Article(id=1320098222022963502, tenantId=1146029695717560320, journalId=1263187385517883426, issueId=1320098188355285873, articleNumber=null, orderNo=null, doi=10.14062/j.issn.0454-5648.20240142, pmid=null, cstr=null, oa=null, hot=null, price=null, onlineType=0, articleFormat=0, articleType=null, articleTypeStr=null, receivedDate=1708617600000, receivedDateStr=2024-02-23, revisedDate=1710000000000, revisedDateStr=2024-03-10, acceptedDate=null, acceptedDateStr=null, onlineDate=1792665542369, onlineDateStr=2026-10-22, pubDate=1726761600000, pubDateStr=2024-09-20, doiRegisterDate=null, doiRegisterDateStr=null, onlineIssueDate=1792665542369, onlineIssueDateStr=2026-10-22, onlineJustAcceptDate=null, onlineJustAcceptDateStr=null, onlineFirstDate=null, onlineFirstDateStr=null, sourceXml=null, magXml=null, createTime=1792665542369, creator=13701087609, updateTime=1792665542369, updator=13701087609, issue=Issue{id=1320098188355285873, tenantId=1146029695717560320, journalId=1263187385517883426, year='2024', volume='52', issue='9', pageStart='2755', pageEnd='3090', issueExtLink='null', onlineDate='null', pubDate='1726761600000', pubDateStr='2024-09-20', beforeIssueId=null, nextIssueId=null, price=null, status=1, issueComplete=1, articleOrder=1, issueType=-1, specialIssue=null, createTime=1792665534341, creator='13701087609', updateTime=1792666312798, updator='13701087609', preIssue=null, nextIssue=null, articleTotal=null, ext={EN=IssueExt(id=1320101453507711442, tenantId=1146029695717560320, journalId=1263187385517883426, issueId=1320098188355285873, language=EN, specialIssueTitle=, coverIllustrator=null, specialIssueEditor=, specialIssueAbout=), CN=IssueExt(id=1320101453507711443, tenantId=1146029695717560320, journalId=1263187385517883426, issueId=1320098188355285873, language=CN, specialIssueTitle=, coverIllustrator=null, specialIssueEditor=, specialIssueAbout=)}, issueFiles=null, downloadFileDto=null}, startPage=2862, endPage=2874, ext={EN=ArticleExt(id=1320098222215901487, articleId=1320098222022963502, tenantId=1146029695717560320, journalId=1263187385517883426, language=EN, title=Research Progress on Polymer-Derived Nitride Ceramics for Wave Transparent at High Temperature, columnId=1321894622285124340, journalTitle=Journal of the Chinese Ceramic Society, columnName=Special Issue on Polymer-Derived Ceramics—Review, runingTitle=null, highlight=null, articleAbstract=

High Mach precision guided aircraft has the important advantages of successful penetration with high level, presenting a strategic deterrent force to safeguard national core interests and maintain world peace. Its extremely high flight speed (>5 Ma) is an important guarantee of breakthrough capability, but causing severe aerodynamic erosion, heating, and ablation. Thus, it is a serious challenge to the communication, precise guidance, detonation and other combat tasks of the front-end antenna cover and antenna window. Therefore, the development of high-temperature transparent materials for antenna covers/windows that integrate various functions such as load-bearing, high-temperature resistance, and wave transmission is an urgent bottleneck problem to be solved.

High temperature resistance is an important indicator of transparent materials. The service speed of low-speed aircraft is low, and organic transparent materials such as phenolic resin and epoxy resin with lower temperature resistance can meet the usage requirements. With the continuous improvement of aircraft flight speed, higher temperature requirements are also expected for the use of transparent materials. The selection of transparent materials has transitioned from organic polymer systems to inorganic ceramic systems. Traditional inorganic transparent ceramics mainly include oxide ceramics such as quartz and glass-ceramics, with short-term usage temperatures around 1 000 ℃. With the development of aircraft flight speed towards high Mach numbers, there is a higher demand for the high-temperature resistance of transparent ceramic materials. Nitride ceramics, represented by silicon nitride (Si—N), boron nitride (B—N), silicon boron nitrogen (Si—B—N), and silicon nitrogen oxide (Si—N—O), exhibit superior high-temperature resistance than oxide ceramics. They are the most promising high-temperature transparent materials to meet the requirements of high Mach number aircraft and have become a research hotspot both domestically and internationally.

In recent years, researchers have conducted a detailed review of the research progress on nitride high-temperature transparent ceramic materials, which are a type of inorganic materials bonded by strong covalent bonds. They have the characteristics of high brittleness, high melting point and high hardness. Most nitride ceramics undergo obvious thermal decomposition reactions before melting, making it more difficult to sintering compared to carbide and boride ceramics. Typical sintering methods such as hot pressing or pressureless sintering have obvious shortcomings when preparing complex and precise structure antenna covers.

The precursor conversion method has the advantages of low processing temperature, controllable composition, easy processing and plasticity, and has become the preferred method for the preparation of high-performance antenna covers. The precursor conversion method first requires the synthesis of organic polymers containing target ceramic elements, which can be transformed into target ceramics after high-temperature (>1 000 ℃) pyrolysis. By utilizing the soluble and fusible properties of polymers, it is possible to prepare complex and precise antenna radomes through close prototyping.

At present, the development of new equipment is increasingly urgent for the precursor of nitride transparent ceramics, and the performance indicators of the precursor are also clearer. Driven by demand, systematic research has been carried out both domestically and internationally on the synthesis, transformation, and applications of nitride wave transmitting ceramic precursors. This not only provides rich material selection schemes for the development of high-temperature performance antenna covers, but also greatly enriches the development of precursor ceramics. This review mainly summarized the research progress in the precursor of nitride wave transmission ceramics in recent years, involving silicon nitride, boron nitride, silicon nitrogen oxide and other nitride wave transmission ceramic precursors, and proposes research directions in the future. It is expected that the work can provide certain reference for relevant researchers, and also look forward to more researchers paying attention to the research of nitride wave transmission precursors, supporting the development of wave transparent materials at high temperature.

Summary and Prospects

Compared with oxide ceramics for wave transparent, nitride ceramics with better high-temperature resistance are the most promising high-temperature wave transparent materials to meet the needs of high Mach number aircraft. Polymer-derived method presenting the advantages of low processing temperature and plasticity, is the promising method for preparing nitride ceramics for the wave transparent at high temperature. This review mainly summarized the research progress on the precursor of nitride wave transmitting ceramics in recent years, involving the synthesis of precursors for ceramics such as silicon nitride, boron nitride, silicon boron nitrogen, and silicon nitrogen oxide, as well as the preparation of target ceramics through thermal decomposition conversion. It also looks forward to the research directions in the future.

, authors=Xin LONG, Chiyuan WANG, Changwei SHAO, Qianlong WANG, authorsList=Xin LONG, Chiyuan WANG, Changwei SHAO, Qianlong WANG, authorCompany=null, correspAuthors=null, authorNote=

LONG Xin (1991-), male, Ph.D, Lecturer. E-mail:

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与氧化物透波陶瓷相比,氮化物透波陶瓷具有更加优异的耐高温性能,是最有希望满足高马赫数飞行器使用需求的高温透波材料。先驱体转化法具有加工成型温度低、可塑成型等优点,是制备氮化物高温透波陶瓷的主流方法。本文主要总结了近年来氮化物透波陶瓷先驱体方面的研究进展,主要涉及氮化硅、氮化硼、硅硼氮和硅氮氧等氮化物透波陶瓷先驱体的合成,以及通过热解转化制备目标陶瓷研究,并展望了今后应该重点关注的研究方向。

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龙鑫(1991—),男,博士,讲师。

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先驱体转化氮化物高温透波陶瓷研究进展
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龙鑫 , 王驰原 , 邵长伟 , 王乾龙
硅酸盐学报 | 聚合物先驱体陶瓷专题—综合评述 2024,52(9): 2862-2874
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硅酸盐学报 |聚合物先驱体陶瓷专题—综合评述 2024 , 52 (9) : 2862 -2874
先驱体转化氮化物高温透波陶瓷研究进展
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龙鑫 , 王驰原, 邵长伟, 王乾龙
作者信息
  • 国防科技大学空天科学学院,新型陶瓷纤维及其复合材料重点实验室,长沙 410073
作者简介:

龙鑫(1991—),男,博士,讲师。

Research Progress on Polymer-Derived Nitride Ceramics for Wave Transparent at High Temperature
Xin LONG , Chiyuan WANG, Changwei SHAO, Qianlong WANG
Affiliations
  • Science and Technology on Ceramic Fibers and Composites Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
  • LONG Xin (1991-), male, Ph.D, Lecturer. E-mail:

出版时间: 2024-09-20 doi: 10.14062/j.issn.0454-5648.20240142
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与氧化物透波陶瓷相比,氮化物透波陶瓷具有更加优异的耐高温性能,是最有希望满足高马赫数飞行器使用需求的高温透波材料。先驱体转化法具有加工成型温度低、可塑成型等优点,是制备氮化物高温透波陶瓷的主流方法。本文主要总结了近年来氮化物透波陶瓷先驱体方面的研究进展,主要涉及氮化硅、氮化硼、硅硼氮和硅氮氧等氮化物透波陶瓷先驱体的合成,以及通过热解转化制备目标陶瓷研究,并展望了今后应该重点关注的研究方向。

高温透波  /  氮化物陶瓷  /  透波陶瓷  /  先驱体转化法

High Mach precision guided aircraft has the important advantages of successful penetration with high level, presenting a strategic deterrent force to safeguard national core interests and maintain world peace. Its extremely high flight speed (>5 Ma) is an important guarantee of breakthrough capability, but causing severe aerodynamic erosion, heating, and ablation. Thus, it is a serious challenge to the communication, precise guidance, detonation and other combat tasks of the front-end antenna cover and antenna window. Therefore, the development of high-temperature transparent materials for antenna covers/windows that integrate various functions such as load-bearing, high-temperature resistance, and wave transmission is an urgent bottleneck problem to be solved.

High temperature resistance is an important indicator of transparent materials. The service speed of low-speed aircraft is low, and organic transparent materials such as phenolic resin and epoxy resin with lower temperature resistance can meet the usage requirements. With the continuous improvement of aircraft flight speed, higher temperature requirements are also expected for the use of transparent materials. The selection of transparent materials has transitioned from organic polymer systems to inorganic ceramic systems. Traditional inorganic transparent ceramics mainly include oxide ceramics such as quartz and glass-ceramics, with short-term usage temperatures around 1 000 ℃. With the development of aircraft flight speed towards high Mach numbers, there is a higher demand for the high-temperature resistance of transparent ceramic materials. Nitride ceramics, represented by silicon nitride (Si—N), boron nitride (B—N), silicon boron nitrogen (Si—B—N), and silicon nitrogen oxide (Si—N—O), exhibit superior high-temperature resistance than oxide ceramics. They are the most promising high-temperature transparent materials to meet the requirements of high Mach number aircraft and have become a research hotspot both domestically and internationally.

In recent years, researchers have conducted a detailed review of the research progress on nitride high-temperature transparent ceramic materials, which are a type of inorganic materials bonded by strong covalent bonds. They have the characteristics of high brittleness, high melting point and high hardness. Most nitride ceramics undergo obvious thermal decomposition reactions before melting, making it more difficult to sintering compared to carbide and boride ceramics. Typical sintering methods such as hot pressing or pressureless sintering have obvious shortcomings when preparing complex and precise structure antenna covers.

The precursor conversion method has the advantages of low processing temperature, controllable composition, easy processing and plasticity, and has become the preferred method for the preparation of high-performance antenna covers. The precursor conversion method first requires the synthesis of organic polymers containing target ceramic elements, which can be transformed into target ceramics after high-temperature (>1 000 ℃) pyrolysis. By utilizing the soluble and fusible properties of polymers, it is possible to prepare complex and precise antenna radomes through close prototyping.

At present, the development of new equipment is increasingly urgent for the precursor of nitride transparent ceramics, and the performance indicators of the precursor are also clearer. Driven by demand, systematic research has been carried out both domestically and internationally on the synthesis, transformation, and applications of nitride wave transmitting ceramic precursors. This not only provides rich material selection schemes for the development of high-temperature performance antenna covers, but also greatly enriches the development of precursor ceramics. This review mainly summarized the research progress in the precursor of nitride wave transmission ceramics in recent years, involving silicon nitride, boron nitride, silicon nitrogen oxide and other nitride wave transmission ceramic precursors, and proposes research directions in the future. It is expected that the work can provide certain reference for relevant researchers, and also look forward to more researchers paying attention to the research of nitride wave transmission precursors, supporting the development of wave transparent materials at high temperature.

Summary and Prospects

Compared with oxide ceramics for wave transparent, nitride ceramics with better high-temperature resistance are the most promising high-temperature wave transparent materials to meet the needs of high Mach number aircraft. Polymer-derived method presenting the advantages of low processing temperature and plasticity, is the promising method for preparing nitride ceramics for the wave transparent at high temperature. This review mainly summarized the research progress on the precursor of nitride wave transmitting ceramics in recent years, involving the synthesis of precursors for ceramics such as silicon nitride, boron nitride, silicon boron nitrogen, and silicon nitrogen oxide, as well as the preparation of target ceramics through thermal decomposition conversion. It also looks forward to the research directions in the future.

wave transparent at high temperature  /  nitride ceramic  /  wave transmitting ceramics  /  polymer-derived method
龙鑫, 王驰原, 邵长伟, 王乾龙. 先驱体转化氮化物高温透波陶瓷研究进展. 硅酸盐学报, 2024 , 52 (9) : 2862 -2874 . DOI: 10.14062/j.issn.0454-5648.20240142
Xin LONG, Chiyuan WANG, Changwei SHAO, Qianlong WANG. Research Progress on Polymer-Derived Nitride Ceramics for Wave Transparent at High Temperature[J]. Journal of the Chinese Ceramic Society, 2024 , 52 (9) : 2862 -2874 . DOI: 10.14062/j.issn.0454-5648.20240142
  • 国家自然科学基金(52073304; 52103364)
  • 国防科技大学自主科研项目(ZK21-26; 22-079)
  • 湖南省自然科学基金(2022JJ 30045)
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2024年第52卷第9期
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doi: 10.14062/j.issn.0454-5648.20240142
  • 接收时间:2024-02-23
  • 首发时间:2026-10-22
  • 出版时间:2024-09-20
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  • 收稿日期:2024-02-23
  • 修回日期:2024-03-10
基金
国家自然科学基金(52073304; 52103364)
国防科技大学自主科研项目(ZK21-26; 22-079)
湖南省自然科学基金(2022JJ 30045)
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    国防科技大学空天科学学院,新型陶瓷纤维及其复合材料重点实验室,长沙 410073
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2种不同金属材料的力学参数
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鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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