Device and method for temperature control in an aircraft cabin

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 13/08 (2006.01)

Patent

CA 2551918

Device and method for temperature control in an aircraft cabin (104) wherein is controlled with a first supply control arrangement the supply of heated air from a first source into a first temperature area (106) of the aircraft cabin (104) depending upon a specified first temperature for the first temperature area and with a first pressure control arrangement (176) a current pressure of the heated air supply from the first source in the first supply control arrangement in the event of a malfunction of the first supply control arrangement depending upon the specified first temperature.

L'invention concerne un dispositif et un procédé de régulation de la température dans la cabine (104) d'un aéronef, l'alimentation d'air chauffé, provenant d'une première source, dans une première zone de température (106) de la cabine (104) de l'aéronef étant commandée au moyen d'un premier agencement de commande de l'alimentation, en fonction d'une première température spécifique destinée à la première zone de température et une pression de courant de l'air chauffé alimenté à partir de la première source dans le premier agencement de commande de l'alimentation étant commandée au moyen d'un premier agencement de commande de la pression (176), dans le cas d'un mauvais fonctionnement du premier agencement de commande de l'alimentation, en fonction de la première température spécifiée.

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