The invention relates to a determination method for an interference film hole
machining angle, and belongs to the technical field of aero-engine
turbine blade
machining. The determination method comprises the following steps that, a
machine tool coordinate
system (x, y, z) is established according to a position axis of a
machine tool, a horizontal rotation axis of the
machine tool serves as a B axis, and a vertical rotation axis of the
machine tool serves as a C axis; according to the
machine tool coordinate
system (x, y, z), an initial coordinate of the interference air film hole and an initial coordinate of a bending guider are determined; and according to the initial coordinate of the interference film hole and the initial coordinate of the bending guider, when the B axis and the C axis are rotated to drive the interference film hole to rotate towards the bending guider, the rotation angle of the B axis and the rotation angle of the C axis are the
machining angle of the interference film hole. According to the determination method, on the premise that the design performance of a
turbine blade
air cooling system is not reduced, shielding of a blade structure is effectively avoided,
electric spark machining of the interference film hole is achieved, and therefore the design performance of an advanced aero-engine is met.