Disclosed is a parachute with an aircraft. The parachute with the aircraft is characterized by comprising a parachute body and the rotor aircraft. A hole is formed in the top of the parachute body, and the rotor aircraft is in seamless connection with the hole formed in the top of the parachute body. The aircraft comprises a plurality of electric rotors, an isolating layer, a flight state computer-control system, a power source, an external power source, a remote controller and a man-machine connecting interface. The isolating layer is a planar object. The flight state computer-control system comprises a satellite positioning terminal, an accelerometer and a communication module. Two or more power transmission lines which are combined with the external power source and a power utilization load of the aircraft to form a circuit are adopted by the aircraft. According to the invention, the parachute with the aircraft can maintain a suspension state and a stretched state of the parachute body at any position, and therefore persons in high buildings can be conveniently rescued. Due to the fact that two or more power transmission lines which are combined with the external power source and the power utilization load of the aircraft to form the circuit are adopted, the external power source can continuously supply electric energy to the aircraft through the power transmission lines, and the air-staying capacity of the aircraft can be enhanced in an almost unlimited mode.


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    Title :

    Parachute with aircraft


    Contributors:

    Publication date :

    2015-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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