AIRCRAFT STRUCTURE WITH SOLAR ENERGY CAPTURE CAPACITY
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United States of America Patent
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Issued Date -
Dec 22, 2016
app pub date -
Jun 27, 2014
filing date -
Jun 28, 2013
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Abstract
An aircraft structure (10), in particular the fuselage, nacelles or wings, includes, over all or part of an outer surface (21) that may undergo lightning impacts, a layer of flexible polymer (30), a photovoltaic film (40) and a protective layer (50) protecting the photovoltaic film. This aircraft structure primarily has a solar energy capture capacity making it possible to meet the needs of an aircraft as well as an ability to protect against the effects of lightning.
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