• DocumentCode
    2395735
  • Title

    Active noise control-from research to reality

  • Author

    Aplin, John

  • Author_Institution
    Flight Controls Group, GEC-Marconi Avionics, Rochester, UK
  • fYear
    1994
  • fDate
    30 Oct-3 Nov 1994
  • Firstpage
    444
  • Lastpage
    449
  • Abstract
    This paper traces the development of active noise control (ANC) from its origins in the University Research Laboratories, to its fulfilment in revenue service with airlines. It begins by identifying the need for ANC in terms of quietening the noise from turboprop or turbojet engines, and proceeds to develop the requirements for a viable ANC system. The algorithm used for controlling noise is described, especially its ability to control many independent tones and tones that fluctuate in frequency and amplitude. The system design is described, detailing those features included in the system to make it easy to use, followed by an outline of the hardware used to implement the system. The method of installing, calibrating, and trialling the system is detailed, concluding with the results from a recent set of flight trials
  • Keywords
    active noise control; aerospace engines; aircraft instrumentation; automatic test equipment; calibration; University Research Laboratories; active noise control; airlines; block transforms; calibration; flight trials; frequency domain control; optimisation; turbojet engines; turboprop engines; Acoustic noise; Active noise reduction; Aerospace electronics; Aircraft propulsion; Blades; Frequency; Low-frequency noise; Noise cancellation; Noise generators; Noise level;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1994. 13th DASC., AIAA/IEEE
  • Conference_Location
    Phoenix, AZ
  • Print_ISBN
    0-7803-2425-0
  • Type

    conf

  • DOI
    10.1109/DASC.1994.369443
  • Filename
    369443