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Method for manufacturing GH5188 engine heat screen through selective laser melting technology

A GH5188, laser selective melting technology, applied in the direction of additive manufacturing, improvement of process efficiency, improvement of energy efficiency, etc., can solve the problems of high scrap rate, long processing procedure, complex and lightweight structure of heat shield parts, etc., to reduce Number of welds, avoidance of weld cracking, effects of solving internal defect problems

Active Publication Date: 2021-12-10
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] GH5188 is a Co-Ni-Cr based solid solution strengthened deformed superalloy, the alloy can be used at a temperature of 950°C-1100°C; the addition of tungsten element for solid solution strengthening makes the alloy have good creep resistance, thermal fatigue resistance and High-temperature strength; at the same time, a relatively high content of chromium and a trace amount of lanthanum are added to make the alloy have good high-temperature oxidation resistance; it is widely used in the manufacture of aero-engine parts, such as heat shields, side walls, flame guides and other high-temperature components; However, in the production process, the GH5188 alloy ingot has obvious micro-segregation, and the subsequent heat treatment process cannot eliminate the micro-segregation, resulting in poor processing plasticity and welding cracking; GH5188 material uses laser selective melting technology, and there are few domestic and foreign studies. Documents explain its formability and performance
[0004] The heat shield parts of the engine are key components working in the high-temperature environment of the engine. They are assembled on the inner wall of the high-temperature area of ​​the engine and play a role in heat insulation; the quality of the heat shield parts determines the overall life of the engine. With the continuous development and maturity of engine technology, high-performance , The demand for high thrust-to-weight ratio engines is becoming more and more significant, resulting in the structure of heat shield parts becoming more complex and lightweight; the heat shield tends to be thinner and space-shaped, and it is difficult to adopt traditional manufacturing processes, and the number of welds is large. The processing process is long; at the same time, GH5188 alloy is a difficult-to-process material, which is prone to cracks during welding and has a high scrap rate

Method used

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  • Method for manufacturing GH5188 engine heat screen through selective laser melting technology
  • Method for manufacturing GH5188 engine heat screen through selective laser melting technology
  • Method for manufacturing GH5188 engine heat screen through selective laser melting technology

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0026] The method of preparing the GH5188 engine heat shield by laser selective melting technology is implemented according to the following steps:

[0027] Step 1, model processing: Use UG software and Magics software to add margins, select placement methods, add supports, and slice according to the thickness of 0.03mm on the 3D model of the heat shield parts. During the slices, set the heat shield parts separately After the laser power, scanning speed, scanning mode, scanning distance, powder layer thickness, and spot compensation of the entity, the outer contour of the heat shield part and the support, output the .Stl format file and process parameter file, and wait for input into the laser selective melting forming equipment;

[0028] In step 1, the heat shield parts are placed at an angle of 45° with the substrate to ensure the final forming accuracy of the heat shield parts and facilitate the removal of supports. Add 1mm of grinding and machining allowance; use Magics so...

Embodiment 2

[0046] The method of preparing the GH5188 engine heat shield by laser selective melting technology is implemented according to the following steps:

[0047] Step 1, model processing: Use UG software and Magics software to add margin, select placement mode, add support, and slice according to the thickness of 0.04mm on the 3D model of heat shield parts. During the slice, set the heat shield parts respectively After the laser power, scanning speed, scanning mode, scanning distance, powder layer thickness, and spot compensation of the entity, the outer contour of the heat shield part and the support, output the .Stl format file and process parameter file, and wait for input into the laser selective melting forming equipment;

[0048] In step 1, the heat shield parts are placed at an angle of 45° with the substrate to ensure the final forming accuracy of the heat shield parts and facilitate the removal of supports. Add 1.5mm of grinding and machining allowance; use Magics software...

Embodiment 3

[0066] The method of preparing the GH5188 engine heat shield by laser selective melting technology is implemented according to the following steps:

[0067] Step 1, model processing: Use UG software and Magics software to add allowances, select placement methods, add supports, and slice according to the thickness of 0.05mm on the 3D model of the heat shield parts. During the slices, set the heat shield parts separately After the laser power, scanning speed, scanning mode, scanning distance, powder layer thickness, and spot compensation of the entity, the outer contour of the heat shield part and the support, output the .Stl format file and process parameter file, and wait for input into the laser selective melting forming equipment;

[0068] In step 1, the heat shield parts are placed at an angle of 45° with the substrate to ensure the final forming accuracy of the heat shield parts and facilitate the removal of supports. Add 2mm of grinding and machine allowance; use Magics s...

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Abstract

The invention discloses a method for manufacturing a GH5188 engine heat screen through a selective laser melting technology, and belongs to the technical field of metal material additive manufacturing. According to the technical scheme, the method for manufacturing the GH5188 engine heat screen through the selective laser melting technology comprises the steps that model processing is conducted; the raw material, GH5188 alloy powder, is taken and subjected to drying treatment; the GH5188 alloy powder is fed in a powder cabin of selective laser melting forming equipment after being dried, a base plate is selected, the base plate is fixed to a workbench, the GH5188 alloy powder is fetched through a scraper, the GH5188 alloy powder is repeatedly laid on the base plate in a trial mode, the whole base plate is completely paved with the powder, a forming cabin is locked, the forming cabin is vacuumized and filled with inert gas for protection, and meanwhile the base plate is preheated; a heat screen part is printed; stress relief annealing, support removal, hot isostatic pressing and heat treatment are conducted on the formed heat screen part; and the performance of the sample is detected. According to the method, integrated forming of the heat screen part is achieved, the number of weld joints is reduced, and welding cracking caused by welding is avoided.

Description

technical field [0001] The invention relates to the technical field of additive manufacturing of metal materials, in particular to a method for preparing a GH5188 engine heat shield by laser selective melting technology. Background technique [0002] Laser selective melting technology (SLM) has the advantages of rapid response, complex structure integration, and mold-free forming. In terms of aerospace, it can significantly solve the development needs of "urgent, difficult, dangerous, and new" parts in the aerospace field; "Vertical" structural constraints to achieve high-performance, high-degree-of-freedom structural manufacturing, and promote the development of aero-engines to high thrust-to-weight ratios from the perspective of components. [0003] GH5188 is a Co-Ni-Cr based solid solution strengthened deformed superalloy, the alloy can be used at a temperature of 950°C-1100°C; the addition of tungsten element for solid solution strengthening makes the alloy have good cr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B22F10/28B22F10/36B22F10/37B22F10/85B33Y10/00B33Y50/02
CPCB22F10/28B22F10/36B22F10/37B22F10/85B33Y10/00B33Y50/02Y02P10/25
Inventor 马慧君董文启任慧娇周冠男薛丽媛
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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