METHOD FOR FORMING AMORPHOUS ALLOY PART
20170259331 · 2017-09-14
Inventors
- Haifeng ZHANG (Shenyang, CN)
- Huameng FU (Shenyang, CN)
- Zhengwang ZHU (Shenyang, CN)
- Aimin WANG (Shenyang, CN)
- Hong LI (Shenyang, CN)
- Hongwei ZHANG (Shenyang, CN)
- Yangde LI (Dongguan, CN)
- Weirong LI (Dongguan, CN)
- Tiezhuang TANG (Dongguan, CN)
- Jiedan YANG (Dongguan, CN)
Cpc classification
B22D17/00
PERFORMING OPERATIONS; TRANSPORTING
B22D17/02
PERFORMING OPERATIONS; TRANSPORTING
B22D41/005
PERFORMING OPERATIONS; TRANSPORTING
International classification
B22D41/005
PERFORMING OPERATIONS; TRANSPORTING
B22D17/02
PERFORMING OPERATIONS; TRANSPORTING
B22D17/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for forming an amorphous alloy part, including: placing a master alloy on a melting platform; heating and melting the master alloy under vacuum to yield an alloy melt; stopping heating and allowing the alloy melt to cool to a temperature between a glass transition temperature and a liquidus temperature thereof; and press-forming and cooling the alloy melt, to form the amorphous alloy part.
Claims
1. A method for forming an amorphous alloy part, the method comprising: 1) placing a master alloy on a melting platform; 2) heating and melting the master alloy under vacuum to yield an alloy melt; 3) stopping heating and allowing the alloy melt to cool to a temperature between a glass transition temperature and a liquidus temperature thereof; and 4) press-forming and cooling the alloy melt, to form the amorphous alloy part.
2. The method of claim 1, wherein the master alloy is prepared by smelting or casting; the master alloy is in a shape of rod, plate, flake, or sphere; and a weight of the master alloy is determined by a shape and a size of the amorphous alloy part.
3. The method of claim 1, wherein the vacuum is a pressure of between 1×10.sup.−6 and 1×10.sup.−1 Pa.
4. The method of claim 1, wherein the melting platform does not react with the master alloy and has no influence on melting and solidification of the master alloy.
5. The method of claim 1, wherein a heating mode of the master alloy is electric arc heating, induction heating, resistance heating, laser heating, plasma heating, infrared heating, or microwave heating.
6. The method of claim 1, wherein in 4), a cooling rate of the alloy melt is between 10.sup.−2 and 10.sup.2 K/min.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0019] The invention is described hereinbelow with reference to the accompanying drawings, in which:
[0020]
[0021]
[0022]
[0023]
[0024] In
DETAILED DESCRIPTION OF THE EMBODIMENTS
[0025] For further illustrating the invention, experiments detailing a method for forming an amorphous alloy part are described below. It should be noted that the following examples are intended to describe and not to limit the invention.
[0026] As shown in
Example 1
[0027] The shaping process of amorphous alloy part in the example is as follows:
[0028] 1. Composition of the master alloy (atomic percentage): 32.8% of Titanium, 30.2% of Zirconium, 5.3% of Nickel, 9% of Copper, and 22.7% of Beryllium.
[0029] 2. Melting the master alloy: the material of the master alloy is prepared and is placed in a crucible. Air is exhausted to form a vacuum at a pressure of between 5×10.sup.−3 and 5×10.sup.−1 Pa (or inert gas is filled in). The master alloy with uniform composition are prepared by induction melting or electric arc melting. The master alloy is casted to form regular master alloy ingot (in the shape of rod, plate, or flake, etc.)
[0030] 3. Cutting the master alloy: the casted master alloy ingot is cut using cutting equipment according to the weight of required amorphous alloy part.
[0031] 4. Shaping and processing amorphous alloy part: the cut master alloy is placed on a melting platform. Air in the vacuum chamber is exhausted to form a vacuum at a pressure of between 1×10.sup.−3 and 1×10.sup.−1 Pa (or inert gas is filled in). The master alloy is heated and melted by induction heating (or other heating modes such as electric arc heating, laser heating, etc.) to yield an alloy melt. Heating is stopped and the alloy melt is freely cooled to a temperature which is 20° C. higher than the melting temperature (in the temperature range between a glass transition temperature (Tg) and a liquidus temperature (Tl) of the amorphous alloy). The alloy melt is pressed using the mold until the mold cannot further move to contact the melting platform (or a specialized shaping platform in which the alloy melt is poured following the melting). Meanwhile, the alloy melt is quickly cooled to form the amorphous alloy part as shown in
Example 2
[0032] The example follows a basic process in Example 1, except that composition of the master alloy (atomic percentage) is: 54.73% of Zirconium, 29.75% of Copper, 4.97% of Nickel, 9.95% of Aluminum, 0.1% of Silver, and 0.5% of Yttrium. The amorphous alloy part prepared in the example is shown in
[0033] As shown in
[0034] The alloy used in the embodiments of the invention can be any amorphous alloy, such as Titanium-based amorphous alloy, Zirconium-based amorphous alloy, Iron-based amorphous alloy, Nickel-based amorphous alloy, Magnesium-based amorphous alloy, Palladium-based amorphous alloy, Silver-based amorphous alloy, Hafnium-based amorphous alloy, Platinum-based amorphous alloy, or other amorphous alloy component of other system.
[0035] Unless otherwise indicated, the numerical ranges involved in the invention include the end values. While particular embodiments of the invention have been shown and described, it will be obvious to those skilled in the art that changes and modifications may be made without departing from the invention in its broader aspects, and therefore, the aim in the appended claims is to cover all such changes and modifications as fall within the true spirit and scope of the invention.