Aircraft heated floor panel

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/18 (2006.01) B32B 15/04 (2006.01) B64C 1/40 (2006.01) B64D 13/08 (2006.01) F24D 13/02 (2006.01) H05B 3/10 (2006.01) H05B 3/22 (2006.01)

Patent

CA 2381592

An aircraft heated floor panel (10/110/210) including a support level (40/140/142), a heater level (42/142/242) and a protective cover layer (16/116/216). The support level and the heater level are formed as a composite structure (18/118/218), such as by curing a series of layers together to form the structure. A thermal conductor (62) may be provided to more evenly distribute a generated heat pattern. Alternatively, a metal sheet (116/216) may be used for the cover layer which performs a heat distributing function. If a metal sheet (216) is used, an elastic-after-bonding adhesive (266) may be used to secure the metal sheet (216) to the heater level (242) to accommodate different rates of thermal expansion.

L'invention porte sur un panneau de sol chauffant pour avion (10/110/210) comportant un niveau porteur (40/140/142), un niveau chauffant (42/142/242) et une couche protectrice de couverture (16/11/216). Les niveaux porteur et chauffant ont une structure composite (18/118/218), obtenue par exemple en faisant durcir ensemble une série de couches. On peut utiliser un conducteur thermique (62) pour repartir plus régulièrement les flux thermique produits. En variante, on peut utiliser comme couche protectrice une feuille métallique (116/216) assurant la fonction de répartition de chaleur. Dans ce dernier cas, on peut utiliser un adhésif restant élastique après la prise (266) pour lier la feuille métallique (216) au niveau chauffant (242), ce qui permet d'accepter différents coefficients de dilatation.

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