• DocumentCode
    3175959
  • Title

    The HALO system-applying the “safe wing” concept to airline operations in ground icing conditions

  • Author

    Peterson, Michael T. ; Nguyen, Lauren ; Edleman, Duane V. ; Coffel, Jerome F.

  • Author_Institution
    Rosemount Aerosp. Inc., Bunsville, MN, USA
  • fYear
    1995
  • fDate
    5-9 Nov 1995
  • Firstpage
    152
  • Lastpage
    157
  • Abstract
    A process has been developed to improve upon the existing “Clean Aircraft” concept as currently defined by FAA guidelines for airline operations. The new “Safe Wing” concept works with existing airline programs for operations in icing conditions. It adds a contamination detection and classification system to the current procedural system. This addition improves overall system safety while eliminating burdensome checks, reducing delays and saving deicing/anti-icing fluid costs. By eliminating unnecessary deicings, if also reduces the environmental impact of using excessive deicing fluid. The HALO contamination detection system is comprised of ultrasonic sensors, processing electronics and a cockpit display. This multisensor system automatically and continuously monitors critical wing areas. The ultrasonic sensors provide area coverage and sensitivity to a variety of contaminants. These sensors are integrated into a HALO system design based on correlating contamination roughness, location and extent with aerodynamic performance. The HALO system development passed a major milestone with an in-service evaluation on a Northwest MD-80 during the 1994-95 winter season. This evaluation was designed to show technology viability in the demanding environment of airline winter operations. The single-sensor evaluation system showed a correct classification rate of greater than 95 percent and sensitivity to a variety of contaminants. A multi-sensor, broad coverage prototype system will be tested in the 1995-96 winter season
  • Keywords
    aircraft computers; aircraft control; aircraft displays; human factors; ice; sensor fusion; snow; surface contamination; ultrasonic transducer arrays; HALO system; airline operations; area coverage; broad coverage prototype system; clean aircraft; cockpit display; commercial airline winter operations; contaminants sensitivity; contamination detection and classification system; contamination roughness; critical wing areas; ground icing conditions; in-service evaluation; multisensor system; procedural system; processing electronics; safe wing concept; simulation; single-sensor evaluation system; surface contaminants; technology viability; ultrasonic sensors; Aerodynamics; Computer displays; Contamination; Costs; Delay; FAA; Guidelines; Multisensor systems; Safety; Sensor systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1995., 14th DASC
  • Conference_Location
    Cambridge, MA
  • Print_ISBN
    0-7803-3050-1
  • Type

    conf

  • DOI
    10.1109/DASC.1995.482822
  • Filename
    482822