Effect of high temperature on compression property and deformation recovery of ceramic fiber reinforced silica aerogel composites
Ceramic fiber reinforced silica aerogel composites are novel insulation materials in the thermal protection field for hypersonic vehicles. Before the aerogel composites are applied in load-bearing structures, it is necessary to investigate their mechanical properties including load-bearing and defor...
Gespeichert in:
Veröffentlicht in: | Science China. Technological sciences 2017-11, Vol.60 (11), p.1681-1691 |
---|---|
Hauptverfasser: | , , , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 1691 |
---|---|
container_issue | 11 |
container_start_page | 1681 |
container_title | Science China. Technological sciences |
container_volume | 60 |
creator | Lyu, ShuangQi Yang, XiaoGuang Shi, DuoQi Qi, HongYu Jing, Xin Li, ShaoLin |
description | Ceramic fiber reinforced silica aerogel composites are novel insulation materials in the thermal protection field for hypersonic vehicles. Before the aerogel composites are applied in load-bearing structures, it is necessary to investigate their mechanical properties including load-bearing and deformation recovery capabilities. High temperature from service conditions will have important effects on the mechanical properties of thermal protection materials. In this paper, compression tests including loading and unloading stages were conducted for ceramic fiber reinforced silica aerogel composites at room temperature and elevated temperatures (300℃, 600℃ and 900℃). Influences of thermal exposure to high temperature and high temperature service environment on the compression property and deformation recovery were both investigated. Scanning electron microscopy (SEM), Fourier transform infrared spectroscopy (FT-IR) and X-ray diffraction (XRD) were applied to help understand the mechanisms of mechanical property variations. The experimental results show that the compression modulus and strength both increase with the increasing thermal exposure temperature and testing temperature, but the deformation recovery capability decreases. The microstructure changes caused by thermal sintering are considered as the main reason for the property variations. Viscous flow and matter transport due to high temperature resulted in the fusion of aerogel particles. This made the particle skeleton thicker and stronger, which led to higher stiffness and strength of the composites. However, matrix cracks induced by the formation and fracture of larger pores made unrecoverable deformation more serious. In the tests at elevated temperatures, the aggregation of aerogel particles in a fused state got more severe because of the addition of mechanical load. As a result, the degradation of deformation recovery capability became more significant. |
doi_str_mv | 10.1007/s11431-016-9092-2 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_1961834715</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><cqvip_id>673737272</cqvip_id><sourcerecordid>1961834715</sourcerecordid><originalsourceid>FETCH-LOGICAL-c446t-cf8f792dd5c3a6d8176c9274ac250b6ed5e8ff010a1b207cd505b1699c1214953</originalsourceid><addsrcrecordid>eNp9UM1LwzAUL6LgmPsDvAU9V_PSNmmOMuYHCF70HNL0ZctYmy3phB39z03dEE--HN6D3xf5Zdk10DugVNxHgLKAnALPJZUsZ2fZBGouc5CUnqebizIXBYPLbBbjmqYpakmhnGRfC2vRDMRbsnLLFRmw22LQwz4g8T0xvtsGjNGlext8goYD0X1LWrQ-dHoYgYDGf2I4jCYmiTtniHUNhoS4PvEMtiS6jTOaaAx-iZsfYx_dgPEqu7B6E3F22tPs43HxPn_OX9-eXuYPr7kpSz7kxtZWSNa2lSk0b2sQ3EgmSm1YRRuObYW1tRSohoZRYdqKVg1wKQ0wKGVVTLPbo2_6x26PcVBrvw99ilQgOdRFKWBkwZFlgo8xoFXb4DodDgqoGstWx7JVKluNZSuWNOyoiYnbLzH8cf5HdHMKWvl-uUu63yQuivSYYMU3i6ePZQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1961834715</pqid></control><display><type>article</type><title>Effect of high temperature on compression property and deformation recovery of ceramic fiber reinforced silica aerogel composites</title><source>Alma/SFX Local Collection</source><source>SpringerLink Journals - AutoHoldings</source><creator>Lyu, ShuangQi ; Yang, XiaoGuang ; Shi, DuoQi ; Qi, HongYu ; Jing, Xin ; Li, ShaoLin</creator><creatorcontrib>Lyu, ShuangQi ; Yang, XiaoGuang ; Shi, DuoQi ; Qi, HongYu ; Jing, Xin ; Li, ShaoLin</creatorcontrib><description>Ceramic fiber reinforced silica aerogel composites are novel insulation materials in the thermal protection field for hypersonic vehicles. Before the aerogel composites are applied in load-bearing structures, it is necessary to investigate their mechanical properties including load-bearing and deformation recovery capabilities. High temperature from service conditions will have important effects on the mechanical properties of thermal protection materials. In this paper, compression tests including loading and unloading stages were conducted for ceramic fiber reinforced silica aerogel composites at room temperature and elevated temperatures (300℃, 600℃ and 900℃). Influences of thermal exposure to high temperature and high temperature service environment on the compression property and deformation recovery were both investigated. Scanning electron microscopy (SEM), Fourier transform infrared spectroscopy (FT-IR) and X-ray diffraction (XRD) were applied to help understand the mechanisms of mechanical property variations. The experimental results show that the compression modulus and strength both increase with the increasing thermal exposure temperature and testing temperature, but the deformation recovery capability decreases. The microstructure changes caused by thermal sintering are considered as the main reason for the property variations. Viscous flow and matter transport due to high temperature resulted in the fusion of aerogel particles. This made the particle skeleton thicker and stronger, which led to higher stiffness and strength of the composites. However, matrix cracks induced by the formation and fracture of larger pores made unrecoverable deformation more serious. In the tests at elevated temperatures, the aggregation of aerogel particles in a fused state got more severe because of the addition of mechanical load. As a result, the degradation of deformation recovery capability became more significant.</description><identifier>ISSN: 1674-7321</identifier><identifier>EISSN: 1869-1900</identifier><identifier>DOI: 10.1007/s11431-016-9092-2</identifier><language>eng</language><publisher>Beijing: Science China Press</publisher><subject>Aerogels ; Ceramic fibers ; Ceramics ; Composite materials ; Compression tests ; Compressive strength ; Deformation effects ; Deformation mechanisms ; Electron microscopy ; Engineering ; Fiber composites ; Fourier transforms ; Fracture mechanics ; High temperature ; Hypersonic vehicles ; Infrared spectroscopy ; Insulation ; Load bearing elements ; Matrix cracks ; Mechanical properties ; Particulate composites ; Recovery ; Silicon dioxide ; Stiffness ; Thermal protection ; Viscous flow ; X-ray diffraction ; 力学性能变化 ; 压缩性能 ; 变形恢复 ; 回复率 ; 复合材料 ; 硅气凝胶 ; 陶瓷纤维增强 ; 高温条件</subject><ispartof>Science China. Technological sciences, 2017-11, Vol.60 (11), p.1681-1691</ispartof><rights>Science China Press and Springer-Verlag GmbH Germany 2017</rights><rights>Copyright Springer Science & Business Media 2017</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c446t-cf8f792dd5c3a6d8176c9274ac250b6ed5e8ff010a1b207cd505b1699c1214953</citedby><cites>FETCH-LOGICAL-c446t-cf8f792dd5c3a6d8176c9274ac250b6ed5e8ff010a1b207cd505b1699c1214953</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://image.cqvip.com/vip1000/qk/60110X/60110X.jpg</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s11431-016-9092-2$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s11431-016-9092-2$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,777,781,27905,27906,41469,42538,51300</link.rule.ids></links><search><creatorcontrib>Lyu, ShuangQi</creatorcontrib><creatorcontrib>Yang, XiaoGuang</creatorcontrib><creatorcontrib>Shi, DuoQi</creatorcontrib><creatorcontrib>Qi, HongYu</creatorcontrib><creatorcontrib>Jing, Xin</creatorcontrib><creatorcontrib>Li, ShaoLin</creatorcontrib><title>Effect of high temperature on compression property and deformation recovery of ceramic fiber reinforced silica aerogel composites</title><title>Science China. Technological sciences</title><addtitle>Sci. China Technol. Sci</addtitle><addtitle>SCIENCE CHINA Technological Sciences</addtitle><description>Ceramic fiber reinforced silica aerogel composites are novel insulation materials in the thermal protection field for hypersonic vehicles. Before the aerogel composites are applied in load-bearing structures, it is necessary to investigate their mechanical properties including load-bearing and deformation recovery capabilities. High temperature from service conditions will have important effects on the mechanical properties of thermal protection materials. In this paper, compression tests including loading and unloading stages were conducted for ceramic fiber reinforced silica aerogel composites at room temperature and elevated temperatures (300℃, 600℃ and 900℃). Influences of thermal exposure to high temperature and high temperature service environment on the compression property and deformation recovery were both investigated. Scanning electron microscopy (SEM), Fourier transform infrared spectroscopy (FT-IR) and X-ray diffraction (XRD) were applied to help understand the mechanisms of mechanical property variations. The experimental results show that the compression modulus and strength both increase with the increasing thermal exposure temperature and testing temperature, but the deformation recovery capability decreases. The microstructure changes caused by thermal sintering are considered as the main reason for the property variations. Viscous flow and matter transport due to high temperature resulted in the fusion of aerogel particles. This made the particle skeleton thicker and stronger, which led to higher stiffness and strength of the composites. However, matrix cracks induced by the formation and fracture of larger pores made unrecoverable deformation more serious. In the tests at elevated temperatures, the aggregation of aerogel particles in a fused state got more severe because of the addition of mechanical load. As a result, the degradation of deformation recovery capability became more significant.</description><subject>Aerogels</subject><subject>Ceramic fibers</subject><subject>Ceramics</subject><subject>Composite materials</subject><subject>Compression tests</subject><subject>Compressive strength</subject><subject>Deformation effects</subject><subject>Deformation mechanisms</subject><subject>Electron microscopy</subject><subject>Engineering</subject><subject>Fiber composites</subject><subject>Fourier transforms</subject><subject>Fracture mechanics</subject><subject>High temperature</subject><subject>Hypersonic vehicles</subject><subject>Infrared spectroscopy</subject><subject>Insulation</subject><subject>Load bearing elements</subject><subject>Matrix cracks</subject><subject>Mechanical properties</subject><subject>Particulate composites</subject><subject>Recovery</subject><subject>Silicon dioxide</subject><subject>Stiffness</subject><subject>Thermal protection</subject><subject>Viscous flow</subject><subject>X-ray diffraction</subject><subject>力学性能变化</subject><subject>压缩性能</subject><subject>变形恢复</subject><subject>回复率</subject><subject>复合材料</subject><subject>硅气凝胶</subject><subject>陶瓷纤维增强</subject><subject>高温条件</subject><issn>1674-7321</issn><issn>1869-1900</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp9UM1LwzAUL6LgmPsDvAU9V_PSNmmOMuYHCF70HNL0ZctYmy3phB39z03dEE--HN6D3xf5Zdk10DugVNxHgLKAnALPJZUsZ2fZBGouc5CUnqebizIXBYPLbBbjmqYpakmhnGRfC2vRDMRbsnLLFRmw22LQwz4g8T0xvtsGjNGlext8goYD0X1LWrQ-dHoYgYDGf2I4jCYmiTtniHUNhoS4PvEMtiS6jTOaaAx-iZsfYx_dgPEqu7B6E3F22tPs43HxPn_OX9-eXuYPr7kpSz7kxtZWSNa2lSk0b2sQ3EgmSm1YRRuObYW1tRSohoZRYdqKVg1wKQ0wKGVVTLPbo2_6x26PcVBrvw99ilQgOdRFKWBkwZFlgo8xoFXb4DodDgqoGstWx7JVKluNZSuWNOyoiYnbLzH8cf5HdHMKWvl-uUu63yQuivSYYMU3i6ePZQ</recordid><startdate>20171101</startdate><enddate>20171101</enddate><creator>Lyu, ShuangQi</creator><creator>Yang, XiaoGuang</creator><creator>Shi, DuoQi</creator><creator>Qi, HongYu</creator><creator>Jing, Xin</creator><creator>Li, ShaoLin</creator><general>Science China Press</general><general>Springer Nature B.V</general><scope>2RA</scope><scope>92L</scope><scope>CQIGP</scope><scope>W92</scope><scope>~WA</scope><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20171101</creationdate><title>Effect of high temperature on compression property and deformation recovery of ceramic fiber reinforced silica aerogel composites</title><author>Lyu, ShuangQi ; Yang, XiaoGuang ; Shi, DuoQi ; Qi, HongYu ; Jing, Xin ; Li, ShaoLin</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c446t-cf8f792dd5c3a6d8176c9274ac250b6ed5e8ff010a1b207cd505b1699c1214953</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Aerogels</topic><topic>Ceramic fibers</topic><topic>Ceramics</topic><topic>Composite materials</topic><topic>Compression tests</topic><topic>Compressive strength</topic><topic>Deformation effects</topic><topic>Deformation mechanisms</topic><topic>Electron microscopy</topic><topic>Engineering</topic><topic>Fiber composites</topic><topic>Fourier transforms</topic><topic>Fracture mechanics</topic><topic>High temperature</topic><topic>Hypersonic vehicles</topic><topic>Infrared spectroscopy</topic><topic>Insulation</topic><topic>Load bearing elements</topic><topic>Matrix cracks</topic><topic>Mechanical properties</topic><topic>Particulate composites</topic><topic>Recovery</topic><topic>Silicon dioxide</topic><topic>Stiffness</topic><topic>Thermal protection</topic><topic>Viscous flow</topic><topic>X-ray diffraction</topic><topic>力学性能变化</topic><topic>压缩性能</topic><topic>变形恢复</topic><topic>回复率</topic><topic>复合材料</topic><topic>硅气凝胶</topic><topic>陶瓷纤维增强</topic><topic>高温条件</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Lyu, ShuangQi</creatorcontrib><creatorcontrib>Yang, XiaoGuang</creatorcontrib><creatorcontrib>Shi, DuoQi</creatorcontrib><creatorcontrib>Qi, HongYu</creatorcontrib><creatorcontrib>Jing, Xin</creatorcontrib><creatorcontrib>Li, ShaoLin</creatorcontrib><collection>中文科技期刊数据库</collection><collection>中文科技期刊数据库-CALIS站点</collection><collection>中文科技期刊数据库-7.0平台</collection><collection>中文科技期刊数据库-工程技术</collection><collection>中文科技期刊数据库- 镜像站点</collection><collection>CrossRef</collection><jtitle>Science China. Technological sciences</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Lyu, ShuangQi</au><au>Yang, XiaoGuang</au><au>Shi, DuoQi</au><au>Qi, HongYu</au><au>Jing, Xin</au><au>Li, ShaoLin</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Effect of high temperature on compression property and deformation recovery of ceramic fiber reinforced silica aerogel composites</atitle><jtitle>Science China. Technological sciences</jtitle><stitle>Sci. China Technol. Sci</stitle><addtitle>SCIENCE CHINA Technological Sciences</addtitle><date>2017-11-01</date><risdate>2017</risdate><volume>60</volume><issue>11</issue><spage>1681</spage><epage>1691</epage><pages>1681-1691</pages><issn>1674-7321</issn><eissn>1869-1900</eissn><abstract>Ceramic fiber reinforced silica aerogel composites are novel insulation materials in the thermal protection field for hypersonic vehicles. Before the aerogel composites are applied in load-bearing structures, it is necessary to investigate their mechanical properties including load-bearing and deformation recovery capabilities. High temperature from service conditions will have important effects on the mechanical properties of thermal protection materials. In this paper, compression tests including loading and unloading stages were conducted for ceramic fiber reinforced silica aerogel composites at room temperature and elevated temperatures (300℃, 600℃ and 900℃). Influences of thermal exposure to high temperature and high temperature service environment on the compression property and deformation recovery were both investigated. Scanning electron microscopy (SEM), Fourier transform infrared spectroscopy (FT-IR) and X-ray diffraction (XRD) were applied to help understand the mechanisms of mechanical property variations. The experimental results show that the compression modulus and strength both increase with the increasing thermal exposure temperature and testing temperature, but the deformation recovery capability decreases. The microstructure changes caused by thermal sintering are considered as the main reason for the property variations. Viscous flow and matter transport due to high temperature resulted in the fusion of aerogel particles. This made the particle skeleton thicker and stronger, which led to higher stiffness and strength of the composites. However, matrix cracks induced by the formation and fracture of larger pores made unrecoverable deformation more serious. In the tests at elevated temperatures, the aggregation of aerogel particles in a fused state got more severe because of the addition of mechanical load. As a result, the degradation of deformation recovery capability became more significant.</abstract><cop>Beijing</cop><pub>Science China Press</pub><doi>10.1007/s11431-016-9092-2</doi><tpages>11</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 1674-7321 |
ispartof | Science China. Technological sciences, 2017-11, Vol.60 (11), p.1681-1691 |
issn | 1674-7321 1869-1900 |
language | eng |
recordid | cdi_proquest_journals_1961834715 |
source | Alma/SFX Local Collection; SpringerLink Journals - AutoHoldings |
subjects | Aerogels Ceramic fibers Ceramics Composite materials Compression tests Compressive strength Deformation effects Deformation mechanisms Electron microscopy Engineering Fiber composites Fourier transforms Fracture mechanics High temperature Hypersonic vehicles Infrared spectroscopy Insulation Load bearing elements Matrix cracks Mechanical properties Particulate composites Recovery Silicon dioxide Stiffness Thermal protection Viscous flow X-ray diffraction 力学性能变化 压缩性能 变形恢复 回复率 复合材料 硅气凝胶 陶瓷纤维增强 高温条件 |
title | Effect of high temperature on compression property and deformation recovery of ceramic fiber reinforced silica aerogel composites |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-18T03%3A55%3A51IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Effect%20of%20high%20temperature%20on%20compression%20property%20and%20deformation%20recovery%20of%20ceramic%20fiber%20reinforced%20silica%20aerogel%20composites&rft.jtitle=Science%20China.%20Technological%20sciences&rft.au=Lyu,%20ShuangQi&rft.date=2017-11-01&rft.volume=60&rft.issue=11&rft.spage=1681&rft.epage=1691&rft.pages=1681-1691&rft.issn=1674-7321&rft.eissn=1869-1900&rft_id=info:doi/10.1007/s11431-016-9092-2&rft_dat=%3Cproquest_cross%3E1961834715%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1961834715&rft_id=info:pmid/&rft_cqvip_id=673737272&rfr_iscdi=true |