Patent ID: 9709392
Date: 2017-07-18
CPC Classifications: F01D,G01B,G01M

Claim:
1. An aero engine rotor assembling method based on concentricity and verticality measurement, wherein, the measurement is: disposing and fixing a measured rotor on a worktable for adjusting concentricity and inclination; making a telescopic-type inductive sensor for measuring an axial mounting reference plane in contact with an axial mounting reference plane of the measured rotor so as to adjust inclination; making a lever-type inductive sensor for measuring a radial mounting reference plane in contact with a radial mounting reference plane of the measured rotor so as to adjust concentricity; an air bearing rotary table driving the measured rotor to rotate at a uniform speed of 6 to 10 r/min via the worktable for adjusting concentricity and inclination, the telescopic-type inductive sensor for measuring the axial mounting reference plane taking samples at uniform interval on the axial mounting reference plane of the measured rotor, and the lever-type inductive sensor for measuring the radial mounting reference plane taking samples at uniform interval on the radial mounting reference plane of the measured rotor; making the sampling points satisfy that there are 1000 to 2000 points every circle; fitting the sampling data on the radial mounting reference plane of the measured rotor by the Least Squares Circle so as to assess the eccentricity, and fitting the sampling data on the axial mounting reference plane of the measured rotor by the Least Square Plane so as to assess the inclination; adjusting a concentricity adjusting knob of the worktable for adjusting concentricity and inclination according to the dimension and the angle of the eccentricity; adjusting an inclination adjusting knob of the worktable for adjusting concentricity and inclination according to the dimension and the angle of the inclination, until the worktable for adjusting concentricity and inclination satisfying that the dimension of the eccentricity of the radial reference plane is in the range of 0 to 3 μm and that the dimension of the inclination of the axial reference plane is in the range of 0 to 2″; making a telescopic-type inductive sensor for measuring an axial mounting measuring plane in contact with an axial mounting measuring plane of the measured rotor, and making a lever-type inductive sensor for measuring a radial mounting measuring plane in contact with a radial mounting measuring plane of the measured rotor; the air bearing rotary table rotating at a uniform speed of 6 to 10 r/min, the telescopic-type inductive sensor for measuring the axial mounting measuring plane taking samples at uniform interval on the axial mounting measuring plane of the measured rotor, and the lever-type inductive sensor for measuring the radial mounting measuring plane respectively taking samples at uniform interval on the radial mounting measuring plane of the measured rotor; making the sampling points satisfy that there are 1000 to 2000 points every circle; fitting the sampled data on the radial mounting measuring plane of the measured rotor obtained with the lever-type inductive sensor for measuring the radial mounting measuring plane by the Least Squares Circle so as to assess the concentricity, and fitting the sampling data on the axial mounting measuring plane of the measured rotor obtained with the telescopic-type inductive sensor for measuring the axial mounting measuring plane by the Least Square Plane so as to assess the verticality; combining the radius of the axial mounting measuring plane and the height difference between the measured rotor and the finally assembled rotor to obtain the influencing weight of this rotor to the assembled rotor on coaxality; measuring respectively all the rotors required for assembling to obtain the influencing weight of each rotor to the assembled rotor on coaxality; vector optimizing the weight of each rotor by genetic algorithm to obtain the assembling angle of each rotor, and calculating the influencing weight of the rotor on coaxality with the following formula: wherein: C representing the concentricity of the radial mounting measuring plane of the measured rotor, φ representing the eccentric angle of the fitting circle center of the radial mounting measuring plane, H representing the height difference between the measured rotor and the finally assembled rotor, R representing the radius of the axial mounting measuring plane, P representing the verticality of the axial mounting measuring plane of the measured rotor, θ representing the angle at the highest point of the fitting plane of the axial mounting measuring plane.