STRUCTURE OF COMPOSITE MATERIAL FOR AIRCRAFT FUSELAGES AND METHOD FOR MANUFACTURE THEREOF
The present invention provides a closed composite material structure for aircraft fuselage shaped on a male jig from which it can be separated in a certain direction, said structure comprising a single outer panel and a plurality of inner longitudinal stiffeners integrated in said panel, such that t...
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| creator | MARTINEZ CEREZO, ALBERTO, RAMON MIGUEZ CHARINES, YOLANDA JORDAN CARNICERO, JAVIER SANCHEZ FERNANDEZ, JULIAN |
| description | The present invention provides a closed composite material structure for aircraft fuselage shaped on a male jig from which it can be separated in a certain direction, said structure comprising a single outer panel and a plurality of inner longitudinal stiffeners integrated in said panel, such that the expansion coefficient of the male jig is greater than the expansion coefficient of the composite material of the structure, thus being able to remove the already manufactured structure, formed by the panel and the integrated inner stiffeners, in a single operation. The present invention further provides a process for manufacturing such a closed structure. |
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The present invention further provides a process for manufacturing such a closed structure.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; TRANSPORTING ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>2009</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=20091202&DB=EPODOC&CC=EP&NR=2128017A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20091202&DB=EPODOC&CC=EP&NR=2128017A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MARTINEZ CEREZO, ALBERTO, RAMON</creatorcontrib><creatorcontrib>MIGUEZ CHARINES, YOLANDA</creatorcontrib><creatorcontrib>JORDAN CARNICERO, JAVIER</creatorcontrib><creatorcontrib>SANCHEZ FERNANDEZ, JULIAN</creatorcontrib><title>STRUCTURE OF COMPOSITE MATERIAL FOR AIRCRAFT FUSELAGES AND METHOD FOR MANUFACTURE THEREOF</title><description>The present invention provides a closed composite material structure for aircraft fuselage shaped on a male jig from which it can be separated in a certain direction, said structure comprising a single outer panel and a plurality of inner longitudinal stiffeners integrated in said panel, such that the expansion coefficient of the male jig is greater than the expansion coefficient of the composite material of the structure, thus being able to remove the already manufactured structure, formed by the panel and the integrated inner stiffeners, in a single operation. The present invention further provides a process for manufacturing such a closed structure.</description><subject>AEROPLANES</subject><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</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>TRANSPORTING</subject><subject>WORKING OF PLASTICS</subject><subject>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2009</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNzLEKwjAQgOEuDqK-w72AYOqg65HemUDTlMtl6FSKxEm0UN8fQX0Ap3_5-NfVkFSy1SwEkcHG0MfklSCgknhsgaMAerGCrMA5UYsXSoBdA4HUxeYjAnaZ8ftRR0KRt9XqNt2Xsvt1UwGTWrcv83Msyzxdy6O8RuprU58P5oTm-Ad5A9g5MS8</recordid><startdate>20091202</startdate><enddate>20091202</enddate><creator>MARTINEZ CEREZO, ALBERTO, RAMON</creator><creator>MIGUEZ CHARINES, YOLANDA</creator><creator>JORDAN CARNICERO, JAVIER</creator><creator>SANCHEZ FERNANDEZ, JULIAN</creator><scope>EVB</scope></search><sort><creationdate>20091202</creationdate><title>STRUCTURE OF COMPOSITE MATERIAL FOR AIRCRAFT FUSELAGES AND METHOD FOR MANUFACTURE THEREOF</title><author>MARTINEZ CEREZO, ALBERTO, RAMON ; MIGUEZ CHARINES, YOLANDA ; JORDAN CARNICERO, JAVIER ; SANCHEZ FERNANDEZ, JULIAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2128017A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2009</creationdate><topic>AEROPLANES</topic><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</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>TRANSPORTING</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>MARTINEZ CEREZO, ALBERTO, RAMON</creatorcontrib><creatorcontrib>MIGUEZ CHARINES, YOLANDA</creatorcontrib><creatorcontrib>JORDAN CARNICERO, JAVIER</creatorcontrib><creatorcontrib>SANCHEZ FERNANDEZ, JULIAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MARTINEZ CEREZO, ALBERTO, RAMON</au><au>MIGUEZ CHARINES, YOLANDA</au><au>JORDAN CARNICERO, JAVIER</au><au>SANCHEZ FERNANDEZ, JULIAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>STRUCTURE OF COMPOSITE MATERIAL FOR AIRCRAFT FUSELAGES AND METHOD FOR MANUFACTURE THEREOF</title><date>2009-12-02</date><risdate>2009</risdate><abstract>The present invention provides a closed composite material structure for aircraft fuselage shaped on a male jig from which it can be separated in a certain direction, said structure comprising a single outer panel and a plurality of inner longitudinal stiffeners integrated in said panel, such that the expansion coefficient of the male jig is greater than the expansion coefficient of the composite material of the structure, thus being able to remove the already manufactured structure, formed by the panel and the integrated inner stiffeners, in a single operation. The present invention further provides a process for manufacturing such a closed structure.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
| title | STRUCTURE OF COMPOSITE MATERIAL FOR AIRCRAFT FUSELAGES AND METHOD FOR MANUFACTURE THEREOF |
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