The invention discloses a flexible jacking mechanism of a missile body. The flexible jacking mechanism comprises an installing plate (1), an outer barrel (2), an inner barrel (3), a floating spring (4), L-shaped plates (5), a guide rod (6), a nut sleeve (7), a fixing sleeve (8), a missile supporting wheel frame A (9) and a missile supporting wheel frame B (10), wherein the fixing sleeve (8) is provided with an outer thread. The inner barrel (3) and the outer barrel (2) are fixedly provided with a spring installing base A (18) and a spring installing base B (19) respectively. The outer portion of the fixing sleeve (8) is in threaded connection with the nut sleeve (7). An annular groove (20) is formed in the lower end of the guide rod (6). The guide rod (6) is sleeved with the floating spring (4). One end of the floating spring (4) is fixed to the spring installing base A (18), and the other end of the floating spring (4) is fixed to the spring installing base B (19). The flexible jacking mechanism has the beneficial effects that the tiny difference of adjustment of various freedom degrees can be automatically compensated for, the buffering function is achieved, and it is guaranteed that a guided missile is accurately fed in a sliding groove of a launching frame.
Flexible jacking mechanism of missile body
2016-02-03
Patent
Electronic Resource
English
IPC: | F16M Rahmen, Gehäuse oder Grundplatten von Kraftmaschinen oder anderen Maschinen oder von Apparaten, nicht auf eine besondere Art von Maschine oder Apparat eingeschränkt, die anderweitig vorgesehen ist , FRAMES, CASINGS, OR BEDS, OF ENGINES OR OTHER MACHINES OR APPARATUS, NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUS PROVIDED FOR ELSEWHERE / 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 / F16F SPRINGS , Federn |