W, Hao Z Y, et al. Experimental study on optimal torque control of fault tolerant permanent magnet motor[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(8): 1622-1628 (in Chinese). 余文涛, 胡育文, 郝振洋, 等. 永磁容错电机最优转矩控制策略实验[J]. 航空学报, 2010, 31(8): 1622-1628.
[5] Hao Z Y, Hu Y W. Design and experimental analysis on the control system of high reliability fault tolerant permanent magnetic motor used in electric actuator[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(1): 141-152 (in Chinese). 郝振洋, 胡育文. 电力作动器用高可靠性永磁容错电机控制系统的设计及其试验分析[J]. 航空学报, 2013, 34(1): 141-152.
[6] Wang W, Guo H, Li Y M. Analysis of winding short circuit in electrical/mechanical hybrid 4-redundancy brushless DC torque motor[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(5): 975-982 (in Chinese). 王巍, 郭宏, 李艳明. 电气/机械混合四余度无刷直流力矩电动机绕组短路分析[J]. 航空学报, 2010, 31(5): 975-982.
[7] Liu Z Y, Deng Z Q, Wang S S, et al. Effect of control strategies on iron losses of bearingless switched reluctance motors[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(12): 2401-2410 (in Chinese). 刘泽远, 邓智泉, 王世山, 等. 控制策略对无轴承开关磁阻电机铁心损耗的影响[J]. 航空学报, 2009, 30(12): 2401-2410.
[8] Song S J, Liu W G, Dieter P, et al. Detailed design of a high speed switched reluctance starter/generator for more/all electric aircraft[J]. Chinese Journal of Aeronautics, 2010, 23(2): 216-226.
[9] Cai Y H, Qi R Y, Cai J, et al. Online modeling for switched reluctance motor using radial basis function neural network and its experimental validation[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(4): 705-714 (in Chinese). 蔡永红, 齐瑞云, 蔡骏, 等. 基于RBF神经网络的开关磁阻电机在线建模及其实验验证[J]. 航空学报, 2012, 33(4): 705-714.
[10] Dai W L. Research on brushless DC starter-generator system for aircraft engine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2008 (in Chinese). 戴卫力. 飞机无刷直流起动发电系统的研究[D]. 南京:南京航空航天大学, 2008.
[11] Zhang Z R, Chen Z H, Yang S S, et al. Research on digital avr of doubly salient electro-magnetic generator[J]. Electrical Application, 2005, 24(10):103-106 (in Chinese). 张卓然, 陈志辉, 杨善水, 等. 电励磁双凸极电机数字电压调节器的研究与实现[J].电气应用, 2005, 24(10):103-106.
[12] Liao Y, Lipo T A. A novel permanent magnet motor with double salient structure[J]. IEEE Transactions on Industry Application, 1995, 31 (5): 1069-1078.
[13] Zhao Y, Wang H Z, Xiao L, et al. Analysis on single-phase short-circuit performances of five-phase fault-tolerant doubly salient electro-magnetic generators[J]. Proceedings of the CSEE, 2013, 33(24): 135-142 (in Chinese). 赵耀, 王慧贞, 肖岚, 等. 五相容错电励磁双凸极电机容错特性分析[J]. 中国电机工程学报, 2013, 33(24): 135-142.
[14] Zhao Y, Wang H Z, Zhao X Z, et al. Analysis on single-phase short-circuit performances of five-phase fault-tolerant doubly salient electro-magnetic generators[J]. Proceedings of the CSEE, 2013, 33(30): 90-97 (in Chinese). 赵耀, 王慧贞, 赵晓中, 等. 五相容错双凸极发电机单相短路故障分析[J]. 中国电机工程学报, 2013, 33(30): 90-97.
[15] Wang L, Yang S H, Zhang Z R, et al. Application of load current feedback compensating in digital voltage regulation for doubly salient brushless dc generator[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(5): 934-938 (in Chinese). 王莉, 杨善水, 张卓然, 等. 负载电流反馈补偿法在双凸极无刷直流发电机数字调压器中的应用[J].航空学报, 2006, 27(5): 934-938.
[16] Chen Z H, Yan Y G, Chen H M. Realization of DSP control of voltage regulator on doubly-salient generator[J]. Journal of Nanjing University of Aeronautics and Astronautics, 2000, 32(3): 251-256 (in Chinese). 陈志辉, 严仰光, 陈鸿茂. 双凸极发电机电压调节的DSP控制实现[J]. 南京航空航天大学学报, 2000, 32(3): 251-256.
[17] Wei J D. Research on characteristics for doubly salient electrical magnet starter/generator[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2008 (in Chinese). 魏佳丹. 电励磁双凸极起动/发电系统特性研究[D].南京: 南京航空航天大学, 2008.
[18] GJB 181-86. Powered aircraft characteristics and requirements for electrical equipment[S]. Beijing: Commission of Science, Technology, and Industry for National Defense, 1986 (in Chinese). GJB 181-86.飞机供电特性及对用电设备的要求[S]. 北京: 国防科学技术工业委员会, 1986.
/
〈 | 〉 |