SIMULATION OF LOADS ON AEROSTRUCTURES DURING AIRCRAFT ASSEMBLY

    公开(公告)号:US20180072433A1

    公开(公告)日:2018-03-15

    申请号:US15558779

    申请日:2016-03-07

    CPC classification number: B64F5/60 B64D13/02 B64D43/02 B64F5/10 G01C21/165

    Abstract: Methods and systems useful during assembly of aircraft are disclosed. One such method comprises loading a fuselage of the aircraft that is unassembled with a wing of the aircraft to obtain a configuration of the fuselage corresponding to when the fuselage is assembled with the wing. The method also comprises calibrating a device of a navigation system of the aircraft when the fuselage is unassembled with the wing and is being loaded to obtain the loaded configuration and, after calibrating the device of the navigation system, assembling the fuselage with the wing.

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