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Towards Dual and Three-Channel Electrical Architecture Design for More-Electric Engines
Technical Paper
2018-01-1935
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
In recent years, the More-Electric Aircraft (MEA) concept has undergone significant development and refinement, striving towards the attainment of reductions in noise and CO2 emissions, increased power transmission efficiency and improved reliability under a range of flight scenarios. The More-Electric Engine (MEE) is increasingly being seen as a key complementary system to the MEA. With this concept, conventional engine auxiliary systems (i.e. fuel pumps, oil pumps, actuators) will be replaced by electrically-driven equivalents, providing even greater scope for the combined aircraft and engine electrical power system optimisation and management. This concept, coupled with extraction of electrical power from multiple engine spools also has the potential to deliver significant fuel burn savings. To date, single or dual channel electrical power generation and distribution systems have been used in engines and aircrafts. However, with the increasing electrification of flight-critical engine auxiliaries along with the requirement for greater load transfer flexibility, a three-channel architecture should be considered.
This paper investigates potential concepts for a three-channel power system architecture in an MEE system. The paper considers issues such as architecture layout and key technologies that may be considered for MEE architecture. Using an extensive database of public domain MEA/MEE power system component failure rates, a detailed fault tree analysis is then presented. This provides a quantitative comparison of dual channel and three-channel architecture candidates under the pertinent failure modes as well as showing the impact of common architecture features on system reliability and robustness. Finally, the paper concludes with a discussion of the ring busbar topology operation and power electronics technology requirements that could successfully implement a flexible and robust three-channel architecture for MEE systems.
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Authors
Citation
Zhang, Q., Sztykiel, M., Norman, P., and Burt, G., "Towards Dual and Three-Channel Electrical Architecture Design for More-Electric Engines," SAE Technical Paper 2018-01-1935, 2018, https://doi.org/10.4271/2018-01-1935.Data Sets - Support Documents
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References
- Hirst , M. , McLoughlin , A. , Norman , P.J. , and Galloway , S.J. Demonstrating the More Electric Engine: A Step towards the Power Optimised Aircraft IET Electr. Power Appl. 5 1 3 2011
- The Institute of Engineering and Technology IET Essent. Eng. Intell. Transp. 2 2013
- Federal Aviation Authority Aviat. Maint. Tech. Handb. - Airframe 1 106 2014
- Moir , I. and Seabridge , A. Aircraft Systems: Mechanical, Electrical, and Avionic Subsystems Integration 2008
- Sinnett , M. Aero Q. 6 11 2007
- Zhang , Z. , Li , J. , Liu , Y. , Xu , Y. et al. Overview and Development of Variable Frequency AC Generators for more Electric Aircraft Generation System Chinese J. Electr. Eng. 3 2 32 40 2017
- Wheeler , P. The More Electric Aircraft: Why Aerospace Needs Power Electronics? Proceedings of the 13th Conference on Power Electronics 44 0 2009
- Sawata , T. et al. Power 1 8
- Mitcham , A.J. and Grum , N. IEE Coloquium All Electr. Aircr. 8/1 8/9 1998
- Tan , N.M.L. , Abe , T. , and Akagi , H. Design and Performance of a Bidirectional Isolated DC-DC Converter for a Battery Energy Storage System IEEE Trans. Power Electron. 27 3 1237 1248 2012
- 2017 2068 2073
- Telford , R. , Jones , C. , Norman , P. , and Burt , G. 2016 1 10
- Brombach , J. , Schröter , T. , Lücken A. , and Schulz , D. Optimized Cabin Power Supply with A/270 V DC Grid on a Modern Aircraft 2011 7th International Conference on Compatibility and Power Electronics (CPE 2011) 2011 425 428
- Stevens , M.B. and Santoso , S. Improving the Reliability of Breaker-and-a-Half Substations Using Sectionalized Busbars IEEE Power and Energy Society General Meeting 2013
- Roboam , X. , Sareni , B. , and De Andrade , A. More Electricity in the Air Ind. Electron. Mag. IEEE 6 4 6 17 2012
- ESRDC 2013
- Nack , D. 2005 1 19
- 2014
- Johansson , C. 2013
- Department of Defense of the USA Mil. Handb. MIL-HDBK-217F 205 1991
- 2012 1 331
- Bryant et al. Fault Tree Handbook with Aerospace Applications Uma ética para quantos? XXXIII 8 218 2002
- 1 18
- Dhillon , B. 1999 214 219
- EASA 2008 750
- Mitcham , A. and Cullen , J. Permanent Magnet Generator Options for the More Electric Aircraft International Conference on Power Electronics, Machines, and Drives 241 245 2002
- 1958 15