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...
Gespeichert in:
| Hauptverfasser: | , , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | RENGGLI, BERNARD, JAMES MILLARD, MICHAEL, LEE MEIBERS, GREGORY, JOSEPH MILLER, JEFFREY, FRANKLIN 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.
L'invention concerne des structures sandwichs en composites à matrice en céramique, des pièces de moteur à turbine à gaz qui comprennent des structures sandwichs, et des procédés de production de telles structures. La structure sandwich en composites à matrice en céramique comprend une partie centrale présentant une première et une deuxième surface en regard l'une de l'autre, une première feuille de surface collée à la première surface, et un élément collé à la seconde surface de manière que la partie centrale se trouve entre la première feuille de surface et l'élément. La première feuille de surface et la partie centrale comportent respectivement des première et deuxième matières composites à matrice en céramique, et la deuxième matière composite à matrice en céramique de la partie centrale comprend une matière de renforcement en céramique sous la forme d'un feutre ou d'une étoffe ajourée. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_WO2012118516A8</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>WO2012118516A8</sourcerecordid><originalsourceid>FETCH-epo_espacenet_WO2012118516A83</originalsourceid><addsrcrecordid>eNqNyrEKwjAQgOEuDqK-w4FrBVNRuobkajIkVy5XKi6lSJxEC_X9cdAHcPrh418WV4OsgzcQtLC_gKHQUvKCkIQ7Ix1jKr8aMUqChjigBXHI2HtxJehoIaA4sgmogZbJdsbH87pY3MfHnDe_roptg2LcLk-vIc_TeMvP_B56qvaqUqo-qpOuD_9dH06VMws</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>CERAMIC MATRIX COMPOSITE STRUCTURES, COMPONENTS FORMED THEREWITH, AND METHODS OF PRODUCING</title><source>esp@cenet</source><creator>RENGGLI, BERNARD, JAMES ; MILLARD, MICHAEL, LEE ; MEIBERS, GREGORY, JOSEPH ; MILLER, JEFFREY, FRANKLIN ; HALL, KATHLEEN, RAFTERY</creator><creatorcontrib>RENGGLI, BERNARD, JAMES ; MILLARD, MICHAEL, LEE ; MEIBERS, GREGORY, JOSEPH ; MILLER, JEFFREY, FRANKLIN ; HALL, KATHLEEN, RAFTERY</creatorcontrib><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.
L'invention concerne des structures sandwichs en composites à matrice en céramique, des pièces de moteur à turbine à gaz qui comprennent des structures sandwichs, et des procédés de production de telles structures. La structure sandwich en composites à matrice en céramique comprend une partie centrale présentant une première et une deuxième surface en regard l'une de l'autre, une première feuille de surface collée à la première surface, et un élément collé à la seconde surface de manière que la partie centrale se trouve entre la première feuille de surface et l'élément. La première feuille de surface et la partie centrale comportent respectivement des première et deuxième matières composites à matrice en céramique, et la deuxième matière composite à matrice en céramique de la partie centrale comprend une matière de renforcement en céramique sous la forme d'un feutre ou d'une étoffe ajourée.</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=20121206&DB=EPODOC&CC=WO&NR=2012118516A8$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20121206&DB=EPODOC&CC=WO&NR=2012118516A8$$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>MEIBERS, GREGORY, JOSEPH</creatorcontrib><creatorcontrib>MILLER, JEFFREY, FRANKLIN</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.
L'invention concerne des structures sandwichs en composites à matrice en céramique, des pièces de moteur à turbine à gaz qui comprennent des structures sandwichs, et des procédés de production de telles structures. La structure sandwich en composites à matrice en céramique comprend une partie centrale présentant une première et une deuxième surface en regard l'une de l'autre, une première feuille de surface collée à la première surface, et un élément collé à la seconde surface de manière que la partie centrale se trouve entre la première feuille de surface et l'élément. La première feuille de surface et la partie centrale comportent respectivement des première et deuxième matières composites à matrice en céramique, et la deuxième matière composite à matrice en céramique de la partie centrale comprend une matière de renforcement en céramique sous la forme d'un feutre ou d'une étoffe ajourée.</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>eNqNyrEKwjAQgOEuDqK-w4FrBVNRuobkajIkVy5XKi6lSJxEC_X9cdAHcPrh418WV4OsgzcQtLC_gKHQUvKCkIQ7Ix1jKr8aMUqChjigBXHI2HtxJehoIaA4sgmogZbJdsbH87pY3MfHnDe_roptg2LcLk-vIc_TeMvP_B56qvaqUqo-qpOuD_9dH06VMws</recordid><startdate>20121206</startdate><enddate>20121206</enddate><creator>RENGGLI, BERNARD, JAMES</creator><creator>MILLARD, MICHAEL, LEE</creator><creator>MEIBERS, GREGORY, JOSEPH</creator><creator>MILLER, JEFFREY, FRANKLIN</creator><creator>HALL, KATHLEEN, RAFTERY</creator><scope>EVB</scope></search><sort><creationdate>20121206</creationdate><title>CERAMIC MATRIX COMPOSITE STRUCTURES, COMPONENTS FORMED THEREWITH, AND METHODS OF PRODUCING</title><author>RENGGLI, BERNARD, JAMES ; MILLARD, MICHAEL, LEE ; MEIBERS, GREGORY, JOSEPH ; MILLER, JEFFREY, FRANKLIN ; HALL, KATHLEEN, RAFTERY</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2012118516A83</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>MEIBERS, GREGORY, JOSEPH</creatorcontrib><creatorcontrib>MILLER, JEFFREY, FRANKLIN</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>MEIBERS, GREGORY, JOSEPH</au><au>MILLER, JEFFREY, FRANKLIN</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>2012-12-06</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.
L'invention concerne des structures sandwichs en composites à matrice en céramique, des pièces de moteur à turbine à gaz qui comprennent des structures sandwichs, et des procédés de production de telles structures. La structure sandwich en composites à matrice en céramique comprend une partie centrale présentant une première et une deuxième surface en regard l'une de l'autre, une première feuille de surface collée à la première surface, et un élément collé à la seconde surface de manière que la partie centrale se trouve entre la première feuille de surface et l'élément. La première feuille de surface et la partie centrale comportent respectivement des première et deuxième matières composites à matrice en céramique, et la deuxième matière composite à matrice en céramique de la partie centrale comprend une matière de renforcement en céramique sous la forme d'un feutre ou d'une étoffe ajourée.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre |
| recordid | cdi_epo_espacenet_WO2012118516A8 |
| source | esp@cenet |
| 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 |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-18T10%3A58%3A52IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=RENGGLI,%20BERNARD,%20JAMES&rft.date=2012-12-06&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EWO2012118516A8%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |