Method for removing ceramic core of hollow blade of turbine of aircraft engine
An aero-engine and hollow blade technology, which is applied in the field of precision casting, can solve the problems of poor core removal quality, difficult operation, unfavorable reactions, etc., and achieve the effects of shortening the core removal cycle, saving production costs, and reducing waste of resources.
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[0017] Hereinafter, the present invention will be further described in conjunction with the embodiments.
[0018] This embodiment uses the core removal method of the present invention to remove the core of a certain type of aeroengine turbine hollow blade. The steps are:
[0019] (1) One-time core removal
[0020] Place the material basket with blades in the de-coring kettle containing 40% caustic potash lye; the pressure is set to 0.50.5MPa, the inner tank temperature is set to 200°C, and the outer tank temperature is set to 480°C; The pressure in the holding state changes to 0.4-0.5MPa, and the exhaust cycle is stable at 15min; water is 30% of the total weight of the lye every 6 hours; the blade is taken out after the reaction is 48 hours, and the material basket with the blade is placed Wash and keep warm in clean, clean water that has been blown into hard air in advance;
[0021] (2) Secondary core removal
[0022] Replace the lye in the de-coring kettle with a concentration of 3...
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