CN108585907A - A kind of Cr2The self-sealing silicon carbide ceramic based composite material and preparation method thereof that AlC is modified - Google Patents
A kind of Cr2The self-sealing silicon carbide ceramic based composite material and preparation method thereof that AlC is modified Download PDFInfo
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Abstract
The invention belongs to ceramic matric composite preparing technical fields, and in particular to a kind of Cr2The self-sealing silicon carbide ceramic based composite material and preparation method thereof that AlC is modified.By Cr2AlC particles are mixed into the matrix slurry for preparing ceramic matric composite, after being prepared into prepreg with fiber, by hot pressing, charing, melting silicon infiltration up to Cr2The self-sealing silicon carbide ceramic based composite material that AlC is modified.Under hot environment, when crack propagation to self-healing phase Cr2At AlC particles, Cr2AlC, which can be aoxidized, generates glass phase packing hole and crackle, the further diffusion of the surrounding mediums such as blocking oxygen, the effect of to play self-healing.In addition, the unique layer structures of Cr2AlC itself are conducive to increase the toughness of matrices of composite material.
Description
Technical field
The invention belongs to ceramic matric composite preparing technical fields, and in particular to a kind of Cr2The self-healing carbon that AlC is modified
SiClx ceramic matric composite and preparation method thereof.
Background technology
As novel high thrust-weight ratio aero-engine high-temperature structural material, ceramic matric composite is overcoming ceramic material
While brittleness, also there are the feature performance benefits such as specific strength height, high temperature resistant.Due to the shadow by factors such as moulding process and internal structures
It rings, ceramic matric composite is inevitably present the faults of construction such as hole and micro-crack, these defects can be the rings such as oxygen
Border medium provides transmission channel, at high temperature so that material internal suffers erosion, to seriously affect the service life of material.Cause
This, studies the ceramic matric composite with self-healing capability and is of great significance.
Self-healing ceramic matric composite is a kind of high-tech composite material to be got up based on bionics concept development, its energy
Enough crackles (or in the case where imposing environmental stimuli) invisible caused by the external world are repaired automatically, and crackle is made to be cured substantially
It closes, to achieve the purpose that performance can continue to, a kind of new method is provided for prevention is potentially hazardous.
In recent years, (ternary transition metal compound, wherein M are transition metal element to MAX phase ceramics;A is major element;X
For C or N) determine that it takes into account the excellent specific property of metal and ceramic material and by extensive due to its own unique structure
Concern.Some researches show that MAX phase ceramics, and significant self-healing capability can be shown under high-temperature oxygen atmosphere, most common to have
Ti3AlC2、Ti2AlC and Cr2AlC, self-healing mechanism are all by generating firm glass phase α-Al in crack surfaces2O3, from
And the further diffusion of oxide isolation is prevented, to achieve the purpose that the self-healing of material, prolong the service life.And for Ti-Al-
The MAX phases of C ternary systems generate α-Al after oxidation2O3While will additionally generate the porous TiO for easily causing matrix defect2, instead
Material mechanical performance is restricted to improve.Cr2AlC is as novel self-healing MAX phases in recent years, at high temperature prior to crack surfaces
Generate fine and close oxidation product α-Al2O3, it is conducive to the healing of crackle in ceramic matrix, still, since the ceramic hardness is low and is used for
Judge its can temperature limit ductile-brittle transition temperature (BDTT)≤1050 DEG C, therefore be not particularly suited for as thermal structure material
Material is used alone.
The document overwhelming majority for being related to high temperature self-healing ceramics both at home and abroad is to utilize existing boron-containing compound in matrix
It is oxidized to glassy state mobile phase packing matrix cracking at high temperature, barrier is provided to material internal diffusion for oxygen, it is final to send out
Wave self-healing function.But some researches show that more than 1100 DEG C oxidation product B2O3It will largely volatilize so that self-healing is mutually broken
It is bad.
Invention content
The present invention is for insufficient a kind of Cr of proposition in the prior art2The self-sealing silicon carbide ceramic base that AlC is modified is compound
Material and preparation method thereof.Technical solution of the invention includes the following steps:
Step 1:By Cr2AlC powders, graphite powder and phenolic resin are added in ethyl alcohol, ball milling 12h~be uniformly mixed for 24 hours.Institute
State phenolic resin: Cr2AlC powder: graphite powder: the quality parts ratio of ethyl alcohol is 30~80: 20~60: 10~50: 110~290.
Step 2:Silicon carbide fibre fabric containing interfacial TCO layer is impregnated in the slurry that step 1 obtains, it is pre- that fiber is made
Leaching material.
Step 3:The prepreg that step 2 is obtained is clipped, hot-forming, is demoulded after cooling, obtains precast body.The heat
It is 120 DEG C~300 DEG C to press temperature, and pressure is 1MPa~10MPa, and hot pressing time is 0.5h~3h.
Step 4:The precast body that step 3 is obtained cracks processing 6h~for 24 hours at 700 DEG C~900 DEG C, and it is porous that charcoal is made
Body.
Step 5:It is cube that Si powder, which is cold-pressed at 10MPa~15MPa, is positioned under charcoal porous body, the Si powder with
The mass ratio 1.5~6: 1 of charcoal porous body.In the case where temperature is 1400 DEG C~1500 DEG C, 10min~60min is kept the temperature, the anti-of Si is passed through
Infiltration should be melted, Cr is obtained2The self-sealing silicon carbide ceramic based composite material that AlC is modified.
The Cr2The grain size of AlC powders is 1 μm~50 μm;The grain size of graphite powder powder is 1~5 μm.
Advantages of the present invention and advantageous effect are:The present invention is modified using MAX with respect to silicon carbide substrate, by Cr2AlC
Self-healing feature apply in carbon/silicon carbide ceramic matrix composite.1. there is self-healing capability by being introduced in SiC matrix
Cr2AlC particles form polynary self-healing system by self-healing constituent element together with the mutual disperse of SiC constituent elements.SiC matrix sheet
Body have certain self-healing capability, and when surrounding medium by crack propagation to self-healing phase when, Cr2AlC and surrounding medium
Effect generates glass phase Al2O3Packing crackle further stops that surrounding medium enters, to realize the material after healing 1500
Still there is excellent oxidation resistance under DEG C high temperature;②Cr2The coefficient of thermal expansion of AlC matches with SiC matrix material, the two
It can be good at combining.Meanwhile the glass phase Al of generation2O3It is well combined with matrix, no peeling phenomenon so that multiple after self-healing
The intensity of condensation material can restore the 75% of green strength;3. due to Cr2AlC has unique stratiform knot as MAX phases itself
Structure, crackle, which will be diffused at bed boundary, to deflect, and on the one hand can effectively be weakened the stress concentration of crack tip, be played toughening
On the other hand the effect of ceramic matric composite extends crackle approach, equally advantageous to extend the diffusion path of surrounding medium
In the service life for improving composite material;4. the melting infiltration that the preparation of this novel self-healing ceramic matric composite uses
(MI) technique, it is with short production cycle compared with PIP and CVI techniques, it is at low cost, it is conducive to engineering application.
Specific implementation mode
Illustrate Cr below in conjunction with specific example2The self-sealing silicon carbide ceramic based composite material and its preparation side that AlC is modified
Method:
Embodiment 1:
Step 1:By 20gCr2AlC powders (5 μm), 50g graphite powders (1 μm) and 80g phenolic resin are added in 290g ethyl alcohol,
Ball milling is uniformly mixed for 24 hours.
Step 2:Silicon carbide fibre fabric containing interfacial TCO layer is impregnated in the slurry that step 1 obtains, it is pre- that fiber is made
Leaching material.
Step 3:The prepreg that step 2 is obtained is clipped, hot-forming, and wherein hot pressing temperature is 160 DEG C, pressure
3MPa, hot pressing time 3h demould after cooling, obtain precast body.
Step 4:The precast body that step 3 is obtained cracks processing 6h at 900 DEG C, and charcoal porous body is made.
Step 5:It is that (cubical size, the density etc. do not influence the step to cube that Si powder is cold-pressed at 10MPa
Reaction process) be positioned under charcoal porous body, the quality of wherein Si powder is 2 times of charcoal porous body.It is protected at being 1500 DEG C in temperature
Cr is obtained by the reaction with porous body using melt of si infiltration in warm 10min2The self-sealing silicon carbide ceramic based composite material that AlC is modified.
Embodiment 2:
Step 1:By 50gCr2150g ethyl alcohol is added in AlC powders (25 μm), 30g graphite powders (3 μm) and 60g phenolic resin
In, ball milling 12h is uniformly mixed.
Step 2:Silicon carbide fibre fabric containing interfacial TCO layer is impregnated in the slurry that step 1 obtains, it is pre- that fiber is made
Leaching material.
Step 3:The prepreg that step 2 is obtained is clipped, hot-forming, and wherein hot pressing temperature is 200 DEG C, pressure
5MPa, hot pressing time 2h demould after cooling, obtain precast body.
Step 4:The precast body that step 3 is obtained cracks processing 12h at 730 DEG C, and charcoal porous body is made.
Step 5:It is that (cubical size, the density etc. do not influence the step to cube that Si powder is cold-pressed at 12MPa
Reaction process) be positioned under charcoal porous body, the quality of wherein Si powder is 2.6 times of charcoal porous body.In the case where temperature is 1480 DEG C
15min is kept the temperature, the self-sealing silicon carbide ceramic base composite wood of Cr2AlC modifications is obtained by the reaction with porous body using melt of si infiltration
Material.
Embodiment 3:
Step 1:By 30gCr2150g ethyl alcohol is added in AlC powders (50 μm), 60g graphite powders (5 μm) and 40g phenolic resin
In, ball milling 18h is uniformly mixed.
Step 2:Silicon carbide fibre fabric containing interfacial TCO layer is impregnated in the slurry that step 1 obtains, it is pre- that fiber is made
Leaching material.
Step 3:The prepreg that step 2 is obtained is clipped, hot-forming, and wherein hot pressing temperature is 260 DEG C, pressure
8MPa, hot pressing time 1.5h demould after cooling, obtain precast body.
Step 4:For 24 hours, charcoal porous body is made in the precast body that step 3 is obtained cracking processing at 850 DEG C.
Step 5:It is that (cubical size, the density etc. do not influence the step to cube that Si powder is cold-pressed at 15MPa
Reaction process) be positioned under charcoal porous body, the quality of wherein Si powder is 5.8 times of charcoal porous body.In the case where temperature is 1400 DEG C
60min is kept the temperature, Cr is obtained by the reaction with porous body using melt of si infiltration2The self-sealing silicon carbide ceramic base composite wood that AlC is modified
Material.
Claims (2)
1. a kind of Cr2The self-sealing silicon carbide ceramic based composite material and preparation method thereof that AlC is modified, it is characterised in that following step
Suddenly:
Step 1:By Cr2AlC powders, graphite powder and phenolic resin are added in ethyl alcohol, ball milling 12h~be uniformly mixed for 24 hours, the phenol
Urea formaldehyde: Cr2AlC powder: graphite powder: the quality parts ratio of ethyl alcohol is 30~80: 20~60: 10~50: 110~290;
Step 2:Silicon carbide fibre fabric containing interfacial TCO layer is impregnated in the slurry that step 1 obtains, fiber prepreg material is made;
Step 3:The prepreg that step 2 is obtained is clipped, hot-forming, is demoulded after cooling, obtains precast body, the hot pressing temperature
Degree is 120 DEG C~300 DEG C, and pressure is 1MPa~10MPa, and hot pressing time is 0.5h~3h;
Step 4:The precast body that step 3 is obtained cracks processing 6h~for 24 hours at 700 DEG C~900 DEG C, and charcoal porous body is made;
Step 5:It is cube that Si powder is cold-pressed at 10MPa~15MPa, is positioned under charcoal porous body, and the Si powder and charcoal are more
The mass ratio of hole body is 1.5~6: 1, in the case where temperature is 1400 DEG C~1500 DEG C, keeps the temperature 10min~60min, passes through the reaction of Si
Melting infiltration, obtains Cr2The self-sealing silicon carbide ceramic based composite material that AlC is modified.
2. a kind of Cr according to claim 12The preparation method for the self-sealing silicon carbide ceramic based composite material that AlC is modified,
It is characterized in that:The Cr2The grain size of AlC powders is 1 μm~50 μm;The grain size of graphite powder powder is 1~5 μm.
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113943160A (en) * | 2021-10-15 | 2022-01-18 | 中国航发北京航空材料研究院 | Preparation method of silicon carbide ceramic matrix composite with self-repairing function |
CN115286401A (en) * | 2022-06-29 | 2022-11-04 | 武汉科技大学 | Cr (chromium) 2 AlC combined silicon carbide refractory material and preparation method thereof |
Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090041609A1 (en) * | 2007-08-07 | 2009-02-12 | Duz Volodymyr A | High-strength discontinuously-reinforced titanium matrix composites and method for manufacturing the same |
CN101486588A (en) * | 2009-03-04 | 2009-07-22 | 中南大学 | Preparation of carbon fiber reinforced carbon-silicon carbide double matrix friction material |
CN101503305A (en) * | 2009-02-03 | 2009-08-12 | 西北工业大学 | Process for preparing self-sealing silicon carbide ceramic based composite material |
CN101508591A (en) * | 2008-11-10 | 2009-08-19 | 西北工业大学 | Process for producing composite material of Ti3SiC2 modified C/SiC |
CN101745432A (en) * | 2008-12-03 | 2010-06-23 | 中国科学院金属研究所 | Wet-chemical method for preparing MAX phase porous catalyst carrier material |
CN102470630A (en) * | 2009-09-28 | 2012-05-23 | 斯奈克玛动力部件公司 | Composite material part having a ceramic matrix, and method for manufacturing same |
CN103910532A (en) * | 2013-01-05 | 2014-07-09 | 中国科学院宁波材料技术与工程研究所 | Coating inorganic fiber toughened MAX phase ceramic composite material, preparation method and uses thereof |
CN103998396A (en) * | 2011-11-30 | 2014-08-20 | 赫拉克勒斯公司 | CMC material part manufacture method |
WO2015080839A1 (en) * | 2013-11-26 | 2015-06-04 | United Technologies Corporation | Gas turbine engine component coating with self-healing barrier layer |
CN106065487A (en) * | 2016-07-15 | 2016-11-02 | 河南大学 | The method that in molten salt system, pulse electrodeposition prepares SiC fiber reinforced magnesium base composite material precursor wire |
CN106083117A (en) * | 2016-06-21 | 2016-11-09 | 中国科学院宁波材料技术与工程研究所 | There is fiber reinforced ceramic matric composite of ternary layered MAX phase boundary surface layer and preparation method thereof |
US20170057879A1 (en) * | 2015-08-28 | 2017-03-02 | Rolls-Royce High Temperature Composites, Inc. | Ceramic Matrix Composite Including Silicon Carbide Fibers In a Ceramic Matrix Comprising a Max Phase Compound |
CN107098702A (en) * | 2017-04-21 | 2017-08-29 | 中国航发北京航空材料研究院 | A kind of preparation method of near-net-shape silicon carbide reaction-sintered material |
-
2018
- 2018-05-03 CN CN201810413978.9A patent/CN108585907B/en active Active
Patent Citations (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090041609A1 (en) * | 2007-08-07 | 2009-02-12 | Duz Volodymyr A | High-strength discontinuously-reinforced titanium matrix composites and method for manufacturing the same |
CN101508591A (en) * | 2008-11-10 | 2009-08-19 | 西北工业大学 | Process for producing composite material of Ti3SiC2 modified C/SiC |
CN101745432A (en) * | 2008-12-03 | 2010-06-23 | 中国科学院金属研究所 | Wet-chemical method for preparing MAX phase porous catalyst carrier material |
CN101503305A (en) * | 2009-02-03 | 2009-08-12 | 西北工业大学 | Process for preparing self-sealing silicon carbide ceramic based composite material |
CN101486588A (en) * | 2009-03-04 | 2009-07-22 | 中南大学 | Preparation of carbon fiber reinforced carbon-silicon carbide double matrix friction material |
CN102470630A (en) * | 2009-09-28 | 2012-05-23 | 斯奈克玛动力部件公司 | Composite material part having a ceramic matrix, and method for manufacturing same |
CN103998396A (en) * | 2011-11-30 | 2014-08-20 | 赫拉克勒斯公司 | CMC material part manufacture method |
CN103910532A (en) * | 2013-01-05 | 2014-07-09 | 中国科学院宁波材料技术与工程研究所 | Coating inorganic fiber toughened MAX phase ceramic composite material, preparation method and uses thereof |
WO2015080839A1 (en) * | 2013-11-26 | 2015-06-04 | United Technologies Corporation | Gas turbine engine component coating with self-healing barrier layer |
EP3074619A1 (en) * | 2013-11-26 | 2016-10-05 | United Technologies Corporation | Gas turbine engine component coating with self-healing barrier layer |
US20170057879A1 (en) * | 2015-08-28 | 2017-03-02 | Rolls-Royce High Temperature Composites, Inc. | Ceramic Matrix Composite Including Silicon Carbide Fibers In a Ceramic Matrix Comprising a Max Phase Compound |
US9856176B2 (en) * | 2015-08-28 | 2018-01-02 | Rolls-Royce High Temperature Composites, Inc. | Ceramic matrix composite including silicon carbide fibers in a ceramic matrix comprising a max phase compound |
CN106083117A (en) * | 2016-06-21 | 2016-11-09 | 中国科学院宁波材料技术与工程研究所 | There is fiber reinforced ceramic matric composite of ternary layered MAX phase boundary surface layer and preparation method thereof |
CN106065487A (en) * | 2016-07-15 | 2016-11-02 | 河南大学 | The method that in molten salt system, pulse electrodeposition prepares SiC fiber reinforced magnesium base composite material precursor wire |
CN107098702A (en) * | 2017-04-21 | 2017-08-29 | 中国航发北京航空材料研究院 | A kind of preparation method of near-net-shape silicon carbide reaction-sintered material |
Non-Patent Citations (5)
Title |
---|
ANN-SOPHIE FARLE 等: "A conceptual study into the potential of Mn+1AXn-phase ceramics for self-healing of crack damage", 《JOURNAL OF EUROPEAN CERAMIC SOCIETY》 * |
J. GONZALEZ-JULIAN 等: "Novel Cr2AlC MAX-phase/SiC fiber composites: Synthesis, processingand tribological response", 《JOURNAL OF THE EUROPEAN CERAMIC SOCIETY》 * |
焦健: "界面层对SiCf/SiC 复合材料力学性能及氧化行为的影响", 《航空制造技术》 * |
陈照峰 等: "《无机非金属材料学》", 28 February 2016, 西北工业大学出版社 * |
雷宇 等: "三元层状陶瓷材料Cr2AlC的研究进展", 《西华大学学报》 * |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113943160A (en) * | 2021-10-15 | 2022-01-18 | 中国航发北京航空材料研究院 | Preparation method of silicon carbide ceramic matrix composite with self-repairing function |
CN113943160B (en) * | 2021-10-15 | 2022-08-09 | 中国航发北京航空材料研究院 | Preparation method of silicon carbide ceramic matrix composite with self-repairing function |
CN115286401A (en) * | 2022-06-29 | 2022-11-04 | 武汉科技大学 | Cr (chromium) 2 AlC combined silicon carbide refractory material and preparation method thereof |
CN115286401B (en) * | 2022-06-29 | 2023-03-31 | 武汉科技大学 | Cr (chromium) 2 AlC combined silicon carbide refractory material and preparation method thereof |
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