Global Patent Index - EP 3013690 A1

EP 3013690 A1 20160504 - AIRCRAFT STRUCTURE WITH SOLAR ENERGY CAPTURE CAPACITY

Title (en)

AIRCRAFT STRUCTURE WITH SOLAR ENERGY CAPTURE CAPACITY

Title (de)

FLUGZEUGSTRUKTUR MIT SONNENENERGIEKAPAZITÄTSERFASSUNG

Title (fr)

STRUCTURE D'AÉRONEF À CAPACITÉ DE CAPTURE D'ÉNERGIE SOLAIRE

Publication

EP 3013690 A1 (FR)

Application

EP 14735539 A

Priority

  • FR 1356246 A
  • EP 2014063761 W

Abstract (en)

[origin: WO2014207236A1] The invention relates to an aircraft structure (10), in particular the fuselage, nacelles or wings, comprising, 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 said 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.

IPC 8 full level

B64D 33/00 (2006.01); B64D 41/00 (2006.01); H01L 31/048 (2006.01)

CPC (source: EP US)

B64D 33/00 (2013.01 - EP US); H01L 31/03926 (2013.01 - US); H01L 31/0445 (2014.12 - EP US); H01L 31/048 (2013.01 - EP US); H01L 31/049 (2014.12 - US); H01L 31/1876 (2013.01 - US); B64D 2211/00 (2013.01 - EP US); Y02E 10/50 (2013.01 - EP US); Y02T 50/50 (2013.01 - EP US)

Designated contracting state (EPC)

AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

Designated extension state (EPC)

BA ME

DOCDB simple family (publication)

FR 3007734 A1 20150102; FR 3007734 B1 20170811; CN 105392701 A 20160309; EP 3013690 A1 20160504; US 2016368613 A1 20161222; WO 2014207236 A1 20141231

DOCDB simple family (application)

FR 1356246 A 20130628; CN 201480036161 A 20140627; EP 14735539 A 20140627; EP 2014063761 W 20140627; US 201414900282 A 20140627