BLADE DE-ICING

A blade (2) comprises a blade body (4) and blade de-icer (20) located on the leading edge (10) of the blade body (4). The blade de-icer (20) comprises a first heater part (26) bonded to an external surface of a face side (6) of the blade body (4) and a separate second heater part (28) bonded to an e...

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Bibliographic Details
Main Authors Picard, Pierre-Alex, Moles, Patrick
Format Patent
LanguageEnglish
French
German
Published 16.09.2020
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Summary:A blade (2) comprises a blade body (4) and blade de-icer (20) located on the leading edge (10) of the blade body (4). The blade de-icer (20) comprises a first heater part (26) bonded to an external surface of a face side (6) of the blade body (4) and a separate second heater part (28) bonded to an external surface of a camber side (8) of the blade body (4). The first and second heater parts (26, 28) each extend to the leading edge (10) of the blade body (4). Each heater part (26, 28) comprises an electrical heating element (34) arranged therein sandwiched between an inner layer (36) and an outer layer (38) of the heater part (26, 28).
Bibliography:Application Number: EP20190290016