• DocumentCode
    2064834
  • Title

    Applying the quality function deployment on the V-22 Osprey

  • Author

    Westervelt, Kerry

  • Author_Institution
    Naval Air Syst. Command, Patuxent River, MD, USA
  • fYear
    2010
  • fDate
    6-13 March 2010
  • Firstpage
    1
  • Lastpage
    12
  • Abstract
    Developing requirements for correction of deficiencies requires detailed analyses of top-level system requirements and subsystem specifications. Application of the quality function deployment provides a rigorous systems engineering process to define the correct requirements accurately. In addition, performing a gap analysis is another important task in order to compare the requirements at the interfaces between systems especially with respect to external environmental factors. On the V-22 Osprey, these tools and processes were applied to optimize cost-wise readiness of the lower nacelle system through a holistic review of inter-related systems in the propulsion function. A dedicated team of systems engineers and subject matter experts from Bell-Boeing, Rolls-Royce, and Naval Air Systems Command (NAVAIR) performed a thorough requirements analysis of the lower nacelle system. This review traced the requirements flow from external environmental factors into the engine inlet, through the engine air particle separator, to the engine, and exhausting through the infrared suppressor.
  • Keywords
    aerospace engines; aerospace propulsion; military aircraft; quality function deployment; V-22 Osprey; cost-wise readiness; engine air particle separator; engine inlet; environmental factor; gap analysis; infrared suppressor; lower nacelle system; propulsion function; quality function deployment; Costs; Humans; Manufacturing; NASA; Quality function deployment; Space missions; Space technology; Supply chain management; Supply chains; Technological innovation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2010 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-3887-7
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2010.5446889
  • Filename
    5446889