CERAMIC MATRIX COMPOSITE STRUCTURES, COMPONENTS FORMED THEREWITH, AND METHODS OF PRODUCING
Ceramic matrix composite sandwich structures, gas turbine engine components that comprise such sandwich structures, and methods of producing such sandwich structures. The ceramic matrix composite sandwich structure includes a core having oppositely-disposed first and second surfaces, a first faceshe...
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| creator | RENGGLI, BERNARD JAMES MILLARD, MICHAEL LEE MILLER, JEFFREY FRANKLIN MEIBERS, GREGORY JOSEPH HALL, KATHLEEN RAFTERY |
| description | Ceramic matrix composite sandwich structures, gas turbine engine components that comprise such sandwich structures, and methods of producing such sandwich structures. The ceramic matrix composite sandwich structure includes a core having oppositely-disposed first and second surfaces, a first facesheet bonded to the first surface, and a member bonded to the second surface so that the core is between the first facesheet and the member. The first facesheet and the core comprise, respectively, first and second ceramic matrix composite materials, and the second ceramic matrix composite material of the core has a ceramic reinforcement material in the form of a felt or an open weave fabric. |
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The ceramic matrix composite sandwich structure includes a core having oppositely-disposed first and second surfaces, a first facesheet bonded to the first surface, and a member bonded to the second surface so that the core is between the first facesheet and the member. The first facesheet and the core comprise, respectively, first and second ceramic matrix composite materials, and the second ceramic matrix composite material of the core has a ceramic reinforcement material in the form of a felt or an open weave fabric.</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; ARTIFICIAL STONE ; AVIATION ; CEMENTS ; CERAMICS ; CHEMISTRY ; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS ; CONCRETE ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; LAYERED PRODUCTS ; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM ; LIME, MAGNESIA ; METALLURGY ; PARACHUTES ; PERFORMING OPERATIONS ; REFRACTORIES ; SLAG ; TRANSPORTING ; TREATMENT OF NATURAL STONE</subject><creationdate>2012</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20120907&DB=EPODOC&CC=CA&NR=2799049A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20120907&DB=EPODOC&CC=CA&NR=2799049A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>RENGGLI, BERNARD JAMES</creatorcontrib><creatorcontrib>MILLARD, MICHAEL LEE</creatorcontrib><creatorcontrib>MILLER, JEFFREY FRANKLIN</creatorcontrib><creatorcontrib>MEIBERS, GREGORY JOSEPH</creatorcontrib><creatorcontrib>HALL, KATHLEEN RAFTERY</creatorcontrib><title>CERAMIC MATRIX COMPOSITE STRUCTURES, COMPONENTS FORMED THEREWITH, AND METHODS OF PRODUCING</title><description>Ceramic matrix composite sandwich structures, gas turbine engine components that comprise such sandwich structures, and methods of producing such sandwich structures. The ceramic matrix composite sandwich structure includes a core having oppositely-disposed first and second surfaces, a first facesheet bonded to the first surface, and a member bonded to the second surface so that the core is between the first facesheet and the member. The first facesheet and the core comprise, respectively, first and second ceramic matrix composite materials, and the second ceramic matrix composite material of the core has a ceramic reinforcement material in the form of a felt or an open weave fabric.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>ARTIFICIAL STONE</subject><subject>AVIATION</subject><subject>CEMENTS</subject><subject>CERAMICS</subject><subject>CHEMISTRY</subject><subject>COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS</subject><subject>CONCRETE</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>LAYERED PRODUCTS</subject><subject>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</subject><subject>LIME, MAGNESIA</subject><subject>METALLURGY</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>REFRACTORIES</subject><subject>SLAG</subject><subject>TRANSPORTING</subject><subject>TREATMENT OF NATURAL STONE</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyj0KAjEQQOFtLES9wxxgBf9AUobJxKRIskwmKDbLIrESXVjvj4UewOrBx5s3VyTWwSMELewvgCl0KXshyMIFpTDl9quRomSwiQMZEEdMZy-uBR0NBBKXTIZkoeNkCvp4Wjaz-_CY6urXRQOWBN26jq--TuNwq8_67lHvjkptDkpv938sHyPZMa0</recordid><startdate>20120907</startdate><enddate>20120907</enddate><creator>RENGGLI, BERNARD JAMES</creator><creator>MILLARD, MICHAEL LEE</creator><creator>MILLER, JEFFREY FRANKLIN</creator><creator>MEIBERS, GREGORY JOSEPH</creator><creator>HALL, KATHLEEN RAFTERY</creator><scope>EVB</scope></search><sort><creationdate>20120907</creationdate><title>CERAMIC MATRIX COMPOSITE STRUCTURES, COMPONENTS FORMED THEREWITH, AND METHODS OF PRODUCING</title><author>RENGGLI, BERNARD JAMES ; MILLARD, MICHAEL LEE ; MILLER, JEFFREY FRANKLIN ; MEIBERS, GREGORY JOSEPH ; HALL, KATHLEEN RAFTERY</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2799049A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2012</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>ARTIFICIAL STONE</topic><topic>AVIATION</topic><topic>CEMENTS</topic><topic>CERAMICS</topic><topic>CHEMISTRY</topic><topic>COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS</topic><topic>CONCRETE</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>LAYERED PRODUCTS</topic><topic>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</topic><topic>LIME, MAGNESIA</topic><topic>METALLURGY</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>REFRACTORIES</topic><topic>SLAG</topic><topic>TRANSPORTING</topic><topic>TREATMENT OF NATURAL STONE</topic><toplevel>online_resources</toplevel><creatorcontrib>RENGGLI, BERNARD JAMES</creatorcontrib><creatorcontrib>MILLARD, MICHAEL LEE</creatorcontrib><creatorcontrib>MILLER, JEFFREY FRANKLIN</creatorcontrib><creatorcontrib>MEIBERS, GREGORY JOSEPH</creatorcontrib><creatorcontrib>HALL, KATHLEEN RAFTERY</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>RENGGLI, BERNARD JAMES</au><au>MILLARD, MICHAEL LEE</au><au>MILLER, JEFFREY FRANKLIN</au><au>MEIBERS, GREGORY JOSEPH</au><au>HALL, KATHLEEN RAFTERY</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CERAMIC MATRIX COMPOSITE STRUCTURES, COMPONENTS FORMED THEREWITH, AND METHODS OF PRODUCING</title><date>2012-09-07</date><risdate>2012</risdate><abstract>Ceramic matrix composite sandwich structures, gas turbine engine components that comprise such sandwich structures, and methods of producing such sandwich structures. The ceramic matrix composite sandwich structure includes a core having oppositely-disposed first and second surfaces, a first facesheet bonded to the first surface, and a member bonded to the second surface so that the core is between the first facesheet and the member. The first facesheet and the core comprise, respectively, first and second ceramic matrix composite materials, and the second ceramic matrix composite material of the core has a ceramic reinforcement material in the form of a felt or an open weave fabric.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ARTIFICIAL STONE AVIATION CEMENTS CERAMICS CHEMISTRY COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS CONCRETE COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM LIME, MAGNESIA METALLURGY PARACHUTES PERFORMING OPERATIONS REFRACTORIES SLAG TRANSPORTING TREATMENT OF NATURAL STONE |
| title | CERAMIC MATRIX COMPOSITE STRUCTURES, COMPONENTS FORMED THEREWITH, AND METHODS OF PRODUCING |
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