The utility model relates to the technical field of
solid rocket combustion chamber shell operation, in particular to a
solid rocket engine
combustion chamber shell operation mechanism which comprises a square
pipe, the top of the square
pipe is fixedly connected with a fixing plate, the top of the fixing plate is connected with an adaptive
assembly in a clamped mode, and the adaptive
assembly comprises a rectangular plate, a connecting rod, a rotating rod and a directional wheel. Through the arrangement of the rectangular plate, the connecting rod, the rotating rod and the directional wheel, during use, a
combustion chamber shell is placed on the directional wheel, the surface of the directional wheel is smooth and free of protrusions, the
combustion chamber shell cannot be abraded, the directional wheel is connected with the rectangular plate, and an operator can adjust the position of the rectangular plate according to the size of the shell; and through matched use of the matched groove holes and bolts, the bolts are tightened to drive the rectangular plates to be fixed, so that the effect of reducing manual carrying of the
combustion chamber shell is achieved, and the situation that
continuous production is not facilitated due to the fact that the appearance of the
combustion chamber shell is damaged easily when the shell is rotated manually is avoided.