arrangement for preventing the automatic opening a locked door or not properly closed and shut up in the aircraft fuselage

摘要

The arrangement can be used to avoid self-opening of a door or cover which is not correctly closed and locked, in an aircraft fuselage. It makes an efficient contribution to improving flight safety in aircraft. The arrangement consists of a door monitoring system (1) which is connected to a cabin pressure regulating device (4) and/or to a cabin temperature regulating device (5) and/or to an air tapping device (36), the regulating devices (4; 5; 36) providing suitable physical additional information from the interior of the fuselage of the aircraft (1). The latter have at least one connection which provides information to determine the aircraft operating mode. IMAGE