CN109913733B - High-corrosion-resistance Ti40-xCu40Al20GdxPreparation method of flame-retardant alloy - Google Patents

High-corrosion-resistance Ti40-xCu40Al20GdxPreparation method of flame-retardant alloy Download PDF

Info

Publication number
CN109913733B
CN109913733B CN201910274017.9A CN201910274017A CN109913733B CN 109913733 B CN109913733 B CN 109913733B CN 201910274017 A CN201910274017 A CN 201910274017A CN 109913733 B CN109913733 B CN 109913733B
Authority
CN
China
Prior art keywords
flame
alloy
retardant
corrosion
retardant alloy
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201910274017.9A
Other languages
Chinese (zh)
Other versions
CN109913733A (en
Inventor
董桂馥
苏康
王通
张倩倩
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dalian University
Original Assignee
Dalian University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dalian University filed Critical Dalian University
Priority to CN201910274017.9A priority Critical patent/CN109913733B/en
Publication of CN109913733A publication Critical patent/CN109913733A/en
Application granted granted Critical
Publication of CN109913733B publication Critical patent/CN109913733B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Manufacture And Refinement Of Metals (AREA)
  • Investigating And Analyzing Materials By Characteristic Methods (AREA)

Abstract

The inventionRelates to a preparation method of flame-retardant alloy, in particular to high-corrosion-resistance Ti40‑xCu40Al20GdxA preparation method of the flame-retardant alloy. The invention is firstly adopted in Ti2Cu2A proper amount of rare earth Gd element is added into the Al flame-retardant alloy to synthesize novel Ti with high corrosion resistance40‑xCu40Al20Gdx(x is 0, 0.1, 0.2, 0.5, 1) flame-retardant alloy, and the idea is expanded for the application of the shape memory alloy with high corrosion resistance. Highly corrosion-resistant Ti of the present invention40‑xCu40Al20The Gdx flame-retardant alloy is prepared by the following steps: taking, weighing and smelting according to atomic percent to obtain the Ti with high corrosion resistance40‑xCu40Al20GdxA flame retardant alloy. Ti prepared by the invention40‑xCu40Al20GdxThe flame-retardant alloy has the advantage of corrosion resistance.

Description

High-corrosion-resistance Ti40-xCu40Al20GdxPreparation method of flame-retardant alloy
Technical Field
The invention relates to high-corrosion-resistance Ti40-xCu40Al20Gdx(x ═ 0, 0.1, 0.2, 0.5, 1) a method for producing a flame-retardant alloy.
Background
The titanium alloy has the advantages of small density, high strength, high temperature resistance, good corrosion resistance and the like, and is widely applied to the field of aerospace. The titanium material yield of China is in the fourth world, but the yield of the high-end titanium material for aerospace only accounts for about 10% of the total amount, and has a gap with the level of 50% of the world, so that innovative research on comprehensive high-performance titanium alloy materials and application needs to be enhanced, and the application level and the dosage of the aerospace titanium alloy are improved. The development of titanium alloy materials with high comprehensive performance and the low-cost manufacturing technology are two major driving forces for expanding the application of titanium alloys. When the titanium alloy is used as an aircraft engine material, the common titanium alloy may generate titanium fire, and in order to solve the problem, research and development of flame-retardant titanium alloy are carried out in various countries. A large number of researches find that the flame-retardant titanium alloy mainly has two systems, namely a Ti-V-Cr system; second, Ti-Al-Cu system. Compared with Ti-Al-Cu system, the Ti-V-Cr system flame-retardant titanium alloy has better comprehensive mechanical property, and the Ti-V-Cr system flame-retardant titanium alloy has been successfully applied to an F119 engine, but is expensive. With Ti2V2Cr series flame-retardant titanium alloy, Ti2Cu2The Al series flame-retardant titanium alloy has poor comprehensive mechanical property and low working temperature. Accordingly, there is a need in the art for flame retardant alloys having high corrosion resistance.
Disclosure of Invention
To solve the existing Ti2Cu2The problem of low corrosion resistance of Al series magnetic memory alloy is solved by the invention that Ti is used as the material2Cu2Adding trace rare earth element Gd into Al series alloy, and preparing a novel Ti with high corrosion resistance by utilizing a vacuum intermediate frequency smelting furnace40- xCu40Al20Gdx(x ═ 0, 0.1, 0.2, 0.5, 1) a new method of flame retarding alloys.
The invention has the following inventive concept: by reaction at Ti2Cu2The Al-series alloy is added with trace rare earth element Gd, so that the strength and the shaping of the alloy can be obviously improved, and meanwhile, the rare earth element plays a role in purifying the crystal boundary of the alloy. Remarkably improve Ti2Cu2The comprehensive performance of the Al-based flame-retardant titanium alloy. This is at Ti2Cu2The Al series flame-retardant titanium alloy has never been reported, and can become a new material for the application and development of the flame-retardant titanium alloy.
Ti of the invention40-xCu40Al20GdxThe flame-retardant alloy is prepared by the following method: taking 40-x parts of Ti, 40 parts of Cu, 20 parts of Al and x (x is 0, 0.1, 0.2, 0.5, 1) parts of rare earth element Gd according to atomic percent, putting the raw materials in a vacuum intermediate frequency induction smelting furnace in the following sequence: firstly placing rare Gd, then placing Cu and Al sheets, finally placing sponge Ti element on the uppermost layer of the smelting furnace, and closing a side furnace door. Before smelting, the mixture is pumped by a mechanical pump and a Roots pump to be vacuum of 6.67 multiplied by 10- 3Pa, and then charging high-purity inert gas to 100 Pa. And starting smelting, and controlling the smelting power not to be higher than 500 Kw. Due to the smelting principle of medium-frequency induction, molten metal can flow and be stirred under the action of an electromagnetic field. Pouring the molten metal liquid into a rod-shaped mold after the molten metal liquid is fully and uniformly mixed to obtain a rod-shaped sample with the diameter of phi 10mm multiplied by 60mm, and taking out the rod-shaped sample after cooling to obtain the Ti with high corrosion resistance40-xCu40Al20GdxA flame retardant alloy.
Further, the inert gas is argon or nitrogen. Argon is preferred.
Preferably, x is 1, to obtain alloy Ti39Cu40Al20Gd1
Preferably, the arc melting is carried out for 10 minutes under the condition that the melting power is 500 Kw.
The Ti with high corrosion resistance prepared by the method of the invention40-xCu40Al20GdxThe flame-retardant alloy is different from the existing Ti2Cu2The Al flame-retardant alloy has the following advantages compared with the Al flame-retardant alloy:
1. ti prepared by the invention40-xCu40Al20GdxThe corrosion rate of the flame-retardant alloy shows a trend of increasing and then decreasing along with the increase of the content of the rare earth Gd, and the corrosion rate of the alloy is almost unchanged when x is more than 0.2; compared with the prior Ti2Cu2The corrosion rate of the Al alloy decreased by about 637%;
2. the corrosion potential of the alloy prepared according to the invention shows a tendency to increase gradually, wherein Ti39Cu40Al20Gd1The corrosion potential of the alloy is-0.17734V at most, which is higher than that of the existing Ti2Cu2The corrosion potential of the Al alloy is improved by about 0.098V;
3. ti prepared by the invention40-xCu40Al20GdxThe corrosion mechanism of the flame retardant alloy is pitting corrosion.
Drawings
FIG. 1 shows Ti prepared in example 140-xCu40Al20GdxMetallographic optical microscopic analysis of the flame-retardant alloy, wherein (a) the figure is an optical micrograph of the alloy with x being 0 in the alloy, (b) the figure is an optical micrograph of the alloy with x being 0.1 in the alloy, (c) the figure is an optical micrograph of the alloy with x being 0.2 in the alloy, (d) the figure is an optical micrograph of the alloy with x being 0.5 in the alloy, and (e) the figure is an optical micrograph of the alloy with x being 1 in the alloy.
FIG. 2 shows Ti prepared in example 140-xCu40Al20Gdx(x ═ 0, 0.1, 0.2, 0.5, 1) XRD pattern of the flame-retardant alloy.
FIG. 3 shows Ti prepared in example 240-xCu40Al20Gdx(x ═ 0, 0.1, 0.2, 0.5, 1) corrosion rate of the flame-retardant alloy as a function of Gd element content.
FIG. 4 shows Ti prepared in example 340-xCu40Al20Gdx(x is 0, 0.1, 0.2, 0.5, 1) graph of anodic polarization curve of flame-retardant alloy, and (a) graph is Ti2Cu2Anodic polarization curve of Al flame-retardant alloy, and (b) figure is Ti39.5Cu40Al20Gd0.5The anodic polarization curve of the alloy is shown in (C) as Ti39Cu40Al20Gd1Anodic polarization curve of alloy.
FIG. 5 shows Ti prepared in example 340-xCu40Al20GdxSEM observation and analysis test picture at room temperature after the flame-retardant alloy is corroded, wherein (a) Ti2Cu2Corrosion morphology of Al alloy; (b) ti39.9Cu40Al20Gd0.1The corrosion morphology of the alloy; (C) ti39.5Cu40Al20Gd0.5The corrosion morphology of the alloy; (d) ti39Cu40Al20Gd1The corrosion morphology of the alloy.
Detailed Description
The invention is described in more detail below with reference to specific examples, without limiting the scope of the invention. Unless otherwise specified, the experimental methods adopted by the invention are all conventional methods, and experimental equipment, materials, reagents and the like used in the experimental method can be obtained from commercial sources. The vacuum medium frequency induction melting furnace used in this example was purchased from Shanghai Cheng optical electric furnace Co., Ltd, and the electrochemical etching was performed on PGSTAT302N electrochemical workstation.
Example 1
In this example, five experiments were carried out according to the x values shown in Table 1.
TABLE 1 Ti40-xCu40Al20GdxAlloy composition
Serial number x number Flame-retardant alloy
1 x=0 Ti2Cu2Al
2 x=0.1 Ti39.9Cu40Al20Gd0.1
3 x=0.2 Ti39.8Cu40Al20Gd0.2
4 x=0.5 Ti39.5Cu40Al20Gd0.5
5 x=1 Ti39Cu40Al20Gd1
High corrosion resistance Ti of the embodiment40-xCu40Al20Gdx(x is 0, 0.1, 0.2, 0.5, 1) of flame-retardant alloyThe preparation method comprises the following steps: taking 40-x parts of Ti, 40 parts of Cu, 20 parts of Al and x parts of rare earth element Gd according to atomic percentage, putting the Ti, the Cu, the Al and the rare earth element Gd into a vacuum medium-frequency induction smelting furnace, and sequentially placing the raw materials according to the following sequence: firstly placing rare Gd, then placing Cu and Al sheets, finally placing sponge Ti element on the uppermost layer of the smelting furnace, and closing a side furnace door. Before smelting, the mixture is pumped by a mechanical pump and a Roots pump to be vacuum of 6.67 multiplied by 10-3Pa, and then filling high-purity argon to 100 Pa. Smelting, controlling the smelting power not to be higher than 500Kw, pouring the alloy liquid into a rod-shaped mould after the molten metal liquid is fully and uniformly mixed to obtain a rod-shaped sample with phi 10mm multiplied by 60mm, and cooling and taking out the rod-shaped sample to obtain the Ti with high corrosion resistance40-xCu40Al20GdxA flame retardant alloy.
Example 2
The present embodiment is different from embodiment 1 in that: the inert gas is argon. The rest is the same as in embodiment 1.
Example 3
The present embodiment is different from embodiment 1 in that: arc melting is carried out for 10 minutes under the condition that the melting power is 500 Kw. The rest is the same as in embodiment 1.
The Ti with high corrosion resistance prepared in example 140-xCu40Al20GdxThe flame-retardant alloy was first subjected to metallographic microscopic analysis, as shown in FIG. 1, from which it can be seen that Ti prepared in the present embodiment40-xCu40Al20GdxThe grain size of the flame-retardant alloy is gradually refined along with the increase of the content of the rare earth Gd.
The Ti with high corrosion resistance prepared in example 140-xCu40Al20GdxXRD test analysis of the flame-retardant alloy is carried out under the condition of room temperature, and the result is shown in figure 2. The XRD diffraction pattern shows that the Ti with high corrosion resistance prepared in the embodiment40- xCu40Al20GdxThe position of the diffraction peak of the flame-retardant alloy is not changed, but the intensity of the diffraction peak is slightly changed, which shows that the microstructure of the alloy is not changed by trace rare earth Gd.
This example systemPrepared high corrosion resistance Ti40-xCu40Al20GdxThe change in corrosion rate of the flame retardant alloy is shown in FIG. 3, from which it can be seen that Ti is prepared in example 240-xCu40Al20GdxThe corrosion rate of the rare earth Gd shows a tendency of gradually rising, then falling and finally almost unchanged.
To investigate the addition of Gd element to the highly corrosion-resistant Ti prepared in example 340-xCu40Al20GdxEffect of the Corrosion characteristics of the alloys, all Ti prepared in example 340-xCu40Al20GdxThe corrosion performance of the alloys was measured in 5% brine, and the results of the anodic polarization curves are shown in FIG. 4, from which it can be seen that Ti prepared in this example40-xCu40Al20GdxThe corrosion potential of the alloy shows a gradually increasing trend. Ti39Cu40Al20Gd1The corrosion potential of the alloy is-0.17734V, and the corrosion current density is 7.558 multiplied by 10-8A/cm2. The alloy has better properties than the prior alloy.
To reveal the Ti prepared in example 340-xCu40Al20GdxThe corrosion mechanism of the alloy is that the surface morphology of the sample after the corrosion treatment is observed by SEM, and the result is shown in FIG. 5, and FIG. 5 shows that the Ti with high corrosion resistance prepared by the embodiment is highly corrosion-resistant40-xCu40Al20GdxThe alloy undergoes pitting corrosion.
The accompanying drawings and experimental data of the examples show that the Gd is added to refine the grains, so that not only can the strength and the plasticity of the alloy be improved, but also the comprehensive mechanical property of the alloy is obviously improved.
The above description is only for the purpose of creating a preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art can substitute or change the technical solution and the inventive concept of the present invention within the technical scope of the present invention.

Claims (5)

1. High-corrosion-resistance Ti40-xCu40Al20GdxThe preparation method of the flame-retardant alloy is characterized by comprising the following steps: taking 40-x parts of Ti, 40 parts of Cu, 20 parts of Al and x (x is 0, 0.1, 0.2, 0.5, 1) parts of rare earth element Gd according to atomic percent, putting the raw materials in a vacuum intermediate frequency induction smelting furnace in the following sequence: firstly placing rare Gd, then placing Cu and Al sheets, finally placing sponge Ti element on the uppermost layer in a smelting furnace, and closing a side furnace door; before smelting, the mixture is pumped by a mechanical pump and a Roots pump to be vacuum of 6.67 multiplied by 10-3Pa, and then charging high-purity inert gas to 100 Pa; smelting, controlling the smelting power not to be higher than 500Kw, pouring the alloy liquid into a rod-shaped mould after the molten metal liquid is fully and uniformly mixed to obtain a rod-shaped sample with phi 10mm multiplied by 60mm, and cooling and taking out the rod-shaped sample to obtain the Ti with high corrosion resistance40-xCu40Al20Gdx flame-retardant alloy.
2. The highly corrosion-resistant Ti according to claim 140-xCu40Al20The preparation method of the Gdx flame-retardant alloy is characterized in that the inert gas is argon or nitrogen.
3. The highly corrosion-resistant Ti according to claim 140-xCu40Al20The preparation method of the Gdx flame-retardant alloy is characterized in that the inert gas is argon.
4. The highly corrosion-resistant Ti according to claim 140-xCu40Al20The preparation method of the Gdx flame-retardant alloy is characterized in that x is 1.
5. The highly corrosion-resistant Ti according to claim 140-xCu40Al20The preparation method of the Gdx flame-retardant alloy is characterized in that the Gdx flame-retardant alloy is subjected to arc melting for 10 minutes under the condition that the melting power is 500 Kw.
CN201910274017.9A 2019-04-08 2019-04-08 High-corrosion-resistance Ti40-xCu40Al20GdxPreparation method of flame-retardant alloy Active CN109913733B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910274017.9A CN109913733B (en) 2019-04-08 2019-04-08 High-corrosion-resistance Ti40-xCu40Al20GdxPreparation method of flame-retardant alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910274017.9A CN109913733B (en) 2019-04-08 2019-04-08 High-corrosion-resistance Ti40-xCu40Al20GdxPreparation method of flame-retardant alloy

Publications (2)

Publication Number Publication Date
CN109913733A CN109913733A (en) 2019-06-21
CN109913733B true CN109913733B (en) 2020-05-19

Family

ID=66968797

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910274017.9A Active CN109913733B (en) 2019-04-08 2019-04-08 High-corrosion-resistance Ti40-xCu40Al20GdxPreparation method of flame-retardant alloy

Country Status (1)

Country Link
CN (1) CN109913733B (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9824611D0 (en) * 1998-11-11 1999-01-06 Rolls Royce Plc A beta titanium alloy
CN103334031A (en) * 2013-07-01 2013-10-02 昆山乔锐金属制品有限公司 Flame-retardant titanium alloy for aerospace aviation engine
CN105803257B (en) * 2016-04-14 2017-05-17 南京理工大学 Method for improving liquid-state fluidity of TiAl-Nb alloy

Also Published As

Publication number Publication date
CN109913733A (en) 2019-06-21

Similar Documents

Publication Publication Date Title
Zhang et al. Recent progress in high-entropy alloys
CN101519760A (en) Production method of 3003-brand cathode aluminum foil
CN115044788B (en) Preparation method of non-ferrous metal material
CN113373366B (en) Multi-element refractory high-entropy alloy and preparation method thereof
CN110541103A (en) High-strength high-plasticity quaternary refractory high-entropy alloy and preparation method thereof
CN111254327B (en) High-silicon aluminum alloy and casting method thereof
CN113462911B (en) Preparation method of tough corrosion-resistant AZ80 magnesium alloy
Zhang et al. Tensile properties and deformation behavior of an extra-low interstitial fine-grained powder metallurgy near alpha titanium alloy by recycling coarse pre-alloyed powder
Zhang et al. Microstructure and mechanical properties of Mg–3.0 Y–2.5 Nd–1.0 Gd–xZn–0.5 Zr alloys produced by metallic and sand mold casting
CN109913733B (en) High-corrosion-resistance Ti40-xCu40Al20GdxPreparation method of flame-retardant alloy
CN113403520A (en) Ternary refractory medium-entropy alloy and preparation method thereof
CN112251659A (en) AlCrFe2Ni2C0.24High-entropy alloy and preparation method thereof
CN109732087B (en) Preparation method of powder metallurgy Ti-Ta binary metal-based layered composite material
CN115233076B (en) CoNiAl magnetic control memory type eutectic medium entropy alloy and preparation method thereof
CN108359834B (en) Preparation method of nano-structure copper alloy for electric spark electrode
CN106834806B (en) Corrosion-resistant zinc alloy and preparation method thereof
RU2476616C1 (en) Wear-resistant alloy on basis of nickel for application of wear and corrosion resistant coatings to structural elements with microplasma or supersonic gas-dynamic sputtering
Mao et al. Effect of rare earth on the microstructure and mechanical properties of as-cast Cu-30Ni alloy
CN103436925A (en) Method for improving room-temperature plasticity of amorphous alloy
CN109825745B (en) Alloy material with high comprehensive performance and preparation method thereof
CN105838951B (en) A kind of magnesium alloy of sacrificial anode containing La
CN115821145B (en) High-strength high-plasticity multiphase high-entropy alloy material and preparation method thereof
CN112126816A (en) Corrosion-resistant rare earth copper alloy
CN112251660B (en) High-strength forged high-entropy alloy and preparation method thereof
CN102051508A (en) Corrosion-resisting AZ91 magnesium alloy

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant