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Induction Generator Used Auxiliary Power Unit, Power Generation and Management of an Electrical Aircraft

Mohd Niyaz Ali Khan, Fariha Khatoon

Abstract


In More Electric Airship (MEA) frameworks, the selection of electro-pressure driven actuators (EHAs) and electromechanical actuators (EMAs) requires a power-on-request electrical power framework with regenerative power administration ability. This paper proposes an Assistant Power Unit (APU) for control age and administrative framework to supply/retain the very unique power request/recovery from the EHA/EMAs. The proposed framework uses an open-end winding acceptance starter/generator (LEWIS/G) to make a different DC transport for the actuators without adding huge equipment portion to the framework. Amid the whole flight mission, the regenerative power is recouped by one side of the OEWIG terminals; in the interim, the power conveyance to the principle DC system of the airplane electrical power framework can be freely controlled by utilizing a similar generator through the opposite side of the terminals. A shut circle control conspire in light of field arranged control and immediate power hypothesis is created to direct both the principle DC transport voltage and the electric incitation DC transport voltage at the same time in flying machine crisis control mode.


Keywords


Induction Motors, Generators, Aircraft, Power Generation Control, Regenerative Power Management

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References


M. E. Elbuluk, M. D. Kankam," Motor Drive Technologies for the Power-by-Wire (PBW) Program: Options, Trends, and Tradeoffs," Proceedings of the IEEE 1995 National Aerospace and Electronics Conference, NAECON'95, pp. 511-522.

Lester Faleiro, "Summary of the European Power Optimized Aircraft (POA) Project," in 25th International Congress of the Aeronautical Sciences, ICAS 2006

I. Moir and A. Seabridge, "Aircraft systems: Mechanical, electrical, and avionics subsystems integration", John Wiley & Sons, 2008

Ciancetta, F.; Rotondale, N.; Del Pizzo, A.; Nardi, M., "Development of a measurement system to test the efficiency of electrical generators for energy recovery on aircraft actuators," in Clean Electrical Power (ICCEP), 2013 International Conference on, vol., no., pp.564-570, 11-13 June 2013

Crowder, R.M., "Electrically powered actuation for civil aircraft," in Actuator Technology: Current Practice and New Developments., IEE Colloquium on (Digest No: 1996/110), vol., no., pp.5/1-5/3, 10 May 1996

Hill, C.I.; Bozhko, S.; Tao Yang; Giangrande, P.; Gerada, C., "More Electric Aircraft Electro-Mechanical Actuator Regenerated Power Management," in Industrial Electronics (ISIE), 2015 IEEE 24th International Symposium on, vol., no., pp.337-342, 3-5 June 2015

Yuhang Deng; Foo, S.Y.; Bhattacharya, I., "Regenerative electric power for More Electric Aircraft," in SOUTHEASTCON 2014, IEEE, vol., no., pp.1-5, 13-16 March 2014

Wheeler, P.; Trentin, A.; Bozhko, S.; Clare, J., "Regeneration of energy onto an aircraft electrical power system from an electromechanical actuator," in Electrical Systems for Aircraft, Railway and Ship Propulsion (ESARS), 2012, vol., no., pp.1-6, 16-18 Oct. 2012

Wu, T.X.; Zumberge, J.; Wolff, M., "On regenerative power management in more electric aircraft (MEA) power system," in Aerospace and Electronics Conference (NAECON), Proceedings of the 2011 IEEE National, vol., no., pp.211-214, 20-22 July 2011

MIL_STD 704 Aircraft Electric Power Characteristics RTCA/DO-160 Environmental Conditions and Test Procedures for Airborne Equipment

K.S.Rajashekara and J.Vithayathil, "Microcomputer-Based Symmetrical Sinusoidal Pulse Width Modulated Inverter", IEEE IECI Proceedings, San Francisco, USA, PP. 34-38, November 1981.

K.S. Rajashekara and V. Rajagopalan, "Simulation of SSPWM Inverter-Fed Induction Motor", International Symposium on Modeling and Simulation of Electrical Machines, Converters and Power Systems, August 24-25, 1987, Quebec City, Canada

H. Stemmler and P. Guggenbach, “Configurations of high-power voltage source inverter drives,” in Proc. Eur. Power Elec. Appl. Conf., Brighton, U.K., 1993, vol. 5, pp. 7–14.

Jia, Yijiang; Rajashekara, Kaushik, "An induction generator based AC/DC hybrid electric power generation system for more electric aircraft," in Industry Applications Society Annual Meeting, 2015 IEEE, vol., no., pp.1-7, 18-22 Oct. 2015.

Jia, Y.; Prasanna, U.R.; Rajashekara, K., "An open-end winding induction generation system for frequency insensitive AC loads in more electric aircraft," Industrial Electronics Society, IECON 2014 - 40th Annual Conference of the IEEE, vol., no., pp.410,416, Oct. 29 2014-Nov. 1 2014.

D. W.Novotnyand T. A. Lipo, Vector Control, and dynamics AC Drives, Oxford, U.K.: Oxford Univ. Press, 1996.

Y. Jia and K. Rajashekara, “An induction generator based AC/DC hybrid electric power generation system for more electric aircraft,” in Proc. 2015 IEEE Ind. Appl. Soc. Annu. Meeting, Addison, TX, USA, 2015, pp. 1–7.

R. C. Bansal, “Three-phase self-excited induction generators: an overview,” IEEE Trans. Energy Convers., vol. 20, no. 2, pp. 292–299, Jun. 2005.

H. Stemmler and P. Guggenbach, "Configurations of high-power voltage source inverter drives," in Proc. 19935thEur. Conf. PowerElectron. Appl., Brighton, U.K., 1993, vol. 5, pp. 7–14.

T. Kawabata, E. C. Ejiogu, Y. Kawabata, and K. Nishiyama, "New open winding configurations for high-power inverters," in Proc. IEEE Intl.Symp. Ind. Electron. Guimaraes, Portugal, 1997, vol. 2, pp. 457–462.

G. Gallegos-Lopez, F. S. Gunawan, and J. E. Walters, “Current control of induction machines in the field-weakened region,” IEEE Trans. Ind. Appl., vol. 43, no. 4, pp. 981–989, Jul./Aug. 2007.

C. Lascu, I. Boldea, and F. Blaabjerg, "A modified direct torque control for an induction motor sensorless drive," IEEE Trans. Ind. Appl., vol. 36, no. 1, pp. 122–130, Jan./Feb. 2000.

P. L. Jansen, R. D. Lorenz, and D. W. Novotny, “Observer-based direct field orientation: analysis and comparison of alternative methods,” in Proc. Conf. Rec. 1993 IEEE Ind. Appl. Soc. Annu. Meeting, Toronto, ON, Canada, 1993, vol. 1, pp. 536–543.

P. L. Jansen and R. D. Lorenz, "A physically insightful approach to the design and accuracy assessment of flux observers for field-oriented induction machine drives," IEEE Trans. Ind. Appl., vol. 30, no. 1, pp. 101–110, Jan./Feb. 1994.

M. S. Huang and C. M. Liaw, “Improved field-weakening control for IFO induction motor,” in IEEE Trans. Aerosp. Electron. Syst., vol. 39, no. 2, pp. 647–659, Apr. 2003.

P. J. Coussens, A. P. Van den Bossche, and J. A. Melkebeek, “Magnetizing current control strategies for nonlinear indirect field oriented control,” in Proc. Conf. Rec. 1995 IEEE Ind. Appl. Conf., Orlando, FL, USA, 1995, vol. 1, pp. 538–545

M. Tarbouchi and H. Le Huy, “Control by exact linearization of an induction motor in field weakening regime,” in Proc. 24th Annu. Conf. IEEE Ind. Electron. Soc., Aachen, Germany, 1998, vol. 3, pp. 1597–1602

Department of Defense (United States of America) Interface Standard, Aircraft Electric Power Characteristics, MIL-STD-704F, Mar. 2004.

G. M. Raimondi et al., “Aircraft embedded generation systems,” in Proc. 2002. Int. Conf. Power Electron., Mach. Drives (Conf. Publ. No. 487), Jun. 4–7, 2002, pp. 217–222.




DOI: http://dx.doi.org/10.36039/AA092018002.

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