The invention relates to the field of military equipment, and aims to provide a missile loading and unloading vehicle and a missile loading and unloading method. The missile loading and unloading vehicle comprises a vehicle body and a plurality of lifting and positioning devices. Each lifting and positioning device includes a bottom plate which is connected with the side end of the vehicle body, an installation plate, a position finding mechanism which is connected with the installation plate at the lower end and is provided with a missile loading frame longitudinal positioning sensor and two missile loading frame transverse positioning sensors, a lifting platform which is connected with the installation plate at the lower end, a bearing seat which is provided with at least two longitudinally-arranged missile bearing frames and of which the two side ends are hinged to the upper end of the lifting platform, a retainer which is disposed at the lower side of the bearing seat to retain one end of the bearing seat and is connected with the lifting platform, and two positioning drive mechanisms, wherein the upper end of each missile bearing frame is provided with a missile bearing recess. The missile loading and unloading vehicle is simple in structure and high in missile loading speed. The missile loading and unloading method can meet the requirement of quick positioning, high precision, closed operation of an automatic control program, strong anti-interference performance, no external interference from a visual system, and high missile loading and unloading speed.
Missile loading and unloading vehicle and missile loading and unloading method
2015-08-12
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 |
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