Experimental testing of a 250 kW fault-tolerant permanent magnet power generation system for large civil aero-engines

Collection of Technical Papers - 5th International Energy Conversion Engineering Conference

Volumn 2, Issue , 2007, Pages 1076-1083

  Sun, Z ^a,c   Ede, J D ^a,c   Wang, J ^a,c   Jewell, G W ^a,c   Cullen, J J A ^b,d   Mitcham, A J ^b,d  

^a UNIVERSITY OF SHEFFIELD   (United Kingdom)

^b ROLLS ROYCE PLC   (United Kingdom)

^c Department of Electrical and Electronic Engineering ^*  (United Kingdom)

^d Strategic Research Centre   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

CIVIL AVIATION; ELECTRIC POWER GENERATION; ENGINES; FAULT TOLERANCE; PERMANENT MAGNETS; POWER CONTROL;

AERO-ENGINES; CIVIL ENGINES; DESTABILIZING OUTPUT POWER; LOW-PRESSURE SHAFTS;

ELECTRIC MACHINERY TESTING;

EID: 35648998968     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-4829     Document Type: Conference Paper

References (9)

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7. J. D. Ede, G. W. Jewell, K. Atallah, and D. J. Powell, "Design of a 250 kW, fault-tolerant PM generator for the more-electric aircraft", 3rd International Energy Conversion Engineering Conference 15-18 August 2005, San Francisco, California, AIAA 2005-5644.
8. K. Atallah, J. Wang, and D. Howe, "Torque ripple minimisation in modular permanent magnet brushless machines", IEEE Trans on Industry Applications, Vol. 39, No. 6, 2003, pp. 1689-1695.
9. J. Wang, K. Atallah, and D. Howe, "Optimal torque control of fault-tolerant permanent magnet brushless machines" IEEE Transactions on Magnetics. Vol. 39, 2003, pp. 2962-2964.