Repair method for abrasion of inner wall of engine turbine rear bearing seat
A repair method and technology of turbine bearings, applied in the direction of coating, metal material coating process, etc., to achieve the effect of strong binding force
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Embodiment 1
[0010] After the aero-engine was overhauled and disassembled, the inner wall of the turbine rear bearing seat was measured to be worn, and the wear amount was 0.3 mm. The iron-based powder provided by the invention was used as the raw material, and the laser cladding equipment with a power of 1kW was used for repair. By weight percentage, powder chemical composition: 0.05% carbon, 19.0% Cr, 7.0% Ni; 5.0% Cu; 0.5 Mn; 1.0% Si; the rest is Fe. The powder particle size is 45 μm. Coaxial powder feeding nozzle laser cladding is adopted, the cladding process parameters are power 400 W, powder feeding rate 3.0% g / min, spot diameter Ф1.0% mm, nozzle scanning speed 8.0% mm, lap rate is 50%, and the single-layer height of cladding is 0.5 mm. Fluorescent and X-ray inspections were performed on the repaired turbine rear bearing seat, and no cracks were found in the metallographic microstructure. Microhardness measurement The hardness of the cladding layer is HV0.1 to 350, reaching 1.0% a...
Embodiment 2
[0012] Aiming at the wear of the inner wall of the turbine rear bearing housing after the overhaul of the aero-engine is measured, and the wear amount is 0.5 mm, the iron-based powder provided by the present invention is used as the raw material, and the laser cladding equipment with a power of 1kW is used for repair. The chemical composition (percentage by weight) of the powder is: 0.07% carbon, 18.0% Cr, 8.0% Ni; 6.0% Cu; 1.0% Mn; 0.6% Si; and the rest is Fe. The particle size of the powder is arbitrarily selected from 45 μm to 105 μm. Coaxial powder feeding nozzle is used for laser cladding, the cladding process parameters are power 500 W, powder feeding rate 4.0% g / min, spot diameter Ф1.2 mm, nozzle scanning speed 10.0% mm, lap rate 50%, the single-layer height of cladding is 0.5 mm. Fluorescence and X-ray inspections were performed on the repaired turbine rear bearing seat, and no cracks were found in the microstructure. Microhardness measurement The hardness of the cla...
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