The invention discloses a TC4
skin self-adaptive tailored blank
laser welding method based on
light beam scanning-pulse cooperation, and belongs to the technical field of high-energy beam precision
welding. The problems that in the
batch production process of the
aerospace thin-wall
titanium alloy standardized cabin, due to
skin assembly gap fluctuation, plate thickness misalignment, V-shaped notches and other shape and position deviations, the shape of a
molten pool is unstable, and
welding seam forming consistency is poor are solved. A collaborative matching method of a scanning path and
pulse energy parameters is adopted to improve the bridging efficiency of a
molten pool and the form stability of a bridging liquid film, and meanwhile, self-
adaptive response adjustment of welding parameters is achieved by combining workpiece form and position deviation changes and real-time monitoring feedback of dynamic bridging behaviors of the
molten pool. According to the technology, continuous and stable welding seam forming under the
assembly working condition of a gap of 0.2-0.4 mm, a misalignment of 0.3-0.6 mm or a V-shaped notch of 20-30 degrees is achieved for the specification of a
skin with the thickness larger than or equal to 1.5 mm, the tensile strength of a welding seam reaches 95% or above of a base material, and meanwhile high welding heat efficiency is maintained. According to the method, the adaptability of the
laser welding technology to the workpiece form and position deviation is remarkably improved through the multi-parameter synergistic effect and process monitoring
feedback regulation and control, and key
technical support is provided for solving the high-quality and stable welding problem of a new-generation
spaceflight standard general cabin structure in the development and
batch production process.