AILE D'AVION COMPORTANT UN DISPOSITIF DE DEGIVRAGE ET/OU ANTIGIVRE ELECTROTHERMIQUE ET PROCEDE DE DEGIVRAGE ASSOCIE

AILE D'AVION COMPORTANT UN DISPOSITIF DE DEGIVRAGE ET/OU ANTIGIVRE ELECTROTHERMIQUE ET PROCEDE DE DEGIVRAGE ASSOCIE

The process involves heating an anti-hoar frost zone (50e) adjacent to a rear curved part (30) of a structural unit (20) by utilizing an electro-thermal device to partially melt the hoar frost accumulated on the rear curved part. De-icing zones (50c-50d) at the rear curved part are heated by utilizi...

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Bibliographische Detailangaben
1. Verfasser: GIAMATI MICHAEL J
Format: Patent
Sprache:fre
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The process involves heating an anti-hoar frost zone (50e) adjacent to a rear curved part (30) of a structural unit (20) by utilizing an electro-thermal device to partially melt the hoar frost accumulated on the rear curved part. De-icing zones (50c-50d) at the rear curved part are heated by utilizing the electro-thermal device to provide hot surface water to the partially accumulated molten hoar frost. An independent claim is also included for an airplane wing including an electro-thermal device.