The invention provides multichannel
spinning and turning integrated equipment for a cylindrical part of a carrier
rocket and a
machining method. The multichannel
spinning and turning integrated equipment comprises a lathe
bed, a main spindle box, a closing-in spindle box, a
spinning roller frame, a
tail top, a
heating system, a
control system and a hydraulic
system. The main spindle box, the closing-in spindle box, the spinning roller frame and the
tail top are installed on the lathe
bed. The main spindle box is connected with the closing-in spindle box and drives the closing-in spindle box to work, a cylindrical part blank is clamped between the closing-in spindle box and the
tail top, the spinning roller frames are located on the two sides of the cylindrical part blank, and the
heating system is installed on the spinning roller frames; the
control system is connected with the main spindle box, the closing-in spindle box, the spinning roller frame, the
heating system and the hydraulic
system. The hydraulic
system is connected with the main spindle box, the closing-in spindle box, the spinning roller frame and the tail top. Through cooperation of the main spindle box, the closing-in spindle box, the spinning roller frame, the tail top and the like, the in-situ
machining function combining forced spinning
machining, closing-in machining and turning machining of cylindrical parts, conical parts and curved-
bus-shaped parts of the carrier
rocket is achieved.