Manufacture method for ultra-fine grain and high-intensity alloy blade forged piece

A technology of high-strength alloy and manufacturing method, which is applied in the manufacture of high-strength GH4169 alloy rotor blade forgings, in the field of ultra-fine grains, can solve the problems of no adjustment space for processes and heating methods, shorten the mold design cycle, and reduce three sets of processes , cost-saving effect

Active Publication Date: 2013-04-03
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0004] It is difficult to achieve ultra-fine-grained, high-strength superalloy precision forged blades with traditional technological processes, and there is no room for adjustment in the process and heating methods. Therefore, it is necessary to optimize the design of the process and heating methods in the technological process. Manufactured blade forgings with an average grain size of tenons finer than grade 8, an average grain size of blade body finer than grade 10, and mechanical properties such as tensile strength and durability reaching the level of "high strength"

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  • Manufacture method for ultra-fine grain and high-intensity alloy blade forged piece

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Embodiment Construction

[0010] Attached below Figure 1~2 The content of the present invention will be described in detail with Examples.

[0011] Such as figure 1 As shown, the traditional alloy blade precision forging process is: 1. Cylindrical blank - 21. Extruded cylindrical blade body - 22. Pier head forming square tenon - 23. Preformed blade body and tenon - 3 Final forming blade body and tenon - 4 Cutting Burr - 5 heat treatment - 6 physical and chemical testing; this process is currently widely used for stainless steel and titanium alloy blades at home and abroad, but it is difficult to achieve ultra-fine-grained, high-strength superalloy precision forged blades with this process. And heating methods, etc. have no room for adjustment.

[0012] Such as figure 2 As shown, the alloy blade precision forging manufacturing flow chart of the present invention: 1. Cylindrical blank - 2. Extrusion forming of diamond-shaped blade body and tenon - 3. Final forging of blade body and tenon - 4 Trimmin...

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Abstract

The invention provides a manufacture method for an ultra-fine grain and high-intensity alloy blade forged piece. The manufacture method for the ultra-fine grain and high-intensity alloy blade forged piece comprises the following manufacture processes of extruding, finally forging, cutting burrs and carrying out thermal treatment and is characterized in that a barium salt furnace is adopted to heat before the extrusion process; an extrusion die is a ''rhombic blade body and rabbet'' split-type square frustum structure; and the throat part of the extrusion die is strengthened. According to the manufacture method for the ultra-fine grain and high-intensity alloy blade forged piece, which is disclosed by the invention, the die design period and the product technology flow are shortened, the material consumption is lowered, and the cost is saved. Meanwhile, the mean grain size of the prepared forged piece performance tissue is less than the tenth grade, and the performance achieves the level of a high-strength forged piece.

Description

technical field [0001] The invention relates to the field of precise forging of high-temperature alloy blades, in particular to a method for manufacturing ultra-fine-grained, high-strength GH4169 alloy rotor blade forgings. Background technique [0002] Compressor blades are important working parts of gas turbines and aeroengines, especially high-pressure compressor rotor blades. Not only do they have to rotate with the compressor disk at a high speed of 3000~10000rpm for a long time, the heat and force conditions are complicated, and the blade body It is extremely thin, and the thickness of the inlet and outlet edges can even reach 0.2mm, so the requirements for material and structure performance are very strict; blade precision forging solves the problem of difficult machining of thin surface materials, and significantly improves the efficiency of blade processing. Forging technology is the comprehensive application of materials thermal processing, precision testing, surfa...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23P15/02B21K3/04B21K29/00
Inventor 邰清安关红王少刚郝德佳国振兴
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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