This disclosure discloses a method, apparatus, electronic device, and readable medium for drilling through holes in gas
turbine blades. One specific embodiment of the method includes: clamping and fixing a gas
turbine blade using a fixture; controlling a drilling device to
drill holes in the gas
turbine blade; controlling the fixture to move the gas
turbine blade, after drilling the film cooling holes, to a preset position on a through-hole
grinding machine tool; correcting and adjusting the position of the gas
turbine blade on the through-hole
grinding machine tool; acquiring a pre-established
machine tool reference coordinate
system; acquiring a device coordinate
system created by the through-hole
grinding equipment; performing spatial alignment
processing on the
machine tool reference coordinate
system and the device coordinate system; extracting the geometric information set corresponding to at least one film cooling hole on the corrected and adjusted gas
turbine blade; and controlling the through-hole grinding equipment to change the grinding tool to perform deburring and chamfering treatment on the film cooling holes. This embodiment improves the deburring and chamfering effect of film cooling holes on gas turbine blades.