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Method for preparing uniform coating on surfaces of complex molded surfaces by using PS-PVD

A PS-PVD, uniform coating technology, applied in coating, metal material coating process, melt spraying and other directions, can solve the problems of limited flame heating range, uneven preheating, low temperature of jet edge, etc. The effect of avoiding repeated inflation and opening positions, reducing thermal stress and precise and uniform preheating

Active Publication Date: 2020-12-11
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, it is difficult to achieve uniform preheating of large workpieces by the plasma flame flow of PS-PVD equipment.
The temperature at the workpiece clamping end is low, which cannot meet the spraying requirements. In the middle of the jet, the workpiece is prone to local overheating and local melting of the workpiece. In addition, it is difficult to preheat and spray multiple workpieces at the same time by using the plasma flame to preheat, resulting in low production efficiency.
There are two main reasons for this. On the one hand, the effective heating range of the flame is limited. The temperature of the PS-PVD plasma jet near the nozzle outlet is the highest, which can reach ~15550K. However, with the increase of the spraying distance, the temperature of the plasma jet decreases continuously. The temperature distribution in the radial direction of the flow is uneven, the temperature in the center of the plasma jet is high, and the temperature at the edge of the jet is low
On the other hand, although PS-PVD has the advantage of winding plating, due to the occlusion of different parts of the workpiece with complex surfaces, the plasma jet has limited heating capacity for non-line-of-sight areas.
[0008] Therefore, according to the PS-PVD process of the prior art, the uniformity of the coating at different positions is very poor due to uneven preheating when a plurality of complex profile workpieces are deposited at one time.

Method used

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  • Method for preparing uniform coating on surfaces of complex molded surfaces by using PS-PVD
  • Method for preparing uniform coating on surfaces of complex molded surfaces by using PS-PVD
  • Method for preparing uniform coating on surfaces of complex molded surfaces by using PS-PVD

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0071] A certain type of ground gas turbine duplex blade is sprayed with YSZ ceramic layer on the surface of PS-PVD, and the blade is preheated before spraying by using flame flow heating and the multi-degree-of-freedom workpiece preheating system of the present invention respectively. Such as figure 2 (a) and figure 2 As shown in (b), after preheating with flame flow for 15 minutes, the temperature difference between the upper and lower edge plates of the blade and the middle position of the blade body is relatively large, and the temperature difference reaches 50-100°C. After preheating, the exhaust side of the blade body appears to be locally overheated; After spraying with the multi-degree-of-freedom workpiece preheating system, the exhaust edge of the blade is intact, and the exhaust hole is not deformed.

[0072] It can be seen that the present invention can achieve accurate and uniform preheating of workpieces to be sprayed, and realize uniform heating of various par...

Embodiment 2

[0074] A certain type of aero-engine duplex blade is sprayed with YSZ ceramic layer on the surface of PS-PVD, and the blade is preheated before spraying by flame flow heating and multi-degree-of-freedom workpiece preheating system. Such as image 3 (a) and image 3 As shown in (b), three sections are taken at the position of the blade body, the M section is the middle section of the blade, the P section is the section 14mm upward from the M section, and the N section is the section 14mm downward from the N section. Select 7 points, use the eddy current thickness gauge to measure the coating thickness of each point, measure each point 3 times to get the average value, and analyze the coating thickness at different profiles of each section.

[0075] Table 1 shows the thickness of the thermal barrier coating at different profiles of the blades heated by the flame flow. From the data in the table, it can be seen that the average thickness of the ceramic layer at the P section of ...

Embodiment 3

[0082] A certain type of aero-engine single-joint blade is sprayed with YSZ ceramic layer on the surface of PS-PVD. The specific steps are:

[0083]S1: Set the spraying parameters, specifically spray gun current 2000A, spray gun working gas flow rate (Ar: 30SLPM; He: 60SLPM), powder feeding speed (5g / min), powder feeding carrier gas (10SLPM), spraying distance (1200mm), walk gun program); set the workpiece preheating program (preheating temperature 800 ℃, preheating time 5min), set the workpiece transfer program;

[0084] S2: Open the fourth switchable vacuum-sealed door K4, put the blade into the fixture, and then fix it on the automatic workpiece rotating table 6 in the preheating working tank 5;

[0085] S3: Close the fourth switchable vacuum sealing door K4, vacuumize, so that the pressure in the spraying working tank 2 is 2 mbar, the pressure in the preheating working tank 5 is 1 mbar, and the pressure in the workpiece transfer working tank 3 is 0.08 mbar;

[0086] S4: ...

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Abstract

The invention discloses a method for preparing a uniform coating on the surfaces of a plurality of workpieces with complex molded surfaces at a time by using plasma physical vapor deposition (PS-PVD).According to the technical scheme, the method can realize accurate and uniform preheating of the workpieces to be sprayed, realize uniform heating of all the parts of the complex molded surfaces, andimprove the uniformity of the coating on the surfaces of the complex molded surfaces. By adoption of the method,under the protection action of vacuum and inert gases and under the condition of no deformation and structure change of a workpiece matrix, a relatively high preheating temperature is allowed, so that the temperature difference between coating particles and the matrix can be reduced, the cooling speed of the coating is decreased, the generation of thermal stresses is reduced, and the coating is not easy to crack. When the gas-phase particles are sprayed onto the surface of the matrix, the gas-phase particles can be fully diffused to form a neatly-arranged columnar structure coating. In addition, the bonding force between the coating and the matrix can be better enhanced.

Description

technical field [0001] The invention belongs to the technical field of coating preparation, in particular to a method for preparing a uniform coating on the surface of a complex profile by using plasma physical vapor deposition (PS-PVD). Background technique [0002] In recent years, the rapid development of aerospace technology requires high-performance gas turbine engines to have a higher thrust-to-weight ratio. Therefore, new and higher requirements are also put forward for the blades inside the engine. The temperature at the front inlet of the turbine for an aero-engine with a thrust-to-weight ratio of 10 is 1850-1988K; The design inlet temperature before the turbine of the engine will be higher, which is expected to reach 2100-2200K. Even if the most advanced film cooling technology is adopted, the surface temperature of the turbine blade will far exceed the limit service temperature of the superalloy material used in the blade when it is in service. In addition, the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C23C4/134
CPCC23C4/134
Inventor 郭洪波郭谦何雯婷彭徽
Owner BEIHANG UNIV