Aircraft structure with integrated reinforcing elements

Aircraft structure with integrated reinforcing elements

The invention provides an integrated aircraft structure (10), such as a fuselage, with reinforcing elements (51, 53) in areas of the structure that need them because they have openings or are subjected to high loads. The structure (10) comprises a skin (13), a plurality of stringers (15) and a plura...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: BALIGAND, ESTELLE, ARÉVALO RODRIGUEZ, ELENA
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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 BALIGAND, ESTELLE
ARÉVALO RODRIGUEZ, ELENA
description The invention provides an integrated aircraft structure (10), such as a fuselage, with reinforcing elements (51, 53) in areas of the structure that need them because they have openings or are subjected to high loads. The structure (10) comprises a skin (13), a plurality of stringers (15) and a plurality of frames (17) with mouseholes for the passage of stringers (15) at their crossing zones. The reinforcing elements (51, 53) are configured with a suitable shape to be superimposed to the stringers (15) in said areas. The invention also provides manufacturing processes of said integrated aircraft structure (10).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2749491A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2749491A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2749491A13</originalsourceid><addsrcrecordid>eNrjZDB3zCxKLkpMK1EoLikqTS4pLUpVKM8syVDIzCtJTS9KLElNUShKzcxLyy9KzsxLV0jNSc1NzSsp5mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BRuYmliaWho6GxkQoAQDT4S5h</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aircraft structure with integrated reinforcing elements</title><source>esp@cenet</source><creator>BALIGAND, ESTELLE ; ARÉVALO RODRIGUEZ, ELENA</creator><creatorcontrib>BALIGAND, ESTELLE ; ARÉVALO RODRIGUEZ, ELENA</creatorcontrib><description>The invention provides an integrated aircraft structure (10), such as a fuselage, with reinforcing elements (51, 53) in areas of the structure that need them because they have openings or are subjected to high loads. The structure (10) comprises a skin (13), a plurality of stringers (15) and a plurality of frames (17) with mouseholes for the passage of stringers (15) at their crossing zones. The reinforcing elements (51, 53) are configured with a suitable shape to be superimposed to the stringers (15) in said areas. The invention also provides manufacturing processes of said integrated aircraft structure (10).</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2014</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=20140702&amp;DB=EPODOC&amp;CC=EP&amp;NR=2749491A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20140702&amp;DB=EPODOC&amp;CC=EP&amp;NR=2749491A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BALIGAND, ESTELLE</creatorcontrib><creatorcontrib>ARÉVALO RODRIGUEZ, ELENA</creatorcontrib><title>Aircraft structure with integrated reinforcing elements</title><description>The invention provides an integrated aircraft structure (10), such as a fuselage, with reinforcing elements (51, 53) in areas of the structure that need them because they have openings or are subjected to high loads. The structure (10) comprises a skin (13), a plurality of stringers (15) and a plurality of frames (17) with mouseholes for the passage of stringers (15) at their crossing zones. The reinforcing elements (51, 53) are configured with a suitable shape to be superimposed to the stringers (15) in said areas. The invention also provides manufacturing processes of said integrated aircraft structure (10).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB3zCxKLkpMK1EoLikqTS4pLUpVKM8syVDIzCtJTS9KLElNUShKzcxLyy9KzsxLV0jNSc1NzSsp5mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BRuYmliaWho6GxkQoAQDT4S5h</recordid><startdate>20140702</startdate><enddate>20140702</enddate><creator>BALIGAND, ESTELLE</creator><creator>ARÉVALO RODRIGUEZ, ELENA</creator><scope>EVB</scope></search><sort><creationdate>20140702</creationdate><title>Aircraft structure with integrated reinforcing elements</title><author>BALIGAND, ESTELLE ; ARÉVALO RODRIGUEZ, ELENA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2749491A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2014</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>BALIGAND, ESTELLE</creatorcontrib><creatorcontrib>ARÉVALO RODRIGUEZ, ELENA</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BALIGAND, ESTELLE</au><au>ARÉVALO RODRIGUEZ, ELENA</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft structure with integrated reinforcing elements</title><date>2014-07-02</date><risdate>2014</risdate><abstract>The invention provides an integrated aircraft structure (10), such as a fuselage, with reinforcing elements (51, 53) in areas of the structure that need them because they have openings or are subjected to high loads. The structure (10) comprises a skin (13), a plurality of stringers (15) and a plurality of frames (17) with mouseholes for the passage of stringers (15) at their crossing zones. The reinforcing elements (51, 53) are configured with a suitable shape to be superimposed to the stringers (15) in said areas. The invention also provides manufacturing processes of said integrated aircraft structure (10).</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP2749491A1
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Aircraft structure with integrated reinforcing elements
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-13T19%3A19%3A41IST&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=BALIGAND,%20ESTELLE&rft.date=2014-07-02&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2749491A1%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