Literature DB >> 30464270

Flight of an aeroplane with solid-state propulsion.

Haofeng Xu1, Yiou He2, Kieran L Strobel1, Christopher K Gilmore1, Sean P Kelley1, Cooper C Hennick1, Thomas Sebastian3, Mark R Woolston3, David J Perreault2, Steven R H Barrett4.   

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.

Entities:  

Year:  2018        PMID: 30464270     DOI: 10.1038/s41586-018-0707-9

Source DB:  PubMed          Journal:  Nature        ISSN: 0028-0836            Impact factor:   49.962


  2 in total

1.  Successively accelerated ionic wind with integrated dielectric-barrier-discharge plasma actuator for low-voltage operation.

Authors:  Shintaro Sato; Haruki Furukawa; Atsushi Komuro; Masayuki Takahashi; Naofumi Ohnishi
Journal:  Sci Rep       Date:  2019-04-09       Impact factor: 4.379

2.  A laser-microfabricated electrohydrodynamic thruster for centimeter-scale aerial robots.

Authors:  Hari Krishna Hari Prasad; Ravi Sankar Vaddi; Yogesh M Chukewad; Elma Dedic; Igor Novosselov; Sawyer B Fuller
Journal:  PLoS One       Date:  2020-04-29       Impact factor: 3.240

  2 in total

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