Damage Tolerance of Silicon Carbide- and Alumina-Matrix Surface Composites

A method for the fabrication of a ceramic‐matrix composite (CMC) layer on the surface of a monolithic substrate via chemical vapor infiltration (CVI) is described. Preforms consisted of tows of fibers wound onto the surface of monolithic cylindrical tubes. Nicalon fibers were wound onto mullite subs...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of the American Ceramic Society 1996-04, Vol.79 (4), p.1117-1120
Hauptverfasser: Day, P. S., Skamser, D. J., Faber, K. T., Jennings, H. M., Johnson, D. Lynn
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 1120
container_issue 4
container_start_page 1117
container_title Journal of the American Ceramic Society
container_volume 79
creator Day, P. S.
Skamser, D. J.
Faber, K. T.
Jennings, H. M.
Johnson, D. Lynn
description A method for the fabrication of a ceramic‐matrix composite (CMC) layer on the surface of a monolithic substrate via chemical vapor infiltration (CVI) is described. Preforms consisted of tows of fibers wound onto the surface of monolithic cylindrical tubes. Nicalon fibers were wound onto mullite substrates and infiltrated with β‐SiC from CH3SiCl3/H2 gas mixtures in a cylindrical cold‐wall reactor. Similarly, Nextel fibers were wound onto A12O3 substrates and infiltrated with α‐Al2O3 from AlCl3/H2/CO2/N2 gas mixtures. Composites with densities as high as 88% of the theoretical value were fabricated in 8 h. The effective fracture strength of the SiC‐ and Al2O3‐matrix surface composites, as determined from diametral compression tests of C‐ring specimens, was found to be insensitive to damage caused to the outer diameter by a Vickers indentation. The tolerance of the SiC‐matrix surface composites to surface damage was retained in specimens subjected to oxidation at 1000°C for 6 h.
doi_str_mv 10.1111/j.1151-2916.1996.tb08558.x
format Article
fullrecord <record><control><sourceid>proquest_osti_</sourceid><recordid>TN_cdi_proquest_miscellaneous_26109102</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>26109102</sourcerecordid><originalsourceid>FETCH-LOGICAL-c4787-2e14131df0f3401fb42ee9b332f8ab66f257273d738386078b2dd67044ed26033</originalsourceid><addsrcrecordid>eNqVkF1v0zAUhi3EJMrGfwgIcZfOH4ntcEUVRtlW2KQOcXnkODa4JHFnp6L79zhKtXt8c2T58fsePQi9I3hJ0rncpVGSnFaEL0lV8eXYYFmWcnl8gRakPD29RAuMMc2FpPgVeh3jLl1JJYsFuvmsevXLZA--M0EN2mTeZlvXOe2HrFahca3JMzW02ao79G5Q-Tc1BnfMtodgVcJr3-99dKOJF-jMqi6aN6d5jn58uXqov-abu_V1vdrkuhBS5NSQgjDSWmxZgYltCmpM1TBGrVQN55aWggrWCiaZ5FjIhrYtF7goTEs5ZuwcvZ1zfRwdRJ269e-07mD0CLQQFSOJ-TAz--AfDyaO0LuoTdepwfhDBMoJrgimCfw4gzr4GIOxsA-uV-EJCIZJMexgUgyTR5gUw0kxHNPn96cWFbXq7CTQxecEhnnaVyTs04z9dZ15-o8CuFnVVwmZIvI5wsXRHJ8jVPgDXDBRws_va9jcrnF5u70Hwv4B7Iidfw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>26109102</pqid></control><display><type>article</type><title>Damage Tolerance of Silicon Carbide- and Alumina-Matrix Surface Composites</title><source>Wiley Online Library Journals Frontfile Complete</source><creator>Day, P. S. ; Skamser, D. J. ; Faber, K. T. ; Jennings, H. M. ; Johnson, D. Lynn</creator><creatorcontrib>Day, P. S. ; Skamser, D. J. ; Faber, K. T. ; Jennings, H. M. ; Johnson, D. Lynn</creatorcontrib><description>A method for the fabrication of a ceramic‐matrix composite (CMC) layer on the surface of a monolithic substrate via chemical vapor infiltration (CVI) is described. Preforms consisted of tows of fibers wound onto the surface of monolithic cylindrical tubes. Nicalon fibers were wound onto mullite substrates and infiltrated with β‐SiC from CH3SiCl3/H2 gas mixtures in a cylindrical cold‐wall reactor. Similarly, Nextel fibers were wound onto A12O3 substrates and infiltrated with α‐Al2O3 from AlCl3/H2/CO2/N2 gas mixtures. Composites with densities as high as 88% of the theoretical value were fabricated in 8 h. The effective fracture strength of the SiC‐ and Al2O3‐matrix surface composites, as determined from diametral compression tests of C‐ring specimens, was found to be insensitive to damage caused to the outer diameter by a Vickers indentation. The tolerance of the SiC‐matrix surface composites to surface damage was retained in specimens subjected to oxidation at 1000°C for 6 h.</description><identifier>ISSN: 0002-7820</identifier><identifier>EISSN: 1551-2916</identifier><identifier>DOI: 10.1111/j.1151-2916.1996.tb08558.x</identifier><identifier>CODEN: JACTAW</identifier><language>eng</language><publisher>Oxford, UK: Blackwell Publishing Ltd</publisher><subject>ALUMINIUM OXIDES ; Applied sciences ; Building materials. Ceramics. Glasses ; BULK DENSITY ; CARBON DIOXIDE ; Ceramic industries ; Chemical industry and chemicals ; CHEMICAL REACTIONS ; CHEMICAL VAPOR DEPOSITION ; CHLORIDES ; COMPOSITE MATERIALS ; Exact sciences and technology ; FIBERS ; FRACTURE PROPERTIES ; HYDROGEN ; IMPREGNATION ; MATERIALS SCIENCE ; MULLITE ; NITROGEN ; ORGANOMETALLIC COMPOUNDS ; SILICON CARBIDES ; Structural ceramics ; SUBSTRATES ; Technical ceramics ; TEMPERATURE GRADIENTS</subject><ispartof>Journal of the American Ceramic Society, 1996-04, Vol.79 (4), p.1117-1120</ispartof><rights>1996 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c4787-2e14131df0f3401fb42ee9b332f8ab66f257273d738386078b2dd67044ed26033</citedby><cites>FETCH-LOGICAL-c4787-2e14131df0f3401fb42ee9b332f8ab66f257273d738386078b2dd67044ed26033</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1111%2Fj.1151-2916.1996.tb08558.x$$EPDF$$P50$$Gwiley$$H</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1111%2Fj.1151-2916.1996.tb08558.x$$EHTML$$P50$$Gwiley$$H</linktohtml><link.rule.ids>314,776,780,881,1411,27903,27904,45553,45554</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&amp;idt=3066037$$DView record in Pascal Francis$$Hfree_for_read</backlink><backlink>$$Uhttps://www.osti.gov/biblio/247931$$D View this record in Osti.gov$$Hfree_for_read</backlink></links><search><creatorcontrib>Day, P. S.</creatorcontrib><creatorcontrib>Skamser, D. J.</creatorcontrib><creatorcontrib>Faber, K. T.</creatorcontrib><creatorcontrib>Jennings, H. M.</creatorcontrib><creatorcontrib>Johnson, D. Lynn</creatorcontrib><title>Damage Tolerance of Silicon Carbide- and Alumina-Matrix Surface Composites</title><title>Journal of the American Ceramic Society</title><description>A method for the fabrication of a ceramic‐matrix composite (CMC) layer on the surface of a monolithic substrate via chemical vapor infiltration (CVI) is described. Preforms consisted of tows of fibers wound onto the surface of monolithic cylindrical tubes. Nicalon fibers were wound onto mullite substrates and infiltrated with β‐SiC from CH3SiCl3/H2 gas mixtures in a cylindrical cold‐wall reactor. Similarly, Nextel fibers were wound onto A12O3 substrates and infiltrated with α‐Al2O3 from AlCl3/H2/CO2/N2 gas mixtures. Composites with densities as high as 88% of the theoretical value were fabricated in 8 h. The effective fracture strength of the SiC‐ and Al2O3‐matrix surface composites, as determined from diametral compression tests of C‐ring specimens, was found to be insensitive to damage caused to the outer diameter by a Vickers indentation. The tolerance of the SiC‐matrix surface composites to surface damage was retained in specimens subjected to oxidation at 1000°C for 6 h.</description><subject>ALUMINIUM OXIDES</subject><subject>Applied sciences</subject><subject>Building materials. Ceramics. Glasses</subject><subject>BULK DENSITY</subject><subject>CARBON DIOXIDE</subject><subject>Ceramic industries</subject><subject>Chemical industry and chemicals</subject><subject>CHEMICAL REACTIONS</subject><subject>CHEMICAL VAPOR DEPOSITION</subject><subject>CHLORIDES</subject><subject>COMPOSITE MATERIALS</subject><subject>Exact sciences and technology</subject><subject>FIBERS</subject><subject>FRACTURE PROPERTIES</subject><subject>HYDROGEN</subject><subject>IMPREGNATION</subject><subject>MATERIALS SCIENCE</subject><subject>MULLITE</subject><subject>NITROGEN</subject><subject>ORGANOMETALLIC COMPOUNDS</subject><subject>SILICON CARBIDES</subject><subject>Structural ceramics</subject><subject>SUBSTRATES</subject><subject>Technical ceramics</subject><subject>TEMPERATURE GRADIENTS</subject><issn>0002-7820</issn><issn>1551-2916</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1996</creationdate><recordtype>article</recordtype><recordid>eNqVkF1v0zAUhi3EJMrGfwgIcZfOH4ntcEUVRtlW2KQOcXnkODa4JHFnp6L79zhKtXt8c2T58fsePQi9I3hJ0rncpVGSnFaEL0lV8eXYYFmWcnl8gRakPD29RAuMMc2FpPgVeh3jLl1JJYsFuvmsevXLZA--M0EN2mTeZlvXOe2HrFahca3JMzW02ao79G5Q-Tc1BnfMtodgVcJr3-99dKOJF-jMqi6aN6d5jn58uXqov-abu_V1vdrkuhBS5NSQgjDSWmxZgYltCmpM1TBGrVQN55aWggrWCiaZ5FjIhrYtF7goTEs5ZuwcvZ1zfRwdRJ269e-07mD0CLQQFSOJ-TAz--AfDyaO0LuoTdepwfhDBMoJrgimCfw4gzr4GIOxsA-uV-EJCIZJMexgUgyTR5gUw0kxHNPn96cWFbXq7CTQxecEhnnaVyTs04z9dZ15-o8CuFnVVwmZIvI5wsXRHJ8jVPgDXDBRws_va9jcrnF5u70Hwv4B7Iidfw</recordid><startdate>199604</startdate><enddate>199604</enddate><creator>Day, P. S.</creator><creator>Skamser, D. J.</creator><creator>Faber, K. T.</creator><creator>Jennings, H. M.</creator><creator>Johnson, D. Lynn</creator><general>Blackwell Publishing Ltd</general><general>Blackwell</general><scope>BSCLL</scope><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>H8D</scope><scope>JG9</scope><scope>L7M</scope><scope>OTOTI</scope></search><sort><creationdate>199604</creationdate><title>Damage Tolerance of Silicon Carbide- and Alumina-Matrix Surface Composites</title><author>Day, P. S. ; Skamser, D. J. ; Faber, K. T. ; Jennings, H. M. ; Johnson, D. Lynn</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c4787-2e14131df0f3401fb42ee9b332f8ab66f257273d738386078b2dd67044ed26033</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1996</creationdate><topic>ALUMINIUM OXIDES</topic><topic>Applied sciences</topic><topic>Building materials. Ceramics. Glasses</topic><topic>BULK DENSITY</topic><topic>CARBON DIOXIDE</topic><topic>Ceramic industries</topic><topic>Chemical industry and chemicals</topic><topic>CHEMICAL REACTIONS</topic><topic>CHEMICAL VAPOR DEPOSITION</topic><topic>CHLORIDES</topic><topic>COMPOSITE MATERIALS</topic><topic>Exact sciences and technology</topic><topic>FIBERS</topic><topic>FRACTURE PROPERTIES</topic><topic>HYDROGEN</topic><topic>IMPREGNATION</topic><topic>MATERIALS SCIENCE</topic><topic>MULLITE</topic><topic>NITROGEN</topic><topic>ORGANOMETALLIC COMPOUNDS</topic><topic>SILICON CARBIDES</topic><topic>Structural ceramics</topic><topic>SUBSTRATES</topic><topic>Technical ceramics</topic><topic>TEMPERATURE GRADIENTS</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Day, P. S.</creatorcontrib><creatorcontrib>Skamser, D. J.</creatorcontrib><creatorcontrib>Faber, K. T.</creatorcontrib><creatorcontrib>Jennings, H. M.</creatorcontrib><creatorcontrib>Johnson, D. Lynn</creatorcontrib><collection>Istex</collection><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>OSTI.GOV</collection><jtitle>Journal of the American Ceramic Society</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Day, P. S.</au><au>Skamser, D. J.</au><au>Faber, K. T.</au><au>Jennings, H. M.</au><au>Johnson, D. Lynn</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Damage Tolerance of Silicon Carbide- and Alumina-Matrix Surface Composites</atitle><jtitle>Journal of the American Ceramic Society</jtitle><date>1996-04</date><risdate>1996</risdate><volume>79</volume><issue>4</issue><spage>1117</spage><epage>1120</epage><pages>1117-1120</pages><issn>0002-7820</issn><eissn>1551-2916</eissn><coden>JACTAW</coden><abstract>A method for the fabrication of a ceramic‐matrix composite (CMC) layer on the surface of a monolithic substrate via chemical vapor infiltration (CVI) is described. Preforms consisted of tows of fibers wound onto the surface of monolithic cylindrical tubes. Nicalon fibers were wound onto mullite substrates and infiltrated with β‐SiC from CH3SiCl3/H2 gas mixtures in a cylindrical cold‐wall reactor. Similarly, Nextel fibers were wound onto A12O3 substrates and infiltrated with α‐Al2O3 from AlCl3/H2/CO2/N2 gas mixtures. Composites with densities as high as 88% of the theoretical value were fabricated in 8 h. The effective fracture strength of the SiC‐ and Al2O3‐matrix surface composites, as determined from diametral compression tests of C‐ring specimens, was found to be insensitive to damage caused to the outer diameter by a Vickers indentation. The tolerance of the SiC‐matrix surface composites to surface damage was retained in specimens subjected to oxidation at 1000°C for 6 h.</abstract><cop>Oxford, UK</cop><pub>Blackwell Publishing Ltd</pub><doi>10.1111/j.1151-2916.1996.tb08558.x</doi><tpages>4</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0002-7820
ispartof Journal of the American Ceramic Society, 1996-04, Vol.79 (4), p.1117-1120
issn 0002-7820
1551-2916
language eng
recordid cdi_proquest_miscellaneous_26109102
source Wiley Online Library Journals Frontfile Complete
subjects ALUMINIUM OXIDES
Applied sciences
Building materials. Ceramics. Glasses
BULK DENSITY
CARBON DIOXIDE
Ceramic industries
Chemical industry and chemicals
CHEMICAL REACTIONS
CHEMICAL VAPOR DEPOSITION
CHLORIDES
COMPOSITE MATERIALS
Exact sciences and technology
FIBERS
FRACTURE PROPERTIES
HYDROGEN
IMPREGNATION
MATERIALS SCIENCE
MULLITE
NITROGEN
ORGANOMETALLIC COMPOUNDS
SILICON CARBIDES
Structural ceramics
SUBSTRATES
Technical ceramics
TEMPERATURE GRADIENTS
title Damage Tolerance of Silicon Carbide- and Alumina-Matrix Surface Composites
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-21T12%3A23%3A56IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_osti_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Damage%20Tolerance%20of%20Silicon%20Carbide-%20and%20Alumina-Matrix%20Surface%20Composites&rft.jtitle=Journal%20of%20the%20American%20Ceramic%20Society&rft.au=Day,%20P.%20S.&rft.date=1996-04&rft.volume=79&rft.issue=4&rft.spage=1117&rft.epage=1120&rft.pages=1117-1120&rft.issn=0002-7820&rft.eissn=1551-2916&rft.coden=JACTAW&rft_id=info:doi/10.1111/j.1151-2916.1996.tb08558.x&rft_dat=%3Cproquest_osti_%3E26109102%3C/proquest_osti_%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=26109102&rft_id=info:pmid/&rfr_iscdi=true