The invention discloses a small-sized electromagnetic clutch dragging type launching ejection device of an unmanned aircraft. The launching ejection device comprises a steering wheel, brake equipment, a slide rail, a dragging cable, a sliding trolley, an unmanned aircraft, power equipment, ejection-angle regulating equipment and an ejection bracket, wherein the slide rail is pivotally connected to a position above the ejection bracket; the ejection-angle regulating equipment is arranged between the slide rail and the ejection bracket; the steering wheel is mounted at one end of the slide rail; the sliding trolley is placed on the slide rail; the unmanned aircraft is arranged on the sliding trolley; the brake equipment is fixed at the end of the travel of the slide rail; one end of the dragging cable is connected with the sliding trolley; the other end of the dragging cable is connected with the power equipment; the power equipment is arranged under the slide rail. Through the technical scheme, the small-sized electromagnetic clutch dragging type launching ejection device of the unmanned aircraft, disclosed by the invention, is high in working liability, good in working concealment, and not limited by altitude and low-temperature environment, so that the launching ejection device is suitable for field operation and manoeuvrable transfer; besides, the launching ejection device is simple in system structure, convenient to operate, easy to maintain, and lower in purchasing cost and using cost.
Small-sized electromagnetic clutch dragging type launching ejection device of unmanned aircraft
2015-11-18
Patent
Electronic Resource
English
IPC: | 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 |