Disclosed are a method and
system for measuring concentricity and the
tip clearance of a rotor and a
stator of an aero-engine. The method comprises the steps that the clearance amount of the rotor and the
stator of the aero-engine at an initial
measurement point is acquired; a clearance maximum jerk value FIR value, the phase of the clearance maximum jerk value FIR value, a
maximum deviation IMP value between a sampling profile curve concave point and a mean profile, the phase of the
maximum deviation IMP value, an eccentric distance ECC value, the phase of the eccentric distance ECC value, a maximum clearance value relative to the rotation center, the phase of the maximum clearance value, a minimum clearance value relative to the rotation center, the phase of the minimum clearance value, a maximum clearance value relative to the geometric center, the phase of the maximum clearance value, a minimum clearance value relative to the geometric center and the phase of the minimum clearance value are obtained; an angle-clearance
distribution diagram is drawn; the clearance amount is corrected in the horizontal placement measurement process; a concentricity error value and the
tip clearance of the rotor and the
stator of the aero-engine are obtained. The
system comprises a sampled
data analysis module, a rotor and stator concentricity calculation module, a
tip clearance analysis and calculation module and a horizontal-measurement deflection correction module. The method and
system are suitable for measuring the concentricity and the tip clearance of the rotor and the stator of the aero-engine.