Fault tolerant, variable frequency, unity power factor converters for safety critical PM drives

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Fault tolerant, variable frequency, unity power factor converters for safety critical PM drives

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The aerospace industry is currently considering a constant voltage, variable frequency supply for aircraft power systems. This variable frequency system is based on a generator directly driven from the aero-engine, in which the frequency is dependent on engine speed. A number of safety critical loads are placed on this system, and it is essential that failure of any one load does not affect the operation of another. The paper develops the concept of fault tolerant input converters for an electric fuel pump. The converters always act as a unity power-factor load, and can tolerate a range of failures, whilst maintaining both the operation of the pump and minimal impact on the electrical supply. Two converter types are proposed and compared for this application. The operation of these two unity power factor converters from a variable frequency supply is demonstrated. The effect of faults in the selected converters on converter operation and the supply itself is then discussed.

Inspec keywords: motor drives; safety; frequency convertors; pumps; permanent magnet motors; electric current control; voltage control; power factor correction; bridge circuits; two-term control; fault tolerance; avionics

Other keywords: H-bridge; PI controller; electric fuel pump; inner inductor current loop; safety critical loads; aero-engine; generator; fault tolerant converters; aerospace industry; aircraft power systems; outer output voltage loop; engine speed; variable frequency converters; unity power factor converters; unity power-factor load; fault tolerant input converters; safety critical PM drives

Subjects: Aerospace industry; Drives; Plant engineering, maintenance and safety; Current control; d.c. machines; a.c. machines; Aircraft electronics; Control of electric power systems; Power convertors and power supplies to apparatus; Health and safety aspects; Voltage control

References

    1. 1)
      • CT-Concept Technology Ltd.: “Concept IHD 215/280/680 Data Sheet & Application Manual – Intelligent Half-Bridge Drivers for IGBTs and Power MOSFETSs”. © 1992…1999 CT-Cocept Techology Ltd., Switzerland.
    2. 2)
      • M.J. Kocher , R.L. Steigerwald . An AC-to-DC converter with high quality input waveforms. IEEE Trans. Ind. Appl. , 4 , 586 - 599
    3. 3)
      • Watson, R.W., Lee, F.C.: `A soft-switched, full-bridge boost converter employing an active-clamp circuit', PESC’96: Proc. IEEE Power Electronics Specialists Conference, 1996, 2, p. 1948–1954.
    4. 4)
    5. 5)
    6. 6)
    7. 7)
      • H. Oishi , H. Okada , K. Ishizaka , R. Itoh . Single-phase step up/down rectifier with improved supply current waveform. IEE Proc. – Electr. Power Appl. , 1 , 6 - 11
    8. 8)
      • Cronin, M.J.: `The all electric aircraft as an energy efficient transport', 801113, SAE Aerospace Congress & Exposition, 13–16 October 1980, Los Angeles, Society of Automotive Engineers.
    9. 9)
      • Nonaka, S., Neba, Y.: `Single-phase PWM current source converter with double-frequency parallel resonance circuit for DC smoothing', IAS’93: Proc. IEEE Industry Applications Society Annual Meeting, 1993, 2, p. 1144–1151.
    10. 10)
    11. 11)
    12. 12)
      • de Souza, A.F., Barbi, I.: `A new ZVS semi-resonant high power factor rectifier with reduced conduction losses', PESC’96: Proc. IEEE Power Electron. Specialists Conference, 1996, 1, p. 203–209.
    13. 13)
      • Berendsen, C.S., Rostaing, G., Champenois, G., Obrecht, G., Saadi, J.: `Detection of sensor faults with observer structures in control loops', Proc. 19th Int. Conf. on Industrial electronics, control and instrumentation (IECON), 1993, 1, p. 344–348.
    14. 14)
    15. 15)
      • S. Manias , P.D. Ziogas , G. Olivier . An AC-to-DC converter with improved input power factor and high power density. IEEE Trans. Ind. Appl. , 6 , 1073 - 1081
    16. 16)
      • Hong, J., Ismail, E., Erickson, R., Khan, I.: `Design of the parallel resonant converter as a low harmonic rectifier', APEC’93: Proc. 8th Annual Conf. on Applied power electronics, 1993, 1, p. 833–840.
    17. 17)
    18. 18)
      • Mehdi, I.S., Leong, P.J.: `Efficiently meeting electric power needs for future aircraft', 859356, Proc. of the Intersociety Energy Conversion Conference 1985 (IECEC ’85), p. 1.382–1.387, Society of Automotive Engineers.
    19. 19)
      • Balocco, D., Derony, E., Ploquin, D., Zardini, C.: `A new single-stage isolated power factor preregulator for avionics distributed power supply systems', PESC’96: Proc. IEEE Power Electronics Specialists Conference, 1996, 2, p. 1717–1723.
    20. 20)
      • B.C. Kuo . (1980) Digital control systems.
    21. 21)
      • R. Matson . (1943) Aircraft electrical engineering.
    22. 22)
      • B.C. Mecrow , A.G. Jack , J.A. Haylock , J. Coles . Fault tolerant permanent magnet machine drives. IEE Proc. B, Electr. Power Appl. , 6 , 437 - 442
    23. 23)
      • K. Astrom , B. Wittenmark . (1996) Computer controlled systems: theory and design.
    24. 24)
      • Lin, R.L., Lee, F.C.: `Novel zero-current-switching-zero-voltage-switching converters', PESC’96: Proc. IEEE Power Electronics Specialists Conference, 1996, 1, p. 438–442.
    25. 25)
      • J.A. Haylock , B.C. Mecrow , A.G. Jack , D.J. Atkinson . Operation of a fault tolerant PM drive for an aerospace fuel pump application. IEE Proc. B, Electr. Power Appl. , 5 , 441 - 448
    26. 26)
      • Motorola Inc., “MC33153 Single IGBT Gate Driver”. Rev. 2, © Motorola Inc, 1998.
    27. 27)
      • Haylock, J.A.: `Fault tolerant drives for safety critical applications', 1998, PhD, University of Newcastle upon Tyne.
    28. 28)
      • Semikron: “Semidriver® High Power IGBT Driver SKHI10, SKHI10/17”. © Semikron, pp. B14-3–B14-10, 1999.
    29. 29)
      • Berendsen, C.S., Champenois, G., Davoine, J., Rostaing, G.: `How to detect and to localise a fault in a DC/DC converter?', Proc. 18th Int. Conference on Industrial electronics, control and instrumentation (IECON), 1992, 1, p. 536–541.
    30. 30)
      • Green, S.R.: `Permanent magnet drives in the more-electric aircraft', 2000, PhD, University of Newcastle upon Tyne.
    31. 31)
      • Mecrow, B.C., Jack, A.G., Haylock, J.A., Coles, J.: `Fault tolerant permanent magnet machine drives', Proc. 7th IEE Int. Conf. on Electric machines and drives, EMD’95, 11–13 September 1995, Durham, UK, p. 433–437.
    32. 32)
    33. 33)
    34. 34)
      • Belaguli, V., Bhat, A.K.S.: `A hybrid resonant converter operated as a low harmonic rectifier with and without active control', PESC’96: Proc. IEEE power electronics specialists Conf., 1996, 1, p. 720–726.
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