Process and system for controlling the pressure in an...

B - Operations – Transporting – 64 – D

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B64D 13/06 (2006.01) B64C 1/14 (2006.01)

Patent

CA 2629858

In a process and a system (10) for controlling the pressure in an aircraft cabin the status of at least one aircraft door is detected by at least one detection device (12a-c, 14a-c, 16a-c, 18a-c). A signal indicative of the status of the aircraft door is transmitted to a unit (36) for controlling an avionics ventilation system. The avionics ventilation system is controlled in dependence upon the signal indicative of the status of the aircraft door in such a way that a build-up of pressure in the aircraft cabin is prevented when the signal indicative of the status of the aircraft door indicates that the aircraft door is not fully closed and secured.

Dans un procédé et système (10) de régulation de la pression dans une cabine d~aéronef, l~état d~au moins une porte d~aéronef est détecté par au moins un dispositif de détection (12a-c, 14a-c, 16a-c, 18a-c). Un signal indiquant l~état de la porte d~aéronef est transmis à un module (36) de commande d~un système de ventilation avionique. Le système de ventilation avionique est commandé en fonction du signal indiquant l~état de la porte d~aéronef de manière à empêcher la pressurisation de la cabine d~aéronef si le signal indiquant l~état de la porte d~aéronef indique que la porte d~aéronef n~est pas complètement fermée et verrouillée.

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