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Forging method of 7-type AerMet100 ultrahigh-strength steel forge piece

A technology for ultra-high-strength steel and forgings, which is applied in the field of forging thermal processing, which can solve the problems of scrapped forgings, difficult operation, and low production efficiency, and achieve the effects of reducing forging times, reducing operation difficulty, and saving production costs

Pending Publication Date: 2022-03-25
SHAANXI HONGYUAN AVIATION FORGING
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The problems of this method are: in the process of bending and forming, special tooling is needed, and the operation is difficult, the number of fires is high, the R is prone to pinching, and the production efficiency is low.
For AerMet100 ultra-high-strength steel with multiple fires and small deformation, problems such as coarse grains and unqualified performance are likely to occur, resulting in the scrapping of forgings

Method used

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  • Forging method of 7-type AerMet100 ultrahigh-strength steel forge piece
  • Forging method of 7-type AerMet100 ultrahigh-strength steel forge piece
  • Forging method of 7-type AerMet100 ultrahigh-strength steel forge piece

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Embodiment Construction

[0026] In order to solve the above problems, a forging method of "7" type AerMet100 ultra-high strength steel forgings is provided, which is billet making + die forging; as Figure 3-5 , the method includes the following steps:

[0027] Step 1: Select the bar as the blank, and conduct a preliminary design on the cross-sectional area of ​​the billet rod. During the design, the cross-sectional area of ​​the blank should be ensured to be 1.1 to 1.25 times the sum of the cross-section of the forging and the burr. Step 2: Machining the distribution groove. The groove should not be too deep, and a smooth transition is required to avoid forging pinch.

[0028] The position of the material distribution groove is to select one end surface of the bar as a reference, and the length L offset to the other end surface of the bar is: the volume V of the long rod of the forging divided by 0.8 to 0.9 times the cross-sectional area S of the bar (L=V / (0.8~0.9)S, where: V is the volume of the ...

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Abstract

The invention belongs to the field of forging hot working, and relates to a forging method of a 7-shaped AerMet100 ultrahigh-strength steel forge piece. Comprising the following steps: step 1, selecting a bar as a blank, wherein the sectional area of the blank is 1.1-1.25 times of the sum of the sections of a forge piece and burrs; 2, a material distribution groove is machined, and the blank is divided into a head material and a rod material through the groove; 3, the blank is placed on a hammer anvil, and head material division is conducted with the groove as the boundary; eccentrically drawing out the rod part material, wherein one side face of the eccentric rod is flush with one side face of the head part; 4, after the blank is turned over by 90 degrees, head rods are distributed, and the head rods and the tips of the head rods are pressed; and 5, shaping the blank obtained in the step 4 to obtain a 7-shaped blank. And the qualified rate of products is improved.

Description

technical field [0001] The invention belongs to the field of forging thermal processing, and relates to a forging method of a "7" type AerMet100 ultra-high-strength steel forging. Background technique [0002] There are often some "7" type forgings with special shapes in aviation products, such as figure 1 As shown, the shape and structure of this type of forging is characterized by the long rod 1 having a large volume and using more materials, the head rod 2 being short and using less material, the long rod 1 and the head rod 2 form a certain angle θ, and the head 3 is relatively small. The head rod 2 is bulky. For this "7" type forging, at present, the traditional manufacturing process is to use billet + bending forming ( figure 2 , figure 2 The bending arrow in indicates the bending direction) + the method of die forging. The problems of this method are: in the bending forming process, special tooling is needed, and the operation is difficult, the fire is frequent, ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B21J5/00B21J5/06B21J5/02B21J1/04B21J3/00B21K3/00
CPCB21J5/002B21J5/06B21J5/02B21J1/04B21J3/00B21K3/00
Inventor 刘亚妮何健张拓燕陈飞张延珍
Owner SHAANXI HONGYUAN AVIATION FORGING
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