• DocumentCode
    1855306
  • Title

    Advanced-aircraft integrated-diagnostics system-concept evaluation

  • Author

    Gaffney, Kevin S. ; Morones, Paul

  • Author_Institution
    Lockheed Fort Worth Co., Fort Worth, TX, USA
  • fYear
    1994
  • fDate
    24-27Jan 1994
  • Firstpage
    20
  • Lastpage
    25
  • Abstract
    An integrated diagnostics system engineering process was utilized to develop an effective diagnostic/health monitoring system which meets user´s needs. Weighing results from reliability, maintainability, and system safety trade studies, a comprehensive aircraft diagnostic/health monitoring system was defined which decreases aircraft turnaround time and increases safety while minimally impacting system reliability. The approach of considering reliability, maintainability, and system safety requirements as the customer´s requirements in a quality function deployment (QFD) analysis can be employed in the design and development of other products which require the amalgamation of complicated and conflicting design requirements
  • Keywords
    aerospace computing; aircraft; maintenance engineering; reliability; safety systems; advanced-aircraft integrated-diagnostics system-concept evaluation; aircraft diagnostic/health monitoring system; maintainability; quality function deployment analysis; reliability; system safety requirements; Aerospace engineering; Air safety; Aircraft propulsion; Health and safety; Maintenance engineering; Monitoring; Product safety; Quality function deployment; Reliability engineering; Systems engineering and theory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 1994. Proceedings., Annual
  • Conference_Location
    Anaheim, CA
  • Print_ISBN
    0-7803-1786-6
  • Type

    conf

  • DOI
    10.1109/RAMS.1994.291073
  • Filename
    291073