DOOR CONTROL DEVICE COUPLED WITH WING DEPLOYING AND FLIGHT VEHICLE HAVING THE SAME

摘要

PURPOSE: An aircraft door control device interlocked with the deployment of a wing and an aircraft having the same are provided to reduce the volume and weight of an aircraft and to reduce additional energy consumption because of a door of which the opening and closing operation is interlocked with the deployment of wings. CONSTITUTION: An aircraft door control device comprises an opening, a door(211), an elastic unit, and a door locking part. The opening is formed in an aircraft body to deploy wings from the inside of the body to the outside. The door is mounted on the body to be rotated between a first state for opening the opening and a second state for closing the opening. The elastic unit applies elasticity to the door so that the door can be rotated from the first state to the second state. The door locking part locks the door in the first state, and unlocks the door while interlocking with the deployment of the wings so that the door can be rotated to the second state when the wings are deployed.