A general
control system of an aircraft anti-terrorism monitoring disposal
system is located in
cockpit and is connected with a
control switch of a monitoring network, an induced
paralysis gas
pipe network and a gun array network. A micro-camera and a
microphone are arranged in each hidden sites on the top of chamber and are connected to form an array, with real-time feedback to the general
control system as well as sound, light and address alarm. The gun array network is arranged in a channel between the
cockpit and a cabin, a plurality of firing gun heads are arranged orderly with interval in a bulkhead on one side of the channel, the bulkhead on the other side is provided with a bullet-proof steel wall, with
anesthesia and live ammunition.
Paralysis-induced gas is stored in a gas
storage tank with a switch valve, the gas
storage tank with a switch valve is communicated with the original
gas supply pipeline of an
engine room through a pipeline with a switch and is merged into the original
gas supply pipeline
system of the
engine room, with no incorporation of
gas supply system of the
cockpit.
System organic, ground connection and monitoring dispose
black box storage. Captain transfers order according to actual situation and ground instruction. The invention can monitor in real time and dispose terrorism incident before serious consequence occurs while ensuring security of the whole aircraft.