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CMAS erosion-resistant zirconium-tantalum thermal barrier coating material and preparation method thereof

A technology of thermal barrier coatings and coating materials, applied in the fields of zirconium-tantalum thermal barrier coatings and thermal barrier coatings, can solve the problem of reducing the mechanical properties and phase stability of materials, low thermal conductivity, and reducing the phase stability of coatings And other issues

Pending Publication Date: 2021-12-10
XIANGTAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

At present, the commonly used TBCs composition is zirconia (6-8YSZ) doped with 7±1wt.% yttria, which has the advantages of low thermal conductivity, suitable thermal expansion coefficient, and high fracture toughness. Compared with the development, the temperature at the front inlet of the turbine continues to increase, and the surface temperature of the blade will be close to 1400 °C. When the coating is in an ultra-high temperature environment above 1300 °C, with the diffusion of yttrium, the supersaturated tetragonal phase (t' Phase) ZrO 2 A martensitic transformation will occur to form a monoclinic (m-phase) ZrO 2 , and produce 3-6% volume expansion, resulting in stress and cracks in the coating; at the same time, when the coating service temperature is higher than 1200 ° C, the service environment is filled with CaO, MgO, Al 2 o 3 and SiO 2 Particles or sediments (collectively referred to as CMAS) as the main component will inevitably infiltrate and corrode the coating, and the zirconium and yttrium elements in the coating will dissolve together in the melt, resulting in a yttrium-poor area at the interface between the coating and CMAS. Reduced coating phase stability, while zirconium is less soluble in CMAS than yttrium, would result in partially yttrium-depleted ZrO 2 Re-precipitation in granular form, accompanied by spheroidization and t-to-m phase transition, reduces the mechanical properties and phase stability of the material, and also changes the parameters such as the elastic modulus and thermal expansion coefficient of the material

Method used

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  • CMAS erosion-resistant zirconium-tantalum thermal barrier coating material and preparation method thereof
  • CMAS erosion-resistant zirconium-tantalum thermal barrier coating material and preparation method thereof
  • CMAS erosion-resistant zirconium-tantalum thermal barrier coating material and preparation method thereof

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Experimental program
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preparation example Construction

[0032] refer to figure 1 , a specific method for preparing a zirconium-tantalum thermal barrier coating includes:

[0033] Raw material TaCl 5 Soluble in absolute ethanol, Y(NO 3 ) 3 ·6H 2 O, ZrO(NO 3 ) 2 Soluble in distilled water and / or absolute ethanol, respectively;

[0034] Mix the raw material solutions and add them dropwise to ammonia water to obtain evenly distributed white colloidal precipitates;

[0035] The precipitate was centrifuged, washed with distilled water, and vacuum filtered, followed by the first drying to obtain the precipitated powder;

[0036] The obtained powder is placed in a sintering furnace for the first high-temperature sintering, followed by ball milling, second drying and heating activation to obtain the desired nanoscale coating powder;

[0037] The obtained coating powder is subjected to physical compaction under a static press through a mold, and a crystallized coating mass with uniform composition is obtained after second high-temper...

Embodiment 1

[0053] Weigh 1.79g tantalum pentachloride (TaCl 5 ), 1.92g yttrium nitrate hexahydrate (Y(NO 3 ) 3 ·6H 2 O) and 3.47g zirconyl nitrate (ZrO(NO 3 ) 2 ), that is, the Ta:Y:Zr atomic ratio of the prepared coating sample is 2:2:6;

[0054] TaCl to be weighed 5 Dissolved in absolute ethanol, Y(NO 3 ) 3 ·6H 2 O and ZrO(NO 3 ) 2 Dissolve in distilled water respectively, mix the three solutions and stir for 0.5h with a magnetic stirrer to fully dissolve the solvent;

[0055] The mixed solution was dropped into ammonia water with a pH value of 11 to obtain a white colloidal precipitate;

[0056] The precipitate was centrifuged and washed twice with distilled water, then filtered through a vacuum device consisting of a sand core filter, rubber hose and Erlenmeyer flask, and then dried at 80°C for 48 hours to obtain a precipitated powder;

[0057] Place the precipitated powder in a sintering furnace for high-temperature sintering, the sintering temperature is 1600°C, and the ...

Embodiment 2

[0064] Weigh 1.43g tantalum pentachloride (TaCl 5 ), 1.53g yttrium nitrate hexahydrate (Y(NO 3 ) 3 ·6H 2 O) and 0.46g zirconyl nitrate (ZrO(NO 3 ) 2 ), that is, the Ta:Y:Zr atomic ratio of the prepared coating sample is 4:4:2 respectively;

[0065] Using the preparation method and corrosion parameters described in Example 1, the required coating samples were prepared, and the CMAS corrosion experiment was carried out. The corrosion interface of the YSZ sample and the zirconium-tantalum sample corroded by CMAS was characterized by scanning electron microscopy (the results are as follows Figure 5 As shown), it is found that the YSZ corrosion interface is severely spheroidized, while the corrosion interface of the zirconium-tantalum block has no obvious spheroidization phenomenon, indicating that compared with the traditional YSZ coating, the zirconium-tantalum coating has better stability after corrosion.

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Abstract

The invention discloses a CMAS erosion-resistant zirconium-tantalum thermal barrier coating material and a preparation method thereof, the components of the coating material comprise Zr element, Y element, Ta element and O element, the content of ZrO2 accounts for 0-60 mol.% of the total substance amount of the material, and the components can further comprise m-YTaO4 and t-ZrO2. Compared with a traditional yttrium oxide stabilized zirconia (YSZ) coating, the obtained coating material has smaller reaction layer thickness and phase change degree after CMAS corrosion in the same environment, and has better CMAS corrosion resistance.

Description

technical field [0001] The invention relates to the technical field of thermal barrier coatings, in particular to the technical field of zirconium-tantalum thermal barrier coatings. Background technique [0002] Thermal Barrier Coatings (TBCs for short) is currently one of the most feasible solutions that can greatly increase the operating temperature of aero-engines. At present, the commonly used TBCs composition is zirconia (6-8YSZ) doped with 7±1wt.% yttria, which has the advantages of low thermal conductivity, suitable thermal expansion coefficient, and high fracture toughness. Compared with the development, the temperature at the front inlet of the turbine continues to increase, and the surface temperature of the blade will be close to 1400°C. When the coating is in an ultra-high temperature environment above 1300°C, with the diffusion of yttrium, the supersaturated tetragonal phase (t' Phase) ZrO 2 A martensitic transformation will occur to form a monoclinic (m-phase...

Claims

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Application Information

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IPC IPC(8): C04B35/48C04B35/495C04B35/505C04B35/626C04B35/622
CPCC04B35/48C04B35/495C04B35/626C04B35/622C04B2235/6562C04B2235/6565C04B2235/6567C04B2235/3225C04B2235/96C04B2235/9669Y02T50/60
Inventor 杨熠尹冰冰杨利琴喻沛
Owner XIANGTAN UNIV