CN106048356A - Multi-element Nb-Si-based super-high-temperature alloy material and preparing method thereof - Google Patents

Multi-element Nb-Si-based super-high-temperature alloy material and preparing method thereof Download PDF

Info

Publication number
CN106048356A
CN106048356A CN201610556028.2A CN201610556028A CN106048356A CN 106048356 A CN106048356 A CN 106048356A CN 201610556028 A CN201610556028 A CN 201610556028A CN 106048356 A CN106048356 A CN 106048356A
Authority
CN
China
Prior art keywords
block
temperature
furnace
alloy
stove
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.)
Pending
Application number
CN201610556028.2A
Other languages
Chinese (zh)
Inventor
郭喜平
张松
乔彦强
曾宇翔
张昊
唐晔
何佳华
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.)
Northwestern Polytechnical University
Original Assignee
Northwestern Polytechnical 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 Northwestern Polytechnical University filed Critical Northwestern Polytechnical University
Publication of CN106048356A publication Critical patent/CN106048356A/en
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • C22C27/02Alloys based on vanadium, niobium, or tantalum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture And Refinement Of Metals (AREA)

Abstract

The invention discloses a multi-element Nb-Si-based super-high-temperature alloy material and a preparing method thereof to solve the technical problem that an existing Nb-Si-based super-high-temperature alloy material is poor in high-temperature oxidation resistance. According to the technical scheme, the multi-element Nb-Si-based super-high-temperature alloy material is composed of 30 at.% to 72 at.% of Nb, 10 at.% to 30 at.% of Ti, 12 at.% to 18 at.% of Si, 2 at.% to 5 at.% of Al, 2 at.% to 8 at.% of Hf, 1 at.%-10 at.% of B, 3 at.%-20 at.% of Cr, 0 at.% to 8 at.% of Zr, 0 at.%-8 at.% of Mo, 0 at.%-0.5 at.% of Ce and 0.03 at.% to 0.3 at.% of Y. The preparing method includes the step of adding Ti, Al, B, Cr, Zr and trace rare earth elements of Ce and Y into the alloy, and the high-temperature oxidization resistance of the multi-element Nb-Si-based super-high-temperature alloy material is improved.

Description

Polynary Nb-Si based ultra-high temperature alloy material and preparation method thereof
Technical field
The present invention relates to a kind of ultra high temperature alloy material, particularly to a kind of polynary Nb-Si based ultra-high temperature alloy material.Also Relate to the preparation method of this polynary Nb-Si based ultra-high temperature alloy material.
Background technology
Nb-Si based ultra-high temperature alloy is owing to having fusing point high (more than 1700 DEG C), medium density (6.6~7.2g/cm3) and Elevated temperature strength high and enjoy vast researcher to pay close attention to.The composition of such alloy is mainly niobio solid solution (Nb mutuallyss, tough Property phase) and intermetallic compound ((Nb, X)5Si3、(Nb,X)3Si, or (Nb, X) Cr2Laves phase, hardening constituent, " X " represents The atoms such as Ti, Hf, Cr and Zr of replacing Nb in lattice).Wherein, (Nb, X)5Si3Have three kinds of crystal formations, i.e. α (Nb, X)5Si3(four Side D8lStructure), β (Nb, X)5Si3(four directions D8mStructure) and γ (Nb, X)5Si3(six side D88Structure).By above-mentioned toughness phase with strong The in situ composites that change phase is constituted has reached preferable balance it is considered to be one has in high/low temperature mechanical property Wish to replace the Ni based single-crystal high-temperature alloy high-temperature structural material that (1200~1400 DEG C) are applied at a higher temperature.
But, Room-Temperature Fracture Toughness and the high-temperature oxidation resistance of such alloy are poor, thus limit it in aviation, boat The application in the field such as it and nuclear industry.Based on composition-tissue-property relationship, alloying, the microalloying including rare earth element is Improve Nb-Si based ultra-high temperature alloy combination property (particularly permissible at the aspect such as room-temperature mechanical property and high-temperature oxidation resistance Obtain preferably balance) effective means.Wherein, Ti, Al, Hf, B, Cr, Zr, Mo and Rare-Earth Ce, Y are several important alloys Change element.Although the alloying research report of these elements existing, but still there are the following problems: (1) alloying research is main Concentrate in the simple alloy system such as ternary, quaternary, and the research in multi-element alloy system is the most relatively fewer;(2) for certain One system alloy, researcher is generally only concerned performance (mechanical property or antioxygenic property) in a certain respect, and do not rise to from The combination property of alloy is considered every possible angle;(3) when studying the alloying action of a certain element, only choose a certain certain content and A scope, can't this element of full appreciation on alloy structure and the impact of performance;(4) generally, researcher Only focus on the alloying action of a certain element-specific, and the compound action between each element is mentioned less.
Document 1 " application publication number is the Chinese invention patent of CN102021458A ", " application publication number is document 2 The Chinese invention patent of CN101974712A " and document 3 " application publication number is the Chinese invention patent of CN101792879A " point Do not disclose Nb-Ti-Si-Zn, Nb-Ti-Si-Sr and Nb-Mo-Si-B/Ge alloy system, but these systems all exist comprehensive Can not be good, the problem that especially high-temperature oxidation resistance is poor.At present, the China about polynary Nb-Si based ultra-high temperature alloy is special Profit is actually rare.From the combination property of alloy, i.e. Room-Temperature Fracture Toughness and ductility, elevated temperature strength, high-temperature creep resistance and The aspects such as antioxygenic property consider, and it is very important for developing polynary Nb-Si based ultra-high temperature alloy material.
Summary of the invention
In order to overcome the deficiency of existing Nb-Si based ultra-high temperature alloy material high-temperature oxidation resistance difference, the present invention provides one Plant polynary Nb-Si based ultra-high temperature alloy material and preparation method thereof.Described polynary Nb-Si based ultra-high temperature alloy material by 30~ The Hf of the Al of the Si of the Ti of the Nb of 72at.%, 10~30at.%, 12~18at.%, 2~5at.%, 2~8at.%, 1~ The Ce and 0.03 of the Mo of the Zr of the Cr of the B of 10at.%, 3~20at.%, 0~8at.%, 0~8at.%, 0~0.5at.%~ The Y composition of 0.3at.%.The preparation method of described polynary Nb-Si based ultra-high temperature alloy material be in alloy add Ti, Al, B, Cr, Zr and trace rare-earth Ce, Y element, improve the high-temperature oxidation resistance of polynary Nb-Si based ultra-high temperature alloy material.
The technical solution adopted for the present invention to solve the technical problems is: a kind of polynary Nb-Si based ultra-high temperature alloy material, Be characterized in: the Al of the Si of the Ti of Nb, 10~30at.%, 12~18at.%, 2~5at.% by 30~72at.%, 2~ The Mo of the Zr of the Cr of the B of the Hf of 8at.%, 1~10at.%, 3~20at.%, 0~8at.%, 0~8at.%, 0~ The Y of the Ce and 0.03~0.3at.% of 0.5at.% forms, and the atomic percentage conc sum of above-mentioned each element is 100%.
The preparation method of a kind of above-mentioned polynary Nb-Si based ultra-high temperature alloy material, is characterized in comprising the following steps:
The first step, choose material N b block, sponge Ti or Ti paper tinsel, Si block, Al block, Hf block, B grain, Cr block, Zr grain, Mo block, Ce block and Y block, its purity is 99.97wt.%, removes raw material surface irregularities and oxide with standby;
Second step, weighs each former material respectively according to Nb-Ti-Si-Al-Hf-B-Cr-Zr-Mo-Ce-Y target component proportioning Material, in terms of 200~250 grams/ingot, and puts it in vacuum non-consumable arc-melting furnace, depends on by fusing point order from low to high Secondary stack, and B grain, Ce block and Y block Ti paper tinsel are wrapped, compacting;
Described Nb-Ti-Si-Al-Hf-B-Cr-Zr-Mo-Ce-Y target component by 30~72at.% Nb, 10~ The B of the Hf of the Al of the Si of the Ti of 30at.%, 12~18at.%, 2~5at.%, 2~8at.%, 1~10at.%, 3~ The Y group of the Ce and 0.03~0.3at.% of the Mo of the Zr of the Cr of 20at.%, 0~8at.%, 0~8at.%, 0~0.5at.% Become, and the atomic percentage conc sum of above-mentioned each element is 100%;
3rd step, is first evacuated to 1~3 × 10-3Pa, is then filled with the argon that purity is 99.999wt.% in stove and enters Row melting, electric current during melting controls 1000~1150A.Electromagnetic agitation power supply, electric current is opened after alloy material is completely melt Control 10~20A, melt back 5~6 times, it is thus achieved that the uniform alloy pig of composition;
4th step, puts into superhigh temperature hypertonic solutions stove by the alloy pig prepared in the 3rd step, simultaneously at alloy pig Around put some sponge Ti to reach the purpose of oxygen uptake;
5th step, is evacuated to 1~3 × 10-3Beginning to warm up during Pa, heating rate is about 15~17 DEG C/min.When in stove Stop evacuation when temperature reaches 950~1050 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect. Continue heating and will heat up rate controlled at 14~16 DEG C/min, be incubated after in-furnace temperature reaches 1400~1500 DEG C 45~ 55h carries out Homogenization Treatments.After insulation terminates, cool to room temperature with the furnace;
6th step, is evacuated to 1~3 × 10-3Beginning to warm up during Pa, heating rate is about 15~17 DEG C/min.When in stove Stop evacuation when temperature reaches 950~1050 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect. Continue heating and will heat up rate controlled at 14~16 DEG C/min, be incubated after in-furnace temperature reaches 1000~1150 DEG C 45~ 55h carries out Ageing Treatment.After insulation terminates, cool to room temperature with the furnace.
The invention has the beneficial effects as follows: the present invention polynary Nb-Si based ultra-high temperature alloy material by 30~72at.% Nb, The B of the Hf of the Al of the Si of Ti, 12~18at.%, 2~5at.%, 2~8at.%, 1~10at.% of 10~30at.%, 3~ The Y group of the Ce and 0.03~0.3at.% of the Mo of the Zr of the Cr of 20at.%, 0~8at.%, 0~8at.%, 0~0.5at.% Become.The preparation method of described polynary Nb-Si based ultra-high temperature alloy material is interpolation Ti, Hf, B and Zr element in alloy, to carry Its Room-Temperature Fracture Toughness high.Add Hf, B, Zr and Mo element, to improve its elevated temperature strength.Add Ti, Al, B, Cr, Zr and trace Rare-Earth Ce, Y element, to improve its high-temperature oxidation resistance, thus obtain the combination property relatively balanced.The present invention's is polynary Nb-Si based ultra-high temperature alloy material is by toughness phase NbssWith hardening constituent (Nb, X)5Si3、(Nb,X)3Si or (Nb, X) Cr2Constitute, its Room-Temperature Fracture Toughness KQValue is 9.2~23.8MPa m1/2, at 1250 DEG C/0.005s-1Under the conditions of compressive strength σpIt is 192.6 ~520.1MPa, the unit are weightening finish after 1250 DEG C/50h aoxidizes is 18.3~156.5mg/cm2
The present invention is described in detail below in conjunction with drawings and Examples.
Accompanying drawing explanation
Fig. 1 is X-ray diffraction (XRD) spectrum of the polynary Nb-Si based ultra-high temperature alloy that embodiment 1 prepares.
Fig. 2 be the polynary Nb-Si based ultra-high temperature alloy that embodiment 1 prepares backscattered electron (BSE) as.
Fig. 3 is that the prepared polynary Nb-Si based ultra-high temperature alloy of embodiment 1 is through 1250 DEG C/0.005s-1Stress after compression- Strain curve.
Fig. 4 is that the prepared polynary Nb-Si based ultra-high temperature alloy of embodiment 1 is through 1250 DEG C/0.005s-1The back of the body of tissue after compression Scattered electron (BSE) as.
Fig. 5 is that the polynary Nb-Si based ultra-high temperature alloy that embodiment 1 prepares dissipates through the back of the body of 1250 DEG C/50h oxidation rear oxidation film Radio (BSE) as.
Detailed description of the invention
Following example are with reference to Fig. 1-5.
The present invention relates to a kind of polynary Nb-Si based ultra-high temperature alloy material can applied at a temperature of 1200 DEG C of environment above Material, its by 30~72at.% the Al of the Si of the Ti of Nb, 10~30at.%, 12~18at.%, 2~5at.%, 2~ The Mo of the Zr of the Cr of the B of the Hf of 8at.%, 1~10at.%, 3~20at.%, 0~8at.%, 0~8at.%, 0~ The Y of the Ce and 0.03~0.3at.% of 0.5at.% forms, and the atomic percentage conc sum of above-mentioned each element is 100%.
The present invention use have the vacuum non-consumable electric arc melting technology of electromagnetic agitation function and 1450 DEG C/50h+1100 DEG C/ 50h heat treatment method prepares this polynary Nb-Si based ultra-high temperature alloy material, and it includes the following step:
The first step, choose Nb block, sponge Ti or Ti paper tinsel, Si block, Al block, Hf block, B grain, Cr block, Zr grain, Mo block, Ce block and Y block, its purity, all at more than 99.97wt.%, removes raw material surface irregularities and oxide with standby;
Second step, weighs each former material respectively according to Nb-Ti-Si-Al-Hf-B-Cr-Zr-Mo-Ce-Y target component proportioning Material, in terms of 200~250 grams/ingot, and puts it in vacuum non-consumable arc-melting furnace, depends on by fusing point order from low to high Secondary stack, and B grain, Ce block and Y block need to be wrapped with Ti paper tinsel, compacting;
Described Nb-Ti-Si-Al-Hf-B-Cr-Zr-Mo-Ce-Y target component by 30~72at.% Nb, 10~ The B of the Hf of the Al of the Si of the Ti of 30at.%, 12~18at.%, 2~5at.%, 2~8at.%, 1~10at.%, 3~ The Y group of the Ce and 0.03~0.3at.% of the Mo of the Zr of the Cr of 20at.%, 0~8at.%, 0~8at.%, 0~0.5at.% Become, and the atomic percentage conc sum of above-mentioned each element is 100%;
3rd step, is first evacuated to 1 × 10-3Pa, is then filled with the argon that purity is 99.999wt.% in stove and melts Refining, electric current during melting controls 1000~1150A.Opening electromagnetic agitation power supply after alloy material is completely melt, electric current controls 10~20A, melt back 5~6 times, to obtain the uniform alloy pig of composition;
4th step, puts into superhigh temperature hypertonic solutions stove by the alloy pig prepared in the 3rd step, simultaneously at alloy pig Around put some sponge Ti to reach the purpose of oxygen uptake;
5th step, is evacuated to 1 × 10-3Beginning to warm up during Pa, heating rate is about 16 DEG C/min.When in-furnace temperature reaches Stop evacuation when 1000 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect.Continue heating and will rise Temperature rate controlled, at 15 DEG C/min, is incubated 50h after in-furnace temperature reaches 1450 DEG C and carries out Homogenization Treatments.After insulation terminates, Sample cools to room temperature with the furnace;
6th step, is evacuated to 1 × 10-3Beginning to warm up during Pa, heating rate is about 16 DEG C/min.When in-furnace temperature reaches Stop evacuation when 1000 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect.Continue heating and will rise Temperature rate controlled, at 15 DEG C/min, is incubated 50h after in-furnace temperature reaches 1100 DEG C and carries out Ageing Treatment.After insulation terminates, examination Sample cools to room temperature with the furnace.
Use X-ray diffractometer (XRD) and scanning electron microscope (SEM) respectively to polynary Nb-Si based ultra-high temperature alloy Sample carries out crystal species analysis and microstructure observation, and alloy structure includes toughness phase NbssWith hardening constituent (Nb, X)5Si3、 (Nb,X)3Si or (Nb, X) Cr2
Use Instron3383 type electronic universal mechanics machine that polynary Nb-Si based ultra-high temperature alloy sample is carried out room Temperature fracture toughness test, its KQValue is 9.2~23.8MPa m1/2
Use Gleeble 3500 type heat/power simulated experiment machine that polynary Nb-Si based ultra-high temperature alloy sample is carried out high temperature Compression performance is tested, and test condition is 1250 DEG C/0.005s-1, its compressive strength σpIt is 192.6~520.1MPa.
Use homemade drawing by high temperature oxidation furnace that polynary Nb-Si based ultra-high temperature alloy sample is carried out high-temperature oxidation resistance Test, test condition is 1250 DEG C/50h, and its unit are oxidation weight gain is 18.3~156.5mg/cm2
Embodiment 1:
Use and have at vacuum non-consumable electric arc melting technology and 1450 DEG C/50h+1100 DEG C/50h heat of electromagnetic agitation function Reason method prepares polynary Nb-Si based ultra-high temperature alloy material, and it includes the following step:
The first step, chooses Nb block, sponge Ti or Ti paper tinsel, Si block, Al block, Hf block, B grain, Cr block, Zr grain and Y block, its purity All at more than 99.97wt.%, remove raw material surface irregularities and oxide with standby;
Second step, according to Nb-22Ti-15Si-5Cr-4Zr-3Al-3Hf-1.5B-0.06Y (at.%) composition proportion respectively Weigh each raw material, in terms of 200 grams/ingot, and put it in vacuum non-consumable arc-melting furnace, by fusing point from low to high suitable Sequence stacks successively, and B grain and Y block need to be wrapped with Ti paper tinsel, compacting;
3rd step, is first evacuated to 1 × 10-3Pa, is then filled with the argon that purity is 99.999wt.% in stove and melts Refining, electric current during melting controls at 1100A.Opening electromagnetic agitation power supply after alloy material is completely melt, electric current controls at 15A, Melt back 6 times, to obtain the uniform alloy pig of composition;
4th step, puts into superhigh temperature hypertonic solutions stove by the alloy pig prepared in the 3rd step, simultaneously at alloy pig Around put some sponge Ti to reach the purpose of oxygen uptake;
5th step, is evacuated to 1 × 10-3Beginning to warm up during Pa, heating rate is about 16 DEG C/min.When in-furnace temperature reaches Stop evacuation when 1000 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect.Continue heating and will rise Temperature rate controlled, at 15 DEG C/min, is incubated 50h after in-furnace temperature reaches 1450 DEG C and carries out Homogenization Treatments.After insulation terminates, Sample cools to room temperature with the furnace;
6th step, is evacuated to 1 × 10-3Beginning to warm up during Pa, heating rate is about 16 DEG C/min.When in-furnace temperature reaches Stop evacuation when 1000 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect.Continue heating and will rise Temperature rate controlled, at 15 DEG C/min, is incubated 50h after in-furnace temperature reaches 1100 DEG C and carries out Ageing Treatment.After insulation terminates, examination Sample cools to room temperature with the furnace.
Use X-ray diffractometer (XRD) and scanning electron microscope (SEM) respectively to Nb-22Ti-15Si-5Cr-4Zr- 3Al-3Hf-1.5B-0.06Y (at.%) supertherm sample (a size of 8mm × 8mm × 8mm) carry out crystal species analysis and Microstructure observation.Seeing figures.1.and.2, alloy structure is by toughness phase Nbss and hardening constituent γ (Nb, X)5Si3Constitute, and γ (Nb,X)5Si3It is evenly distributed on continuous print Nbss matrix.
Use Instron3383 type electronic universal mechanics machine to Nb-22Ti-15Si-5Cr-4Zr-3Al-3Hf- 1.5B-0.06Y (at.%) supertherm sample (a size of 30mm × 5mm × 2.5mm) carries out Room-Temperature Fracture Toughness test, Its KQValue is 14.1MPa m1/2
Use Gleeble 3500 type heat/power simulated experiment machine to Nb-22Ti-15Si-5Cr-4Zr-3Al-3Hf-1.5B- 0.06Y (at.%) supertherm sample (a size of Φ 6mm × 9mm) carries out compressive property test, and test condition is 1250℃/0.005s-1.With reference to Fig. 3 and Fig. 4, alloy compressive strength σpFor 345.2MPa, in compression process, Nbss occurs to become continuously Shape, γ (Nb, X)5Si3Particle surface bends, and is evenly distributed on Nbss matrix.
Use homemade drawing by high temperature oxidation furnace to Nb-22Ti-15Si-5Cr-4Zr-3Al-3Hf-1.5B-0.06Y (at.%) supertherm sample (a size of 8mm × 8mm × 8mm) carries out high-temperature oxidation resistance test, and test condition is 1250 DEG C/50h, its unit are oxidation weight gain is 58.9mg/cm2.With reference to Fig. 5, alloy oxide film is comparatively dense, can effectively hinder Block is to internal diffusion, thus makes it have preferable high-temperature oxidation resistance.
Embodiment 2:
Use and have at vacuum non-consumable electric arc melting technology and 1450 DEG C/50h+1100 DEG C/50h heat of electromagnetic agitation function Reason method prepares polynary Nb-Si based ultra-high temperature alloy material, and it includes the following step:
The first step, chooses Nb block, sponge Ti or Ti paper tinsel, Si block, Al block, Hf block, B grain, Cr block and Y block, and its purity all exists More than 99.97wt.%, removes raw material surface irregularities and oxide with standby;
Second step, weighs respectively respectively according to Nb-22Ti-16Si-8Hf-3Cr-3Al-2B-0.06Y (at.%) composition proportion Raw material, in terms of 250 grams/ingot, and puts it in vacuum non-consumable arc-melting furnace, by fusing point order from low to high successively Stack, and B grain and Y block need to be wrapped with Ti paper tinsel, compacting;
3rd step, is first evacuated to 2 × 10-3Pa, is then filled with the argon that purity is 99.999wt.% in stove and melts Refining, electric current during melting controls at 1000A.Opening electromagnetic agitation power supply after alloy material is completely melt, electric current controls at 10A, Melt back 5 times, to obtain the uniform alloy pig of composition;
4th step, puts into superhigh temperature hypertonic solutions stove by the alloy pig prepared in the 3rd step, simultaneously at alloy pig Around put some sponge Ti to reach the purpose of oxygen uptake;
5th step, is evacuated to 2 × 10-3Beginning to warm up during Pa, heating rate is about 15 DEG C/min.When in-furnace temperature reaches Stop evacuation when 950 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect.Continue heating and will rise Temperature rate controlled, at 14 DEG C/min, is incubated 45h after in-furnace temperature reaches 1400 DEG C and carries out Homogenization Treatments.After insulation terminates, Sample cools to room temperature with the furnace;
6th step, is evacuated to 2 × 10-3Beginning to warm up during Pa, heating rate is about 15 DEG C/min.When in-furnace temperature reaches Stop evacuation when 950 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect.Continue heating and will rise Temperature rate controlled, at 14 DEG C/min, is incubated 45h after in-furnace temperature reaches 1000 DEG C and carries out Ageing Treatment.After insulation terminates, examination Sample cools to room temperature with the furnace.
The mode using embodiment 1 carries out crystal species analysis and microstructure observation understands, Nb-22Ti-16Si-8Hf- The tissue of 3Cr-3Al-2B-0.06Y (at.%) supertherm sample is by toughness phase Nbss, hardening constituent γ (Nb, X)5Si3With (Nb,X)3Si is constituted, and γ (Nb, X)5Si3(Nb, X)3Si is evenly distributed on continuous print Nbss matrix.
The mode using embodiment 1 carries out Room-Temperature Fracture Toughness test and understands, Nb-22Ti-16Si-8Hf-3Cr-3Al- The K of 2B-0.06Y (at.%) supertherm sampleQValue is 16.3MPa m1/2
The mode using embodiment 1 carries out compressive property test and understands, Nb-22Ti-16Si-8Hf-3Cr-3Al- Compressive strength σ of 2B-0.06Y (at.%) supertherm samplepFor 383.7MPa, in compression process, Nbss occurs to become continuously Shape, γ (Nb, X)5Si3(Nb, X)3Si particle surface bends, and is evenly distributed on Nbss matrix.
The mode using embodiment 1 carries out high-temperature oxidation resistance test and understands, Nb-22Ti-16Si-8Hf-3Cr-3Al- 2B-0.06Y (at.%) the unit are oxidation weight gain of supertherm sample is 96.6mg/cm2, alloy oxide film causes relatively Close, oxygen can be stoped to internal diffusion, thus make it have preferable high-temperature oxidation resistance.
Embodiment 3:
Use and have at vacuum non-consumable electric arc melting technology and 1450 DEG C/50h+1100 DEG C/50h heat of electromagnetic agitation function Reason method prepares polynary Nb-Si based ultra-high temperature alloy material, and it includes the following step:
The first step, chooses Nb block, sponge Ti or Ti paper tinsel, Si block, Al block, Hf block, B grain, Cr block and Y block, and its purity all exists More than 99.97wt.%, removes raw material surface irregularities and oxide with standby;
Second step, weighs respectively respectively according to Nb-22Ti-16Si-8Hf-3Cr-3Al-2B-0.06Y (at.%) composition proportion Raw material, in terms of 200 grams/ingot, and puts it in vacuum non-consumable arc-melting furnace, by fusing point order from low to high successively Stack, and B grain and Y block need to be wrapped with Ti paper tinsel, compacting;
3rd step, is first evacuated to 3 × 10-3Pa, is then filled with the argon that purity is 99.999wt.% in stove and melts Refining, electric current during melting controls at 1150A.Opening electromagnetic agitation power supply after alloy material is completely melt, electric current controls at 20A, Melt back 5 times, to obtain the uniform alloy pig of composition;
4th step, puts into superhigh temperature hypertonic solutions stove by the alloy pig prepared in the 3rd step, simultaneously at alloy pig Around put some sponge Ti to reach the purpose of oxygen uptake;
5th step, is evacuated to 3 × 10-3Beginning to warm up during Pa, heating rate is about 17 DEG C/min.When in-furnace temperature reaches Stop evacuation when 1050 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect.Continue heating and will rise Temperature rate controlled, at 16 DEG C/min, is incubated 55h after in-furnace temperature reaches 1400 DEG C and carries out Homogenization Treatments.After insulation terminates, Sample cools to room temperature with the furnace;
6th step, is evacuated to 3 × 10-3Beginning to warm up during Pa, heating rate is about 17 DEG C/min.When in-furnace temperature reaches Stop evacuation when 1050 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect.Continue heating and will rise Temperature rate controlled, at 16 DEG C/min, is incubated 55h after in-furnace temperature reaches 1150 DEG C and carries out Ageing Treatment.After insulation terminates, examination Sample cools to room temperature with the furnace.

Claims (2)

1. a polynary Nb-Si based ultra-high temperature alloy material, it is characterised in that: Nb, 10~the 30at.% by 30~72at.% The B of the Hf of the Al of the Si of Ti, 12~18at.%, 2~5at.%, 2~8at.%, 1~10at.%, 3~20at.% The Y composition of the Ce and 0.03~0.3at.% of the Mo of the Zr of Cr, 0~8at.%, 0~8at.%, 0~0.5at.%, and above-mentioned The atomic percentage conc sum of each element is 100%.
2. the preparation method of polynary Nb-Si based ultra-high temperature alloy material described in a claim 1, it is characterised in that include following Step:
The first step, chooses material N b block, sponge Ti or Ti paper tinsel, Si block, Al block, Hf block, B grain, Cr block, Zr grain, Mo block, Ce block With Y block, its purity is 99.97wt.%, removes raw material surface irregularities and oxide;
Second step, weighs each raw material respectively according to Nb-Ti-Si-Al-Hf-B-Cr-Zr-Mo-Ce-Y target component proportioning, with 200~250 grams/ingot meter, and put it in vacuum non-consumable arc-melting furnace, fold successively by fusing point order from low to high Put, and B grain, Ce block and Y block Ti paper tinsel are wrapped, compacting;
Described Nb-Ti-Si-Al-Hf-B-Cr-Zr-Mo-Ce-Y target component by 30~72at.% Nb, 10~30at.% The Cr of the B of the Hf of the Al of the Si of Ti, 12~18at.%, 2~5at.%, 2~8at.%, 1~10at.%, 3~20at.%, 0 ~the Y composition of the Ce of the Mo of the Zr of 8at.%, 0~8at.%, 0~0.5at.% and 0.03~0.3at.%, and above-mentioned each unit The atomic percentage conc sum of element is 100%;
3rd step, is first evacuated to 1~3 × 10-3Pa, is then filled with the argon that purity is 99.999wt.% in stove and melts Refining, electric current during melting controls 1000~1150A;Opening electromagnetic agitation power supply after alloy material is completely melt, electric current controls 10~20A, melt back 5~6 times, it is thus achieved that the uniform alloy pig of composition;
4th step, puts into superhigh temperature hypertonic solutions stove by the alloy pig prepared in the 3rd step, simultaneously around alloy pig Put some sponge Ti to reach the purpose of oxygen uptake;
5th step, is evacuated to 1~3 × 10-3Beginning to warm up during Pa, heating rate is about 15~17 DEG C/min;Work as in-furnace temperature Stop evacuation when reaching 950~1050 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect;Continue Heat and will heat up rate controlled at 14~16 DEG C/min, after in-furnace temperature reaches 1400~1500 DEG C, being incubated 45~55h enter Row Homogenization Treatments;After insulation terminates, cool to room temperature with the furnace;
6th step, is evacuated to 1~3 × 10-3Beginning to warm up during Pa, heating rate is about 15~17 DEG C/min;Work as in-furnace temperature Stop evacuation when reaching 950~1050 DEG C, and in stove, be filled with the argon that purity is 99.999wt.% protect;Continue Heat and will heat up rate controlled at 14~16 DEG C/min, after in-furnace temperature reaches 1000~1150 DEG C, being incubated 45~55h enter Row Ageing Treatment;After insulation terminates, cool to room temperature with the furnace.
CN201610556028.2A 2016-01-28 2016-07-14 Multi-element Nb-Si-based super-high-temperature alloy material and preparing method thereof Pending CN106048356A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN2016100584702 2016-01-28
CN201610058470 2016-01-28

Publications (1)

Publication Number Publication Date
CN106048356A true CN106048356A (en) 2016-10-26

Family

ID=57186836

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610556028.2A Pending CN106048356A (en) 2016-01-28 2016-07-14 Multi-element Nb-Si-based super-high-temperature alloy material and preparing method thereof

Country Status (1)

Country Link
CN (1) CN106048356A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107326239A (en) * 2017-09-04 2017-11-07 北京航空航天大学 A kind of Nb Si based multicomponent alloys of rapid solidification containing Sc
CN107513652A (en) * 2017-09-05 2017-12-26 北京航空航天大学 A kind of quick solidification Nb Si based multicomponent alloys
CN107523733A (en) * 2017-09-04 2017-12-29 北京航空航天大学 A kind of directional solidification Nb Si based multicomponent alloys
CN110643874A (en) * 2019-10-22 2020-01-03 华侨大学 Nb-Si base multi-component alloy material for improving oxidation resistance in wide temperature range
CN112191802A (en) * 2020-09-23 2021-01-08 西北工业大学 Preparation method of Nb-Si-based ultrahigh-temperature alloy directional solidification blade simulation piece

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101974712A (en) * 2010-10-15 2011-02-16 北京航空航天大学 Nb-Ti-Si-Sr alloy material and preparation method thereof
CN102021458A (en) * 2010-10-15 2011-04-20 北京航空航天大学 Nb-Ti-Si-Zn alloy material and preparation method thereof

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101974712A (en) * 2010-10-15 2011-02-16 北京航空航天大学 Nb-Ti-Si-Sr alloy material and preparation method thereof
CN102021458A (en) * 2010-10-15 2011-04-20 北京航空航天大学 Nb-Ti-Si-Zn alloy material and preparation method thereof

Non-Patent Citations (5)

* Cited by examiner, † Cited by third party
Title
姚成方 等: ""电弧熔炼Nb-Ti- Si-Cr-Hf-Al-B-Y超高温合金母合金锭的组织形成和成分分布特点"", 《材料工程》 *
曾宇翔 等: ""Zr含量对Nb-Ti-Si基超高温合金组织及抗氧化性能的影响"", 《金属学报》 *
郭喜平: ""Nb-Si 基超高温合金制备技术及抗氧化硅化物渗层"", 《中国材料进展》 *
郭海生 等: ""高温均匀化及时效处理对Nb-Ti-Si基超高温合金组织的影响"", 《稀有金属材料与工程》 *
陈丽群 等: ""Cr 含量对 Nb- Ti- Si- Cr 基超高温合金组织及抗氧化性能的影响"", 《材料热处理学报》 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107326239A (en) * 2017-09-04 2017-11-07 北京航空航天大学 A kind of Nb Si based multicomponent alloys of rapid solidification containing Sc
CN107523733A (en) * 2017-09-04 2017-12-29 北京航空航天大学 A kind of directional solidification Nb Si based multicomponent alloys
CN107326239B (en) * 2017-09-04 2019-06-18 北京航空航天大学 One kind quickly solidifying Nb-Si based multicomponent alloy containing Sc
CN107513652A (en) * 2017-09-05 2017-12-26 北京航空航天大学 A kind of quick solidification Nb Si based multicomponent alloys
CN110643874A (en) * 2019-10-22 2020-01-03 华侨大学 Nb-Si base multi-component alloy material for improving oxidation resistance in wide temperature range
CN112191802A (en) * 2020-09-23 2021-01-08 西北工业大学 Preparation method of Nb-Si-based ultrahigh-temperature alloy directional solidification blade simulation piece
CN112191802B (en) * 2020-09-23 2022-04-12 西北工业大学 Preparation method of Nb-Si-based ultrahigh-temperature alloy directional solidification blade simulation piece

Similar Documents

Publication Publication Date Title
CN106048356A (en) Multi-element Nb-Si-based super-high-temperature alloy material and preparing method thereof
Niu et al. Strengthening of nanoprecipitations in an annealed Al0. 5CoCrFeNi high entropy alloy
Qin et al. CoCrFeMnNi high-entropy alloys reinforced with Laves phase by adding Nb and Ti elements
CN108677077B (en) Refractory high-entropy alloy with high specific strength and high plasticity and preparation method thereof
Zhang et al. Microstructures and tensile properties of Ti2AlNb and Mo-modified Ti2AlNb alloys fabricated by hot isostatic pressing
CN107739956A (en) A kind of Nb microalloyings Ni Co Fe Cr Al high-entropy alloys
CN104498844B (en) A kind of large scale TRIP amorphous composite material and preparation method thereof
US11242585B2 (en) Iron-based superalloy for high temperature 700 ° C. with coherent precipitation of cuboidal B2 nanoparticles
CN108517452A (en) One kind having both high intensity and soft magnet performance AlCoCuFeNixHigh-entropy alloy and preparation method thereof
Huang et al. High temperature oxidation behavior and mechanism of Al0. 3CuCrFeNi2 high-entropy alloy with a coherent γ/γ'microstructure
Ishijima et al. Microstructure and bend ductility of W-0.3 mass% TiC alloys fabricated by advanced powder-metallurgical processing
CN105925846A (en) Zr-Sn-Nb-Hf alloy bar and manufacture method thereof
CN112962010A (en) Aluminum-rich high-entropy alloy and preparation method and application thereof
CN110358964B (en) MoVNbTiCr for nuclear powerxHigh-entropy alloy and preparation method thereof
CN106048355B (en) The preparation method of Nb Si based ultra-high temperature alloy pigs
Wei et al. Phase precipitation behavior and mechanical properties of multi-phase Nb–Ti–C and Nb–Ti–Al–C alloys
Xue et al. Phase Equilibria in Co-rich Co-Al-W alloys at 1300 C and 900 C
CN113308635B (en) Low-thermal-neutron absorption cross section entropy alloy with nanometer precipitated phase and preparation method
CN110205506A (en) A kind of low activation multi-principal elements alloy and preparation method thereof
CN106011574B (en) A kind of Nb-Si based alloys of no hafnium high antioxidant and preparation method thereof
Zhang et al. Microstructure and mechanical properties of tungsten composite reinforced by fibre network
Yuan et al. Titanium effect on the microstructure and properties of laminated high boron steel plates
CN105506428B (en) A kind of preparation method of the vanadium alloy of anti-helium ion sputtering
Huang et al. Effect of initial grain size on oxidation resistance of L12-strengthened Al-Fe-Cr-Cu-Ni high-entropy alloy at 900℃
CN106011575A (en) Nb-Ti-Ta-C (niobium-titanium-tantalum-carbon) alloy bar and preparation method thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20161026