The invention belongs to the technical field of precision
machining, and discloses a preparation method of a gas
turbine swirler, which is characterized in that the gas
turbine swirler is decomposed into three parts, namely an inner ring, an outer ring and blades, then the inner ring, the outer ring and the blades are independently formed by adopting a
machining method, and then the inner ring, the outer ring and the blades are connected by adopting a
brazing method. In order to guarantee the
brazing quality, a mounting head is machined on the heads of the blades a blade-shaped groove is correspondingly machined in the inner ring, a bayonet is correspondingly machined in the outer ring, then the outer ring, the blades and the inner ring are tensioned through an
assembly tool to guarantee that
brazing faces are tightly attached,
spot welding is used for positioning, and the blades are conveyed into a furnace to be subjected to vacuum brazing after being completed. The roughness of the inner wall of the hollow blade is guaranteed by splitting the structure of the swirler and combining with independent
machining, the tensile strength performance of brazing seams between the blades and the inner ring and the brazing seams between the blades and the outer ring is excellent under the
room temperature and high temperature environment, the strength performance is better than that of
base metal, the performance of the
base metal cannot be lost, and the machining period is effectively shortened.