The invention relates to a novel efficient drone which comprises a take-off and landing platform, a drone body and a control system, wherein the take-off and landing platform comprises a positioning support frame, a traveling mechanism and an unmanned aerial vehicle take-off and landing platform, and at least three positioning electromagnets and at least one homeward voyage guided radar are uniformly distributed on the unmanned aerial vehicle take-off and landing platform; the drone body comprises undercarriages, a fuselage, fixed wings, spiral wings, a turbofan engine, a piston engine and driving propellers; the control system comprises a flight attitude control unit, a wireless data communication unit, a function expansion unit, a data processing unit, a flight navigation unit and a landing navigation unit; and the undercarriages and the fixed wings are installed at the outer side of the fuselage. According to the invention, on one hand, the transport capacity of the unmanned aerial vehicle system is improved, and on the other hand, the operation efficiency of the drone can be effectively improved, thereby greatly improving the service performance of the drone and widening the range of application of the drone.
Novel efficient drone
2015-11-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen |
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