A review of more electric aircraft technology

2013 International Conference on Energy Efficient Technologies for Sustainability, ICEETS 2013

Volumn , Issue , 2013, Pages 750-753

  Naayagi, R T ^a  

^a S A ENGINEERING COLLEGE   (India)

Author keywords

270V DC systems; 230V variable frequency AC systems; Electro hydraulic actuators; Electro mechanical actuators; More Electric Aircraft; Power By Wire

Indexed keywords

AC SYSTEMS; DC SYSTEM; ELECTRO-HYDRAULIC ACTUATOR; MORE ELECTRIC AIRCRAFT; POWER-BY-WIRE;

AEROSPACE INDUSTRY; AIR TRANSPORTATION; AIRCRAFT; ELECTROMECHANICAL ACTUATORS; ELECTROMECHANICAL DEVICES; ENERGY EFFICIENCY; GREENHOUSE GASES; SUSTAINABLE DEVELOPMENT;

AIRCRAFT HYDRAULIC SYSTEMS;

EID: 84881066314     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICEETS.2013.6533478     Document Type: Conference Paper

References (48)

1. UK Transport and climate change data, UK Department of Transport Factsheets, pp.1-20, 2007.
2. Hoffman A.C et al, "Advanced Secondary Power System for Transport Aircraft", NASA Technical paper 2463, 1985.
3. D. Bossche, "More Electric Control surface actuation; A standard for the next generation of transport aircraft", in Proc. European Power Electronic Conference 2003, pp. 1-8.
4. th International Conference on New Actuators, pp. 346-355, June 2008.
5. C.R. Avery, S.G. Burrow, P.H. Mellor, "Electrical generation and distribution for the more electric aircraft", in Proc. IEEE Universities Power Engineering Conference 2007, pp. 1007-1012.
6. A. Emadi and M. Ehsani, "Aircraft Power Systems: Technology, State of the Art, and Future Trends", IEEE Aerospace and Electronic Systems Magazine, vol. 15, no.1, pp. 28-32, January 2000.
7. M. Bailey, N. Hale, G. Ucerpi, J.A. Hunt, S. Mollov, A.J. Forsyth, "Distributed Electrical Power Management Architecture", in Proc. IEE Colloquium on Electrical Machines and Systems for the More Electric Aircraft, pp. 7/1-7/4, 1999.
8. J.S. Cloyd, "Status of the United States air force's More Electric Aircraft Initiative", IEEE Aerospace and Electronic Systems Magazine, vol.13, no. 4, pp. 17-22, April 1998.
9. A.M. Cross, A.J. Forsyth, G. Mason, "Modelling and Simulation Strategies for the Electric Systems of Large Passenger Aircraft", in Proc. Society of Automotive Engineers Power Systems Conference, October 2002, 2002-01-3255.
10. J.A. Rosero, J.A. Ortega, E. Aldabas and L. Romeral, "Moving towards a More Electric Aircraft", IEEE Aerospace and Electronic Systems Magazine, vol. 22, no. 3, pp. 3-9, 2007.
11. I. Moir, "More Electric Aircraft-System Consideration", in Proc. IEE Colloquium on Electrical Machines and Systems for the More Electric Aircraft, pp. 10/1-10/9, November 1999.
12. J.W. Ramsey, "Power-By-Wire", Avionics Magazine, 1 May 2001.
13. A. Charlotte, "A380: 'more electric' aircraft", Aviation Today, 1 October 2001.
14. Solihull, "More-Electric Aircraft Technologies Move from Paper to Platform; TRW Well Down the Road In Proving Its More-Electric Systems Capability" Issue of Business Wire, Jan 17, 2001.
15. th Nov 2008.
16. S. Cutts, "A Collaborative Approach to the More Electric Aircraft", IEE International Conference on Power Electronics, Machines and Drives, April 2002.
17. M. Rinaldi, S. Jones, "Aircraft Electrical system architectures to support more electric aircraft", in Proc. Society of Aerospace Engineers Conference, pp. 10.1-10.7, April 2004.
18. E.H.J. Pallet, Aircraft Electrical Systems, Longman Scientific & Technical, Third edition, 1987.
19. J.A. Weimer, "Electric power technology for the more electric aircraft", in Proc. IEEE Digital Avionics Systems Conference, pp.445-450, October 1993.
20. J.A. Weimer, "The role of electrical machines and drivers in the more electric aircraft", in Proc. IEEE Electrical Machines and Drives Conference, pp. 11-15, June 2003.
21. M.A. Maldonado, N.M. Shah, K.J. Cleek, P.S. Walia, G.J. Korba, "Power Management and Distribution System for a More Electric Aircraft (MADMEL) Program status", in Proc. Energy Conversion Engineering Conference, pp.274-279, August 1997.
22. H. Zhang, C. Saudemont, B. Robyns, M. Petit, "Comparison of Technical Features between a More Electric Aircraft and a Hybrid Electric Vehicle", in Proc. IEEE Vehicle Power and Propulsion Conference, pp.1-6, September 2008.
23. th Annual Applied Power Electronics Conference and Exposition, pp. 906-911, March 1993.
24. L. Faleiro, "Beyond the More Electric Aircraft", Aerospace America, pp. 35-40, September 2005.
25. M.J. Provost, "The more electric aero-engine: A general overview from an engine manufacturer", in Proc. IEEE Power Electronics, Machines and Drives Conference, pp.246-251, April 2002.
26. C. Anghel, M. Xu, "Study on main engine start for more electric architecture aircraft", in Proc. Society of Aerospace Engineers Conference, pp.1-4, November 2006.
27. S.D. Soban, E. Upton, "Towards electric aircraft: Progress under the NASA URETI for aero propulsion and power technology", in Proc. Society of Aerospace Engineers Conference, pp.1-16, November 2006.
28. Stephen L. Botten, Chris R. Whitley, and Andrew D. King, "Flight Control Actuation Technology for Next-Generation All-Electric Aircraft", Technology Review Journal, pp. 55-68, Fall/Winter 2000.
29. W.R. Schley, "The State of the art and remaining challenges in electric actuation for flight and propulsion control", in Proc. Society of Aerospace Engineers Conference, pp.14.1-14.11, April 2004.
30. R.I. Jones, "More Electric Aircraft: the past and the future?", in Proc. IEE Colloquium on Electrical Machines and Systems for the More Electric Aircraft, pp.1/1-1/4, 1999.
31. J.W. Bennett, B.C. Mecrow, A.G. Jack, D.J. Atkinson, S. Sheldon, B. Cooper, G. Mason, C. Sewell, D. Cudley, "A prototype electrical actuator for aircraft flaps and slats", in Proc. IEEE Electrical Machines and Drives Conference, pp.41-47, May 2005.
32. M.E. Roth, L.M. Taylor, I.G. Hansen, "Status of electrical actuator applications", in Proc. Energy Conversion Engineering Conference, pp.191-196, August 1996.
33. A.M. Cross, A.J. Forsyth, D.R. Trainer and N. Baydar, "Simulation of power quality issues in more electric aircraft actuator supplies", in Proc. European Power Electronic Conference 2003, pp.1-11.
34. G.M. Raimondi, T. Sawata, P. Green, "Fan Shaft Driven Generator", in Proc. Society of Aerospace Engineers Conference, pp.9.1-9.7, April 2004.
35. "More Electric Aircraft", Conference reports From: Aircraft Engineering and Aerospace Technology, Volume 77, Issue 1, 2005.
36. Raimondi, G.M; Sawata, T; Holme, M; Barton, A; White, G; Coles, J; Mellor, P.H; Sidell, N; "Aircraft embedded generation systems", in Proc. of International Conference on Power Electronics Machines and Drives, pp. 217-222, 2002.
37. M. David Kankam and Malik E. Elbuluk, "A Survey of Power Electronics Applications in Aerospace Technologies", NASA Technical Memorandum, NASA TM-2001-211298, pp. 1-14, November 2001.
38. M.H. Taha, "Power electronics for aircraft application", in Proc. IEE colloquium on Power Electronics for Demanding Applications, pp.7/1-7/4, 1999.
39. D.R. Newcombe, L. Coulbeck, S. Dessiatoun, I. Ivakhnenko, T. Sawata, M.G. Holme, "Reliability and thermal performance of IGBT Plastic modules for the more electric aircraft", in Proc. IEEE Symposium on Power Semiconductor Devices and ICs, pp.118-121, April 2003.
40. Homeyer, W.G., Bowles, E.E., Lupan, S.P., Rodriguez, C, Walia, P.S., Shah, N.M., Maldonado, M.A., "Advanced power converters for More Electric Aircraft applications", in Proc. Energy Conversion Engineering Conference, pp.137-141, August 1996.
41. K. Furmanczyk, M. Stefanich, "Power Conversion Technologies for reducing harmonics on the More Electric Aircraft", in Proc. Society of Aerospace Engineers Conference, pp.1-11, November 2006.
42. B. Sarlioglu, C. Huggett, "Advances in active power converter topologies for power quality solutions for more electric aircraft", in Proc. Society of Aerospace Engineers Conference, pp. 1-7, November 2006.
43. K.C. Reinhardt, M.A. Marciniak, "Wide band gap power electronics for the more electric aircraft", in Proc. Energy Conversion Engineering Conference, pp.127-132, August 1996.
44. A.J. Lockyer, C.A. Martin, D.K. Linder, P.S. Walia and B.F. Carpenter, "Power systems and requirements for integration of smart structures into aircraft"', Journal of Intelligent Material Systems and Structures, Vol.15, pp.305-315, April 2004.
45. th IET Power Electronics, Machines and Drives Conference, pp. 1-6, 2010.
46. R.T. Naayagi, A.J. Forsyth, and R. Shuttleworth, "High-power bidirectional DC-DC converter for aerospace applications", IEEE Transactions on Power Electronics, vol. 27, no. 11, pp. 4366-4379, Nov 2012.
47. Steven Musil, "Boeing: Here's our plan to nix 787 battery fire risk", Available: http://news.cnet.com/8301-11386-3-57574484-76/boeing- heres-our-plan-to-nix-787-battery-fire-risk/, Last accessed: March 2013.
48. Boeing's Battery Blues, IEEE Spectrum, vol.50, no.3 (Int), p.9-10, March 2013.