Aircraft cabin pressure controller

B - Operations – Transporting – 64 – D

Patent

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Details

340/145, 341/39

B64D 13/04 (2006.01) G05D 16/20 (2006.01)

Patent

CA 1135372

ABSTRACT OF THE DISCLOSURE In a cabin pressure control system having primary and standby controllers, control is switched from the primary to standby upon occurrence of a malfunction which prevents the primary controller from maintaining pressurization properly. If failure is a result of insufficient inflow of pressurized air or of excessive leakage, transfer is prevented and the problem is annunciated to the crew.

303846

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