TiCB—Al seed alloy, manufacturing method thereof and heritable aluminum alloy
11629392 · 2023-04-18
Assignee
- Shandong University (Shandong, CN)
- SHANDONG MAIAOJING NEW MATERIALS COMPANY LIMITED (Shandong, CN)
- SHANDONG AL&MG MELT TECHNOLOGY COMPANY LIMTTED (Shandong, CN)
Inventors
- Xiangfa Liu (Jinan, CN)
- Jinfeng Nie (Linyi, CN)
- Qianqian Sun (Jinan, CN)
- Guiliang Liu (Linyi, CN)
- Mengxia Han (Jinan, CN)
Cpc classification
C22C1/1073
CHEMISTRY; METALLURGY
C22C1/1068
CHEMISTRY; METALLURGY
C22C1/1047
CHEMISTRY; METALLURGY
C22C21/003
CHEMISTRY; METALLURGY
International classification
Abstract
The present disclosure provides a TiCB—Al seed alloy, a manufacturing method thereof and a heritable aluminum alloy. The TiCB—Al seed alloy includes an Al matrix and TiC.sub.B@TiBC seed crystals dispersed on the Al matrix, wherein the TiC.sub.B@TiBC seed crystal comprises a core part and a shell part, the core part contains B-doped TiC.sub.B, and the shell part covers at least a part of the core part and contains a TiBC ternary phase, wherein the B-doped TiC.sub.B refers to a TiC.sub.B phase formed by B atoms occupying C vacancies in a TiC.sub.x crystal, and the TiBC ternary phase refers to a ternary phase composed of Ti, B and C, wherein x<1.
Claims
1. A TiCB—Al seed alloy, comprising an Al matrix and a plurality of TiC.sub.B@TiBC seed crystals dispersed on the Al matrix, wherein each TiC.sub.B@TiBC seed crystal comprises a core part and a shell part, the core part contains B-doped TiC.sub.B, and the shell part covers at least a part of the core part and contains a TiBC ternary phase, wherein the B-doped TiC.sub.B refers to a TiC.sub.B phase formed by B atoms occupying C vacancies in a TiC.sub.x crystal, and the TiBC ternary phase refers to a ternary phase composed of Ti, B and C, wherein x<1.
2. The TiCB—Al seed alloy of claim 1, wherein a content of C in the core part is higher than a content of C in the shell part, and a content of B in the core part is lower than a content of B in the shell part.
3. The TiCB—Al seed alloy of claim 1, wherein the B-doped TiC.sub.B is represented by TiC.sub.xB.sub.y, wherein 0.72<x<0.81, and 0<y<0.17.
4. The TiCB—Al seed alloy of claim 1, wherein a content of the plurality of TiC.sub.B@TiBC seed crystals is 0.08 wt % to 10.24 wt % based on 100 wt % of the TiCB—Al seed alloy.
5. The TiCB—Al seed alloy of claim 4, wherein a content of Ti is 0.06 wt % to 7.77 wt %, a content of C is 0.01 wt % to 1.30 wt %, and a content of B is 0.01 wt % to 1.17 wt % based on 100 wt % of the TiCB—Al seed alloy.
6. The TiCB—Al seed alloy of claim 1, wherein a morphology of each TiC.sub.B@TiBC seed crystal is different from those of a hexagonal sheet-like TiB.sub.2 crystal and an octahedral-like or tetrahedral-like TiC.sub.x crystal.
7. The TiCB—Al seed alloy of claim 6, wherein each TiC.sub.B@TiBC seed crystal is generally spherical and a diameter of the TiC.sub.B@TiBC seed crystal is between 50 nm and 800 nm.
8. A method of manufacturing a TiCB—Al seed alloy, comprising: (1) preparing 0.64 wt % to 75.00 wt % of an Al—Al.sub.3BC master alloy, 0.06 wt % to 7.77 wt % of a sponge titanium, and a balance of a commercial-purity aluminum, wherein a content of Al.sub.3BC in the Al—Al.sub.3BC master alloy is 3.0 wt % to 15.0 wt % of a total weight of the Al—Al.sub.3BC master alloy; (2) melting the commercial-purity aluminum and the Al—Al.sub.3BC master alloy and heating to 850° C. to 1300° C.; (3) adding the sponge titanium, and holding for 5 min to 60 min after the sponge titanium being dissolved to obtain a melt; and (4) pouring the melt to obtain the TiCB—Al seed alloy of claim 1.
9. An aluminum alloy, comprising α-Al and a plurality of TiC.sub.B@TiBC seed crystals, each TiC.sub.B@TiBC seed crystal having a core part and a shell part, wherein the core part contains a B-doped TiC.sub.B, and the shell part covers at least a part of the core part and contains a TiBC ternary phase, and wherein the B-doped TiC.sub.B refers to TiC.sub.B phase formed by B atoms occupying C vacancies in a TiC.sub.x crystal, and the TiBC ternary phase refers to a ternary phase composed of Ti, B, and C, where x<1.
10. The aluminum alloy of claim 9, wherein a content of the plurality of TiC.sub.B@TiBC seed crystals is 0.001 wt % to 5.120 wt % based on 100 wt % of the aluminum alloy, the aluminum alloy is an Al—Zn series alloy, and a content of Al is 60.0 wt %-98.9 wt %, a content of Zn is 1.0 wt %-10.0 wt %, and a content of Zr is 0.0 wt %-0.8 wt % based on 100 wt % of the heritable Al—Zn series alloy.
11. The aluminum alloy of claim 9, wherein a content of the plurality of TiC.sub.B@TiBC seed crystals is 0.001 wt % to 5.120 wt % based on 100 wt % of the aluminum alloy, the aluminum alloy is a heritable an Al—Si series alloy, and a content of Al is 60.0 wt %-99.5 wt %, and a content of Si is 0.4 wt %-13.0 wt % based on 100 wt % of the Al—Si series alloy.
12. The aluminum alloy of claim 10, wherein an average grain size of α-Al in the Al—Zn series alloy measured by a TP-1 standard method is between 20 μm and 150 μm.
13. The aluminum alloy of claim 11, an average grain size of α-Al in the Al—Si series alloy measured by a KBI ring mold method or the TP-1 standard method is between 35 μm and 250 μm.
14. The aluminum alloy of claim 12, wherein an average grain size of α-Al in a casting obtained after remelting the Al—Zn series alloy is smaller than the average grain size of α-Al in the heritable Al—Zn series alloy before remelting.
15. The aluminum alloy of claim 13, wherein an average grain size of α-Al in a casting obtained after remelting the Al—Si series alloy is smaller than the average grain size of α-Al in the Al—Si series alloy before prior to remelting.
16. The aluminum alloy of claim 14, wherein the average grain size of α-Al in the casting obtained by remelting the Al—Zn series alloy at 700° C. to 820° C. and holding for 15 min to 100 min is between 5 μm and 150 μm.
17. The aluminum alloy of claim 15, wherein the average grain size of α-Al in the casting obtained after remelting the Al—Si series alloy at 680° C. to 820° C. and holding for 15 min to 180 min is between 5 μm and 200 μm.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1) The patent or application file contains at least one drawing/photograph executed in color. Copies of this patent or patent application with color drawing(s)/photograph(s) will be provided by the Office upon request and payment of the necessary fee.
(2) The above and other aspects, features, and other advantages of the present disclosure will be more clearly understood from the following detailed description taken in conjunction with the accompanying drawings, in which:
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DETAILED DESCRIPTION
(11) Hereinafter, embodiments of the present disclosure will be described below with reference to the accompanying drawings.
(12) However, the present disclosure may be exemplified in many different forms and should not be construed as limited to the specific embodiments set forth herein. More specifically, these embodiments are provided so that the disclosure will be thorough and complete, and the scope of the present disclosure will be fully convey to those skilled in the art.
(13) It should be understood that when the terms “include(s)” and/or “contain(s)” are used in the specification, they list the presence of the stated materials and/or ingredients, but do not exclude the presence or addition of one or more other materials and/or ingredients.
(14) A TiCB—Al Seed Alloy
(15) Hereinafter, a TiCB—Al seed alloy according to an embodiment of the present disclosure is described with reference to
(16) The TiCB—Al seed alloy according to the embodiment of the present disclosure includes an Al matrix and TiC.sub.B@TiBC seed crystals dispersed on the Al matrix, the TiC.sub.B@TiBC seed crystal comprises a core part and a shell part, wherein the core part contains B-doped TiC.sub.B, and the shell part covers at least a part of the core part and contains a TiBC ternary phase, wherein the B-doped TiC.sub.B refers to a TiC.sub.B phase formed by B atoms occupying C vacancies in a TiC.sub.x crystal, and the TiBC ternary phase refers to a ternary phase composed of Ti, B and C, wherein x<1.
(17)
(18) As shown in
(19) In addition, it can be seen from
(20) This shows that the core part of the particle contains B-doped TiC.sub.B, which refers to the TiC.sub.B phase formed by B atoms occupying the C vacancy of TiC.sub.x (x<1 due to the presence of C vacancy in TiC.sub.x) crystal. The shell part of the particle contains TiBC ternary phase, which refers to the ternary phase composed of Ti, B and C. Therefore, the TiCB—Al seed alloy according to embodiments of the present disclosure includes TiC.sub.B@TiBC (core@shell) seed crystals.
(21) It should be understood that the B-doped TiC.sub.B and TiBC ternary phases are two completely different phases. B-doped TiC.sub.B is formed by B atoms occupying C vacancies in the TiC.sub.x crystal, and thus the B-doped TiC.sub.B still retains the crystal structure of the TiC.sub.x crystal. However, the TiBC ternary phase is a ternary phase composed of Ti, B and C, which does not have the crystal structure of TiC.sub.x, and thus it is different from crystal structure of TiC.sub.B.
(22) According to an embodiment of the present invention, the B-doped TiC.sub.B may be represented by TiC.sub.xB.sub.y, where 0.72<x<0.81, 0<y<0.17. Generally, a range of x in TiC.sub.x prepared according to a melt method satisfies 0.72<x<0.81. In addition, considering a maximum doping amount of B without destroying a lattice structure of TiC.sub.x, y according to the embodiment of the present disclosure satisfies 0<y<0.17.
(23) It should be understood that the present disclosure is only intended to prove the core-shell structure of the TiC.sub.B@TiBC seed crystal through
(24) According to the embodiment of the present disclosure, the content of the TiC.sub.B@TiBC seed crystals may be 0.08 wt % to 10.24 wt % based on 100 wt % of the TiCB—Al seed alloy. Alternatively, based on 100 wt % of the TiCB—Al seed alloy, the content of the TiC.sub.B@TiBC seed crystals may be 0.26 wt % to 2.90 wt %. Alternatively, based on 100 wt % of the TiCB—Al seed alloy, the content of the TiC.sub.B@TiBC seed crystals may be 1.12 wt % to 4.62 wt %. Alternatively, based on 100 wt % of the TiCB—Al seed alloy, the content of the TiC.sub.B@TiBC seed crystals may be 4.62 wt % to 10.24 wt %.
(25) In addition, according to the embodiment of the present disclosure, in the TiCB—Al seed alloy, based on 100 wt % of the TiCB—Al seed alloy, the content of Ti may be 0.06 wt % to 7.77 wt %, the content of C may be 0.01 wt % to 1.30 wt %, and the content of B may be 0.01 wt % to 1.17 wt %.
(26) Alternatively, based on 100 wt % of the TiCB—Al seed alloy, the content of Ti may be 0.2 wt % to 2.20 wt %, the content of C may be 0.03 wt % to 0.37 wt %, and the content of B may be 0.03 wt % to 0.33 wt %. Alternatively, based on 100 wt % of the TiCB—Al seed alloy, the content of Ti may be 0.85 wt % to 3.5 wt %, the content of C may be 0.14 wt % to 0.59 wt %, and the content of B may be 0.13 wt % to 0.53 wt %. Alternatively, based on 100 wt % of the TiCB—Al seed alloy, the content of Ti may be 3.50 wt % to 7.77 wt %, the content of C may be 0.59 wt % to 1.30 wt %, and the content of B may be 0.53 wt % to 1.17 wt %.
(27) According to an embodiment of the present disclosure, as shown in
(28) In addition, as shown in
(29)
(30) It should be understood that in
(31)
(32) As shown in
(33) A Preparation Method of the TiCB—Al Seed Alloy
(34) Hereinafter, a manufacturing method of the TiCB—Al seed alloy according to an embodiment of the present disclosure will be described. However, it should be understood that the TiCB—Al seed alloy according to the embodiment of the present disclosure is not limited by the manufacturing method described below, and the TiCB—Al seed alloy having the above-described TiC.sub.B@TiBC (core@ shell) structure manufactured by other methods is also within the scope of protection of the present disclosure.
(35) The method for manufacturing the TiCB—Al seed alloy according to the embodiment of the present disclosure includes: (1) preparing 0.64 wt % to 75.00 wt % of an Al—Al.sub.3BC master alloy, 0.06 wt % to 7.77 wt % of a sponge titanium, and a balance of a commercial-purity aluminum, wherein a content of Al.sub.3BC in the Al—Al.sub.3BC master alloy is 3.0 wt % to 15.0 wt % of a total weight of the Al—Al.sub.3BC master alloy; (2) melting the commercial-purity aluminum and the Al—Al.sub.3BC master alloy and heating to 850° C. to 1300° C.; (3) adding the sponge titanium, and holding for 5 min to 60 min after the sponge titanium being dissolved to obtain a melt; (4) pouring the melt to obtain the TiCB—Al seed alloy.
(36) In step (1), the Al—Al.sub.3BC master alloy may comprise Al and Al.sub.3BC, wherein Al.sub.3BC in the Al—Al.sub.3BC master alloy is 3.0 wt % to 15.0 wt % of the total weight of the Al—Al.sub.3BC master alloy, and the balance may be Al. In addition, it should be understood that the Al—Al.sub.3BC master alloy may also contain other impurity elements. As an example, the Al—Al.sub.3BC master alloy may be an Al—Al.sub.3BC master alloy produced by Shandong Al & Mg Melt Technology Co., Ltd., but the present disclosure is not limited thereto.
(37) In addition, the content of titanium in the sponge titanium may be 99.5 wt %, and the content of aluminum in the commercial-purity aluminum may be 99.7 wt %, but the present disclosure is not limited thereto.
(38) In step (2), the commercial-purity aluminum and the Al—Al.sub.3BC master alloy are added to, for example, a furnace for melting and are heated to 850° C. to 1300° C. In step (3), the sponge titanium is added after the temperature is stable to react with Al.sub.3BC. In order to dissolve the sponge titanium as soon as possible and promote the reaction, mechanical (or electromagnetic) stirring may be applied. The temperature is held for 5 min to 60 min after the sponge titanium is dissolved, so that the sponge titanium and Al.sub.3BC can fully react.
(39) In step (4), the fully reacted melt is casted into, for example, a cast iron mold to obtain the TiCB—Al seed alloy according to the embodiment of the present disclosure.
(40) According to the embodiment of the present disclosure, alternatively, in step (1), the content of the Al—Al.sub.3BC master alloy may be 2.1 wt % to 75.00 wt %, the content of the sponge titanium may be 0.2 wt % to 2.20 wt %, the heating temperature in step (2) may be 850° C. to 1100° C. and the holding time in step (3) may be 5 min to 40 min. Alternatively, in step (1), the content of the Al—Al.sub.3BC master alloy may be 8.93 wt % to 75.00 wt %, the content of the sponge titanium may be 0.85 wt % to 3.5 wt %, the heating temperature in step (2) may be from 950° C. to 1200° C. and the holding time in step (3) may be 10 min to 45 min. Alternatively, in step (1), the content of the Al—Al.sub.3BC master alloy may be 36.77 wt % to 75.00 wt %, the content of the sponge titanium may be 3.5 wt % to 7.77 wt %, the heating temperature in step (2) may be 1000° C. to 1300° C. and the holding time in step (3) may be 20 min to 60 min.
(41) Hereinafter, two specific examples of the manufacturing method of the TiCB—Al seed alloy according to the present disclosure and the prepared TiCB—Al seed alloy will be described with reference to
Example 1
(42) In Example 1, 30.0 wt % of Al-8.5Al.sub.3BC master alloy, 1.75 wt % of sponge titanium and a balance of the commercial-purity aluminum are prepared. Wherein, Al-8.5Al.sub.3BC master alloy means that Al.sub.3BC accounts for 8.5 wt % of the total weight of Al-8.5Al.sub.3BC master alloy. The commercial-purity aluminum and Al-8.5Al.sub.3BC master alloy are melted in a furnace and heated to 950° C. After the temperature is stable, the sponge titanium is added, mechanical (or electromagnetic) stirring is applied to ensure that the sponge titanium is dissolved gradually and reacts with Al.sub.3BC, and the temperature is held for 18 min. Then the melt obtained after the reaction is stirred evenly and poured into the cast iron mold to obtain the TiCB—Al seed alloy.
(43) As shown in
Example 2
(44) In Example 2, 40.0 wt % of Al-5Al.sub.3BC master alloy, 1.37 wt % of sponge titanium and a balance of the commercial-purity aluminum are prepared. Wherein, Al-5Al.sub.3BC master alloy means that Al.sub.3BC accounts for 5 wt % of the total weight of Al-5Al.sub.3BC master alloy. The commercial-purity aluminum and Al-5Al.sub.3BC master alloy are melted in a furnace and heated to 950° C. After the temperature is stable, the sponge titanium is added, mechanical (or electromagnetic) stirring is applied to ensure that the sponge titanium is dissolved gradually and reacts with Al.sub.3BC, and the temperature is held for 15 min. Then the melt obtained after the reaction is stirred evenly and poured into the cast iron mold to obtain the TiCB—Al seed alloy.
(45) As shown in
(46) Hereinafter, a comparison result of the refinement of α-Al in A356 (Si-containing aluminum alloy) by using the TiCB—Al seed alloy according to the present disclosure and a conventional Al-5Ti-1B master alloy will be described with reference to
(47) The TiCB—Al seed alloy shown in
(48) In the refinement experiment of A356 using the TiCB—Al seed alloy according to the present disclosure and the conventional Al-5Ti-1B master alloy, the A356 is melted firstly, 0.1 wt % of the TiCB—Al seed alloy or 0.1 wt % of the Al-5Ti-1B master alloy is added at 720° C. and held for a certain time (as shown in
(49) As shown in
(50) Therefore, the TiCB—Al seed alloy according to the present disclosure can solve the technical problem that the existing aluminum alloy refiner is prone to occur refinement “poisoning” caused by Si, and can achieve high-efficiency refinement without degradation for Al—Si series alloys.
(51) In addition, the TiCB—Al seed alloy according to the present disclosure has low cost, excellent and stable refinement effect. In addition, since the TiCB—Al seed alloy according to the embodiment of the present disclosure contains an Al matrix, it can be added to an aluminum alloy at a relatively low temperature to refine α-Al, so that it is easy to be applied to a production site.
(52) Although the application of the TiCB—Al seed alloy according to the present disclosure to A356 has been described above as an example, it should be understood that the TiCB—Al seed alloy according to the present disclosure can also be applied to other aluminum alloys (for example, 7050 ultra-high strength aluminum alloy and other Al—Si series alloys mentioned in the background) to refine α-Al, and a heritable aluminum alloy described below is also the case where the TiCB—Al seed alloy according to the present disclosure is applied to aluminum alloys to refine α-Al as crystal nucleus of α-Al.
(53) A Heritable Aluminium Alloy
(54) Hereinafter, a heritable aluminum alloy according to an embodiment of the present disclosure is described with reference to
(55) The heritable aluminum alloy according to the embodiment of the present disclosure includes α-Al and TiC.sub.B@TiBC seed crystals using as seed crystals of α-Al and including a core part and a shell part, wherein the core part contains a B-doped TiC.sub.B, and the shell part covers at least a part of the core part and contains a TiBC ternary phase, and wherein the B-doped TiC.sub.B refers to TiC.sub.B phase formed by B atoms occupying C vacancies in a TiC.sub.x crystal, and the TiBC ternary phase refers to a ternary phase composed of Ti, B, and C, where x<1.
(56) Different from the existence form of the TiC.sub.B@TiBC seed crystals dispersed on α-Al matrix in the TiCB—Al seed alloy, the TiC.sub.B@TiBC seed crystals in the heritable aluminum alloy act as (basically act as due to the process error) the seed crystals of α-Al, rather than dispersing on the α-Al matrix.
(57) Since the TiC.sub.B@TiBC seed crystals have been described in detail above, detailed description will not be made herein in order to avoid redundancy.
(58) According to the embodiment of the present disclosure, a content of the TiC.sub.B@TiBC seed crystals may be 0.001 wt % to 5.120 wt % based on 100 wt % of the heritable aluminum alloy. Alternatively, the content of the TiC.sub.B@TiBC seed crystals may be 0.001 wt % to 2.120 wt % based on 100 wt % of the heritable aluminum alloy. Alternatively, the content of the TiC.sub.B@TiBC seed crystal may be 0.1 wt % to 1.0 wt % based on 100 wt % of the heritable aluminum alloy. Alternatively, the content of the TiC.sub.B@TiBC seed crystals may be 2.0 wt % to 4.0 wt % based on 100 wt % of the heritable aluminum alloy. Alternatively, the content of the TiC.sub.B@TiBC seed crystal may be 2.5 wt % to 5.120 wt % based on 100 wt % of the heritable aluminum alloy.
(59) According to one embodiment of the present disclosure, the heritable aluminum alloy may be a heritable Al—Zn series alloy. Based on 100 wt % of the heritable Al—Zn series alloy, a content of Al may be 60.0 wt % to 98.9 wt %, a content of Zn may be 1.0 wt % to 10.0 wt %, and a content of Zr may be 0.0 wt % to 0.8 wt %. In addition, the heritable Al—Zn series alloy may further contain at least one of Mg, Cu, Si, Mn, Ni, Fe, Ti, and Cr.
(60) According to the embodiment of the present disclosure, an average grain size of α-Al in the heritable Al—Zn series alloy measured using a TP-1 standard method (standard measurement method known in the art) is between 20 μm and 150 μm.
(61) According to the embodiment of the present disclosure, an average grain size of α-Al in a casting obtained after remelting the heritable Al—Zn series alloy is smaller than the average grain size of α-Al in the heritable Al—Zn series alloy before remelting. This is because the TiC.sub.B@TiBC seed crystals can be directly used as the nucleus of α-Al without assistance of TiAl.sub.3 or a titanium-rich layer, which overcomes a poisoning influence of Zr element in the melt, so the casting obtained after remelting and casting have finer α-Al grain structure, even ultra-fine grain structure.
(62) According to the embodiment of the present disclosure, the average grain size of α-Al in the casting obtained by remelting the heritable Al—Zn series alloy at 700° C. to 820° C. and holding for 15 min to 100 min is between 5 μm and 150 μm.
(63) According to another embodiment of the present disclosure, the heritable aluminum alloy may be a heritable Al—Si series alloy. Based on 100 wt % of the heritable Al—Si series alloy, a content of Al may be 60.0 wt % to 99.5 wt %, and a content of Si may be 0.4 wt % to 13.0 wt %. In addition, the heritable Al—Si series alloy may further comprise at least one of Mg, Cu, Zn, Mn, Ni, Fe, Ti, Cr, and Zr.
(64) According to the embodiment of the present disclosure, an average grain size of α-Al in the heritable Al—Si series alloy measured using the KBI ring mold method or the TP-1 standard method is between 35 μm and 250 μm.
(65) According to the embodiment of the present disclosure, an average grain size of α-Al in a casting obtained after remelting the heritable Al—Si series alloy is smaller than the average grain size of α-Al in the heritable Al—Si series alloy before remelting. This is because the TiC.sub.B@TiBC seed crystals can be directly used as the nucleus of α-Al without assistance of TiAl.sub.3 or a titanium-rich layer, which overcomes a poisoning influence of Si element in the melt, so the casting obtained after remelting have finer α-Al grain structure, even ultra-fine grain structure.
(66) According to the embodiment of the present disclosure, the average grain size of α-Al in the casting obtained after remelting the heritable Al—Si series alloy at 680° C. to 820° C. and holding for 15 min to 180 min is between 5 μm and 200 μm.
(67) Although the heritable Al—Zn series alloy and the heritable Al—Si series alloy have been described above as two specific examples of the heritable aluminum alloys, the present disclosure is not limited thereto. The heritable aluminum alloy of the present disclosure may also comprise other series of aluminum alloys.
(68) In addition, the heritable aluminum alloy according to the present disclosure can be manufactured by melting a corresponding proportion of pure aluminum and the TiCB—Al seed alloy to a certain temperature (for example, 700° C. to 850° C.) in a holding furnace or an induction furnace, adding raw materials corresponding to elements contained in corresponding heritable aluminum alloy to be completely dissolved, and pouring to obtain the heritable aluminum alloy according to the present disclosure.
(69) According to the present disclosure, when the heritable aluminum alloy (for example, the heritable Al—Zn series alloy or the heritable Al—Si series alloy), for example, having ultra-fine grain, prepared by using the TiCB—Al seed alloy is applied to industrial production, it is only need to remelt the heritable aluminum alloy of the present disclosure and it is not need to add a refiner or perform a melt treatment technology related to grain refinement (for example, it is not need to add the TiCB—Al seed alloy according to the present disclosure to the aluminum alloy for refinement treatment), and a casting obtained by remelting the heritable aluminum alloy of the present disclosure can obtain an ultra-fine grain structure, and thus the heritable aluminum alloy of the present disclosure can be simply and efficiently applied to industrial production.
(70) Hereinafter, three specific examples of the heritable aluminum alloy according to the present disclosure are described.
Example 3
(71)
(72) The heritable Al—Zn series alloy according to Example 3 includes 6.0 wt % of Zn, 0.15 wt % of Zr, 2.3 wt % of Mg, 2.2 wt % of Cu, 0.12 wt % of Si, 0.15 wt % of Fe, 0.1 wt % of Mn, 0.06 wt % of Ti, 0.04 wt % of Cr, 0.8 wt % of TiC.sub.B@TiBC seed crystal and a balance of Al. An average grain size of α-Al in an as-cast alloy measured by the TP-1 standard method is 39 μm, as shown in
(73) An average grain size of α-Al in an alloy casting obtained by remelting the heritable Al—Zn series alloy of
(74) In addition, the heritable Al—Zn series alloy in Example 3 contains Zr, and even in this case, the heritable Al—Zn series alloy can obtain an ultra-fine grain structure with the average grain size of 25 μm after remelting and holding for 60 min (a relatively long holding time). Therefore, it can be confirmed by Example 3 that the TiCB—Al seed alloy according to the present disclosure can solve the technical problem that the existing aluminum alloy refiner is prone to occur refinement “poisoning” caused by Zr, and can realize efficient refinement of Zr-containing aluminum alloy without degradation (the heritable Al—Zn series alloy may still have an ultra-fine grain structure after holding for 60 min and thus the refinement effect does not degrade).
Example 4
(75)
(76) The heritable Al—Si series alloy according to Example 4 includes 6.5 wt % of Si, 0.4 wt % of Mg, 0.01 wt % of TiC.sub.B@TiBC seed crystals, and a balance of Al. An average grain size of α-Al in an as-cast alloy measured by the KBI ring mold method is 123 μm, as shown in
(77) An average grain size of α-Al in an alloy casting obtained by remelting the heritable Al—Si alloy of
Example 5
(78)
(79) The heritable Al—Si series alloy according to Example 5 includes 0.8 wt % of Si, 1.0 wt % of Mg, 0.25 wt % of Cu, 0.6 wt % of Fe, 0.25 wt % of Zn, 0.15 wt % of Mn, 0.15 wt % of Ti, 0.2 wt % of Cr, 0.008 wt % of TiC.sub.B@TiBC seed crystals, and a balance of Al. An average grain size of α-Al in an as-cast alloy measured by the TP-1 standard method is 79 μm, as shown in
(80) An average grain size of α-Al in an alloy casting obtained by remelting the heritable Al—Si alloy of
(81) According to the heritable Al—Si series alloys of Examples 4 and 5, even after remelting and holding for 120 min (Example 4) or 100 min (Example 5), an ultra-fine grain structure with an average grain size of 84 μm (Example 4) or 62 μm (Example 5) of α-Al can be obtained. Therefore, it can be confirmed by Examples 4 and 5 that the TiCB—Al seed alloy according to the present disclosure can solve the technical problem that the existing aluminum alloy refiner is prone to occur refinement “poisoning” caused by Si, and can realize efficient refinement of Si-containing aluminum alloy without degradation (the heritable Al—Si series alloy may still have an ultra-fine grain structure after holding for a relatively long time (120 min or 100 min) and thus the refinement effect does not degrade).
(82) According to the embodiments of the present disclosure described above, the following technical effects can be achieved, but the technical effects are not limited thereto.
(83) According to the present disclosure, the TiCB—Al seed alloy can solve the technical problem that the existing aluminum alloy refiner is prone to occur refinement “poisoning” caused by Zr and Si, can realize efficient refinement of Zr-containing or Si-containing aluminum alloy without degradation, and the fine grain structure of the refined aluminum alloy can be inherited after remelting.
(84) According to the present disclosure, the TiCB—Al seed alloy has low cost and has excellent and stable refinement effect. In addition, since the TiCB—Al seed alloy according to the embodiment of the present disclosure contains an Al matrix, it can be added to an aluminum alloy at a relatively low temperature to refine α-Al, so that it is easy to be applied to a production site.
(85) According to the present disclosure, when the heritable aluminum alloy (for example, the heritable Al—Zn series alloy or the heritable Al—Si series alloy), for example, having ultra-fine grain, prepared by using the TiCB—Al seed alloy is applied to industrial production, it is only need to remelt the heritable aluminum alloy of the present disclosure and it is not need to add a refiner or perform a melt treatment technology related to grain refinement, and a casting obtained by remelting and casting the heritable aluminum alloy of the present disclosure can obtain an ultra-fine grain structure, and thus the heritable aluminum alloy of the present disclosure can be simply and efficiently applied to industrial production.
(86) Although some embodiments of the present disclosure have been shown and described, those skilled in the art should appreciate that modifications may be made to these embodiments without departing from the principles and spirit of the present disclosure, the scope of which is defined by the claims and their equivalents.