Thermal barrier coating capable of resisting CMAS molten settling erosion and preparing method of coating
A technology of thermal barrier coatings and deposits, which is applied in coatings, fusion spraying, metal material coating processes, etc., can solve problems such as premature failure of thermal barrier coatings, achieve good interface matching, and low manufacturing costs Effect
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[0034] The present invention adopts ordinary atmospheric plasma spraying (using 9MB type plasma spraying gun) or high-energy plasma spraying to prepare 18YSZ / 8YSZ or 48YSZ / 8YSZ coatings, and the ceramic top layer has good high-temperature heat insulation performance and high-temperature stability, and at the same time, the ceramic top layer has Excellent protection against molten CMAS deposits, the coating prepared by this method matches well with the metal substrate, the bonding strength of the coating is 25-40MPa, and the porosity of the ceramic top layer is less than 10%. The preparation method of the coating includes:
[0035] Step 1: Dry the 8YSZ powder and 18YSZ or 48YSZ powder for the preparation of the ceramic layer, and the MCrAlY (M is Ni or NiCo) powder for the preparation of the bonding layer in an oven at 100±10°C for 60 to 120 minutes.
[0036] Step 2: Pre-treatment of the sprayed sample. Clean the sample to be sprayed with acetone to remove the oil on the surface...
Embodiment 1
[0044] Step 1: Take NiCrAlY (Ni22Cr6Al1Y, wherein the mass fraction of Cr is 22%, the mass fraction of Al is 6%, the mass fraction of Y is 1%, and the rest is Ni) bonding layer powder, 8YSZ powder, 48YSZ powder, and spray Dry in an oven at 90°C for 60 minutes.
[0045] Step 2: Pre-treatment of the sprayed sample, clean the sample to be sprayed with acetone, remove the oil on the surface of the sample, and use 20 mesh corundum sand for sandblasting treatment. The sandblasting process conditions are pressure 0.1MPa, sandblasting distance 60mm, spraying The sanding angle is 80°. After sandblasting, use a high-pressure air gun to blow air at a pressure of 0.3 MPa to remove residual sand grains on the surface of the sample.
[0046] Step 3: Preparation of the metal bonding layer, using supersonic flame spraying equipment, with a barrel length of 100mm, spraying the NiCrAlY bonding layer, the spraying process is oxygen flow rate 38L / h, kerosene flow rate 18L / h, powder feeding amount...
Embodiment 2
[0051] Step 1: Take NiCrAlY (Ni25Cr8Al0.8Y, wherein the mass fraction of Cr is 25%, the mass fraction of Al is 8%, the mass fraction of Y is 0.8%, and the rest is Ni) bonding layer powder, 8YSZ powder, and 18YSZ powder , Use an oven to dry at 110°C for 120 minutes before spraying.
[0052] Step 2: Pre-treatment of the sprayed sample, clean the sample to be sprayed with acetone, remove the oil on the surface of the sample, and use 60 mesh corundum sand for sandblasting treatment. The sandblasting process conditions are pressure 0.3MPa, sandblasting distance 80mm, spraying The sanding angle is 70°. After sandblasting, use a high-pressure air gun to blow air at a pressure of 0.5 MPa to remove residual sand grains on the surface of the sample.
[0053] Step 3: Preparation of metal bonding layer, using supersonic flame spraying equipment, with a barrel length of 100mm, spraying NiCrAlY bonding layer, the spraying process is oxygen flow rate 40L / h, kerosene flow rate 22L / h, powder f...
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