COMPOSITE ARTICLE
A composite article (21) for use in an aircraft brake heat pack, the article comprises a core layer (22) having a face portion and a wear layer (23) attached to the face portion, wherein the wear layer (23) has a density lower than the core layer (22). The core layer (22) may be fabricated from comp...
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| creator | JOHNSON, DAVID CALLUM |
| description | A composite article (21) for use in an aircraft brake heat pack, the article comprises a core layer (22) having a face portion and a wear layer (23) attached to the face portion, wherein the wear layer (23) has a density lower than the core layer (22). The core layer (22) may be fabricated from compressed C-C or from C-C impregnated with boron and/or silicon. The wear layer (23) may be fabricated from C-C.
L'invention concerne un article composite (21) s'utilisant dans un système puits de chaleur de freins d'aéronef. Ledit article comprend une couche médiane (22) présentant une section de face et une couche d'usure (23) fixée à la section de face. La couche d'usure (23) présente une masse volumique inférieure à celle de la couche médiane (22). Ladite couche médiane (22) peut être produite à partir de C-C comprimé ou de C-C imprégné de bore et/ou de silicium. La couche d'usure (23) peut être produite à partir de C-C. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CA2531799C</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CA2531799C</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CA2531799C3</originalsourceid><addsrcrecordid>eNrjZBB09vcN8A_2DHFVcAwK8XT2ceVhYE1LzClO5YXS3Azybq4hzh66qQX58anFBYnJqXmpJfHOjkamxobmlpbOxoRVAACzaRz9</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>COMPOSITE ARTICLE</title><source>esp@cenet</source><creator>JOHNSON, DAVID CALLUM</creator><creatorcontrib>JOHNSON, DAVID CALLUM</creatorcontrib><description>A composite article (21) for use in an aircraft brake heat pack, the article comprises a core layer (22) having a face portion and a wear layer (23) attached to the face portion, wherein the wear layer (23) has a density lower than the core layer (22). The core layer (22) may be fabricated from compressed C-C or from C-C impregnated with boron and/or silicon. The wear layer (23) may be fabricated from C-C.
L'invention concerne un article composite (21) s'utilisant dans un système puits de chaleur de freins d'aéronef. Ledit article comprend une couche médiane (22) présentant une section de face et une couche d'usure (23) fixée à la section de face. La couche d'usure (23) présente une masse volumique inférieure à celle de la couche médiane (22). Ladite couche médiane (22) peut être produite à partir de C-C comprimé ou de C-C imprégné de bore et/ou de silicium. La couche d'usure (23) peut être produite à partir de C-C.</description><language>eng ; fre</language><subject>ARTIFICIAL STONE ; BLASTING ; BRAKES ; CEMENTS ; CERAMICS ; CHEMISTRY ; CLUTCHES ; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS ; CONCRETE ; COUPLINGS FOR TRANSMITTING ROTATION ; ENGINEERING ELEMENTS AND UNITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; LIGHTING ; LIME, MAGNESIA ; MECHANICAL ENGINEERING ; METALLURGY ; REFRACTORIES ; SLAG ; THERMAL INSULATION IN GENERAL ; TREATMENT OF NATURAL STONE ; WEAPONS</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=20120103&DB=EPODOC&CC=CA&NR=2531799C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20120103&DB=EPODOC&CC=CA&NR=2531799C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JOHNSON, DAVID CALLUM</creatorcontrib><title>COMPOSITE ARTICLE</title><description>A composite article (21) for use in an aircraft brake heat pack, the article comprises a core layer (22) having a face portion and a wear layer (23) attached to the face portion, wherein the wear layer (23) has a density lower than the core layer (22). The core layer (22) may be fabricated from compressed C-C or from C-C impregnated with boron and/or silicon. The wear layer (23) may be fabricated from C-C.
L'invention concerne un article composite (21) s'utilisant dans un système puits de chaleur de freins d'aéronef. Ledit article comprend une couche médiane (22) présentant une section de face et une couche d'usure (23) fixée à la section de face. La couche d'usure (23) présente une masse volumique inférieure à celle de la couche médiane (22). Ladite couche médiane (22) peut être produite à partir de C-C comprimé ou de C-C imprégné de bore et/ou de silicium. La couche d'usure (23) peut être produite à partir de C-C.</description><subject>ARTIFICIAL STONE</subject><subject>BLASTING</subject><subject>BRAKES</subject><subject>CEMENTS</subject><subject>CERAMICS</subject><subject>CHEMISTRY</subject><subject>CLUTCHES</subject><subject>COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS</subject><subject>CONCRETE</subject><subject>COUPLINGS FOR TRANSMITTING ROTATION</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>LIME, MAGNESIA</subject><subject>MECHANICAL ENGINEERING</subject><subject>METALLURGY</subject><subject>REFRACTORIES</subject><subject>SLAG</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TREATMENT OF NATURAL STONE</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBB09vcN8A_2DHFVcAwK8XT2ceVhYE1LzClO5YXS3Azybq4hzh66qQX58anFBYnJqXmpJfHOjkamxobmlpbOxoRVAACzaRz9</recordid><startdate>20120103</startdate><enddate>20120103</enddate><creator>JOHNSON, DAVID CALLUM</creator><scope>EVB</scope></search><sort><creationdate>20120103</creationdate><title>COMPOSITE ARTICLE</title><author>JOHNSON, DAVID CALLUM</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2531799C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2012</creationdate><topic>ARTIFICIAL STONE</topic><topic>BLASTING</topic><topic>BRAKES</topic><topic>CEMENTS</topic><topic>CERAMICS</topic><topic>CHEMISTRY</topic><topic>CLUTCHES</topic><topic>COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS</topic><topic>CONCRETE</topic><topic>COUPLINGS FOR TRANSMITTING ROTATION</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>LIME, MAGNESIA</topic><topic>MECHANICAL ENGINEERING</topic><topic>METALLURGY</topic><topic>REFRACTORIES</topic><topic>SLAG</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TREATMENT OF NATURAL STONE</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>JOHNSON, DAVID CALLUM</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JOHNSON, DAVID CALLUM</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMPOSITE ARTICLE</title><date>2012-01-03</date><risdate>2012</risdate><abstract>A composite article (21) for use in an aircraft brake heat pack, the article comprises a core layer (22) having a face portion and a wear layer (23) attached to the face portion, wherein the wear layer (23) has a density lower than the core layer (22). The core layer (22) may be fabricated from compressed C-C or from C-C impregnated with boron and/or silicon. The wear layer (23) may be fabricated from C-C.
L'invention concerne un article composite (21) s'utilisant dans un système puits de chaleur de freins d'aéronef. Ledit article comprend une couche médiane (22) présentant une section de face et une couche d'usure (23) fixée à la section de face. La couche d'usure (23) présente une masse volumique inférieure à celle de la couche médiane (22). Ladite couche médiane (22) peut être produite à partir de C-C comprimé ou de C-C imprégné de bore et/ou de silicium. La couche d'usure (23) peut être produite à partir de C-C.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
| recordid | cdi_epo_espacenet_CA2531799C |
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| subjects | ARTIFICIAL STONE BLASTING BRAKES CEMENTS CERAMICS CHEMISTRY CLUTCHES COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS CONCRETE COUPLINGS FOR TRANSMITTING ROTATION ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING LIME, MAGNESIA MECHANICAL ENGINEERING METALLURGY REFRACTORIES SLAG THERMAL INSULATION IN GENERAL TREATMENT OF NATURAL STONE WEAPONS |
| title | COMPOSITE ARTICLE |
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