The invention belongs to the technical field of salt spray tests, and particularly relates to a test device and method for simulating hot
corrosion of an engine
turbine blade material, and the method comprises the following steps: after a sample is cleaned and dried, a
nozzle is controlled by a mechanical arm to atomize a saturated
salt solution, and the saturated
salt solution is precisely sputtered to the surface of the sample preheated to 300-500 DEG C to form a uniform salt film; the sample is placed in a
heating furnace at the temperature of 600-1000 DEG C to be subjected to heat preservation for 50-55 min and then cooled by
compressed air for 5-10 min, and cold and hot circulation A
corrosion kinetic curve is drawn based on the unit area weight increment,
corrosion products are removed through a molten alkali
electrolysis method, and the hot corrosion rate is calculated. The device comprises a groove
type test bed with a high-temperature-resistant
coating, a slit type
nozzle driven by a mechanical arm, an
infrared heating device and a cold and hot circulation
system. According to the method, the salt film is deposited through precise
position control of the mechanical arm, the cold and hot alternating working condition is simulated, the problems that a traditional salt
coating method is not uniform and a salt leaching method is distorted in environment are solved by combining corrosion dynamics and microscopic characteristic analysis, and scientific evaluation of the corrosion resistance of the aero-engine blade material is achieved.