CN1344810A - In-situ compounding process of preparing silicon carbide particle reinforced molybdenum silicide based composite material - Google Patents
In-situ compounding process of preparing silicon carbide particle reinforced molybdenum silicide based composite material Download PDFInfo
- Publication number
- CN1344810A CN1344810A CN 01141978 CN01141978A CN1344810A CN 1344810 A CN1344810 A CN 1344810A CN 01141978 CN01141978 CN 01141978 CN 01141978 A CN01141978 A CN 01141978A CN 1344810 A CN1344810 A CN 1344810A
- Authority
- CN
- China
- Prior art keywords
- mosi
- sic
- temperature
- reaction
- matrix material
- 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.)
- Granted
Links
Images
Landscapes
- Ceramic Products (AREA)
Abstract
By means of controlling the compounding technological parameters of in-situ, eliminating the low temperature solid-solid reaction among Mo, Si and C element powder and utilizing the their soild-liquid reaction, composite MoSi2-SiC powder is in-situ compounded and densified through secondary heating so as to prepare fine dispersed SiC particle reinforced MoSi2 composite two-phase material with clean interface and no SiO2 glass phase and other transition phases. The composite material has high temperature oxidation resistance of MoSi2, improved low temperature and high temperature mechanical performance as well as the preparation process is easy to control and simple in equipment.
Description
Technical field:
The invention belongs to the alloy material preparation field, particularly the preparation of intermetallic compound silicon molybdenum thing based composites.
Background technology:
MoSi
2Has fusing point, lower density (6.24g/cm up to 2030~2050 ℃
3), good resistance of oxidation with the thermal conductivity of metal same level and low thermal expansivity, can satisfy the basic demand as high-temperature structural material.The more important thing is that though this compound shows the fragility same with pottery in room temperature, it has the tough-brittle transition behavior, more than ductile-brittle transition temperature, the motion of dislocation and significant reaction activate, and intensity is controlled by plastic deformation.Therefore, under use temperature, will have higher reliability than structural ceramics.In addition, MoSi
2Can or form matrix material with considerable element and compounds aurification, make it keep Thermodynamically stable.Like this, just multiple means and possibility are provided for improving performance.Therefore, MoSi
2Be considered to the high-temperature structural material that has competitive power that occurs after the structural ceramics of Ni, Ti superalloy and use temperature>1000 of 800~1000 ℃ of use temperatures ℃, getting a good chance of as use temperature is that 1000~1600 ℃ various high-temperature structural materials are used.
But low toughness under the room temperature, high temperature down with the deficiency of ceramic phase specific tenacity, particularly lower creep resistance is hanged down and has been limited MoSi
2Application as high-temperature structural material.Therefore keeping MoSi
2Under the prerequisite that oxidation-resistance does not reduce substantially, how to improve MoSi
2Low-temperature flexibility and hot strength are exploitation MoSi
2The key of high-temperature structural material.Existing work shows that soft or hard second phase can be improved its room temperature and mechanical behavior under high temperature simultaneously.In numerous enhancing bodies, SiC has good chemical stability, high intensity and Young's modulus, and low thermal expansivity, high fusing point is with MoSi
2Good chemical compatibility and physical compatibility are arranged, same MoSi
2-sample has good oxidation-resistance, is considered to strengthen MoSi
2One of the most effective enhancing body.
At present, preparation MoSi
2The original position recombining process of-SiC matrix material has: replacement(metathesis)reaction, reactive plasma deposition, mechanical alloying, XD
TM, burning synthetic induction heating thermal explosion pattern, the auxiliary SHS that reaches of electric field add quasi-hot isostatic pressing simultaneously, and the reaction of direct hot pressing element simple substance mixture and element powders is synthetic synchronously etc.Wherein, replacement(metathesis)reaction (Henager C H Jr, et al.Mater.Sci.Eng.A, 1992, A155:109~114), reactive plasma deposition (Lawrynowicz D E, et al.High-Temperature Ordered IntermetallicsAlloy VI, P923.), mechanical alloying (Jayashankar S, et al.J.Mater.Res., 1428~1441.), XD 1993,8 (6):
TMIn the sample of (Aikin R M Jr, et al.Mater.Sci.Eng.A, 1992, A155:121~133.) these prepared except MoSi
2Outside the SiC two-phase, all there is other transition phases (Mo for example to some extent
5Si
3, Mo
≤ 5Si
3C
≤ 1Deng) and glassy phase, and former three second phase volume fraction can not arbitrarily be regulated and control XD
TMProcess using hot pressing and hot isostatic pressing two procedures are compact formed, and preparation section is many, control is quite complicated; Burning synthetic sample is because the too fast structural constituent of reaction is difficult to control, there is macrosegregation, tissue odds is even, sometimes also reaction is incomplete, the hot-forming back second phase SiC particle is obviously assembled, size big (up to 20 μ m), and equipment complexity (Chrysanthou A, et al.J.Mater.Sci., 1996,31 (16): 4221~4226; Bartlett A H et al.J.Mater.Sci., 1998,33 (6): 1653~1660.); Direct hot pressing element simple substance mixture (Alman D E, et al.Scrip.Metall.Mater., 1994,273~278.) and synthetic synchronously (the Alman D E of the reaction of element powders 31 (3):, et al.Scrip.Metall.Mater., 1993,28 (12): 1525~1530) also have transition phase in Zhi Bei the sample, and the former C fiber does not change into SiC fully, reaction not exclusively, the synthetic synchronously compact formed matrix material of hot isostatic pressing technique that adopts of the reaction of element powders, the equipment complexity, the cost height, the second phase SiC particle size is big, assemble serious, skewness.The MoSi of above-mentioned many prepared
2The mechanical property that the appearance meeting of glassy phase significantly reduces material in the-SiC matrix material is mechanical behavior under high temperature especially, and the second phase SiC particle size is big, assemble remarkable improvement serious, that skewness also is unfavorable for composite materials property, and Mo
5Si
3Can reduce the high temperature oxidation resistance of matrix material etc. the existence of transition phase.
The objective of the invention is to prepare silicon carbide particle reinforced molybdenum silicide based composite material, do not reducing MoSi by control original position recombining process parameter
2Under the prerequisite of high temperature oxidation resistance, improve MoSi to greatest extent
2The low temperature of-SiC matrix material and mechanical behavior under high temperature, and technology is easy to control, equipment is simple.
Summary of the invention:
The present invention is by control original position recombining process parameter, solid eliminate low temperature between Mo, Si and the C element powder solid-reaction, and utilize the solid-liquid reaction original position between them to synthesize MoSi
2-SiC composite powder, and with fine and close this MoSi of secondary hot pressing
2-SiC composite powder prepares interface cleaning, no SiO
2Glassy phase and Mo
5Si
3, Mo
≤ 5Si
3C
≤ 1Wait other transition phases, small and dispersed SiC particle to strengthen MoSi
2Two-phase composite material.The concrete related MoSi of the present invention
2The chemical constitution of-SiC matrix material by volume per-cent is MoSi
2-0%SiC~MoSi
2-100%SiC, the content of element powders calculates by the stoichiometric ratio of corresponding composition proportioning matrix material.The concrete preparation process of matrix material is as follows: be pressed into the green compact sample after element powders is weighed up and mixes by proportioning, green density is 60~75% of a mixed powder theoretical density.The green compact sample carries out reaction in and synthesizes after 400~600 ℃ of vacuum outgass in the mobile pure argon, stove is chilled to room temperature then.Reaction in synthetic technology is: 1410~1470 ℃ of temperature, 120 ℃/min of temperature rise rate, soaking time 0.5~1h.After material fragmentation with reaction in after synthetic becomes 180 μ m~450 μ m powder, carry out hot-forming, 1700~1750 ℃ of temperature, soaking time 1~2h, 30~the 40MPa that exerts pressure is cooled to 400~500 ℃ with the speed of 10~20 ℃/min, naturally cools to room temperature at last.Decompression gradually behind pressurize to 1200 in the process of cooling after hot pressing~1300 ℃.All the time feeding mobile Ar gas in the hot pressing protects.
The invention has the advantages that by control original position recombining process parameter, solid can eliminate low temperature between Mo, Si and the C element powder solid-reaction, effectively utilize the solid-liquid reaction original position between them to synthesize MoSi
2~SiC composite powder by secondary hot pressing, makes the matrix material of the densification of acquisition can guarantee to have only MoSi again
2With the SiC two-phase, interface cleaning, no SiO
2Glassy phase and Mo
5Si
3, Mo
≤ 5Si
3C
≤ 1Wait other transition phases, the second phase SiC particle small and dispersed to be distributed in MoSi
2On the matrix, therefore, this matrix material can be guaranteed do not reducing MoSi
2In the time of high temperature oxidation resistance, can improve the low temperature and the mechanical behavior under high temperature of matrix material to greatest extent.Because the present invention only need control original position recombining process parameter, need not hot isostatic apparatus, so technology easy, be easy to control, equipment is simple.
Description of drawings:
Fig. 1 is MoSi
2The XRD spectral line of-SiC matrix material.
Fig. 2 is MoSiC30 matrix material MoSi
2HREM picture with SiC two-phase phase boundary.
Fig. 3 is the metallographic structure of MoSiC30 matrix material.
Fig. 4 is MoSi
2-SiC matrix material room temperature fracture toughness property is with the variation of SiC volume fraction.
Fig. 5 is single MoSi
2(a) and MoSiC30 (b) compression true stress-strain curve.
Synthetic and the commercial powder MoSi that mixes of hot pressing of original position when Fig. 6 is stress 80MPa
2The creep curve of-30%SiC relatively.
Embodiment
Embodiment: test MoSi
2The chemical constitution of-SiC matrix material by volume per-cent is MoSi
2-30%SIC writes a Chinese character in simplified form into MoSiC30, and the content of element powders is calculated as by the stoichiometric ratio of forming MoSiC30: Mo: Si: C=51.71: 42.90: 5.39wt%.Used starting material are Mo powder, Si powder and Graphite Powder 99, and mean particle size and purity are Mo:8 μ m, 99.0%; Si:7 μ m, 99.0%; C:22, μ m, 99.9%.After element powders weighed up by proportioning, add the different ZrO of an amount of diameter
2Ball and dehydrated alcohol, wet mixing 10h on the roller ball mill.The powder that mixes is pressed into φ 30 * 15mm circle base sample, and pressed density is 70% of a mixed powder theoretical density.Circle base sample carries out original position in the pure argon 99.91% after 500 ℃ of vacuum outgass synthetic, and stove is chilled to room temperature then.Concrete technology is: 1450 ℃ of temperature, 120 ℃/min of temperature rise rate, soaking time 1h.After material fragmentation with reaction in after synthetic becomes 180 μ m powder, carry out hot-formingly, pressed compact is of a size of about φ 50mm * 8mm, 1740 ℃ of temperature, soaking time 2h, 40MPa exerts pressure, speed with 10 ℃/min is cooled to 500 ℃, naturally cools to room temperature at last.Decompression gradually after the pressurize to 1300 ℃ in the process of cooling after hot pressing.All the time feeding mobile Ar gas in the hot pressing protects.
The MoSiC30 matrix material that obtains through above-mentioned technology only contains MoSi
2With the SiC two-phase, do not contain Mo
5Si
3, Mo
≤ 5Si
3C
≤ 1Wait other transition phases, nor have SiO
2Glassy phase, interface cleanness are seen Fig. 1, Fig. 2.The SiC particle size is 3~5 μ m, and evenly tiny, disperse is distributed in MoSi
2On the matrix, see Fig. 3.The porosity of this matrix material is (0.044 ± 0.014) %, can think to reach complete densification.The room temperature fracture toughness property of this material is than single MoSi
2Have clear improvement, see Fig. 4.1000 ℃, 1200 ℃, 1400 ℃ high temperature compressed flow curve is apparently higher than single MoSi
2, its high-temperature stream varying stress, yield strength significantly improve, and see Fig. 5.Its high temperature creep drag is much higher than the MoSi of the prior powder metallurgy prepared that adopts the commercial mixed powder of hot pressing
2-30%SiC matrix material is seen Fig. 6.
Claims (2)
1, a kind of in-situ compounding process for preparing silicon carbide particle reinforced molybdenum silicide based composite material, MoSi
2The chemical constitution of-SiC matrix material by volume per-cent is MoSi
2-0%SiC~MoSi
2-100%SiC, the content of element powders calculates by the stoichiometric ratio of forming this matrix material, it is characterized in that reaction in synthetic technology is: 1410~1470 ℃ of temperature, temperature rise rate 〉=120 ℃/min, soaking time 0.5~1h.After material fragmentation with reaction in after synthetic becomes-40~-80 order powder, carry out hot-forming, 1700~1750 ℃ of temperature, soaking time 1~2h, 30~the 40MPa that exerts pressure is cooled to 400~500 ℃ with the speed of 10~20 ℃/min, naturally cools to room temperature at last.Decompression gradually after 1200~1300 ℃ in the process of cooling after hot pressing.
2, in-situ compounding process as claimed in claim 1, the preparation that it is characterized in that matrix material are to be pressed into the green compact sample after element powders is weighed up and mixes by proportioning, and green density is 60~75% of a mixed powder theoretical density.The green compact sample carries out reaction in and synthesizes after 400~600 ℃ of vacuum outgass in the mobile pure argon.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 01141978 CN1215185C (en) | 2001-09-26 | 2001-09-26 | In-situ compounding process of preparing silicon carbide particle reinforced molybdenum silicide based composite material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 01141978 CN1215185C (en) | 2001-09-26 | 2001-09-26 | In-situ compounding process of preparing silicon carbide particle reinforced molybdenum silicide based composite material |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1344810A true CN1344810A (en) | 2002-04-17 |
CN1215185C CN1215185C (en) | 2005-08-17 |
Family
ID=4676531
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 01141978 Expired - Fee Related CN1215185C (en) | 2001-09-26 | 2001-09-26 | In-situ compounding process of preparing silicon carbide particle reinforced molybdenum silicide based composite material |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN1215185C (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1321092C (en) * | 2006-03-14 | 2007-06-13 | 西北工业大学 | Method for preparing anti-oxidation multiple phase coating of carbon/carbon composite material surface |
CN101812622B (en) * | 2010-02-08 | 2011-07-20 | 吉林大学 | Ceramic-intermetallic compound composite material containing binder and preparation method thereof |
CN101386551B (en) * | 2008-10-29 | 2011-12-28 | 陕西科技大学 | Method for preparing carbon/carbon compound material nano silicon carbide-silicon molybdenum composite coating |
CN104261835A (en) * | 2014-09-19 | 2015-01-07 | 中南大学 | Method for preparing molybdenum disilicide heating element |
CN105731471A (en) * | 2016-01-28 | 2016-07-06 | 陕西科技大学 | Preparation method of MoSi2-Mo5Si3-SiO2 composite material |
-
2001
- 2001-09-26 CN CN 01141978 patent/CN1215185C/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1321092C (en) * | 2006-03-14 | 2007-06-13 | 西北工业大学 | Method for preparing anti-oxidation multiple phase coating of carbon/carbon composite material surface |
CN101386551B (en) * | 2008-10-29 | 2011-12-28 | 陕西科技大学 | Method for preparing carbon/carbon compound material nano silicon carbide-silicon molybdenum composite coating |
CN101812622B (en) * | 2010-02-08 | 2011-07-20 | 吉林大学 | Ceramic-intermetallic compound composite material containing binder and preparation method thereof |
CN104261835A (en) * | 2014-09-19 | 2015-01-07 | 中南大学 | Method for preparing molybdenum disilicide heating element |
CN105731471A (en) * | 2016-01-28 | 2016-07-06 | 陕西科技大学 | Preparation method of MoSi2-Mo5Si3-SiO2 composite material |
CN105731471B (en) * | 2016-01-28 | 2017-12-05 | 陕西科技大学 | A kind of MoSi2‑Mo5Si3‑SiO2The preparation method of composite |
Also Published As
Publication number | Publication date |
---|---|
CN1215185C (en) | 2005-08-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101215173B (en) | Method for preparing ZrB2-SiC-ZrC diphase ceramic material | |
CN106834878B (en) | A kind of method that microwave sintering prepares endogenous high-entropy alloy-base composite material | |
CN101456737B (en) | Boron carbide base composite ceramic and preparation method thereof | |
JPS5924751B2 (en) | Sintered shaped body | |
CA2178819A1 (en) | Low temperature, pressureless sintering of silicon nitride | |
CN104045350B (en) | Method for preparing silicon nitride /silicon carbide ceramic composite by use of reaction sintering process | |
CN104894641B (en) | It is a kind of high fine and close(LaxCa1‑x)B6Polycrystalline cathode material and preparation method thereof | |
CN108439995B (en) | Complex phase ceramic and preparation method thereof | |
CN102219536A (en) | B4C/SiC whisker/SiC multiphase ceramic matrix composite and preparation method thereof | |
CN109295336A (en) | A kind of reticular structure titanium silicon mutually enhances the preparation method of TiAl based composites | |
CN105859301A (en) | Silicon nitride ceramic and preparation method thereof | |
CN102976760A (en) | RE2O3-added ZrB2-SiC composite ceramic material and preparation method thereof | |
CN101407421B (en) | Method for preparing non-grain boundary phase porous silicon nitride ceramic based on siliconizing nitridation | |
Izhevskyi et al. | Microstructure and properties tailoring of liquid-phase sintered SiC | |
Souto et al. | Sintering of commercial mulite powder: Effect of MgO dopant | |
CN1215185C (en) | In-situ compounding process of preparing silicon carbide particle reinforced molybdenum silicide based composite material | |
Zhang et al. | Effects of different types of sintering additives and post-heat treatment (PHT) on the mechanical properties of SHS-fabricated Si3N4 ceramics | |
JPH0222175A (en) | Production and sintering of reaction bonded silicon nitride composite material containing silicon carbide whisker or silicon nitride powder | |
Abilev et al. | Structural-phase state and properties of SiC ceramics obtained by ultrasound-assisted liquid-phase sintering with eutectic additives | |
Sun et al. | Synthesis and consolidation of ternary compound Ti3SiC2 from green compact of mixed powders | |
Lee et al. | Characterization of forsterite ceramics | |
CN107417271A (en) | A kind of preparation method of the bar-shaped brilliant enhancing dimension stone of magnesia alumina spinel of rare earth aluminium (silicon) hydrochlorate | |
CN109053192A (en) | A kind of preparation method of MgAlON transparent ceramic powder | |
CN108411154A (en) | A kind of fire-retardant graphene titanium-aluminium matrix composites and preparation method | |
JPH0812441A (en) | Production of silicon nitride-based sintered compact |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C06 | Publication | ||
PB01 | Publication | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |