A Method of Improving Microstructure Uniformity of gh4169 Disc Forging

A GH4169, uniform structure technology, applied in the field of forging thermal processing, can solve the problems of uneven structure of preform, affect the comprehensive performance of forgings, increase machining hours, etc., to shorten the forging process, reduce the input of raw materials, and avoid machining. The effect of billet process

Active Publication Date: 2022-04-19
AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The microstructure of GH4169 alloy is very sensitive to the thermal processing process. Improper process control can easily lead to uneven microstructures such as mixed grains and coarse grains, which will affect the overall performance of forgings.
The current forging process of GH4169 disc forgings is usually manufactured by upsetting cake + die forging. In the upsetting cake process, the upper and lower flat dies are used to vertically compress the cylindrical bar. Due to the friction between the upper and lower surfaces of the bar, the entire bar is deformed during compression. There is a very large difference in the deformation amount of each part, resulting in a dead zone of deformation on the upper and lower end faces or a small deformation zone and a large deformation zone in the center. The recrystallization degree of each part is very different, which leads to uneven structure of the preform. The uniform structure is further inherited into the forging, resulting in the uneven structure of the forging
To solve this problem, the domestic method usually used is to machine the billet after upsetting the cake, and adjust the deformation of each part of the forging during the die forging process. For disc forgings with large differences in plate and disc edge thickness, this method is difficult to apply. In addition, changing the shape of the blank through machining increases the machining man-hours, and at the same time increases the loss of materials, resulting in an increase in manufacturing costs; in order to improve the GH4169 alloy disc forging The uniformity of the overall structure, the hot die forging and isothermal forging forming methods have also been developed in China. The increase of the mold temperature can reduce the temperature drop during the forging process of the forging, promote lubrication, and improve the metal fluidity, but it still cannot change the upsetting cake. The problem of uneven deformation, and because the mold needs a long time to preheat, the manufacturing cycle is prolonged and the manufacturing cost is increased

Method used

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  • A Method of Improving Microstructure Uniformity of gh4169 Disc Forging

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Embodiment 3

[0038] An engine low-pressure turbine disc forging, such as figure 2 As shown, the weight of the forging is 170 kg, the outer dimension of the forging is about Φ580mm×120mm, and the size of the GH4169 alloy bar used is Φ230mm×520mm.

[0039] First, the design and manufacture of two sets of molds were completed, and the mold for billet making was designed. The upper mold cavity of the mold was "M" shaped, and the lower mold cavity was "W" shaped. The cavity was repeatedly optimized by numerical simulation. During the billet making process The minimum equivalent strain is about 0.25, and H13 steel is used to complete the blank mold processing; the final forging mold is designed, and the cavity is repeatedly optimized by numerical simulation. Processing of forging dies.

[0040]After spraying glass lubricant on the surface of the above-mentioned bar material, aluminum silicate fiber is used for soft sheathing, and then the bar material is heated to 1000°C by step-type heating m...

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Abstract

The invention belongs to the field of forging thermal processing, and specifically relates to a method for improving the uniformity of the structure of a GH4169 disc forging; the invention can realize forming by adopting two-fire forging, and the invention adopts an "M"-shaped upper mold cavity and a lower mold cavity It is in the shape of "W", the mold and the final forging die ensure that the minimum equivalent strain in the final forging process is not less than 0.25, and the billet is made by die forging. The forging temperature is controlled at 980 ° C ~ 1020 ° C, and the forging rate is controlled at 1 mm / s ~ 20 mm / s, the mold heating temperature is controlled at 300°C to 500°C; sand blowing and grinding are used to remove surface defects such as scale and forging cracks on the surface of the prefabricated billet; finally, the final forging of the disc forging is performed, and the forging temperature is controlled at 990°C to 1010°C. The forging rate is controlled at 0.5mm / s-5mm / s, and the mold heating temperature is ≥350°C; the method of the invention can effectively improve the uniformity of the structure of the GH4169 plate forging, and further improve the consistency of the performance of different parts of the forging.

Description

technical field [0001] The invention belongs to the field of forging thermal processing, and in particular relates to a method for improving the uniformity of the structure of a GH4169 disk forging. Background technique [0002] my country's advanced aero-engines use a large number of GH4169 alloys to manufacture key rotating discs such as compressor discs and turbine discs. The quality of the alloy disc forgings determines the safety of aero-engines to a certain extent. The microstructure of GH4169 alloy is very sensitive to the thermal processing process, and improper process control can easily lead to uneven microstructures such as mixed grains and coarse grains, which in turn affect the comprehensive performance of forgings. The current forging process of GH4169 disc forgings is usually manufactured by upsetting cake + die forging. In the upsetting cake process, the upper and lower flat dies are used to vertically compress the cylindrical bar. Due to the friction between...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B21J13/02B21J1/04B21J1/06B21J1/02B21J1/00B21J5/02B21K1/32
CPCB21J13/02B21J1/04B21J1/06B21J1/02B21J1/003B21J5/02B21K1/32
Inventor 王涛万志鹏姜嘉赢李钊韦康张勇
Owner AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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