Rigid bar for solar panels

A rigid bar comprising a tubular core (1) and composite materials consisting of fibres embedded in resin. The composite material comprises two types of fibres having thermal dilation coefficients varying inversely to the temperatures to which the bar is subjected. Le barreau comprend un noyau tubula...

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Hauptverfasser:	LECUYER FRANCK HENRI DENIS, LE DANTEC ERIC JOSEPH MARIE
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION BUILDING BUILDING MATERIALS COSMONAUTICS FIXED CONSTRUCTIONS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS STRUCTURAL ELEMENTS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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creator	LECUYER FRANCK HENRI DENIS LE DANTEC ERIC JOSEPH MARIE
description	A rigid bar comprising a tubular core (1) and composite materials consisting of fibres embedded in resin. The composite material comprises two types of fibres having thermal dilation coefficients varying inversely to the temperatures to which the bar is subjected. Le barreau comprend un noyau tubulaire (1) en un matériau composite constitué par des fibres noyées dans une résine. Suivant l'invention, ledit matériau composite comprend des fibres d'au moins des premier et deuxième types différents, les deux types de fibres présentant des coefficients de dilatation thermique variant en sens inverses dans le domaine des températures subies par le barreau.Application à la réalisation de supports à géométrie stable dans l'espace, ou d'éléments d'instruments de métrologie.
format	Patent
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The composite material comprises two types of fibres having thermal dilation coefficients varying inversely to the temperatures to which the bar is subjected. Le barreau comprend un noyau tubulaire (1) en un matériau composite constitué par des fibres noyées dans une résine. Suivant l'invention, ledit matériau composite comprend des fibres d'au moins des premier et deuxième types différents, les deux types de fibres présentant des coefficients de dilatation thermique variant en sens inverses dans le domaine des températures subies par le barreau.Application à la réalisation de supports à géométrie stable dans l'espace, ou d'éléments d'instruments de métrologie.</description><edition>6</edition><language>eng ; fre</language><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; AVIATION ; BUILDING ; BUILDING MATERIALS ; COSMONAUTICS ; FIXED CONSTRUCTIONS ; LAYERED PRODUCTS ; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM ; PERFORMING OPERATIONS ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; STRUCTURAL ELEMENTS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>1997</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=19970814&DB=EPODOC&CC=FR&NR=2744785A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19970814&DB=EPODOC&CC=FR&NR=2744785A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LECUYER FRANCK HENRI DENIS</creatorcontrib><creatorcontrib>LE DANTEC ERIC JOSEPH MARIE</creatorcontrib><title>Rigid bar for solar panels</title><description>A rigid bar comprising a tubular core (1) and composite materials consisting of fibres embedded in resin. The composite material comprises two types of fibres having thermal dilation coefficients varying inversely to the temperatures to which the bar is subjected. Le barreau comprend un noyau tubulaire (1) en un matériau composite constitué par des fibres noyées dans une résine. Suivant l'invention, ledit matériau composite comprend des fibres d'au moins des premier et deuxième types différents, les deux types de fibres présentant des coefficients de dilatation thermique variant en sens inverses dans le domaine des températures subies par le barreau.Application à la réalisation de supports à géométrie stable dans l'espace, ou d'éléments d'instruments de métrologie.</description><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BUILDING</subject><subject>BUILDING MATERIALS</subject><subject>COSMONAUTICS</subject><subject>FIXED CONSTRUCTIONS</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>PERFORMING OPERATIONS</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>STRUCTURAL ELEMENTS</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><subject>WORKING OF PLASTICS</subject><subject>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1997</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJAKykzPTFFISixSSMsvUijOzwGyChLzUnOKeRhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJvFuQkbmJibmFqaOhMRFKANu0Ikg</recordid><startdate>19970814</startdate><enddate>19970814</enddate><creator>LECUYER FRANCK HENRI DENIS</creator><creator>LE DANTEC ERIC JOSEPH MARIE</creator><scope>EVB</scope></search><sort><creationdate>19970814</creationdate><title>Rigid bar for solar panels</title><author>LECUYER FRANCK HENRI DENIS ; LE DANTEC ERIC JOSEPH MARIE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR2744785A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>1997</creationdate><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BUILDING</topic><topic>BUILDING MATERIALS</topic><topic>COSMONAUTICS</topic><topic>FIXED CONSTRUCTIONS</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>PERFORMING OPERATIONS</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>STRUCTURAL ELEMENTS</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>LECUYER FRANCK HENRI DENIS</creatorcontrib><creatorcontrib>LE DANTEC ERIC JOSEPH MARIE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LECUYER FRANCK HENRI DENIS</au><au>LE DANTEC ERIC JOSEPH MARIE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Rigid bar for solar panels</title><date>1997-08-14</date><risdate>1997</risdate><abstract>A rigid bar comprising a tubular core (1) and composite materials consisting of fibres embedded in resin. The composite material comprises two types of fibres having thermal dilation coefficients varying inversely to the temperatures to which the bar is subjected. Le barreau comprend un noyau tubulaire (1) en un matériau composite constitué par des fibres noyées dans une résine. Suivant l'invention, ledit matériau composite comprend des fibres d'au moins des premier et deuxième types différents, les deux types de fibres présentant des coefficients de dilatation thermique variant en sens inverses dans le domaine des températures subies par le barreau.Application à la réalisation de supports à géométrie stable dans l'espace, ou d'éléments d'instruments de métrologie.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record>
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language	eng ; fre
recordid	cdi_epo_espacenet_FR2744785A1
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subjects	AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION BUILDING BUILDING MATERIALS COSMONAUTICS FIXED CONSTRUCTIONS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS STRUCTURAL ELEMENTS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
title	Rigid bar for solar panels
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