PROPULSION SYSTEM FOR AIRCRAFT
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United States of America Patent
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Issued Date -
Dec 28, 2017
app pub date -
Jun 27, 2017
filing date -
Jun 28, 2016
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Abstract
An aircraft comprising a turbine engine, an atomizer, a reservoir, a conduit connecting the reservoir to the atomizer, and a unit for controlling the flow of liquid in the atomizer. The turbine engine, the atomizer, the reservoir, the conduit and the control unit are fixed to the aircraft. This allows cleaning in flight of at least some parts of the turbine engine.
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