Aircraft i.e. airplane, manufacturing method, involves fixing sub-assembly to fuselage wall by fixing members that are distinct from sub-assembly and have main vertical axis, where sub-assembly includes two wings rigidly fixed to each other

摘要

The method involves placing a sub-assembly (16) at a wall of a fuselage, where the sub-assembly comprises two wings (6) that are rigidly fixed to each other. The sub-assembly is fixed to the fuselage wall by fixing members e.g. bolts, which are distinct from the sub-assembly and have a main vertical axis. The sub-assembly is fixed to the fuselage wall such that the fixing members traverse a side wall of the sub-assembly, where the fuselage wall comprises composite material. Upper and lower panels of an aerofoil are connected by the side wall. An independent claim is also included for an aircraft comprising a sub-assembly.