The invention is relative to a de-icing system (10) for critical surfaces (21, 22, 23, 24, 25, 26) of aircraft (20), comprising:- at least one infrared laser generator (30), able to emit a laser beam (40) having a predetermined wavelengthλ,- a set of embedded networks (50) of optical fiber wires (60), each optical fiber wire (60) comprising an input (61) connected to the laser generator (30) and, at least, an output (62) configured to be able to spread the laser beam (40) from the laser generator (30),- wherein each output (62) of the optical fiber wire (60) is able to spread the laser beam (40) through one of a set of orifices (70) previously drilled onto a leading edge (21) of wings (22), and/or onto the leading edge (21) of horizontal tail plane (23), and/or onto the leading edge of the vertical tail plane (24) configured to be able to melt and remove ice or snow accretion(80)on critical surfaces (21, 22, 23, 24, 25, 26) of the aircraft (20) during the flight.
DE-ICING SYSTEM FOR CRITICAL SURFACES OF AIRCRAFT
ENTEISUNGSSYSTEM FÜR KRITISCHE FLUGZEUGOBERFLÄCHEN
SYSTÈME DE DÉGIVRAGE POUR DES SURFACES CRITIQUES D'AÉRONEF
2020-01-08
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
NTIS | 1971
British Library Conference Proceedings | 1994
|NTIS | 1978
NTRS | 1978
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