A high temperature protective coating material suitable for single crystal nickel base superalloy blades

A nickel-based superalloy, protective coating technology, applied in metal material coating process, coating, vacuum evaporation plating and other directions, can solve the problem of poor anti-oxidation performance, and achieve excellent high-temperature oxidation resistance and non-diffusion. Obvious, thermally grown oxide film flattening effect

Active Publication Date: 2021-09-17
INST OF METAL RESEARCH - CHINESE ACAD OF SCI +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

But pure γ'-Ni 3 Al cannot form a single alumina protective film, and its oxidation resistance is not as good as traditional high-temperature protective coating materials such as MCrAlY coating, β-NiAl coating and NiPtAl coating that can form a single alumina protective film

Method used

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  • A high temperature protective coating material suitable for single crystal nickel base superalloy blades
  • A high temperature protective coating material suitable for single crystal nickel base superalloy blades

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0023] Vacuum smelting and casting targets are used, the chemical composition of which is Ni-8Co-7Cr-10Al-2.5Re-6Ta-0.1Hf-0.2Y (wt.%), and ground into a flat plate with a size of 380×128×8 mm. The target is installed on a magnetron sputtering apparatus, and a coating is prepared on the surface of the blade of the single crystal nickel-based superalloy René N5, and the thickness of the coating is 30-35 μm. The chemical composition of the coating was measured by EPMA: 9.1wt.% Co, 7.9wt.% Cr, 10.4wt.% Al, 2.0wt.% Re, 5.6wt.% Ta, 0.1wt.% Hf, 0.2wt.% Y, 64.7 wt.% Ni.

[0024] Such as figure 1 , using XRD to analyze the phase composition of the coating, it can be seen that the main crystal phase of the coating is γ'-Ni 3 Al. Subsequently, the γ' phase coating sample of the present invention, the comparative NiCrAlY coating sample and the René N5 substrate sample were subjected to a cyclic oxidation test at 1050° C.×500 h. The result is as figure 2 It can be seen from the obser...

Embodiment 2

[0026] Vacuum smelting casting target material, its chemical composition is Ni-9Co-6Cr-12Al-2W-2Mo-4Ta-0.05Hf-0.3Y (wt.%), processed into a flat plate with a size of 380×128×8mm. The target was installed on the magnetron sputtering apparatus, and the blade prepared by the second-generation single crystal superalloy René N5 was used as the substrate. After the substrate was cleaned, it was loaded into a vacuum chamber to prepare the coating. After the coating was deposited, the as-prepared samples were taken out after the temperature of the vacuum chamber dropped to room temperature, and then placed in a vacuum annealing furnace for annealing at 1050 °C for 1 h. According to EDS energy spectrum analysis, the chemical composition of the coating is: 9.8wt.% Co, 6.4wt.% Cr, 11.2wt.% Al, 1.7wt.% W, 1.6wt.% Mo, 3.6wt.% Ta, 0.1wt .%Y, 65.6wt.%Ni. Wherein the Hf content is too low to be detected.

[0027] Using XRD to analyze the phase composition of the coating, the main crystal ph...

Embodiment 3

[0029] Vacuum melting casting target, its chemical composition is Ni-7Co-8.5Cr-10Al-2.5Re-4.5W-0.5Mo-6.5Ta-0.2Hf-0.1Y (wt.%), processed into a size of Φ100mm×40mm Cylindrical targets. The blade prepared by the second-generation single crystal superalloy CMSX-4 is used as the substrate, and the substrate is loaded into a vacuum chamber after surface cleaning. The coating was deposited using multi-arc ion plating technology, and the specific parameters were as follows: vacuum chamber temperature 200°C, argon gas pressure 0.1Pa, arc current 70A, DC bias voltage -50V, duty cycle 20%. After the coating was deposited, the as-prepared samples were taken out after the temperature of the vacuum chamber dropped to room temperature, and then placed in a vacuum annealing furnace for 2 hours at 600°C and 1 hour at 1050°C.

[0030] In this embodiment, the coating thickness is 35-40 μm. According to EDS energy spectrum analysis, the chemical composition of the coating is: 7.2wt.% Co, 8.3wt...

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Abstract

The invention provides a high-temperature protective coating material suitable for single-crystal nickel-based superalloy blades. The chemical composition of the high-temperature protective coating material is 1.5-10.0wt.%Cr, 3.0-12.0wt.%Co, 8.0 ~12.0wt.%Al, 0~3.0wt.%Re, 0~6.0wt.%W, 0~2.0wt.%Mo, 0.5~7.0wt.%Ta, 0.01~0.2wt.%Hf, 0.1~0.3 wt.% Y, the balance Ni; the phase equilibrium structure of the high temperature protective coating material is γ' phase at 1050°C. The high-temperature oxidation performance of the coating prepared by adopting the high-temperature protective coating material is better than MCrAlY (M=Ni, Co, or NiCo) and β-NiAl coating, which is equivalent to NiPtAl coating, and forms between coating-matrix Metallurgical combination, but it will not form a secondary reaction zone with the single crystal substrate like MCrAlY coating, β-NiAl coating and NiPtAl coating, thus avoiding the problem that the coating damages the mechanical properties of the single crystal substrate. The coating prepared by using the material can be used as an independent high temperature and corrosion resistant coating, and can also be used as a thermal barrier coating bonding layer. The thermal shock resistance life of the prepared thermal barrier coating is better than that of NiPtAl / YSZ thermal barrier coating.

Description

technical field [0001] The invention belongs to the field of high-temperature protective coatings, and particularly provides a high-temperature protective coating material suitable for single-crystal nickel-based superalloy blades. Background technique [0002] Gas turbine engines are the core of advanced aircraft, high-speed ships, and high-efficiency clean power stations. Single crystal blades, high-efficiency cooling, and thermal barrier coatings are also known as the three key technologies of gas turbine engines. The thermal barrier coating is mainly composed of two parts, the outer layer is a low thermal conductivity ceramic layer, and the inner layer is a metal bonding layer. Among them, the role of the ceramic layer is to reduce the temperature of the blade, and the metal bonding layer can form a protective oxide film at high temperature, thereby protecting the internal alloy material. Traditional metal bonding layers mainly include diffusion coatings and MCrAlY clad...

Claims

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Application Information

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Patent Type & AuthorityPatents(China)
IPC IPC(8): C22C19/05C23C14/35C23C14/16C23C14/58
CPCC22C19/057C22C19/058C23C14/165C23C14/35C23C14/5806
Inventor朱圣龙姚红蕊鲍泽斌沈明礼王成牛云松王福会陈明辉
OwnerINST OF METAL RESEARCH - CHINESE ACAD OF SCI