Integral repair method for longitudinal intensive damage of blade crown of aero-engine turbine rotor blade
A technology of turbine rotor and repair method, which is applied in the direction of process efficiency improvement, energy efficiency improvement, additive manufacturing, etc., can solve the problems of blade crown geometric continuous structure damage, difficult to achieve blade repair, and matrix material degradation, etc., and achieves improvement of environmental strength. , Conducive to standardized operations, remove the effect of thorough
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[0031] The technical solution of the present invention will be further described in detail below in conjunction with the accompanying drawings, but the protection scope of the present invention is not limited to the following description.
[0032] Such as Figure 1~7 As shown in , an integral repair method for the longitudinal dense damage of the turbine rotor blade shroud, including the following steps:
[0033] S1. Grinding and removing the damaged blade crown, taking the upper surface of the integral casting cover plate of the blade as the reference, removing all structures above the reference, and exposing the metallic luster plane, such as figure 2 shown.
[0034] In step S1, the grinding removal method is CNC lathe or manual grinding and removal.
[0035] S2. Remove the surface cracks under the cast cover plate, and remove the cracks and the surrounding surface as a whole, such as image 3 As shown, the laser additive manufacturing technology is used to fill the surf...
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