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Forging and heat treatment method of Haynes 242 alloy forge piece

A heat treatment method, aging heat treatment technology, applied in the direction of metal processing equipment, etc., can solve the problem of less reference information, and achieve the effect of uniform grain structure, good high-temperature durability and mechanical properties, and fine grain size

Inactive Publication Date: 2022-02-15
GUIZHOU AVIATION TECHN DEV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, there are few reports about Haynes242 alloy as a new type of aviation parts material at present, and there are very few reference information that can be consulted. Therefore, we can only explore through continuous experiments in order to realize the technical scheme of Haynes242 alloy as a material for aviation parts. Therefore, it is necessary to Research on forging and heat treatment methods of Haynes242 alloy

Method used

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  • Forging and heat treatment method of Haynes 242 alloy forge piece
  • Forging and heat treatment method of Haynes 242 alloy forge piece
  • Forging and heat treatment method of Haynes 242 alloy forge piece

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1-5

[0026] A kind of forging method of Haynes242 alloy forgings, Haynes242 alloy blanks are carried out upsetting, punching, saddle reaming, final rolling according to the heating temperature condition shown in Table 1, and the holding time is blank effective thickness * 6min / 10mm, make Its deformation amount is 30%, obtains Haynes242 alloy forging, and the grain size of described forging is as shown in table 1;

[0027] Table 1

[0028]

[0029]

Embodiment 6

[0031] The Haynes242 alloy forging obtained by forging Examples 1-5 is carried out solution heat treatment 60min under the conditions shown in Table 2 respectively; Its grain size is as shown in Table 2:

[0032]

[0033] Combining the results of Table 1 and Table 2, it can be seen that the forging temperature is 1030°C or 1050°C, and the heat treatment system is 1038°C or 1060°C.

Embodiment 7

[0035] Two samples were randomly taken from each group of Haynes242 alloy forgings forged in Examples 1-5 and solution heat treated at 1038°C, 1060°C, 1080°C, and 1093°C respectively, and all samples were aged at 649°C for 48 hours. Afterwards, 649°C high-temperature tensile and 649°C durability tests were carried out, and two test materials were taken from each group for measurement. The results are shown in Table 3:

[0036] table 3

[0037]

[0038]

[0039] It can be seen from the results in Table 3 that the forgings subjected to solution heat treatment at 1038°C and 1060°C have the characteristics of high strength and poor plasticity; the forgings treated at 1093°C solution heat treatment have poor plasticity and low strength, while the Forgings subjected to solution heat treatment at 1080°C have better properties.

[0040] The forging samples after 1080°C×60min solution heat treatment and 649°C×48h aging heat treatment were subjected to 649°C high temperature comb...

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Abstract

The invention belongs to the field of ring rolling forming of aviation annular forgings, and particularly relates to a forging and heat treatment method of Haynes 242 alloy forge piece. The method comprises the steps that a Haynes 242 alloy blank is subjected to upsetting, punching, trestle chambering and finishing rolling under the condition of 1030-1120 DEG C, the deformation of the Haynes 242 alloy blank is made to be 20-40%, the Haynes 242 alloy forge pieces are obtained, and then the Haynes 242 alloy forge pieces are sequentially subjected to solid solution heat treatment and aging heat treatment. The Haynes 242 alloy forge pieces prepared through the method are uniform in grain structure and fine in grain size and have good high-temperature durability and mechanical property.

Description

technical field [0001] The invention belongs to the field of ring rolling forming of aviation ring forgings, in particular to a forging and heat treatment method for Haynes242 alloy forgings. Background technique [0002] Haynes 242 alloy is an age hardenable material that has excellent strength and ductility in the aged condition and good machinability in the annealed condition. Haynes242 alloy has a higher yield strength than typical solid solution strengthened nickel-based alloys (such as HASTELLOYS alloy), and it also has excellent ductility under fully heat-treated conditions. This translates into excellent sealing properties for gas turbine rings and casings, especially when combined with the low coefficient of expansion and excellent ductility after thermal expansion of the Haynes 242 alloy. Haynes242 alloy has excellent strength and ductility and can be used as a low temperature direct aging product. This, combined with its low thermal expansion, makes it an excell...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C22F1/10B21J5/00
CPCC22F1/10B21J5/002
Inventor 龚忠兴邹朝江王华东项春花王攀智赵泽敏张正吴永安杨家典
Owner GUIZHOU AVIATION TECHN DEV