AIRCRAFT WING ASSEMBLIES
An aircraft (10) and an aircraft wing assembly (90) for an aircraft. The wing assembly (90) includes a wing body assembly including a wing body (110); and at least one protruding portion (130) connected to the wing body (110). The protruding portion (130) extends aftwardly from an aft side of the wi...
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| creator | PEPIN, Francois LEBLOND, David MOKHTARIAN, Farzad KAFYEKE, Fassi |
| description | An aircraft (10) and an aircraft wing assembly (90) for an aircraft. The wing assembly (90) includes a wing body assembly including a wing body (110); and at least one protruding portion (130) connected to the wing body (110). The protruding portion (130) extends aftwardly from an aft side of the wing body assembly, a leading edge (112) of the wing body assembly defining a leading edge line (122), a trailing edge (114) of the wing body assembly defining a trailing edge line (124) extending between the inboard end (102) and the outboard end (104), the trailing edge (114) including a trailing edge of the protruding portion, the trailing edge line being a smooth line, a chord distance being defined longitudinally from the leading edge line to the trailing edge line, the chord distance at a center of the protruding portion (130) being greater than the chord distance inboard of protruding portion and outboard of the protruding portion. |
| format | Patent |
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The wing assembly (90) includes a wing body assembly including a wing body (110); and at least one protruding portion (130) connected to the wing body (110). The protruding portion (130) extends aftwardly from an aft side of the wing body assembly, a leading edge (112) of the wing body assembly defining a leading edge line (122), a trailing edge (114) of the wing body assembly defining a trailing edge line (124) extending between the inboard end (102) and the outboard end (104), the trailing edge (114) including a trailing edge of the protruding portion, the trailing edge line being a smooth line, a chord distance being defined longitudinally from the leading edge line to the trailing edge line, the chord distance at a center of the protruding portion (130) being greater than the chord distance inboard of protruding portion and outboard of the protruding portion.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2020</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=20200617&DB=EPODOC&CC=EP&NR=3666642A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200617&DB=EPODOC&CC=EP&NR=3666642A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PEPIN, Francois</creatorcontrib><creatorcontrib>LEBLOND, David</creatorcontrib><creatorcontrib>MOKHTARIAN, Farzad</creatorcontrib><creatorcontrib>KAFYEKE, Fassi</creatorcontrib><title>AIRCRAFT WING ASSEMBLIES</title><description>An aircraft (10) and an aircraft wing assembly (90) for an aircraft. The wing assembly (90) includes a wing body assembly including a wing body (110); and at least one protruding portion (130) connected to the wing body (110). The protruding portion (130) extends aftwardly from an aft side of the wing body assembly, a leading edge (112) of the wing body assembly defining a leading edge line (122), a trailing edge (114) of the wing body assembly defining a trailing edge line (124) extending between the inboard end (102) and the outboard end (104), the trailing edge (114) including a trailing edge of the protruding portion, the trailing edge line being a smooth line, a chord distance being defined longitudinally from the leading edge line to the trailing edge line, the chord distance at a center of the protruding portion (130) being greater than the chord distance inboard of protruding portion and outboard of the protruding portion.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJBw9AxyDnJ0C1EI9_RzV3AMDnb1dfLxdA3mYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGZkBgYuRoaEyEEgC1AR9S</recordid><startdate>20200617</startdate><enddate>20200617</enddate><creator>PEPIN, Francois</creator><creator>LEBLOND, David</creator><creator>MOKHTARIAN, Farzad</creator><creator>KAFYEKE, Fassi</creator><scope>EVB</scope></search><sort><creationdate>20200617</creationdate><title>AIRCRAFT WING ASSEMBLIES</title><author>PEPIN, Francois ; LEBLOND, David ; MOKHTARIAN, Farzad ; KAFYEKE, Fassi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3666642A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2020</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>PEPIN, Francois</creatorcontrib><creatorcontrib>LEBLOND, David</creatorcontrib><creatorcontrib>MOKHTARIAN, Farzad</creatorcontrib><creatorcontrib>KAFYEKE, Fassi</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PEPIN, Francois</au><au>LEBLOND, David</au><au>MOKHTARIAN, Farzad</au><au>KAFYEKE, Fassi</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT WING ASSEMBLIES</title><date>2020-06-17</date><risdate>2020</risdate><abstract>An aircraft (10) and an aircraft wing assembly (90) for an aircraft. The wing assembly (90) includes a wing body assembly including a wing body (110); and at least one protruding portion (130) connected to the wing body (110). The protruding portion (130) extends aftwardly from an aft side of the wing body assembly, a leading edge (112) of the wing body assembly defining a leading edge line (122), a trailing edge (114) of the wing body assembly defining a trailing edge line (124) extending between the inboard end (102) and the outboard end (104), the trailing edge (114) including a trailing edge of the protruding portion, the trailing edge line being a smooth line, a chord distance being defined longitudinally from the leading edge line to the trailing edge line, the chord distance at a center of the protruding portion (130) being greater than the chord distance inboard of protruding portion and outboard of the protruding portion.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | AIRCRAFT WING ASSEMBLIES |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-27T17%3A08%3A42IST&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=PEPIN,%20Francois&rft.date=2020-06-17&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3666642A1%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 |