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Flight of an aeroplane with solid-state propulsion

Author

Listed:
  • Haofeng Xu

    (Massachusetts Institute of Technology)

  • Yiou He

    (Massachusetts Institute of Technology)

  • Kieran L. Strobel

    (Massachusetts Institute of Technology)

  • Christopher K. Gilmore

    (Massachusetts Institute of Technology)

  • Sean P. Kelley

    (Massachusetts Institute of Technology)

  • Cooper C. Hennick

    (Massachusetts Institute of Technology)

  • Thomas Sebastian

    (Massachusetts Institute of Technology Lincoln Laboratory)

  • Mark R. Woolston

    (Massachusetts Institute of Technology Lincoln Laboratory)

  • David J. Perreault

    (Massachusetts Institute of Technology)

  • Steven R. H. Barrett

    (Massachusetts Institute of Technology)

Abstract

Since the first aeroplane flight more than 100 years ago, aeroplanes have been propelled using moving surfaces such as propellers and turbines. Most have been powered by fossil-fuel combustion. Electroaerodynamics, in which electrical forces accelerate ions in a fluid1,2, has been proposed as an alternative method of propelling aeroplanes—without moving parts, nearly silently and without combustion emissions3–6. However, no aeroplane with such a solid-state propulsion system has yet flown. Here we demonstrate that a solid-state propulsion system can sustain powered flight, by designing and flying an electroaerodynamically propelled heavier-than-air aeroplane. We flew a fixed-wing aeroplane with a five-metre wingspan ten times and showed that it achieved steady-level flight. All batteries and power systems, including a specifically developed ultralight high-voltage (40-kilovolt) power converter, were carried on-board. We show that conventionally accepted limitations in thrust-to-power ratio and thrust density4,6,7, which were previously thought to make electroaerodynamics unfeasible as a method of aeroplane propulsion, are surmountable. We provide a proof of concept for electroaerodynamic aeroplane propulsion, opening up possibilities for aircraft and aerodynamic devices that are quieter, mechanically simpler and do not emit combustion emissions.

Suggested Citation

  • Haofeng Xu & Yiou He & Kieran L. Strobel & Christopher K. Gilmore & Sean P. Kelley & Cooper C. Hennick & Thomas Sebastian & Mark R. Woolston & David J. Perreault & Steven R. H. Barrett, 2018. "Flight of an aeroplane with solid-state propulsion," Nature, Nature, vol. 563(7732), pages 532-535, November.
  • Handle: RePEc:nat:nature:v:563:y:2018:i:7732:d:10.1038_s41586-018-0707-9
    DOI: 10.1038/s41586-018-0707-9
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    Cited by:

    1. Burston, Martin & Ranasinghe, Kavindu & Gardi, Alessandro & Parezanović, Vladimir & Ajaj, Rafic & Sabatini, Roberto, 2022. "Design principles and digital control of advanced distributed propulsion systems," Energy, Elsevier, vol. 241(C).

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