Patent attributes
A method of producing a shim for use in an aircraft, the method comprising: providing an aircraft airframe; measuring a surface of the airframe; creating a digital model of the airframe using those measurements; providing an aircraft skin; measuring a surface of the aircraft skin; creating a digital model of the aircraft skin using those measurements; digitally assembling the digital model of the airframe with the digital model of the aircraft skin; using the digitally assembled models, creating a digital model of a shim, the digital model of the shim substantially filling a gap between the digitally assembled digital models of the airframe and the skin; and producing a physical shim using the digital model of the shim.