Low-cost nontoxic thermal barrier coating and manufacturing method thereof
A technology of thermal barrier coating and manufacturing method, which is applied in coating, metal material coating process, melt spraying and other directions, can solve the problems of difficulty in meeting the turbine inlet temperature, poor high temperature stability, low oxidation resistance, etc. Sintering resistance and high temperature thermal stability, thermal conductivity reduction, effect of reducing thermal conductivity
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- Publication Date
- 2015-11-25
- Estimated Expiration
- Not applicable · inactive patent
Abstract
Description
technical field
[0001] The invention relates to the technical field of ceramic material processing, in particular to a low-cost non-toxic thermal barrier coating and a manufacturing method thereof. Background technique
[0002] With the development of aviation gas turbines in the direction of high flow ratio, high thrust-to-weight ratio, and high inlet temperature, the working temperature in the combustion chamber has far exceeded the service temperature limit of Ni-based superalloys. The preparation of thermal barrier coatings on the surface of superalloy substrates has a very direct effect on improving the temperature bearing capacity of the substrates, thereby effectively increasing the working temperature of parts and prolonging their service life.
[0003] Thermal barrier coating is generally a functional coating that utilizes materials with relatively low thermal conductivity and is coated on the surface of superalloy substrates with appropriate technology to play a ro...
Examples
Embodiment Construction
[0014] The low-cost non-toxic thermal barrier coating is characterized in that it is made of the following raw materials in parts by weight: cerium oxide 22, zirconium dioxide 30, yttrium oxide 36, nano-silicon carbide 1.1, aluminum powder 8.4, ring Oxygen resin 5, NiCoCrAlYTa alloy powder 75, fly ash 22, magnesium carbonate 1, polyvinyl alcohol fiber 5, dibutyl phthalate 3, tetraethoxysilane 4.
[0015] The preparation method comprises the following steps:
[0016] (1) Treat nano-silicon carbide and NiCoCrAlYTa alloy powder at 715-835°C for 30-50 minutes at high temperature, quickly cool to room temperature, add magnesium carbonate for ultrasonic grinding for 20-40 minutes, heat to melt, stir for 5-8 hours, and vacuum atmosphere Condensation molding, grinding into powder to obtain a modified metal bonding layer;
[0017] (2) Add aluminum powder and polyvinyl alcohol fiber to a ball mill and grind for 10-20 minutes, spray into molten epoxy resin and mix well, add dibutyl phth...