The invention discloses a large
thermoplastic composite
machine body assembling device and a using method thereof.The assembling device comprises two sets of elevated sliding rail assemblies, two sets of movable crown blocks, an AGV, four sets of
barrel shape-preserving frames, a
photogrammetry system and two sets of
numerical control positioning systems, and the two sets of elevated sliding rail assemblies are symmetrically arranged at a certain interval between the two sets of elevated sliding rail assemblies; an AGV can pass through the middle, the two sets of movable crown blocks stretch across the tops of the two sets of elevated sliding rail assemblies side by side, the two sets of
numerical control positioning systems are correspondingly arranged below the two sets of movable crown blocks, the
barrel shape-preserving frame can fix one half of a
thermoplastic composite
machine body
barrel, and a set of zero point
positioning system is arranged on the upper end face of the
barrel shape-preserving frame. The lower surface of the lower end of the
machine body is provided with a set of ball head
assembly, the machine body cylinder capable of being provided with the half
thermoplastic composite material is fixed to the movable crown block, the lower surface of the lower end of the machine body is provided with a set of ball head
assembly, the machine body cylinder capable of being provided with the half thermoplastic
composite material is fixed to the AGV, the upper surface of the lower end of the machine body is provided with a set of ball head
assembly, and the machine body cylinder capable of being provided with the half thermoplastic
composite material is fixed to the
numerical control positioning system. The technical scheme provided by the invention can be directly popularized to the technical field of mounting and lifting of aircraft floors of different sizes and types in the aeronautical manufacturing industry.