CN103396125B - Preparation method for boron-carbon-nitrogen porous ceramic - Google Patents

Preparation method for boron-carbon-nitrogen porous ceramic Download PDF

Info

Publication number
CN103396125B
CN103396125B CN201310331011.3A CN201310331011A CN103396125B CN 103396125 B CN103396125 B CN 103396125B CN 201310331011 A CN201310331011 A CN 201310331011A CN 103396125 B CN103396125 B CN 103396125B
Authority
CN
China
Prior art keywords
carbon nitrogen
boron carbon
organic precursor
bcn
boron
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.)
Expired - Fee Related
Application number
CN201310331011.3A
Other languages
Chinese (zh)
Other versions
CN103396125A (en
Inventor
温广武
张涛
覃春林
钟博
夏龙
宋亮
王新宇
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.)
Harbin Institute of Technology
Harbin Institute of Technology Weihai
Original Assignee
Harbin Institute of Technology Weihai
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 Harbin Institute of Technology Weihai filed Critical Harbin Institute of Technology Weihai
Priority to CN201310331011.3A priority Critical patent/CN103396125B/en
Publication of CN103396125A publication Critical patent/CN103396125A/en
Application granted granted Critical
Publication of CN103396125B publication Critical patent/CN103396125B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Inorganic Fibers (AREA)

Abstract

The invention relates to a preparation method for boron-carbon-nitrogen porous ceramic. A boron-carbon-nitrogen (BCN) organic precursor-polyacrylonitrile fiber compound is prepared by using a boron-carbon-nitrogen (BCN) organic precursor as a binder and nano polyacrylonitrile fibers prepared by an electrostatic spinning method as a skeleton. The compound is sintered under a nitrogen (N2) protection atmosphere in a furnace by heating to a temperature of 1,400 DEG C at a speed of 3 DEG C/min and keeping the temperature for 1.5 h. The BCN porous ceramic prepared by the method is uniform in aperture, simple in process and low in cost, has excellent thermal shock resistance, high temperature oxidation resistance and high specific strength, and is suitable for preparing high-temperature resistant components and thermal insulated components of spacecrafts.

Description

A kind of preparation method of boron carbon nitrogen porous ceramics
Technical field
The present invention relates to a kind of composite ceramic material preparation method, specifically the preparation method of a kind of boron carbon nitrogen (BCN) porous ceramics.It is combined and is prepared BCN porous ceramics by the nano polypropylene nitrile fiber that adopts BCN organic precursor method to prepare with method of electrostatic spinning.
Background technology
Along with the development of modern aerospace technology, traditional lagging material shows obvious deficiency.Research and develop high performance matrix material, become at present one of emphasis of Materials science research in the world.In order to prepare, to be applicable to resistance to elevated temperatures good, the novel material of the heat-proof quality that specific tenacity is high and excellent, and researchist has started to pay close attention to the porous ceramic film material of thermotolerance and scale resistance excellence.Boron carbon nitrogen (BCN) ternary ceramics and other ceramic phase ratio, have density little, can processing, self-lubricating, high strength at high temperature, thermostability and the low expansion that anti-oxidant, dielectricity is adjustable, good.Its oxidation resistance temperature is more much higher than carbon fiber, therefore, is having wide application aspect aerospace flight technology field, the protective layer that can be used as anti-ablation cover, radome, anti-NEUTRON PROTECTION cover and reentry.But the preparation of current most of boron carbon nitrogen (BCN) pottery or the vapour deposition process based on traditional, be difficult to prepare large-sized block ceramic, and boron carbon nitrogen (BCN) material of vesicular structure have not been reported.Because boron carbon nitrogen (BCN) pottery itself is difficult to sintering, high to the purity requirement of raw material, this give prepare boron carbon nitrogen (BCN) porous ceramics, particularly shaped piece, foam, fiber has brought very large difficulty.
Summary of the invention
Technical problem to be solved by this invention be to provide a kind of method simply, easily operation, production cost is low, ceramic porous nickel, the preparation method of the boron carbon nitrogen porous ceramics that high temperature oxidation resistance is good.
The technical scheme that the present invention solves the problems of the technologies described above employing is: a kind of preparation method of boron carbon nitrogen porous ceramics, is characterized in that: it comprises the following steps:
(1) first preparing boron carbon nitrogen (BCN) organic precursor method 1:0.3 ~ 6 is dissolved in trichlorine boron azine and aniline in toluene in molar ratio; Room temperature lower magnetic force stirs 2~5h, then removes by filter white precipitate; Then the filtrate of clarification is placed in to 80~120 ℃ of heating jacket reflux 10~30 minutes, is cooled to room temperature; Under 30~45 ℃ of conditions, unnecessary toluene solvant is fallen in underpressure distillation, obtains faint yellow thick boron carbon nitrogen (BCN) organic precursor method, stand-by;
(2) nano polypropylene nitrile (PAN) fiber of being prepared by method of electrostatic spinning adds in above-mentioned boron carbon nitrogen (BCN) organic precursor method preparing, dipping 10 ~ 15min, then ultrasonic dispersion 15 ~ 35min, obtain boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, wherein polyacrylonitrile nanofiber mass content is 40 ~ 55%, and the mass content of boron carbon nitrogen (BCN) organic precursor method is 60 ~ 45%;
(3) by disperse after boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying in ceramic boat, every layer of boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is of a size of 100 × 100mm, thickness is 1 ~ 5mm, weight 1 ~ 6g; Between every upper and lower two-layer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, spray boron carbon nitrogen (BCN) precursor 2 ~ 5g, boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying number of plies is 15 ~ 50 layers again;
(4) the above-mentioned ceramic boat that boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is housed is gone in sintering oven, and with 3 oc/min rises to 1400 oc is also incubated 1.5h, adopts N in stove 2atmosphere protection; Nitrogen original pressure (Pressure of Ambient Temperature before heating up) is controlled at 1.5 ~ 3.5 MPas (MPa);
(5) insulation cools to room temperature with the furnace after finishing, and can obtain black boron carbon nitrogen (BCN) porous ceramics.
The present invention is take boron carbon nitrogen (BCN) organic precursor method as binding agent, and nano polypropylene nitrile fiber prepared by method of electrostatic spinning is that skeleton is prepared into boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body.Boron carbon nitrogen (BCN) organic precursor method Heat stability is good, does not occur being cross-linked at 150 ℃, cracking phenomenon below.Organic and characteristic inorganic materials are connected, prepare black boron carbon nitrogen (BCN) porous ceramics.Against existing technologies, the inventive method simply, easily operation, reproducible, production cost is low, the boron carbon nitrogen porous ceramics porous nickel of preparation, pottery porosity is adjustable, controls the porosity of B-C-N ceramic by controlling the number of plies of polyacrylonitrile fibre and sintering air pressure.Boron carbon nitrogen porous ceramics high temperature oxidation resistance is good.Ceramic yield can reach 78%.The boron carbon nitrogen porous ceramics of preparation has good heat-shock resistance, high temperature oxidation resistance and high specific tenacity.There is huge using value at spacecraft high temperature resistant component, heat insulating member.
Accompanying drawing explanation
Fig. 1 is the SEM microscopic appearance figure of boron carbon nitrogen (BCN) porous ceramics.
Embodiment
Below in conjunction with embodiment, the present invention will be further described.
A preparation method for boron carbon nitrogen porous ceramics, it comprises the following steps:
(1) prepare boron carbon nitrogen (BCN) organic precursor method.Trichlorine boron azine and aniline are dissolved in toluene 1:0.3 ~ 6 in molar ratio; Room temperature lower magnetic force stirs 2~5h, then removes by filter white precipitate; Then the filtrate of clarification is placed in to 80~120 ℃ of heating jacket reflux 10~30 minutes, is cooled to room temperature; Under 30~45 ℃ of conditions, unnecessary toluene solvant is fallen in underpressure distillation, obtains faint yellow thick boron carbon nitrogen (BCN) organic precursor method, stand-by;
?(2) nano polypropylene nitrile (PAN) fiber of being prepared by method of electrostatic spinning adds in above-mentioned boron carbon nitrogen (BCN) organic precursor method preparing, dipping 10 ~ 15min, then ultrasonic dispersion 15 ~ 35min, make boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, wherein polyacrylonitrile nanofiber mass content is 40 ~ 55%, and the mass content of boron carbon nitrogen (BCN) organic precursor method is 60 ~ 45%;
(3) by boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying in ceramic boat, every layer of boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is of a size of 100 × 100mm, thickness is 1 ~ 5mm, weight 1 ~ 6g; Between every upper and lower two-layer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, spray boron carbon nitrogen (BCN) precursor 2 ~ 5g, boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying number of plies is 15 ~ 50 layers;
(4) above-mentioned multilayer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is placed in to ceramic boat and goes to sintering oven, and with 3 oc/min rises to 1400 oc is also incubated 1.5h, adopts N in stove 2atmosphere protection; Nitrogen original pressure (Pressure of Ambient Temperature before heating up) is controlled at 1.5 ~ 3.5 MPas (MPa);
(5) insulation cools to room temperature with the furnace after finishing, and can obtain black boron carbon nitrogen (BCN) porous ceramics.
BCN porous ceramics scanning electron microscope microscopic appearance prepared by the present invention as shown in Figure 1.Porous nickel distributes as can see from Figure 1, and pore dimension is about 5-10 μ m.Carbon nano fiber diameter after the carbonization of polyacrylonitrile fibre fiber is about 100nm, and middle and boron carbon nitrogen (BCN) lamella interconnects.
Boron carbon nitrogen (BCN) porous ceramics productive rate is the test result 1500 ℃ time according to thermogravimetric analysis (TG).Boron carbon nitrogen (BCN) ceramic yield=(quality m after 1500 ℃ of thermal treatments 1)/(spraying BCN precursor quality m 2+ PAN fiber quality m 3).
The molecular-weight average of boron carbon nitrogen (BCN) precursor is affected by the consumption of polymerization time, temperature and aniline.In polymerized at room temperature process, increase successively to 5h molecular-weight average from 2h; Polymerization temperature is higher, the corresponding also increase of precursor molecular-weight average obtaining; At polymerization time 2h, trichlorine boron azine: aniline=1:0.3(mol ratio) time, molecular weight minimum 2261; Polymerization time 5h arrives trichlorine boron azine: when aniline=1:4.5, molecular-weight average has maximum 6782.When trichlorine boron azine: form white solid when aniline=1:6.
Embodiment 1: a kind of preparation method of boron carbon nitrogen porous ceramics, it comprises the following steps:
(1) prepare boron carbon nitrogen (BCN) organic precursor method by trichlorine boron azine and aniline in molar ratio 1:0.3 be dissolved in toluene; Room temperature lower magnetic force stirs 2h, then removes by filter white precipitate; Then the filtrate of clarification is placed in to 80 oin C heating jacket, reflux 10 minutes, is cooled to room temperature; Under 35 ℃ of conditions, unnecessary toluene solvant is fallen in underpressure distillation, obtains faint yellow thick boron carbon nitrogen (BCN) organic precursor method, stand-by;
(2) nano polypropylene nitrile (PAN) fiber of being prepared by method of electrostatic spinning adds in above-mentioned boron carbon nitrogen (BCN) organic precursor method preparing, dipping 10min, then ultrasonic dispersion 15min, make boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, wherein polyacrylonitrile nanofiber mass content is 40%, and the mass content of boron carbon nitrogen (BCN) organic precursor method is 60%;
(3) by boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying in ceramic boat, every layer of boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is of a size of 100 × 100mm, thickness is 1mm, weight 1g; Between every upper and lower two-layer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, spray boron carbon nitrogen (BCN) precursor 2g, boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying number of plies is 15 layers;
(4) above-mentioned multilayer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is placed in to ceramic boat and goes to sintering oven, and with 3 oc/min rises to 1400 oc is also incubated 1.5h, adopts N in stove 2atmosphere protection; Nitrogen original pressure (Pressure of Ambient Temperature before heating up) is controlled at 3.5 MPas (MPa);
(5) insulation cools to room temperature with the furnace after finishing, and can obtain black boron carbon nitrogen (BCN) porous ceramics.
B-C-N ceramic productive rate is 72.5%, and porosity is 58%.
Embodiment 2: a kind of preparation method of boron carbon nitrogen porous ceramics, it comprises the following steps:
(1) prepare boron carbon nitrogen (BCN) organic precursor method by trichlorine boron azine and aniline in molar ratio 1:1 be dissolved in toluene; Room temperature lower magnetic force stirs 3h, then removes by filter white precipitate; Then the filtrate of clarification is placed in to 90 ℃ of heating jacket reflux 18 minutes, is cooled to room temperature; Under 40 ℃ of conditions, unnecessary toluene solvant is fallen in underpressure distillation, obtains faint yellow thick boron carbon nitrogen (BCN) organic precursor method, stand-by;
(2) nano polypropylene nitrile (PAN) fiber of being prepared by method of electrostatic spinning adds in above-mentioned boron carbon nitrogen (BCN) organic precursor method preparing, dipping 15min, then ultrasonic dispersion 20min, make boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, wherein polyacrylonitrile nanofiber mass content is 50%, and the mass content of boron carbon nitrogen (BCN) organic precursor method is 50%;
(3) by boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying in ceramic boat, every layer of boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is of a size of 100 × 100mm, thickness is 3mm, weight 3g; Between every upper and lower two-layer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, spray boron carbon nitrogen (BCN) precursor 2g, boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying number of plies is 20 layers;
(4) above-mentioned multilayer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is placed in to ceramic boat and goes to sintering oven, and with 3 oc/min rises to 1400 oc is also incubated 1.5h, adopts N in stove 2atmosphere protection; Nitrogen original pressure (Pressure of Ambient Temperature before heating up) is controlled at 2.8 MPas (MPa);
(5) insulation cools to room temperature with the furnace after finishing, and can obtain black boron carbon nitrogen (BCN) porous ceramics.
B-C-N ceramic productive rate is 77.6%, and porosity is 69.1%.
Embodiment 3: a kind of preparation method of boron carbon nitrogen porous ceramics, it comprises the following steps:
(1) prepare boron carbon nitrogen (BCN) organic precursor method by trichlorine boron azine and aniline in molar ratio 1:3 be dissolved in toluene; Room temperature lower magnetic force stirs 4h, then removes by filter white precipitate; Then the filtrate of clarification is placed in to 100 ℃ of heating jacket reflux 25 minutes, is cooled to room temperature; Under 40 ℃ of conditions, unnecessary toluene solvant is fallen in underpressure distillation, obtains faint yellow thick boron carbon nitrogen (BCN) organic precursor method, stand-by;
(2) nano polypropylene nitrile (PAN) fiber of being prepared by method of electrostatic spinning adds in above-mentioned boron carbon nitrogen (BCN) organic precursor method preparing, dipping 15min, then ultrasonic dispersion 30min, make boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, wherein polyacrylonitrile nanofiber mass content is 55%, and the mass content of boron carbon nitrogen (BCN) organic precursor method is 45%;
(3) by boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying in ceramic boat, every layer of boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is of a size of 100 × 100mm, thickness is 3.6mm, weight 3.5g; Between every upper and lower two-layer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, spray boron carbon nitrogen (BCN) precursor 3g, boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying number of plies is 35 layers;
(4) above-mentioned multilayer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is placed in to ceramic boat and goes to sintering oven, and with 3 oc/min rises to 1400 oc is also incubated 1.5h, adopts N in stove 2atmosphere protection; Nitrogen original pressure (Pressure of Ambient Temperature before heating up) is controlled at 2.0 MPas (MPa);
(5) insulation cools to room temperature with the furnace after finishing, and can obtain black boron carbon nitrogen (BCN) porous ceramics.
B-C-N ceramic productive rate is 76.9%, and porosity is 70.4%.
Embodiment 4: a kind of preparation method of boron carbon nitrogen porous ceramics, it comprises the following steps:
(1) prepare boron carbon nitrogen (BCN) organic precursor method by trichlorine boron azine and aniline in molar ratio 1:6 be dissolved in toluene; Room temperature lower magnetic force stirs 5h, then removes by filter white precipitate; Then the filtrate of clarification is placed in to 120 ℃ of heating jacket reflux 30 minutes, is cooled to room temperature; Under 45 ℃ of conditions, unnecessary toluene solvant is fallen in underpressure distillation, obtains faint yellow thick boron carbon nitrogen (BCN) organic precursor method, stand-by;
(2) nano polypropylene nitrile (PAN) fiber of being prepared by method of electrostatic spinning adds in above-mentioned boron carbon nitrogen (BCN) organic precursor method preparing, dipping 15min, then ultrasonic dispersion 35min, make boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, wherein polyacrylonitrile nanofiber mass content is 48%, and the mass content of boron carbon nitrogen (BCN) organic precursor method is 52%;
(3) by boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying in ceramic boat, every layer of boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is of a size of 100 × 100mm, thickness is 5mm, weight 5.8g; Between every upper and lower two-layer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body, spray boron carbon nitrogen (BCN) precursor 5g, boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body laying number of plies is 50 layers;
(4) above-mentioned multilayer boron carbon nitrogen (BCN) organic precursor method-polyacrylonitrile nanofiber complex body is placed in to ceramic boat and goes to sintering oven, and with 3 oc/min rises to 1400 oc is also incubated 1.5h, adopts N in stove 2atmosphere protection; Nitrogen original pressure (Pressure of Ambient Temperature before heating up) is controlled at 1.5 MPas (MPa);
(5) insulation cools to room temperature with the furnace after finishing, and can obtain black boron carbon nitrogen (BCN) porous ceramics.
B-C-N ceramic productive rate is 78.2%, and porosity is 74.5%.

Claims (1)

1. a preparation method for boron carbon nitrogen porous ceramics, is characterized in that: it comprises the following steps:
(1) first preparing boron carbon nitrogen organic precursor method 1:0.3 ~ 6 is dissolved in trichlorine boron azine and aniline in toluene in molar ratio; Room temperature lower magnetic force stirs 2~5h, then removes by filter white precipitate; Then the filtrate of clarification is placed in to 80~120 ℃ of heating jacket reflux 10~30 minutes, is cooled to room temperature; Under 30~45 ℃ of conditions, unnecessary toluene solvant is fallen in underpressure distillation, obtains faint yellow thick boron carbon nitrogen organic precursor method, stand-by;
(2) the nano polypropylene nitrile fiber of being prepared by method of electrostatic spinning adds in the above-mentioned boron carbon nitrogen organic precursor method preparing, dipping 10 ~ 15min, then ultrasonic dispersion 15 ~ 35min, obtain boron carbon nitrogen organic precursor method-polyacrylonitrile nanofiber complex body, wherein polyacrylonitrile nanofiber mass content is 40 ~ 55%, and the mass content of boron carbon nitrogen organic precursor method is 60 ~ 45%;
(3) by disperse after boron carbon nitrogen organic precursor method-polyacrylonitrile nanofiber complex body laying in ceramic boat, every layer of boron carbon nitrogen organic precursor method-polyacrylonitrile nanofiber complex body is of a size of 100 × 100mm, thickness is 1 ~ 5mm, weight 1 ~ 6g; Between every upper and lower two-layer boron carbon nitrogen organic precursor method-polyacrylonitrile nanofiber complex body, spray boron carbon nitrogen organic precursor method 2 ~ 5g, boron carbon nitrogen organic precursor method-polyacrylonitrile nanofiber complex body laying number of plies is 15 ~ 50 layers again;
(4) the above-mentioned ceramic boat that boron carbon nitrogen organic precursor method-polyacrylonitrile nanofiber complex body is housed is gone in sintering oven, and with 3 oc/min rises to 1400 oc is also incubated 1.5h, adopts N in stove 2atmosphere protection; Nitrogen original pressure is controlled at 1.5 ~ 3.5 MPas;
(5) insulation cools to room temperature with the furnace after finishing, and can obtain black boron carbon nitrogen porous ceramics.
CN201310331011.3A 2013-08-01 2013-08-01 Preparation method for boron-carbon-nitrogen porous ceramic Expired - Fee Related CN103396125B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310331011.3A CN103396125B (en) 2013-08-01 2013-08-01 Preparation method for boron-carbon-nitrogen porous ceramic

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310331011.3A CN103396125B (en) 2013-08-01 2013-08-01 Preparation method for boron-carbon-nitrogen porous ceramic

Publications (2)

Publication Number Publication Date
CN103396125A CN103396125A (en) 2013-11-20
CN103396125B true CN103396125B (en) 2014-07-02

Family

ID=49559916

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310331011.3A Expired - Fee Related CN103396125B (en) 2013-08-01 2013-08-01 Preparation method for boron-carbon-nitrogen porous ceramic

Country Status (1)

Country Link
CN (1) CN103396125B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103896589B (en) * 2014-03-06 2015-04-29 哈尔滨工业大学(威海) Method for preparing silicon-boron-carbon-nitrogen porous ceramic with nano pore structure
CN109825900B (en) * 2019-01-23 2021-03-02 中国人民解放军国防科技大学 Preparation method of BCN (BCN-BCN) nano ceramic fiber
CN111454396B (en) * 2020-05-25 2021-10-08 福建华夏蓝新材料科技有限公司 Weather-resistant polyacrylate emulsion and preparation method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6838162B1 (en) * 1999-09-16 2005-01-04 Sgl Technik Gmbh Fiber-bundle-reinforced composite material having a ceramic matrix, method for manufacturing a composite material and method for manufacturing elements formed of a composite material
CN101700978A (en) * 2009-11-11 2010-05-05 哈尔滨工业大学 Method for preparing SiBCN(O) ceramic material
CN101723675A (en) * 2009-10-21 2010-06-09 哈尔滨工业大学 Boron nitride ceramic organic precursor and preparation method thereof
CN101774814A (en) * 2010-01-14 2010-07-14 天津大学 Ceramic and carbon nano-fiber composite material and preparation method thereof
CN102503423A (en) * 2011-11-22 2012-06-20 东华大学 Preparation method of SiBNC bulk ceramics

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19711829C1 (en) * 1997-03-21 1998-09-03 Daimler Benz Ag Process for the production of a fiber-reinforced composite ceramic

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6838162B1 (en) * 1999-09-16 2005-01-04 Sgl Technik Gmbh Fiber-bundle-reinforced composite material having a ceramic matrix, method for manufacturing a composite material and method for manufacturing elements formed of a composite material
CN101723675A (en) * 2009-10-21 2010-06-09 哈尔滨工业大学 Boron nitride ceramic organic precursor and preparation method thereof
CN101700978A (en) * 2009-11-11 2010-05-05 哈尔滨工业大学 Method for preparing SiBCN(O) ceramic material
CN101774814A (en) * 2010-01-14 2010-07-14 天津大学 Ceramic and carbon nano-fiber composite material and preparation method thereof
CN102503423A (en) * 2011-11-22 2012-06-20 东华大学 Preparation method of SiBNC bulk ceramics

Non-Patent Citations (8)

* Cited by examiner, † Cited by third party
Title
A.H. Tavakoli et al..Kinetic effect of boron on the thermal stability of Si–(B–)C–N polymer-derived ceramics.《Acta Materialia》.2010,第58卷
A.Mulleretal..Si/B/C/N/Alprecursor-derivedceramics:Synthesis high temperature behaviour and oxidation resistance.《Journal of the European Ceramic Society》.2004
Kinetic effect of boron on the thermal stability of Si–(B–)C–N polymer-derived ceramics;A.H. Tavakoli et al.;《Acta Materialia》;20100731;第58卷;第6002-6003页 *
Si/B/C/N/Al precursor-derived ceramics: Synthesis, high temperature behaviour and oxidation resistance;A.Muller et al.;《Journal of the European Ceramic Society》;20041231;第24卷(第12期);第3409-3411页 *
SiBNC多元陶瓷先驱体的最新发展与展望;雷成乐等;《材料导报A》;20120930;第26卷(第9期);第44-47页 *
杨旭敏等.硼碳氮材料的研究进展》.《材料导报》.2008,第22卷
硼碳氮材料的研究进展》;杨旭敏等;《材料导报》;20080831;第22卷;第316-321页 *
雷成乐等.SiBNC多元陶瓷先驱体的最新发展与展望.《材料导报A》.2012,第26卷(第9期),

Also Published As

Publication number Publication date
CN103396125A (en) 2013-11-20

Similar Documents

Publication Publication Date Title
CN109053207B (en) Yttrium silicate modified silicon carbide fiber reinforced silicon carbide composite material and preparation method thereof
CN111409321B (en) Preparation method of carbon fiber hard felt with density gradient
CN101717255B (en) Precusor conversion preparation method of carbon fibre reinforced silicon carbide composite material
CN106966742B (en) Alumina fiber reinforced mullite ceramic containing interface phase and preparation method thereof
CN110423119B (en) Preparation method of ablation-resistant C/SiC ceramic matrix composite
CN108017362B (en) Preparation method of modified carbon fiber heat-insulation composite material
CN102795871A (en) Method for quickly preparing C/SiC ceramic matrix composite material
JP2007535461A (en) Process for producing carbon fiber reinforced ceramic composites
CN102173844B (en) Carbon fiber reinforced boron nitride composite and preparation method thereof
CN113666765B (en) Continuous fiber reinforced high-entropy ceramic matrix composite and preparation method thereof
CN103396125B (en) Preparation method for boron-carbon-nitrogen porous ceramic
CN113045326A (en) Preparation method of modified carbon/carbon composite material
CN105541416A (en) Preparation method for HfC-SiC coating on C/C composite material surface
CN105237020B (en) A kind of fibre reinforced ZrB2- ZrN multiphase ceramic matrix composites and preparation method thereof
CN106565262A (en) Preparation method for low-density refractory and antioxidative carbon-ceramic composite material
CN112745143A (en) ZrO preparation by adopting sol-gel method2-SiO2Method for coating C/C composite material with-SiC
CN113788684B (en) Gradient density carbon-ceramic composite material and preparation method thereof
CN106966703A (en) Alumina fibre enhancing aluminium oxide ceramics of the phase containing interface and preparation method thereof
CN103724038A (en) Preparation method of ceramic matrix hybrid composite material
CN102808240A (en) Preparation method of high-temperature-resistant silicon carbide fiber
CN105734720A (en) Preparation method for improving strength and modulus of SiC fibers
CN112374917A (en) High-temperature ceramic coating and preparation method thereof
CN109265189A (en) Microwave-absorbing ceramic based composites fast preparation method with electromagnetic resistivity gradual change matrix
CN106747555A (en) A kind of matrix containing self toughening, thermostructural composite of continuous lod and preparation method thereof
CN103724046A (en) SiC foam 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
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140702

Termination date: 20160801