AN AIRCRAFT WING WITH A WING TIP DEVICE AND A STRUT

AN AIRCRAFT WING WITH A WING TIP DEVICE AND A STRUT

An aircraft wing (1) has a wing tip device (3) joined thereto. The root (7) of the wing tip device (3) is joined to the tip of the wing (1) at a first connection (11). An external strut (9) extends between the wing (1) and the wing tip device (3), the strut (9) being joined to the wing (1) at a seco...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: HOBDAY, John, WILLIAMS, Llifon, THOMPSON, Robert, LYNAS, Christopher
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 HOBDAY, John
WILLIAMS, Llifon
THOMPSON, Robert
LYNAS, Christopher
description An aircraft wing (1) has a wing tip device (3) joined thereto. The root (7) of the wing tip device (3) is joined to the tip of the wing (1) at a first connection (11). An external strut (9) extends between the wing (1) and the wing tip device (3), the strut (9) being joined to the wing (1) at a second connection (13). The second connection (13) is inboard of the first connection, such that loadings on the wing tip device (3) generated during use, are transferred, via the strut (9), to a location on the wing (1) that is inboard of where the root (7) of the wing tip device (3) is joined to the tip of the wing.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3126227A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3126227A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3126227A13</originalsourceid><addsrcrecordid>eNrjZDB29FNw9AxyDnJ0C1EI9_RzBxIhHgqOEHaIZ4CCi2uYp7OrgqOfC1A0OCQoNISHgTUtMac4lRdKczMouLmGOHvophbkx6cWFyQmp-allsS7BhgbGpkZGZk7GhoToQQACj4mBQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AN AIRCRAFT WING WITH A WING TIP DEVICE AND A STRUT</title><source>esp@cenet</source><creator>HOBDAY, John ; WILLIAMS, Llifon ; THOMPSON, Robert ; LYNAS, Christopher</creator><creatorcontrib>HOBDAY, John ; WILLIAMS, Llifon ; THOMPSON, Robert ; LYNAS, Christopher</creatorcontrib><description>An aircraft wing (1) has a wing tip device (3) joined thereto. The root (7) of the wing tip device (3) is joined to the tip of the wing (1) at a first connection (11). An external strut (9) extends between the wing (1) and the wing tip device (3), the strut (9) being joined to the wing (1) at a second connection (13). The second connection (13) is inboard of the first connection, such that loadings on the wing tip device (3) generated during use, are transferred, via the strut (9), to a location on the wing (1) that is inboard of where the root (7) of the wing tip device (3) is joined to the tip of the wing.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2017</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=20170208&amp;DB=EPODOC&amp;CC=EP&amp;NR=3126227A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20170208&amp;DB=EPODOC&amp;CC=EP&amp;NR=3126227A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HOBDAY, John</creatorcontrib><creatorcontrib>WILLIAMS, Llifon</creatorcontrib><creatorcontrib>THOMPSON, Robert</creatorcontrib><creatorcontrib>LYNAS, Christopher</creatorcontrib><title>AN AIRCRAFT WING WITH A WING TIP DEVICE AND A STRUT</title><description>An aircraft wing (1) has a wing tip device (3) joined thereto. The root (7) of the wing tip device (3) is joined to the tip of the wing (1) at a first connection (11). An external strut (9) extends between the wing (1) and the wing tip device (3), the strut (9) being joined to the wing (1) at a second connection (13). The second connection (13) is inboard of the first connection, such that loadings on the wing tip device (3) generated during use, are transferred, via the strut (9), to a location on the wing (1) that is inboard of where the root (7) of the wing tip device (3) is joined to the tip of the wing.</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>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB29FNw9AxyDnJ0C1EI9_RzBxIhHgqOEHaIZ4CCi2uYp7OrgqOfC1A0OCQoNISHgTUtMac4lRdKczMouLmGOHvophbkx6cWFyQmp-allsS7BhgbGpkZGZk7GhoToQQACj4mBQ</recordid><startdate>20170208</startdate><enddate>20170208</enddate><creator>HOBDAY, John</creator><creator>WILLIAMS, Llifon</creator><creator>THOMPSON, Robert</creator><creator>LYNAS, Christopher</creator><scope>EVB</scope></search><sort><creationdate>20170208</creationdate><title>AN AIRCRAFT WING WITH A WING TIP DEVICE AND A STRUT</title><author>HOBDAY, John ; WILLIAMS, Llifon ; THOMPSON, Robert ; LYNAS, Christopher</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3126227A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2017</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>HOBDAY, John</creatorcontrib><creatorcontrib>WILLIAMS, Llifon</creatorcontrib><creatorcontrib>THOMPSON, Robert</creatorcontrib><creatorcontrib>LYNAS, Christopher</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HOBDAY, John</au><au>WILLIAMS, Llifon</au><au>THOMPSON, Robert</au><au>LYNAS, Christopher</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AN AIRCRAFT WING WITH A WING TIP DEVICE AND A STRUT</title><date>2017-02-08</date><risdate>2017</risdate><abstract>An aircraft wing (1) has a wing tip device (3) joined thereto. The root (7) of the wing tip device (3) is joined to the tip of the wing (1) at a first connection (11). An external strut (9) extends between the wing (1) and the wing tip device (3), the strut (9) being joined to the wing (1) at a second connection (13). The second connection (13) is inboard of the first connection, such that loadings on the wing tip device (3) generated during use, are transferred, via the strut (9), to a location on the wing (1) that is inboard of where the root (7) of the wing tip device (3) is joined to the tip of the wing.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3126227A1
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title AN AIRCRAFT WING WITH A WING TIP DEVICE AND A STRUT
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-25T00%3A52%3A07IST&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=HOBDAY,%20John&rft.date=2017-02-08&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3126227A1%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