Method for monitoring and locking aircraft compartment doors
First Claim
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1. A method of monitoring an aircraft, comprising:
- checking security of a plurality of spaces within the aircraft and closing doors or hatches providing access to the plurality of spaces prior to a period of non-use of the aircraft, the period of non-use being a period when no passengers are on board the aircraft;
locking the doors or the hatches, after checking security prior to the period of non-use of the aircraft, via a monitoring and locking system having a central locking and unlocking control device, the central locking and unlocking device including a central control computer that operates remote locks equipped with a radio frequency emitter and receiver device to lock and unlock the doors or the hatches which are provided with a radio frequency control device connected to the radio frequency emitter and receiver device of the central control computer;
checking, via the monitoring and locking system, prior to a period of use of the aircraft, a status of the locks to the doors or hatches providing access to the plurality of spaces to determine whether at least one lock of the locks has experienced forced entry during the period of non-use;
performing, before the period of use of the aircraft, a security check only of at least a space sealed by a door or a hatch equipped with the at least one lock of the locks when the at least one lock has been determined via the monitoring and locking system to have experienced forced entry during the period of non-use; and
determining via the monitoring and locking system that a security check does not need to be performed in the plurality of spaces before the period of use when the monitoring and locking system determines that none of the locks have experienced forced entry during the period of non-use.
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Abstract
The invention relates to a system for monitoring and locking aircraft compartment doors (1, 2, 3, 4), characterized in that said system includes a centralized device (12) for controlling the locking/unlocking in the form of a central processing unit (12) for controlling remote bolt devices having a radio transceiver device and a plurality of remote bolt devices (6) for locking/unlocking said doors provided with a radio control device connected to the transceiver device of the control device.
33 Citations
17 Claims
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1. A method of monitoring an aircraft, comprising:
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checking security of a plurality of spaces within the aircraft and closing doors or hatches providing access to the plurality of spaces prior to a period of non-use of the aircraft, the period of non-use being a period when no passengers are on board the aircraft; locking the doors or the hatches, after checking security prior to the period of non-use of the aircraft, via a monitoring and locking system having a central locking and unlocking control device, the central locking and unlocking device including a central control computer that operates remote locks equipped with a radio frequency emitter and receiver device to lock and unlock the doors or the hatches which are provided with a radio frequency control device connected to the radio frequency emitter and receiver device of the central control computer; checking, via the monitoring and locking system, prior to a period of use of the aircraft, a status of the locks to the doors or hatches providing access to the plurality of spaces to determine whether at least one lock of the locks has experienced forced entry during the period of non-use; performing, before the period of use of the aircraft, a security check only of at least a space sealed by a door or a hatch equipped with the at least one lock of the locks when the at least one lock has been determined via the monitoring and locking system to have experienced forced entry during the period of non-use; and determining via the monitoring and locking system that a security check does not need to be performed in the plurality of spaces before the period of use when the monitoring and locking system determines that none of the locks have experienced forced entry during the period of non-use. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17)
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Specification