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Preparation method for an AlSiY coating of directional solidification alloy high-pressure turbine blade

A directional solidification, vortex blade technology, applied in metal material coating process, coating, ion implantation plating and other directions, can solve the problems of short service life of the coating, not full-life coating, and high production cost of the coating. High bonding strength, avoiding recrystallization, reliable and stable quality

Active Publication Date: 2014-07-23
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0002] Nickel-based directionally solidified alloy high-vortex blades were originally protected by arc-plating NiCrAlY coating, which is prone to coating shedding during blade production and operation, and the service life of the coating is short, not a full-life coating, so Coating removal and re-coating are required for blades that have reached the end of their life, and the cost of engine refurbishment and coating production is high

Method used

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  • Preparation method for an AlSiY coating of directional solidification alloy high-pressure turbine blade
  • Preparation method for an AlSiY coating of directional solidification alloy high-pressure turbine blade
  • Preparation method for an AlSiY coating of directional solidification alloy high-pressure turbine blade

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Embodiment 1

[0031] (1) Pre-treatment process: firstly, the blades of the directionally solidified alloy DZ22 gas turbine engine are subjected to wet sand blowing treatment, using white corundum sand, the particle size is 140 mesh, the wind pressure is 0.2MPa, and the water pressure is 2.1kg / cm 2 , the sand blowing distance is 120mm, and then the blades after the wet sand blasting treatment are ultrasonically cleaned and soaked in acetone, then dried and inspected for appearance, and weighed;

[0032] (2) Use cathodic arc plating equipment to apply AlSiY coating to the pretreated blades: first, ion cleaning is performed on the blades, and the specific process parameters are as follows: the pressure is 5.31×10 -2 Pa, arc current 450A, voltage 250V, arc plating time 2min; then carry out AlSiY coating plating, the specific process parameters are, the pressure is 5.31×10 -2 Pa, arc current 450A, voltage 30V, arc plating time 35min;

[0033] (3) Weigh the coated blades and conduct visual inspe...

Embodiment 2

[0050] (1) Pre-treatment process: firstly, wet blowing sand treatment is carried out on the directional solidification alloy DZ22 gas turbine engine blade, using white corundum sand, the particle size is 325 mesh, the wind pressure is 0.4MPa, and the water pressure is 2.2kg / cm 2, the sand blowing distance is 380mm, and then the blades after the wet sand blowing treatment are ultrasonically cleaned and soaked in acetone, then dried and inspected for appearance, and weighed;

[0051] (2) Use cathodic arc plating equipment to apply AlSiY coating to the pretreated blades: first, ion cleaning is performed on the blades, and the specific process parameters are as follows: the pressure is 5.30×10 -2 Pa, arc current 650A, voltage 250V, arc plating time 6min; then carry out AlSiY coating plating, the specific process parameters are, the pressure is 5.30×10 -2 Pa, arc current 600A, voltage 50V, arc plating time 45min;

[0052] (3) Weigh the coated blades and conduct visual inspection; ...

Embodiment 3

[0056] (1) Pre-treatment process: firstly, the blades of directional solidification alloy DZ22 gas turbine engine are subjected to wet blowing sand treatment, using white corundum sand, the particle size is 200 mesh, the wind pressure is 0.3MPa, and the water pressure is 2.1kg / cm 2 , the blasting distance is 200mm, and then ultrasonic cleaning and acetone dipping are performed on the blades after wet sand blasting treatment, and then drying and appearance inspection are carried out, and weighing;

[0057] (2) Use cathodic arc plating equipment to apply AlSiY coating to the pretreated blades: first, ion cleaning is performed on the blades, and the specific process parameters are as follows: the pressure is 5.31×10 -2 Pa, arc current 500A, voltage 250V, arc plating time 3min; then carry out AlSiY coating plating, the specific process parameters are, the pressure is 5.31×10 -2 Pa, arc current 500A, voltage 40V, arc plating time 40min;

[0058] (3) Weigh the coated blades and con...

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Abstract

The invention relates to the technical field of quality control for thermal spraying coating, concretely relating to a preparation method for an AlSiY coating of a directional solidification alloy high-pressure turbine blade. The method comprises: first, performing a wet blasting process to the blade; then cleaning by ultrasonic and rinse-cleaning by acetone the wet blasted blade; drying and carrying out an appearance inspection; weighting; second, plating an AlSiY coating on the pretreated blade by using cathodic arc plating technique; weighting the blade after being coated and carrying out an appearance inspection; performing vacuum heat treatment to the coated blade: first, preheating a vacuum heating furnace to a temperature of 200 DEG C with the vacuum degree set lower than 0.2 Pa, then heating up the vacuum heating furnace to the temperature of 850-890 DEG C within 2-4 hours and keeping for 30-35 hours to obtain the deposited AlSiY coating through heat diffusion; and wet blasting the coating of the blade after the vacuum heat treatment to obtain the final product.

Description

technical field [0001] The invention relates to the technical field of thermal spraying coating quality control, in particular to a method for preparing an AlSiY coating of a directionally solidified alloy high-vortex blade. Background technique [0002] Nickel-based directionally solidified alloy high-vortex blades were originally protected by arc-plating NiCrAlY coating, which is prone to coating shedding during blade production and operation, and the service life of the coating is short, not a full-life coating, so Coating removal and re-coating are required for blades that have reached the end of their life, and the cost of engine refurbishment and coating production is high. Contents of the invention [0003] The purpose of the present invention is to address the deficiencies in the prior art and provide a method for preparing AlSiY coatings on directionally solidified alloy high-turbulence blades, which does not require rework of the coatings until the end of the bla...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C23C4/12C23C4/18C23C4/02C23C4/06C23C14/02C23C14/16C23C14/32C23C14/58
Inventor 袁福河王璐张凡云穆坤桐张玉忱
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION