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A kind of molybdenum alloy containing anti-oxidation composite coating and preparation method thereof

A composite coating, molybdenum alloy technology, applied in the coating, metal material coating process, solid-state diffusion coating and other directions, can solve the problems of large difference in thermal expansion coefficient, easy cracks at joints, poor oxidation resistance at medium temperature and so on , to achieve the effect of narrowing the difference in thermal expansion coefficient, good bonding, and favorable anti-scour ability.

Active Publication Date: 2022-06-07
NANCHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

According to the research status at home and abroad, the main problems of the silicide coating prepared on the surface of molybdenum alloy include: (1) single MoSi 2 Although the coating has excellent high-temperature oxidation resistance, it has poor medium-temperature oxidation resistance, and "Pesting" pulverization and oxidation will occur at 400-600 °C; (2) MoSi 2 The thermal expansion coefficient difference between the coating and the substrate is large, and cracks are prone to occur inside the coating and at the junction with the substrate interface, resulting in failure of the coating and poor thermal shock resistance; (3) MoSi 2 SiO formed on the surface after coating oxidation 2 Membrane has good fluidity at high temperature, so the ability to resist gas scour is insufficient
However, there is no mature method to solve the above problems at the same time

Method used

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  • A kind of molybdenum alloy containing anti-oxidation composite coating and preparation method thereof
  • A kind of molybdenum alloy containing anti-oxidation composite coating and preparation method thereof
  • A kind of molybdenum alloy containing anti-oxidation composite coating and preparation method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0031] Step 1: Prepare Mo-based alloys

[0032] According to the ratio of 85at%Mo, 15at%Cr for batching, using a planetary ball mill for wet grinding, ball ratio 5:1, speed 120r / min, ball milling time 30h, after the ball mill is completed, the powder is placed in a vacuum drying box for drying. The dried powder is then pressed into a cold isostatic mold. The pressed specimen was sintered at a low pressure at 1600 °C and 0.6Mpa, and the holding time was 3h, and the Mo-15Cr matrix alloy was prepared.

[0033] Step Two: Prepare (Mo, X)Si on the surface of the resulting alloy in step one 2-(Cr,X)Si 2 Base composite coating

[0034] The surface of the alloy is polished and polished step by step with 240#, 400#, 600# and 1000# silica carbide sandpaper, and blown dry after ultrasonic cleaning in absolute ethanol. The treated specimen is placed in an alumina crucible, placed in a tubular furnace, and NH is introduced into the furnace tube 3 The flow rate is 200ml / min, the surface nitridin...

Embodiment 2

[0036] Step 1: Prepare Mo-based alloys

[0037] According to the proportion of 75at%Mo, 25at%Cr for batching, using a planetary ball mill for wet grinding, ball ratio 5:1, speed 120r / min, ball milling time 30h, after the ball mill is completed, the powder is placed in a vacuum drying box for drying. The dried powder is then pressed into a cold isostatic mold. The pressed specimen was sintered at a low pressure at 1600 °C and 0.6Mpa, and the incubation time was 3h, and the Mo-25Cr matrix alloy was prepared.

[0038] Step Two: Prepare (Mo, X)Si on the surface of the resulting alloy in step one 2 -(Cr,X)Si 2 Base composite coating

[0039]The surface of the alloy is polished and polished step by step with 240#, 400#, 600# and 1000# silica carbide sandpaper, and blown dry after ultrasonic cleaning in absolute ethanol. The treated specimen is placed in an alumina crucible, placed in a tubular furnace, and NH is introduced into the furnace tube 3 The flow rate is 200ml / min, the surface ...

Embodiment 3

[0041] Step 1: Prepare Mo-based alloys

[0042] According to the ratio of 30at%Cr, 10at%Al, 5at%W, the margin is Mo for batching, using a planetary ball mill for wet grinding, ball ratio 5:1, speed 120r / min, ball milling time 30h, after the ball mill is completed, the powder is placed in a vacuum drying box for drying. The dried powder is then pressed into a cold isostatic mold. The pressed specimen was sintered at low pressure at 1600 °C and 0.6Mpa, and the incubation time was 3h, and the Mo-30Cr-10Al-5W matrix alloy was prepared.

[0043] Step Two: Prepare (Mo, X)Si on the surface of the resulting alloy in step one 2 -(Cr,X)Si 2 Base composite coating

[0044]The surface of the molybdenum matrix alloy is gradually sanded and polished with 240#, 400#, 600# and 1000# silicon carbide sandpaper, and blown dry after ultrasonic cleaning in absolute ethanol. The treated specimen is placed in an alumina crucible, placed in a tubular furnace, and NH is introduced into the furnace tube 3 ...

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Abstract

The invention discloses a molybdenum alloy containing an anti-oxidation composite coating and a preparation method thereof, relates to the technical field of high-temperature alloy heat protection, and comprises a molybdenum alloy substrate and a composite coating on its surface, and the composite coating contains at least (Mo, X) Si 2 Phase and (Cr,X)Si 2 Phase, the composite coating can also have a double-layer structure, the outer layer contains at least (Mo,X)Si 2 Phase and (Cr,X)Si 2 phase, the inner layer contains at least (Mo,X) 5 Si 3 phase; where, (Mo,X)Si 2 Where X stands for Cr, Ti or W, (Cr,X)Si 2 X represents Mo, Ti or W, and the preparation method includes the preparation of a molybdenum alloy substrate and the preparation of a composite coating on the surface of the alloy by co-infiltration. The present invention adopts the combination of substrate alloying and surface modification, alloying, composite method and multilayer Preparation of (Mo,X)Si 2 -(Cr,X)Si 2 The molybdenum alloy protected by the base composite coating has excellent medium and high temperature oxidation resistance.

Description

Technical field [0001] The present invention relates to the field of thermal protection technology for superalloys, specifically to a molybdenum alloy containing an antioxidant composite coating and a preparation method thereof. Background [0002] Molybdenum and its alloys have the advantages of high melting point, low resistivity, high thermal conductivity, low coefficient of thermal expansion and high temperature strength, and are the key materials for the preparation of rocket nozzles, nozzle throat linings, radiation hoods, thermal insulation screens and heating components, and have broad application prospects in aerospace, nuclear industry, machinery, metallurgy and other fields. However, molybdenum and molybdenum alloys will be rapidly oxidized into volatile MoO in an air environment above 600 °C 3 , which seriously restricts its use as a high-temperature material. [0003] At present, the main ways of molybdenum high-temperature oxidation resistance are alloying and surfa...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C23C10/44C22C27/04C22C1/04C23C10/52
CPCC23C10/44C22C27/04C22C1/045C23C10/52
Inventor 谭敦强易志强唐晔熊伟龙文海强
Owner NANCHANG UNIV