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.
AIRCRAFT STRUCTURE WITH SOLAR ENERGY CAPTURE CAPACITY
2016-12-22
Patent
Electronic Resource
English
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