WO2016158462A1

WO2016158462A1 - Forging method

Info

Publication number: WO2016158462A1
Application number: PCT/JP2016/058547
Authority: WO
Inventors: 幸夫米田; 努棚橋; 登林; 伸幸竹原; 大毅松本
Original assignee: 本田技研工業株式会社; Ｔｈｋリズム株式会社; 株式会社戸畑タ－レット工作所
Priority date: 2015-04-02
Filing date: 2016-03-17
Publication date: 2016-10-06
Also published as: JPWO2016158462A1; DE112016001543T5; CN107427898B; JP6371468B2; CN107427898A; DE112016001543B4; US20180105909A1

Abstract

The problem addressed by the present invention is to provide a forging method that can increase the strength of the forged product and suppress reductions in hardness in the usage environment. The forging method includes a warm forging step (S105) for warm forging a metal workpiece that has been solution treated, and an artificial aging step (S106), following the warm forging step (S105), for artificial preliminary aging of the workpiece at a temperature the same or greater than the temperature of the usage environment after the workpiece is manufactured. The equivalent plastic strain before and after warm forging is set at 0.1 - 2.5.

Description

Forging method

The present invention relates to a forging method.

In recent automobile development, development of lightweight and high-strength members is being promoted in order to improve fuel efficiency. For example, Patent Document 1 discloses a technique for manufacturing a forged product made of an aluminum alloy by warm forging in order to increase the strength of the forged product (see Patent Document 1).

JP 2010-137284 A

However, if the forged product is left as it is after forging in the warm state, the forged product may change over time and the hardness may not be stabilized under the usage environment of the vehicle.

Therefore, an object of the present invention is to provide a forging method that increases the strength of a forged product and suppresses a decrease in hardness under a use environment.

As means for solving the above-mentioned problems, the present invention provides a warm forging process in which a solution-treated metal workpiece is warm-forged at a recrystallization temperature or lower, and a use after manufacturing after the warm-forging process. And an artificial aging step for artificially pre-aging the workpiece at a temperature equal to or higher than the environmental temperature.

Here, the warm forging means that the workpiece is forged using a mold in a heated state and at a temperature equal to or lower than a temperature at which the structure of the metal workpiece is recrystallized (recrystallization temperature). .

According to such a configuration, it is possible to suppress the change in hardness during use after manufacture while increasing the strength of the forged product (workpiece) by precipitation strengthening by artificial aging, and therefore it is difficult for the forged product to change over time. .

In the warm forging step, the equivalent plastic strain before and after the warm forging is preferably 0.1 to 2.5.

Here, the equivalent plastic strain before and after forging is calculated by, for example, CAE (Ccomputer Aided Engineering) analysis.

Further, in the warm forging step, the equivalent plastic strain before and after the warm forging is preferably set to 0.4 to 2.1.

According to the present invention, it is possible to provide a forging method that increases the strength of a forged product and suppresses the change over time in the use environment.

It is process drawing of the forging method which concerns on this embodiment. It is a figure which shows the tie rod which is an example of the workpiece | work in the forging method which concerns on this embodiment, (a) is after a cutting | disconnection, (b) is after cold forging (preformation), (c) is after warm forging, d) shows after deburring. It is a microscope picture of the workpiece | work of equivalent plastic strain 0.42. It is a microscope picture of the workpiece | work of the equivalent plastic distortion 1.39. It is a microscope picture of the workpiece | work of equivalent plastic strain 2.07. It is a microscope picture of the workpiece | work of equivalent plastic strain 2.66. It is a graph which shows one effect of the forging method which concerns on this embodiment, and has shown the relationship between a rolling reduction and elongation. It is a graph which shows one effect of the forging method concerning this embodiment, and has shown relation between distortion and tensile strength. It is a graph which shows one effect of the forging method concerning this embodiment. It is a graph which shows one effect of the forging method concerning this embodiment, and has shown relation between use time and hardness. It is a graph which shows one effect of the forging method concerning a comparative example, and has shown relation between use time and hardness.

An embodiment of the present invention will be described with reference to FIGS.

As shown in FIG. 1, the forging method according to this embodiment includes a warm forging step (S105) in which a workpiece 10 is formed by warm forging, a forged product having high strength, and a product that is used in a vehicle use environment. An artificial aging step (S106) for artificially pre-aging the workpiece 10 after warm forging so as not to change with time. Here, a case where the workpiece 10 is made of an aluminum alloy is illustrated.

Further, here, as shown in FIG. 2, a case where the workpiece 10 is a generally rod-shaped tie rod that steers a knuckle that rotatably supports a wheel is illustrated. Accordingly, the manufactured workpiece 10 (tie rod) includes a hemispherical boss portion 11 that fits outside the knuckle ball joint, a round rod-like shaft portion 12 that is connected to the actuator side rod, the boss portion 11 and the shaft portion. 12 and a neck 13 formed between the two.

The outer diameter of the workpiece 10 is generally reduced in the order of the shaft portion 12, the boss portion 11, and the neck portion 13. These equivalent plastic strains are equivalent to the equivalent plastic strain of the shaft portion 12 (0.2 etc.), the equivalent plastic strain of the boss portion 13 (0.9 etc.), based on the workpiece 10 before strain (before forging), The equivalent plastic strain (2.2 etc.) of the neck 11 increases in the order (see FIG. 9).

<Cutting step, S101>
In step S101, an appropriately sized workpiece 10 is cut out from an aluminum alloy material (see FIG. 2A).

<Cold forging process, S102>
In step S102, the cut workpiece 10 is cold-forged and preformed (see FIG. 2B). Cold forging refers to forging the workpiece 10 at a temperature lower than the recrystallization temperature of the aluminum alloy and at a lower temperature (for example, lower than room temperature (about 25 ° C.)).

<Solution process, S103>
In step S103, the workpiece 10 after cold forging is subjected to a solution treatment. Specifically, the workpiece 10 is heated to a solution treatment temperature (for example, 540 ° C.) using an appropriate furnace so that the alloy components are dissolved in the workpiece 10 to facilitate aging precipitation and distortion due to cold forging. Eliminate.

<Warm heating process, S104>
In step S104, the workpiece 10 after the solution treatment is heated to a warm temperature for warm forging. The warm heating temperature is set to normal temperature or higher and lower than the recrystallization temperature. Specifically, in this embodiment, since the workpiece 10 is made of an aluminum alloy, the warm heating temperature is set to, for example, 100 ° C. to the recrystallization temperature or less.

<Warm forging process, S105>
In step S105, the workpiece 10 heated to a warm temperature (below the recrystallization temperature) is warm forged (see FIG. 2C).

In warm forging, the equivalent plastic strain of the workpiece 10 in the forging direction (compression direction) is set in the normal range of 0.1 to 2.5.

This is because the tensile strength of the workpiece 10 after production decreases when the equivalent plastic strain becomes higher than 2.5. This is because, when the equivalent plastic strain is higher than 2.5, a part of the dislocation structure generated by forging becomes a cell (recrystallization process) (see FIG. 6).

Here, as shown in FIG. 8, the equivalent plastic strain is preferably in a suitable range of 0.1 to 2.1 (see FIGS. 3, 4, and 5). Further, the equivalent plastic strain is preferably in the optimum range of 0.4 to 2.1. This is because the tensile strength is improved satisfactorily.

As shown in FIG. 8, when the equivalent plastic strain is increased, the dislocation density in the workpiece 10 is gradually increased, and the tensile strength is also gradually increased.

As shown in FIG. 7, when the equivalent plastic strain increases, the elongation (%) of the workpiece 10 after manufacture tends to decrease. In addition, when elongation becomes small, the toughness of the workpiece | work 10 will become low and the workpiece | work 10 will become weak. The range of tensile strength of a general aluminum alloy hot forged product is about “285 to 385 MPa. In the present invention, even when the equivalent plastic strain is around 0.1, the hot forging of a general aluminum alloy is performed. It can be seen that it has a tensile strength near the upper limit value (see FIG. 8).

<Artificial aging process, S106>
In step S106, the workpiece 10 after warm forging is artificially aged. Specifically, the workpiece 10 is artificially aged in advance at a predetermined artificial aging temperature and a predetermined artificial aging time so that the product (workpiece 10) does not change over time during use after manufacturing.

The predetermined artificial aging temperature is set to a temperature equal to or higher than the operating environment temperature to which the product (work 10) after manufacture is exposed. This is because the change over time of the product (workpiece 10) during use after manufacture can be reduced. For example, when the manufactured product (workpiece 10) is a tie rod, the predetermined artificial aging temperature is set to 150 to 200 ° C. (see FIG. 10).

The predetermined artificial aging time is determined by a preliminary test or the like, and is set as short as possible within a range that does not change with time after manufacture.

<Deburring (trimming) process>
In step S107, the workpiece 10 after artificial aging is deburred (trimmed) (see FIG. 2D). Specifically, the burr 14 of the workpiece 10 formed by warm forging is cut off.

<Finishing process>
In step S108, the workpiece 10 after deburring is finished. Specifically, for example, the surface of the workpiece 10 is polished and cleaned.

Such a forging method can increase the hardness of the workpiece 10 by artificially aging the workpiece 10 after warm forging (see FIG. 9). That is, since the work 10 is artificially aged, the hardness of the product (work 10) does not change and does not decrease during use after manufacture (see FIG. 10).

On the other hand, when artificial aging is not performed after warm forging and the product is used as it is, a change with time progresses during use of the product (workpiece 10), and the hardness of the product may change without stability (FIG. 9 Comparative example, see FIG. 11).

As mentioned above, although one Embodiment of this invention was described, this invention is not limited to this, It can change suitably.

In the above-described embodiment, the configuration in which the workpiece 10 is made of an aluminum alloy is exemplified, but a configuration in which other types of metals are used may be used.

10 Workpiece 11 Boss part 12 Shaft part 13 Neck part 14 Boss part

Claims

A warm forging process in which a solution-treated metal workpiece is warm-forged at a temperature below the recrystallization temperature;
After the warm forging step, an artificial aging step for artificially pre-aging the workpiece at a temperature equal to or higher than the use environment temperature after production,
The forging method characterized by including.
The forging method according to claim 1, wherein, in the warm forging step, the equivalent plastic strain before and after the warm forging is set to 0.1 to 2.5.
The forging method according to claim 1, wherein, in the warm forging step, an equivalent plastic strain before and after the warm forging is set to 0.4 to 2.1.