The invention relates to the technical field of
electromagnetic lock manufacturing, in particular to a cabin door
electromagnetic lock for
aviation. The cabin door
electromagnetic lock comprises a main engine electronic
loop device used for producing currents, a magnetizer communicated with the main engine electronic
loop device, and armature fixed into a cabin door, wherein an electrifying switch used for controlling on-off of the currents produced by the main engine electronic
loop device is arranged in the main engine electronic loop device, a
copper coil used for generating magnetic force is arranged in the magnetizer, and the armature is used for being attracted by the magnetizer under the effect of the magnetic force. According to the cabin door electromagnetic lock, the
copper coil is used for replacing an
electromagnet, the electrifying switch adjusts magnitude of the currents and on-off of the currents to control the size and existence of a
magnetic field of the magnetizer, and electromagnetic attracting lock force can be adjusted and controlled conveniently. Moreover, the structure design gap of a
locking mechanism does not need to be reserved, the structural gap when the cabin door is in a
closed state is reduced, and the problem that when the cabin door is closed, due to rigid
impact of the
locking mechanism, the structure is damaged is avoided.