CN102674845A - Preparation method of silicon carbide fibers with silicon nitride surface layer - Google Patents

Preparation method of silicon carbide fibers with silicon nitride surface layer Download PDF

Info

Publication number
CN102674845A
CN102674845A CN2012101382790A CN201210138279A CN102674845A CN 102674845 A CN102674845 A CN 102674845A CN 2012101382790 A CN2012101382790 A CN 2012101382790A CN 201210138279 A CN201210138279 A CN 201210138279A CN 102674845 A CN102674845 A CN 102674845A
Authority
CN
China
Prior art keywords
fiber
atmosphere
ammonia
heated
fusion
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
Application number
CN2012101382790A
Other languages
Chinese (zh)
Other versions
CN102674845B (en
Inventor
邵长伟
王珊珊
宋永才
谢征芳
王浩
王军
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.)
National University of Defense Technology
Original Assignee
National University of Defense Technology
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 National University of Defense Technology filed Critical National University of Defense Technology
Priority to CN 201210138279 priority Critical patent/CN102674845B/en
Publication of CN102674845A publication Critical patent/CN102674845A/en
Application granted granted Critical
Publication of CN102674845B publication Critical patent/CN102674845B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Inorganic Fibers (AREA)
  • Ceramic Products (AREA)

Abstract

The invention relates to a preparation method of silicon carbide fibers with a silicon nitride surface layer. The preparation method comprises the following steps of: using polycarbosilane (PCS) which is prepared by using organic silicon polymers through high-temperature cracking as raw materials, conducting melt-spinning to obtain continuous PCS polymer fibers, placing the continuous PCS polymer fibers in the atmosphere of air or activated gas for non-melting treatment, placing the non-melting fibers in a high-temperature atmosphere furnace for high-temperature nitration and decarbonization under the atmosphere of ammonia with certain concentration, and further sintering for densification at high temperature to obtain the silicon carbide fibers with the silicon nitride surface layer. The preparation method of the silicon carbide fibers with the silicon nitride surface layer has the advantages that the process and the equipment are simple, the cost of the prepared silicon carbide fibers is low and the resistivity is adjustable.

Description

A kind of preparation method with the silicon carbide fiber on silicon nitride top layer
Technical field
The present invention relates to a kind of preparation method of silicon carbide fiber, especially relate to a kind of silicon nitride (Si that has 3N 4) silit (SiC) fiber preparation method on top layer.
Background technology
Silit (SiC) fiber is that important high-performance strengthens one of ceramic fiber, have excellent intensity, modulus, creep resistance, fire-resistant oxidation resistant property, with the consistency and the high band wave absorbtion of ceramic matrix.The SiC fiber is a kind of outstanding functional structure material, has a extensive future at numerous areas such as aerospace, nuclear power.Each developed country of the world gives very big concern to this, at present, Japan has realized the production of SiC fiber industry, and China's technical application is blocked.At home; The National University of Defense technology was through the exploratory development in surplus 30 years; Independent development goes out serial SiC fiber, comprises that KD-I SiC fiber, KD-II SiC fiber, KA-SA high-temperature resistant type SiC fiber and KD-X inhale ripple SiC fiber, and fibre quality index has reached or approaching external like product level.
Based on SiC fiber excellent mechanical property, high-temperature stability and microwave absorbing property, it becomes universally acknowledged one of the enhancing body of high performance structures Wave suction composite material that is suitable as most.Stealth material by the SiC fiber production has the dual nature of inhaling ripple and carrying.But the SiC fiber that utilizes present more sophisticated precursor method to prepare is a kind of n type, semiconductor material, and resistivity is 10 6About Ω cm.And wideband section stealth material requires the resistivity of SiC fiber can carry out regulation and control (10 in a big way -2-10 7Ω cm).For this reason, developed the resistivity regulate and control method of multiple SiC fiber, mainly contained: chemical reaction method, physics blending method, controlling fiber interface shape method, controlling fiber oxygen level method and surface-coated method.As adjusting its electromagnetic parameter, at surface deposition B at fiber surface metal lining nickel, cobalt 4The C layer can change the fiber dielectric properties.Wherein, have cracking carbon (PyC) coating of conductivity and SP 1 (BN), silicon nitride (Si through coating with insulating property 3N 4), aluminum oxide (Al 2O 3) to wait inorganic coating be modal fiber electrical property regulate and control method.
Silicon nitride (Si 3N 4) pottery has good insulation performance property, also has compactness, stability simultaneously, characteristics such as HS, highly heatproof and shockproof stability, high temperature creep are little, wear-resisting, high antioxidant, and Si 3N 41400-1500 ℃ of high temperature pre-oxidation treatment, can on ceramic material surfaces, form Si 2N 2The O phase can significantly improve Si 3N 4The scale resistance and the hot strength of pottery, therefore, preparation has gradient silicon nitride (Si 3N 4) continuous SiC fiber of surface structure has important use and be worth.
CVD and PIP are the common coatings technology of ceramic based material.But for preparation silicon nitride (Si 3N 4) top layer, CVD technology not only needs special processing unit, and is controlling deposit thickness and guaranteeing that coating also has difficulties aspect evenly continuous; Possibly cause synnema internal fiber coating to coat problems such as incomplete; And the cracking at high temperature of PIP processing requirement possibly produce than macrolesion fiber, and is prone to form strong interface combination; Have tangible skin-core structure, these all might reduce the mechanical property and the wave-sucking performance of fiber.
Summary of the invention
The technical problem that the present invention will solve is, overcomes the deficiency of prior art, provides a kind of technology and equipment simple, low cost of manufacture, the regulatable preparation method with the silicon carbide fiber on silicon nitride top layer of resistivity.
The technical solution adopted for the present invention to solve the technical problems is that a kind of preparation method with the silicon carbide fiber on silicon nitride top layer may further comprise the steps:
(1) organosilicon polymer is placed reaction kettle, vacuumize for five times repeatedly, fill after purity is 99.999% high pure nitrogen or argon gas; Be heated to 400-500 ℃ of (preferred 430-480 ℃) cracking 1-6h (preferred 3-4 h); Crude product dissolves after-filtration through toluene, again filtrating is heated to 300-400 ℃ (preferred 350-380 ℃) and carries out underpressure distillation, removes and desolvates and lower-molecular substance; Cooling gets Polycarbosilane (PCS);
(2) step (1) gained Polycarbosilane is placed the molten tube of melt spinning device; Under 99.999% high pure nitrogen or argon gas inert atmosphere protection, be heated to 280-380 ℃; After treating that its fine melt becomes even melt, at 250-320 ℃, under the 0.1-0.8MPa (preferred 0.6-0.7 MPa); Carry out drawing-off with 200-600m/min (preferred 450-550 m/min) speed, get continuous P CS fiber;
(3) take one of following three kinds of methods to carry out not melt processed and produce the PCS fusion-free fibre: (a) step (2) gained continuous P CS fiber is placed not melt processed device; Vacuumize; Filling purity is 99.999% high pure nitrogen; Behind the triplicate, feed reactive atmosphere to 0.1MPa, (preferred 15-20 ℃/min) heat-up rate is heated to 300-450 ℃ (preferably 350-400 ℃) by 10-30 ℃/min; And after 1-6 hour (preferred 3-5 hour) handled in this temperature insulation, make fusion-free fibre; (b) step (2) gained continuous P CS fiber is placed not melt processed device; Heat-up rate by 10-20 ℃/hour (preferred 12-16 ℃/hour) in air atmosphere is heated to 150-250 ℃ (preferred 180-220 ℃); Insulation oxide treatment 2-4 hour makes fusion-free fibre; (c) step (2) gained continuous P CS fiber is placed electron beam irradiation, after irradiation dose reached 5-20MGy (preferred 12-16 MGy), anneal made fusion-free fibre;
(4) step (3) gained fusion-free fibre is placed high-temperature atmosphere furnace; At ammonia; Or ammonia and nitrogen or ammonia and argon gas etc. mix under the mixed atmosphere that forms; (preferred 130-160 ℃/h) speed is warming up to 600-1000 ℃ (preferred 700-900 ℃), and insulation was handled 1-2 hour under 1200-1400 ℃ of temperature, made to have Si by 100-200 ℃/h 3N 4Top layer SiC fiber.
In the step (1), said organosilicon polymer is the silane polymer that constitutes main chain with Si-Si key and Si-C key, and its structure is linearity or ring-type, preferred polysilane, polydimethyl silane, polymethyl silicane, polyphenylene silane or ring silicon-carbon alkane etc.
In the step (3), in the not melt processed of PCS fiber, said reactive atmosphere is ethene or acetylene.
In the step (4), said ammonia mixes with nitrogen, argon gas etc. in the mixed atmosphere that forms, volumetric concentration >=10% of preferred ammonia.
The present invention utilizes ammonia in infiltration of continuous fibre radial gas chemistry and original position decarburizing reaction, controls its diffusion depth and carries out the gradient nitrogenize, and preparation has silit (SiC) fiber on gradient silicon nitride top layer.Following positive effect is compared with prior art arranged: (1) the present invention places high-temperature atmosphere furnace under the ammonia atmosphere of proper concn, to carry out the high-temperature ammonolysis decarburization fusion-free fibre; Preparation gradient silicon nitride top layer; Can realize the regulation and control on a large scale of fabric resistor rate through the processing parameter of control nitrogenize decarburization; (2) the present invention directly adds reactive atmosphere adjusting electrical property and surface structure in firing process, compares with the PIP coating technology with the CVD technology, and technology is simple, and it is convenient to implement, and low cost of manufacture utilizes the production unit of SiC fiber just can implement, and is easy to industriallization; (3) silit with silicon nitride top layer (SiC) fiber of the present invention's preparation, with respect to general silicon carbide fiber, high temperature resistant and good in oxidation resistance.
Description of drawings
Fig. 1 is embodiment 1 obtained SEM microscopic appearance figure with the SiC fiber on silicon nitride top layer;
Fig. 2 is the EDX figure on embodiment 1 gained SiC fiber silicon nitride top layer.
Embodiment
Below in conjunction with specific embodiment the present invention is done further explain.
Embodiment 1
Present embodiment may further comprise the steps:
(1) polysilane is placed reaction kettle, vacuumizes for five times repeatedly, fill 99.999% high pure nitrogen after; Be heated to 400 ℃ of cracking 2h, crude product dissolves after-filtration through toluene, again filtrating is heated to 300 ℃ and carries out underpressure distillation; Remove and desolvate and lower-molecular substance, cooling gets Polycarbosilane (PCS);
(2) step (1) gained Polycarbosilane being placed the molten tube of melt spinning device, is to be heated to 300 ℃ under the protection of 99.999% high pure nitrogen in purity, treat that its fine melt becomes even melt after; At 280 ℃; 0.4MPa down, carry out drawing-off, get continuous P CS fiber with 300m/min speed;
(3) step (2) gained continuous P CS fiber is placed not melt processed device; Vacuumize, filling purity is 99.999% high pure nitrogen, behind the triplicate; Feed acetylene gas to 0.1MPa; Heat-up rate by 20 ℃/min is heated to 380 ℃, and after this temperature insulation is handled 3 hours, makes fusion-free fibre;
(4) step (3) gained fusion-free fibre is placed high-temperature atmosphere furnace, under ammonia atmosphere, be warming up to 1000 ℃ by 120 ℃/hour speed, insulation was handled 1 hour under 1400 ℃ of temperature, made to have gradient Si 3N 4Top layer SiC fiber.
Present embodiment is obtained, and to have a SEM microscopic appearance figure of SiC fiber on silicon nitride top layer as shown in Figure 1.
EDX is carried out on present embodiment gained SiC fiber silicon nitride top layer analyze (referring to Fig. 2): fiber surface is a silicon nitride structure, and Fibre diameter is 12.3
Figure 2012101382790100002DEST_PATH_IMAGE001
M, tensile strength is 2.2GPa, and Young's modulus is 270GPa, and the fiber oxygen level is 0.65wt%, and nitrogen content is 6.25wt%, resistivity is 2.6 * 10 8Ω cm.Handled 1 hour in 1400 ℃ of air, strength retention ratio is 65%.
Embodiment 2
Present embodiment may further comprise the steps:
Step (1) and (2) operation are with embodiment 1;
(3) step (2) gained continuous P CS fiber is placed not melt processed device, the heat-up rate by 15 ℃/hour in air atmosphere is heated to 220 ℃, and insulation oxide treatment 4 hours makes fusion-free fibre;
(4) step (3) gained fusion-free fibre is placed high-temperature atmosphere furnace, under the mixed atmosphere of ammonia and nitrogen (volume ratio 1:1) formation, be warming up to 1000 ℃ by 150 ℃/hour speed, insulation was handled 2 hours under 1200 ℃ of temperature, made to have Si 3N 4Top layer SiC fiber.
The continuous SiC fiber that present embodiment makes, top layer EDX analysis revealed, fiber surface are silicon nitride structure, Fibre diameter is 12
Figure 148159DEST_PATH_IMAGE001
M, tensile strength is 2.1GPa, and Young's modulus is 260GPa, and the fiber oxygen level is 0.95wt%, and nitrogen content is 5.88wt%, resistivity is 3.5 * 10 7Ω cm.Handled 1 hour in 1400 ℃ of air, strength retention ratio is 68%.
Embodiment 3
Present embodiment may further comprise the steps:
Step (1) and (2) operation are with embodiment 1;
(3) step (2) gained continuous P CS fiber is placed the electron accelerator irradiation case, after irradiation dose reached 10MGy, anneal obtained the electron beam irradiation fusion-free fibre.
(4) step (3) gained electron beam irradiation fusion-free fibre is placed high-temperature atmosphere furnace, under ammonia and argon gas (volume ratio 1:1) mixed atmosphere, be warming up to 700 ℃ by 160 ℃/hour speed, 2h is handled in insulation under 1300 ℃ of temperature, obtains having Si 3N 4The continuous SiC fiber on top layer.
The continuous SiC fiber that present embodiment makes, top layer EDX analysis revealed fiber surface is a silicon nitride structure, Fibre diameter is 11 M, tensile strength is 2.6GPa, and Young's modulus is 285GPa, and the fiber oxygen level is 0.62wt%, and nitrogen content is 4.36wt%, resistivity is 2.6 * 10 6Ω cm.Handled 1 hour in 1400 ℃ of air, strength retention ratio is 66%.

Claims (5)

1. the preparation method with the silicon carbide fiber on silicon nitride top layer is characterized in that, may further comprise the steps:
(1) organosilicon polymer is placed reaction kettle, vacuumize for five times repeatedly, fill after purity is 99.999% high pure nitrogen or argon gas; Be heated to 400-500 ℃ of cracking 1-6h; Crude product dissolves after-filtration through toluene, again filtrating is heated to 300-400 ℃ and carries out underpressure distillation, removes and desolvates and lower-molecular substance; Cooling gets Polycarbosilane;
Said organosilicon polymer is the silane polymer that constitutes main chain with Si-Si key and Si-C key, and its structure is linearity or ring-type;
(2) step (1) gained Polycarbosilane is placed the molten tube of melt spinning device; Under 99.999% high pure nitrogen or argon gas inert atmosphere protection, be heated to 280-380 ℃; After treating that its fine melt becomes even melt, at 250-320 ℃, under the 0.1-0.8MPa; Carry out drawing-off with 200-600m/min speed, get continuous P CS fiber;
(3) take one of following three kinds of methods to carry out not melt processed and produce the PCS fusion-free fibre: (a) step (2) gained continuous P CS fiber is placed not melt processed device; Vacuumize, filling purity is 99.999% high pure nitrogen, behind the triplicate; Feed reactive atmosphere to 0.1MPa; Heat-up rate by 10-30 ℃/min is heated to 300-450 ℃, and after this temperature insulation is handled 1-6 hour, makes fusion-free fibre; (b) step (2) gained continuous P CS fiber is placed not melt processed device, the heat-up rate by 10-20 ℃/hour in air atmosphere is heated to 150-250 ℃, and insulation oxide treatment 2-4 hour makes fusion-free fibre; (c) step (2) gained continuous P CS fiber is placed electron beam irradiation, after irradiation dose reached 5-20MGy, anneal made fusion-free fibre;
(4) step (3) gained fusion-free fibre is placed high-temperature atmosphere furnace; At ammonia; Or ammonia mixes with argon gas under the mixed atmosphere that forms with nitrogen or ammonia; Speed by 100-200 ℃/h is warming up to 600-1000 ℃, and insulation was handled 1-2 hour under 1200-1400 ℃ of temperature, makes to have Si 3N 4The SiC fiber on top layer.
2. the preparation method with the silicon carbide fiber on silicon nitride top layer according to claim 1 is characterized in that, in the step (1), said organosilicon polymer is polysilane, polydimethyl silane, polymethyl silicane, polyphenylene silane or ring silicon-carbon alkane.
3. the preparation method with the silicon carbide fiber on silicon nitride top layer according to claim 1 and 2 is characterized in that, in the step (3), in the not melt processed of PCS fiber, said reactive atmosphere is ethene atmosphere or acetylene atmosphere.
4. the preparation method with the silicon carbide fiber on silicon nitride top layer according to claim 1 and 2 is characterized in that, in the step (4), and in the mixed atmosphere of said ammonia and nitrogen, ammonia and argon gas, the volumetric concentration of ammonia >=10%.
5. the preparation method with the silicon carbide fiber on silicon nitride top layer according to claim 1 is characterized in that, may further comprise the steps:
(1) organosilicon polymer is placed reaction kettle, vacuumize for five times repeatedly, fill after purity is 99.999% high pure nitrogen or argon gas; Be heated to 430-480 ℃ of cracking 3-4 h; Crude product dissolves after-filtration through toluene, again filtrating is heated to 350-380 ℃ and carries out underpressure distillation, removes and desolvates and lower-molecular substance; Cooling gets Polycarbosilane;
Said organosilicon polymer is polysilane, polydimethyl silane, polymethyl silicane, polyphenylene silane or ring silicon-carbon alkane;
(2) step (1) gained Polycarbosilane is placed the molten tube of melt spinning device; Under 99.999% high pure nitrogen or argon gas inert atmosphere protection, be heated to 280-380 ℃; After treating that its fine melt becomes even melt, at 250-320 ℃, under the 0.6-0.7 MPa; Carry out drawing-off with 450-550 m/min speed, get continuous P CS fiber;
(3) take one of following three kinds of methods to carry out not melt processed and produce the PCS fusion-free fibre: (a) step (2) gained continuous P CS fiber is placed not melt processed device; Vacuumize, filling purity is 99.999% high pure nitrogen, behind the triplicate; Feed reactive atmosphere to 0.1MPa; Heat-up rate by 15-20 ℃/min is heated to 350-400 ℃, and after this temperature insulation is handled 3-5 hour, makes fusion-free fibre; (b) step (2) gained continuous P CS fiber is placed not melt processed device, the heat-up rate by 12-16 ℃/hour in air atmosphere is heated to 180-220 ℃, and insulation oxide treatment 2-4 hour makes fusion-free fibre; (c) step (2) gained continuous P CS fiber is placed electron beam irradiation, after irradiation dose reached 12-16 MGy, anneal made fusion-free fibre;
Said reactive atmosphere is ethene atmosphere or acetylene atmosphere;
(4) step (3) gained fusion-free fibre is placed high-temperature atmosphere furnace; At ammonia, or under the mixed atmosphere of ammonia and nitrogen or ammonia and argon gas, be warming up to 700-900 ℃ by the speed of 130-160 ℃/h; Insulation was handled 1-2 hour under 1200-1400 ℃ of temperature, made to have Si 3N 4Top layer SiC fiber;
In the mixed atmosphere of said ammonia and nitrogen, ammonia and argon gas, the volumetric concentration of ammonia >=10%.
CN 201210138279 2012-05-07 2012-05-07 Preparation method of silicon carbide fibers with silicon nitride surface layer Active CN102674845B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201210138279 CN102674845B (en) 2012-05-07 2012-05-07 Preparation method of silicon carbide fibers with silicon nitride surface layer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201210138279 CN102674845B (en) 2012-05-07 2012-05-07 Preparation method of silicon carbide fibers with silicon nitride surface layer

Publications (2)

Publication Number Publication Date
CN102674845A true CN102674845A (en) 2012-09-19
CN102674845B CN102674845B (en) 2013-06-19

Family

ID=46807474

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201210138279 Active CN102674845B (en) 2012-05-07 2012-05-07 Preparation method of silicon carbide fibers with silicon nitride surface layer

Country Status (1)

Country Link
CN (1) CN102674845B (en)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103952796A (en) * 2014-04-28 2014-07-30 中国人民解放军国防科学技术大学 Preparation method of silicon-nitrogen-boron continuous ceramic fibers
CN105503270A (en) * 2015-12-17 2016-04-20 湖南博望碳陶有限公司 Method for preparing SiC coating
CN105601341A (en) * 2015-12-17 2016-05-25 湖南博望碳陶有限公司 Method for preparing brake disc with beta-silicon carbide coating
CN105752952A (en) * 2016-01-28 2016-07-13 哈尔滨工业大学 Method for preparing super-long silicon nitride nanowires on surface of porous green-body or powdery silicon carbide-polycarbosilane in in-situ and non-in-situ mode
CN105886081A (en) * 2016-04-27 2016-08-24 饶秀琴 Lubricating oil and abrasion-resistant cleaning lubricating oil additive
CN106835359A (en) * 2017-02-06 2017-06-13 厦门大学 A kind of preparation method of the silicon nitrogen carbon ceramic fibers of graded
CN107868998A (en) * 2016-09-23 2018-04-03 中国科学院上海应用物理研究所 A kind of silicon nitride fiber and preparation method thereof
CN108193322A (en) * 2017-12-25 2018-06-22 晋江瑞碧科技有限公司 A kind of preparation method of SiC nano fiber
CN108238799A (en) * 2016-12-27 2018-07-03 中国科学院上海应用物理研究所 A kind of preparation method of silicon-containing ceramic coating
CN108752012A (en) * 2018-05-02 2018-11-06 中国航发北京航空材料研究院 A kind of preparation method of fiber surface boron nitride/silicon nitride compound interface layer
CN108842438A (en) * 2018-06-06 2018-11-20 中国人民解放军国防科技大学 Preparation method of high-temperature-resistant SiC fibers
CN109368644A (en) * 2018-11-24 2019-02-22 冯良荣 A method of preparing carbonitride of silicium
CN109385693A (en) * 2018-10-24 2019-02-26 中国人民解放军国防科技大学 Preparation method of Si-B-N ceramic fiber
CN109516808A (en) * 2018-12-13 2019-03-26 湖南博翔新材料有限公司 A method of preparation silicon carbide ceramic fiber containing beryllium is bathed by gallium
CN109750390A (en) * 2019-01-14 2019-05-14 贵州师范大学 A kind of preparation method of the hollow silicon carbide of micron/silicon nitride ceramics fiber
CN109825901A (en) * 2019-01-28 2019-05-31 江西嘉捷信达新材料科技有限公司 Aluminium, silicon carbide/boron nitride fiber of zirconium codope and preparation method thereof
CN110105070A (en) * 2019-05-24 2019-08-09 中国人民解放军国防科技大学 Continuous silicon carbide fiber with controllable electrical property and wide range and preparation method thereof
CN112358621A (en) * 2020-11-12 2021-02-12 江西信达航科新材料科技有限公司 High-temperature-resistant silicon carbide fiber precursor polycarbosilane and preparation method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5223461A (en) * 1989-06-05 1993-06-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Ceramic silicon-boron-carhon fibers from organic silicon-boron-polymers
EP0855373A1 (en) * 1997-01-23 1998-07-29 Oji Paper Company Limited Process for producing silicon carbide fibers
US6069102A (en) * 1997-08-04 2000-05-30 University Of Florida Creep-resistant, high-strength silicon carbide fibers
CN101787588A (en) * 2010-01-21 2010-07-28 中国人民解放军国防科学技术大学 Method for preparing continuous silicon carbide fiber by PCS fiber
CN101994169A (en) * 2010-09-14 2011-03-30 张卫中 Continuous silicon carbide fiber preparation method and production device

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5223461A (en) * 1989-06-05 1993-06-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Ceramic silicon-boron-carhon fibers from organic silicon-boron-polymers
EP0855373A1 (en) * 1997-01-23 1998-07-29 Oji Paper Company Limited Process for producing silicon carbide fibers
US6069102A (en) * 1997-08-04 2000-05-30 University Of Florida Creep-resistant, high-strength silicon carbide fibers
CN101787588A (en) * 2010-01-21 2010-07-28 中国人民解放军国防科学技术大学 Method for preparing continuous silicon carbide fiber by PCS fiber
CN101994169A (en) * 2010-09-14 2011-03-30 张卫中 Continuous silicon carbide fiber preparation method and production device

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103952796A (en) * 2014-04-28 2014-07-30 中国人民解放军国防科学技术大学 Preparation method of silicon-nitrogen-boron continuous ceramic fibers
CN105503270A (en) * 2015-12-17 2016-04-20 湖南博望碳陶有限公司 Method for preparing SiC coating
CN105601341A (en) * 2015-12-17 2016-05-25 湖南博望碳陶有限公司 Method for preparing brake disc with beta-silicon carbide coating
CN105503270B (en) * 2015-12-17 2018-05-22 湖南博望碳陶有限公司 A kind of preparation method of SiC coatings
CN105601341B (en) * 2015-12-17 2018-08-24 湖南博望碳陶有限公司 A method of it is prepared with beta silicon carbide coating brake disc
CN105752952A (en) * 2016-01-28 2016-07-13 哈尔滨工业大学 Method for preparing super-long silicon nitride nanowires on surface of porous green-body or powdery silicon carbide-polycarbosilane in in-situ and non-in-situ mode
CN105752952B (en) * 2016-01-28 2017-08-25 哈尔滨工业大学 A kind of method for preparing overlength beta-silicon nitride nanowire in porous body or powder shaped carborundum Polycarbosilane surface in situ and ex situ
CN105886081A (en) * 2016-04-27 2016-08-24 饶秀琴 Lubricating oil and abrasion-resistant cleaning lubricating oil additive
CN107868998A (en) * 2016-09-23 2018-04-03 中国科学院上海应用物理研究所 A kind of silicon nitride fiber and preparation method thereof
CN108238799A (en) * 2016-12-27 2018-07-03 中国科学院上海应用物理研究所 A kind of preparation method of silicon-containing ceramic coating
CN106835359A (en) * 2017-02-06 2017-06-13 厦门大学 A kind of preparation method of the silicon nitrogen carbon ceramic fibers of graded
CN108193322A (en) * 2017-12-25 2018-06-22 晋江瑞碧科技有限公司 A kind of preparation method of SiC nano fiber
CN108752012A (en) * 2018-05-02 2018-11-06 中国航发北京航空材料研究院 A kind of preparation method of fiber surface boron nitride/silicon nitride compound interface layer
CN108752012B (en) * 2018-05-02 2020-11-13 中国航发北京航空材料研究院 Preparation method of boron nitride/silicon nitride composite interface layer on fiber surface
CN108842438B (en) * 2018-06-06 2020-08-07 中国人民解放军国防科技大学 Preparation method of high-temperature-resistant SiC fibers
CN108842438A (en) * 2018-06-06 2018-11-20 中国人民解放军国防科技大学 Preparation method of high-temperature-resistant SiC fibers
CN109385693A (en) * 2018-10-24 2019-02-26 中国人民解放军国防科技大学 Preparation method of Si-B-N ceramic fiber
CN109385693B (en) * 2018-10-24 2021-02-05 中国人民解放军国防科技大学 Preparation method of Si-B-N ceramic fiber
CN109368644A (en) * 2018-11-24 2019-02-22 冯良荣 A method of preparing carbonitride of silicium
CN109516808A (en) * 2018-12-13 2019-03-26 湖南博翔新材料有限公司 A method of preparation silicon carbide ceramic fiber containing beryllium is bathed by gallium
CN109516808B (en) * 2018-12-13 2021-06-15 湖南泽睿新材料有限公司 Method for preparing beryllium-containing silicon carbide ceramic fiber through gallium bath
CN109750390A (en) * 2019-01-14 2019-05-14 贵州师范大学 A kind of preparation method of the hollow silicon carbide of micron/silicon nitride ceramics fiber
CN109825901A (en) * 2019-01-28 2019-05-31 江西嘉捷信达新材料科技有限公司 Aluminium, silicon carbide/boron nitride fiber of zirconium codope and preparation method thereof
CN109825901B (en) * 2019-01-28 2021-07-30 江西嘉捷信达新材料科技有限公司 Aluminum and zirconium co-doped silicon carbide/boron nitride fiber and preparation method thereof
CN110105070A (en) * 2019-05-24 2019-08-09 中国人民解放军国防科技大学 Continuous silicon carbide fiber with controllable electrical property and wide range and preparation method thereof
CN112358621A (en) * 2020-11-12 2021-02-12 江西信达航科新材料科技有限公司 High-temperature-resistant silicon carbide fiber precursor polycarbosilane and preparation method thereof

Also Published As

Publication number Publication date
CN102674845B (en) 2013-06-19

Similar Documents

Publication Publication Date Title
CN102674845B (en) Preparation method of silicon carbide fibers with silicon nitride surface layer
Zhao et al. Synthesis, pyrolysis of a novel liquid SiBCN ceramic precursor and its application in ceramic matrix composites
CN102634868B (en) Preparation method of silicon carbide fiber with boron nitride structure surface layer
EP2543650B1 (en) Method for manufacturing high-density fiber reinforced ceramic composite materials
Zhang et al. Progress of a novel non-oxide Si-BCN ceramic and its matrix composites
CN105384940B (en) A kind of synthetic method of spinning-grade polyaluminocarbosilane precursor
CN102634867B (en) Preparation method of near-stoichiometric silicon carbide fiber
CN103952796B (en) A kind of preparation method of silicon nitrogen boron continuous ceramic fiber
CN102424597A (en) Preparation method of C/C-SIC ceramic composite material
CN110423119B (en) Preparation method of ablation-resistant C/SiC ceramic matrix composite
Liu et al. Synthesis, characterization, and microstructure of ZrC/SiC composite ceramics via liquid precursor conversion method
CN103254440B (en) Method of preparing liquid anaerobic polyferrocarbosilane
CN111454061A (en) Polycarbosilane non-melting pretreatment and cracking conversion method for three-dimensional ceramic
Wang et al. Synthesis and pyrolysis of a novel preceramic polymer PZMS from PMS to fabricate high‐temperature‐resistant ZrC/SiC ceramic composite
CN102808240A (en) Preparation method of high-temperature-resistant silicon carbide fiber
Wang et al. Synthesis of ZrC–SiC powders from hybrid liquid precursors with improved oxidation resistance
CN106521710A (en) Preparation method of titanium-boron-containing carbonizedsilicon base ceramic fiber
CN110424068B (en) SiC fiber prepared by doping ultrahigh-temperature ceramic composite material and method and application thereof
CN109400168B (en) SiC fiber containing SiBCN coating and SiC coating which are alternately formed, and preparation method and application thereof
CN103613365A (en) Method for synthesizing silicon-oxygen-carbon ceramic material by utilizing polysiloxane resin
Cai et al. Synthesis, characterization, and microstructure of hafnium boride‐based composite ceramics via preceramic method
Chen et al. Synthesis of cyano-polycarbosilane and investigation of its pyrolysis process
Shcherbakova et al. Nanometallocarbosilanes: synthesis, physicochemical properties and structure
Li et al. In-situ fabrication of lightweight SiC (Al, rGO) bulk ceramics derived from silicon oxycarbide for aerospace components
Liu et al. Synthesis, characterization, and ceramization of a SiC–ZrC–C preceramic polymer precursor

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