System and method for pumping recirculation air from an...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 13/06 (2006.01)

Patent

CA 2732154

System and method for pumping recirculation air from an aircraft cabin A system (10) for conveying recirculation air from an aircraft cabin comprises a plurality of conveying devices (12a-12j) which are arranged in a manner distributed along an aircraft cabin region (14). A control device (16) is configured to control the conveying devices (12a-12j) in the normal operation of the system (10) in such a manner that each conveying device (12a-12j) removes a predetermined air volume flow from the aircraft cabin region (14). The control device (16) is furthermore configured to control, in the event of a failure of a conveying device (12c), at least some of the remaining still functional conveying devices (12a, 12b, 12d-12j) in such a manner that the entire air volume flow removed from the aircraft cabin region (14) by the remaining still functional conveying devices (12a, 12b, 12d-12j) is increased by an amount corresponding to an air volume flow amount removed from the aircraft cabin region (14) by the failed conveying device (12c) in the normal operation of the system (10).

La présente invention concerne un système (10) pour acheminer de l'air de recirculation issu d'une cabine d'aéronef, comprenant une pluralité de dispositifs d'acheminement (12a-12j) qui sont répartis le long d'une zone de cabine d'aéronef (14). Un dispositif de commande (16) est agencé pour commander les dispositifs d'acheminement (12a-12j) lorsque le système (10) se trouve dans un mode de fonctionnement normal, de sorte que chaque dispositif d'acheminement (12a-12j) évacue un débit volumique d'air prédéterminé hors de la zone de cabine d'aéronef (14). Le dispositif de commande (16) est également agencé pour, en cas de panne affectant un dispositif d'acheminement (12c), commander au moins une partie des dispositifs d'acheminement (12a, 12b et 12d bis 12j) encore fonctionnels restants de sorte que le débit volumique d'air global évacué de la zone de cabine d'aéronef (14) par les dispositifs d'acheminement (12a, 12b, 12d-12j) encore fonctionnels restants, est augmenté d'une valeur qui correspond à une valeur de débit volumique d'air évacué de la zone de cabine d'aéronef (14) par le dispositif d'acheminement (12c) en panne lorsque le système (10) se trouve dans un mode de fonctionnement normal.

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