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Pilot Controls for a Hybrid Turbine-Electric 17-Engine AircraftNASA 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 presentation 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.
Document ID
20230013526
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Tim Etherington
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Trey Arthur
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
September 18, 2023
Subject Category
Aircraft Stability and Control
Aircraft Propulsion and Power
Meeting Information
Meeting: 42nd Digital Aviation System Conference (DASC)
Location: Barcelona
Country: ES
Start Date: October 1, 2023
End Date: October 5, 2023
Sponsors: American Institute of Aeronautics and Astronautics, Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: 533127.02.22.07.05
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
autothrottle
single throttle
automation trends
flight controls
electric-hybrid aircraft
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