Research on Cooling Method in Surfacing Repair Process of Aero Compressor Blade

Abstract EN

For the cooling method in surfacing repairing, most of the research focuses on the method based on the fixture structure.

However, due to the low thermal conductivity and ultrathin alloy blade, the heat transfer speed from the molten pool to fixture is slow.

When the heat is transferred to the fixture, most of the molten pool has solidified and absorbed or segregated out some impurities.

Therefore, how to cool the welding area directly is more critical.

For this reason, the thermal cycle characteristics of typical points of the blade and the heat transfer process of the key area of the fixture are analyzed, the original cooling time is calculated, and two innovative cooling methods based on lateral forced convection cooling and vertical jet impact forced convection cooling are proposed.

For lateral forced cooling, with “AF-field” lateral convection cooling modeling, the cooling effects of characteristic points and sections under different flow velocities are calculated.

For vertical jet impact cooling, the pressure, flow rate, and convective heat flux distribution on the wall under different impact heights and nozzle diameter are calculated.

The influence of different inlet flow rates on cooling performance is influenced, based on the analysis results of impact modeling, the moving heat sink model is established, and the cooling effect under different heat sink-source distances is calculated.

The heat transfer rules of two methods are analyzed in detail through modeling and simulations.

The results show that both methods can improve the cooling effect and the vertical jet impact cooling method has an effect that is more obvious.

When the nozzle radius is 2 mm, the impact height is 4d, the inlet flow velocity is 35 m/s, and the distance is 7 mm, and the cooling time under the vertical jet impact method is shortened by 12.5%, which can achieve better cooling effect.

The experiment further validates the effectiveness of the modeling and simulations.