An energy harvester for an aircraft comprises a first portion, a second portion and an energy storing unit. The first portion includes a charge collecting device having an electrical permittivity different to the one of air. The charge collecting device is configured to be exposed to an air flow. The second portion is configured to be exposed to air and includes a conductive material. The energy storing unit is electrically connected between the first portion and the second portion.
ENERGY HARVESTER, AIRCRAFT COMPONENT COMPRISING THE ENERGY HARVESTER AND AN AIRCRAFT COMPRISING THE ENERGY HARVESTER OR THE AIRCRAFT COMPONENT
2015-06-25
Patent
Electronic Resource
English
European Patent Office | 2015
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