An aircraft propulsion system for Mach .6 flight is being developed which utilizes two turboshaft engines driving a pusher propeller through driveshafts and a combining gearbox. This system will provide greater operational safety as well as improved aircraft efficiency. This report describes design features, installation considerations, and operational characteristics of the system, and reviews methods of system analysis.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Lear Fan Propulsion System


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Turbine Powered Executive Aircraft Meeting ; 1980



    Publication date :

    1980-04-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Lear - system integration

    British Library Online Contents | 1996


    Qualitaetssicherungsinstrumente bei Lear

    Laepple,R. / Lear,Bremen,DE | Automotive engineering | 2003


    Lear introduces "omnimatic."

    Engineering Index Backfile | 1949


    Lear the Legend

    Lewis, T. | British Library Online Contents | 2001


    Lear gyromatic navigator

    Engineering Index Backfile | 1941