Oxidation-inhibited thermal barrier coating and preparing method thereof
A thermal barrier coating and anti-oxidation technology, which is applied in coatings, anti-corrosion coatings, fire-resistant coatings, etc., can solve the problems of not easy to deposit thick coatings, low deposition speed, and not very ideal, and achieve excellent oxidation resistance, The effect of simple preparation process and low price
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Embodiment 1
[0019] The base material is superalloy M38G, and the sample size is 15×25×5mm 3 . Using a two-dimensional workbench, six-sided explosive spraying was carried out on the sample. The prepared thermal barrier coating consists of three parts: an anti-oxidation connection layer, a diffusion barrier layer and an insulating ceramic layer as a surface layer. The connection layer is Ni-25Cr-5Al-0.5Y, and the diffusion barrier layer is Ni-50Al, ZrO 2 -8Y 2 o 3 material for the ceramic layer. Its composition and thickness parameters are shown in Table 1; the detonation spraying parameters of each layer are shown in Table 2.
[0020] Table 1 The thermal barrier coating with three-layer structure in Example 1
[0021] Composition Thickness (μm)
[0022] Ni-25Cr-5Al-0.5Y 120
[0023] Ni-50Al 5
[0024] ZrO 2 -8Y 2 3 250
[0025] Table 2 Example 1 detonation spraying process parameters
[0026] Process parameters Ni-25Cr...
Embodiment 2
[0035] Two structures of thermal barrier coatings were prepared, namely a two-layer structure system and a three-layer structure system. Thermal barrier coating I with a double-layer structure, the connection layer is made of Co-29Cr-6Al-1Y alloy, and the ceramic layer is ZrO 2 -8Y 2 o 3 ; The method for preparing thermal barrier coatings by detonation spraying disclosed in Chinese patent (application number: 01133423.1) is adopted. Three-layer thermal barrier coating II, the composition of each layer is Co-29Cr-6Al-1Y (connection layer), Ni-55Al (intermediate layer), ZrO 2 -8Y 2 o 3 (ceramic layer), the thickness of each layer is shown in Table 3, and the explosion spraying parameters of each layer are shown in Table 4.
[0036] Table 3 The thermal barrier coating of Example 2
[0037] Type Composition (wt.%) Thickness (μm)
[0038] I Co-29Cr-6Al-1Y / ZrO 2 -8Y 2 o 3 100 / 300
[0039] II Co-29Cr-6Al-1Y / Ni-55Al / ZrO 2 -8 Y 2O 3 100 / 10 / ...
Embodiment 3
[0050] The base material is M22 alloy, and the sample size is 15×25×2mm 3 . Preparation of two three-layer thermal barrier coatings III and IV, namely: III is NiCoCrAlY / NiAl / ZrO 2 -8Y 2 o 3 , IV is NiCoCrAlY / Al 2 o 3 / ZrO 2 -8Y 2 o 3 system. The connecting layer of the two systems is made of Ni-21Co-22Cr-10Al-1Y alloy, and the thickness of each layer is shown in Table 5. The thermal barrier coating was prepared by detonation spraying disclosed in the Chinese patent (application number: 01133423.1), and the detonation spraying parameters of each layer are shown in Table 6.
[0051] Table 5 The thermal barrier coating of Example 3
[0052] Type Composition (wt.%) Thickness (μm)
[0053] Ni-21Co-22Cr-10Al-1Y 80
[0054] III
[0055] / Ni-60Al / ZrO 2 -8Y 2 o 3 / 15 / 350
[0056] Ni-21Co-22Cr-10Al-1Y 80
[0057] IV
[0058] / Al 2 o 3 / ZrO 2 -8Y 2 o 3 ...
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