| 摘要 |
The purpose of the present invention is to solve a conventional technical problem and, more specifically, to provide a fixture which is capable of supporting, fixing and/or controlling positions of a main structure of an aircraft to prevent occurrence of assembly errors which are generated during the assembly of the aircraft made of composite materials. The present invention provides a fixture which has a fuselage of an aircraft fixed thereby and which comprises: at least one rail formed from the center of the fuselage to the outside; a column movable along the rail; and a sucking unit which is installed on the column and which fixes the fuselage by sucking a surface of the fuselage when the column comes close to the fuselage. The fixture for fixing a main structure of an aircraft according to the present invention is provided to prevent a torsional phenomenon from occurring during the assembly of the aircrafts which are different in size from each other; to securely fix the fuselage of the aircraft while preventing the fuselage from being tilted to the left or to the right; and to allow an operator to easily secure a working space. |
