The invention belongs to the technical field of engine
nacelle part production, and particularly relates to an intelligent
welding system and method for an engine
nacelle combined type air inlet fairing. An inner
spoiler moving groove and an outer
spoiler moving groove are machined in the air inlet duct
casting blank borne by the air inlet duct positioning
assembly through the inner
cutting assembly and the outer
cutting assembly correspondingly, and the air inlet duct
casting blank is formed into an air inlet duct component; a first clamping feeding assembly, a second clamping feeding assembly, a third clamping feeding assembly and a fourth clamping feeding assembly are used for feeding an inner reinforcing part, a heating part, a
noise reduction and sound absorption part preassembled with a
spoiler assembly and an annular cover plate into a cavity of the air
inlet channel component, and the fed parts are welded and fixed into the cavity of the air
inlet channel component through a
welding assembly; in this way, intelligent
welding and assembling operation of the combined air inlet fairing can be achieved, and the combined air inlet fairing has the advantages of being high in structural strength, good in
noise reduction and sound
absorption effect and capable of achieving automatic deicing of the lip and air
inlet distortion control.