STRUCTURAL PANEL WITH INTEGRATED STIFFENING

The invention relates to the field of structural panels, more specifically, but not exclusively, to the field of aircraft fuselage panels. The invention concerns a stiffened panel (10) comprising at least one stiffener (4), known as a longitudinal stiffener, extending substantially from one extremit...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: GAUDIN JOCELYN, MEYER CEDRIC
Format: Patent
Sprache:eng
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 GAUDIN JOCELYN
MEYER CEDRIC
description The invention relates to the field of structural panels, more specifically, but not exclusively, to the field of aircraft fuselage panels. The invention concerns a stiffened panel (10) comprising at least one stiffener (4), known as a longitudinal stiffener, extending substantially from one extremity of the panel to the other and whose trace on the surface of said panel's skin (1) follows a path having non-zero geodesic curvature between the two extremities of said stiffener. This configuration makes it possible to optimize both the panel's stiffness and its resistance to the force flow to which it is subjected in operation by minimizing its mass through an optimum definition of the orientation of the stiffeners relative to said force flow.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2012009372A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2012009372A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2012009372A13</originalsourceid><addsrcrecordid>eNrjZNAODgkKdQ4JDXL0UQhw9HP1UQj3DPFQ8PQLcXUPcgxxdVEIDvF0c3P18_Rz52FgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgaGRgYGlsbmRo6GxsSpAgApRCYT</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>STRUCTURAL PANEL WITH INTEGRATED STIFFENING</title><source>esp@cenet</source><creator>GAUDIN JOCELYN ; MEYER CEDRIC</creator><creatorcontrib>GAUDIN JOCELYN ; MEYER CEDRIC</creatorcontrib><description>The invention relates to the field of structural panels, more specifically, but not exclusively, to the field of aircraft fuselage panels. The invention concerns a stiffened panel (10) comprising at least one stiffener (4), known as a longitudinal stiffener, extending substantially from one extremity of the panel to the other and whose trace on the surface of said panel's skin (1) follows a path having non-zero geodesic curvature between the two extremities of said stiffener. This configuration makes it possible to optimize both the panel's stiffness and its resistance to the force flow to which it is subjected in operation by minimizing its mass through an optimum definition of the orientation of the stiffeners relative to said force flow.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC ; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS ; HELICOPTERS ; INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES ; LAYERED PRODUCTS ; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM ; PERFORMING OPERATIONS ; PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE ; TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION ; TECHNICAL SUBJECTS COVERED BY FORMER USPC ; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS ; TRANSPORTING ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</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&amp;date=20120112&amp;DB=EPODOC&amp;CC=US&amp;NR=2012009372A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20120112&amp;DB=EPODOC&amp;CC=US&amp;NR=2012009372A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GAUDIN JOCELYN</creatorcontrib><creatorcontrib>MEYER CEDRIC</creatorcontrib><title>STRUCTURAL PANEL WITH INTEGRATED STIFFENING</title><description>The invention relates to the field of structural panels, more specifically, but not exclusively, to the field of aircraft fuselage panels. The invention concerns a stiffened panel (10) comprising at least one stiffener (4), known as a longitudinal stiffener, extending substantially from one extremity of the panel to the other and whose trace on the surface of said panel's skin (1) follows a path having non-zero geodesic curvature between the two extremities of said stiffener. This configuration makes it possible to optimize both the panel's stiffness and its resistance to the force flow to which it is subjected in operation by minimizing its mass through an optimum definition of the orientation of the stiffeners relative to said force flow.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</subject><subject>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</subject><subject>HELICOPTERS</subject><subject>INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES</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>PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</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>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAODgkKdQ4JDXL0UQhw9HP1UQj3DPFQ8PQLcXUPcgxxdVEIDvF0c3P18_Rz52FgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgaGRgYGlsbmRo6GxsSpAgApRCYT</recordid><startdate>20120112</startdate><enddate>20120112</enddate><creator>GAUDIN JOCELYN</creator><creator>MEYER CEDRIC</creator><scope>EVB</scope></search><sort><creationdate>20120112</creationdate><title>STRUCTURAL PANEL WITH INTEGRATED STIFFENING</title><author>GAUDIN JOCELYN ; MEYER CEDRIC</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2012009372A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2012</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</topic><topic>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</topic><topic>HELICOPTERS</topic><topic>INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES</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>PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</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>GAUDIN JOCELYN</creatorcontrib><creatorcontrib>MEYER CEDRIC</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GAUDIN JOCELYN</au><au>MEYER CEDRIC</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>STRUCTURAL PANEL WITH INTEGRATED STIFFENING</title><date>2012-01-12</date><risdate>2012</risdate><abstract>The invention relates to the field of structural panels, more specifically, but not exclusively, to the field of aircraft fuselage panels. The invention concerns a stiffened panel (10) comprising at least one stiffener (4), known as a longitudinal stiffener, extending substantially from one extremity of the panel to the other and whose trace on the surface of said panel's skin (1) follows a path having non-zero geodesic curvature between the two extremities of said stiffener. This configuration makes it possible to optimize both the panel's stiffness and its resistance to the force flow to which it is subjected in operation by minimizing its mass through an optimum definition of the orientation of the stiffeners relative to said force flow.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_US2012009372A1
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
HELICOPTERS
INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES
LAYERED PRODUCTS
LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
PERFORMING OPERATIONS
PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE
TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
TECHNICAL SUBJECTS COVERED BY FORMER USPC
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TRANSPORTING
WORKING OF PLASTICS
WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
title STRUCTURAL PANEL WITH INTEGRATED STIFFENING
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-24T18%3A46%3A05IST&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=GAUDIN%20JOCELYN&rft.date=2012-01-12&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2012009372A1%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