The invention discloses a heat treatment method for recovering the performance of a K465
alloy turbine blade and belongs to the technical field of
metallurgy. The heat treatment method comprises the following steps of 1, blade feeding, 2, furnace heating and then heat preservation: in vacuum or
inert gas protective
atmosphere, carrying out heat preservation at a temperature of 950-960 DEG C for 40-45min, carrying out heat preservation at a temperature of 1190-1200 DEG C for 2-2.5h and carrying out heat preservation at a temperature of 1230 DEG C for 4-4.5h, and 3, furnace cooling: (1), carrying out cooling from a temperature of 1230 DEG C to a temperature of 1000 DEG C at a
cooling rate of 40+ / -25 DEG C / min by
inert gas-based
differential pressure cooling, and (2), feeding
inert gas at a temperature of 1000 DEG C, carrying out cooling to a temperature of 300 DEG C, and opening a furnace door at a temperature below 300 DEG C and carrying out cooling. The heat treatment method can obviously recover the performance (such as
creep deformation) of the K465
alloy turbine blade after a service cycle. Through the heat treatment method, transgranular gamma' polygonal or flower basket-shaped morphology is transformed into the cubical morphology so that morphology squaring is promoted.