NASA is exploring the development of a 180-passenger subsonic single engine aft turbine aircraft where the aft turbine provides electric power in a hybrid design to wing mounted electric engines. A pilot-in-the-loop study was conducted at Langley Research Center in Hampton, Virginia to explore the design of a flight deck for the hybrid electric aircraft with 16 wing fans and an aft mounted turbine engine. Current flight deck designs provide control inceptors for each propulsion engine and display of all engine parameters for all primary aircraft engines. Automation trends and increasing automation in flight controls and throttle controls indicate less controls instead of more. The design team researched state-of-the-art and recommended study of three, two, and one throttle levers. Engine displays were researched and two were recommended for initial evaluation. 16 airline pilots evaluated the three throttle configurations and two engine display options. Engine failures for known probable indications were evaluated against all throttle and display configurations. This included one, four symmetric, eight non-symmetric, and sixteen momentary electric engine failures with the loss of the aft turbine. The turbine engine was evaluated for complete and partial failure during critical phases of takeoff as well as enroute. This paper details the pilot study including pilot comments supporting the potential for increased automation and a single throttle control. Detailed recommendations are provided for a novel single throttle control and additional pilot controls to support selection of engines during start, shutdown, and engine troubleshooting procedures. This design deviates significantly from current practice of providing throttles for each propulsion engine. Engine display recommendations are provided based on pilot feedback during a guided post-evaluation interview. Recommendations for future study are documented with supporting research and current observations about upcoming flight deck certifications.


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    Title :

    Pilot Controls for a Hybrid Turbine-Electric 17 Engine Aircraft


    Contributors:

    Conference:

    42nd Digital Aviation System Conference (DASC) ; 2023 ; Barcelona, ES


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





    Pilot Controls for a Hybrid Turbine-Electric 17 Engine Aircraft

    Etherington, Timothy / Arthur, Trey | IEEE | 2023




    HYBRID ELECTRIC AIRCRAFT ENGINE

    ZATORSKI DAREK TOMASZ / HIGGINS CRAIG WILLIAM | European Patent Office | 2022

    Free access