WING TO FUSE JUNCTION SHAPING, AND ASSOCIATED SYSTEMS AND METHODS

Wing to fuse junction shaping, and associated systems and methods are disclosed herein. An aircraft includes: a fuselage, a wing, and a fairing that covers a junction between the wing and the fuselage. The fairing is configured to receive an inboard section of the wing. An outer surface of the fairi...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Mokhtarian, Farzad, Pepin, François, Bochud, Pascal, Kafyeke, Fassi
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 Mokhtarian, Farzad
Pepin, François
Bochud, Pascal
Kafyeke, Fassi
description Wing to fuse junction shaping, and associated systems and methods are disclosed herein. An aircraft includes: a fuselage, a wing, and a fairing that covers a junction between the wing and the fuselage. The fairing is configured to receive an inboard section of the wing. An outer surface of the fairing includes an upstream bump proximate to a leading edge of the wing, a midsection sculpting, and a downstream bump proximate to a trailing edge of the wing.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2020398970A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2020398970A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2020398970A13</originalsourceid><addsrcrecordid>eNrjZHAM9_RzVwjxV3ALDXZV8Ar1cw7x9PdTCPZwDABK6Cg4-rkoOAYH-zt7Ooa4uigERwaHuPoGg4V9XUM8_F2CeRhY0xJzilN5oTQ3g7Kba4izh25qQX58anFBYnJqXmpJfGiwkYGRgbGlhaW5gaOhMXGqAHAEK8k</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>WING TO FUSE JUNCTION SHAPING, AND ASSOCIATED SYSTEMS AND METHODS</title><source>esp@cenet</source><creator>Mokhtarian, Farzad ; Pepin, François ; Bochud, Pascal ; Kafyeke, Fassi</creator><creatorcontrib>Mokhtarian, Farzad ; Pepin, François ; Bochud, Pascal ; Kafyeke, Fassi</creatorcontrib><description>Wing to fuse junction shaping, and associated systems and methods are disclosed herein. An aircraft includes: a fuselage, a wing, and a fairing that covers a junction between the wing and the fuselage. The fairing is configured to receive an inboard section of the wing. An outer surface of the fairing includes an upstream bump proximate to a leading edge of the wing, a midsection sculpting, and a downstream bump proximate to a trailing edge of the wing.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; HELICOPTERS ; 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&amp;date=20201224&amp;DB=EPODOC&amp;CC=US&amp;NR=2020398970A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20201224&amp;DB=EPODOC&amp;CC=US&amp;NR=2020398970A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Mokhtarian, Farzad</creatorcontrib><creatorcontrib>Pepin, François</creatorcontrib><creatorcontrib>Bochud, Pascal</creatorcontrib><creatorcontrib>Kafyeke, Fassi</creatorcontrib><title>WING TO FUSE JUNCTION SHAPING, AND ASSOCIATED SYSTEMS AND METHODS</title><description>Wing to fuse junction shaping, and associated systems and methods are disclosed herein. An aircraft includes: a fuselage, a wing, and a fairing that covers a junction between the wing and the fuselage. The fairing is configured to receive an inboard section of the wing. An outer surface of the fairing includes an upstream bump proximate to a leading edge of the wing, a midsection sculpting, and a downstream bump proximate to a trailing edge of the wing.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAM9_RzVwjxV3ALDXZV8Ar1cw7x9PdTCPZwDABK6Cg4-rkoOAYH-zt7Ooa4uigERwaHuPoGg4V9XUM8_F2CeRhY0xJzilN5oTQ3g7Kba4izh25qQX58anFBYnJqXmpJfGiwkYGRgbGlhaW5gaOhMXGqAHAEK8k</recordid><startdate>20201224</startdate><enddate>20201224</enddate><creator>Mokhtarian, Farzad</creator><creator>Pepin, François</creator><creator>Bochud, Pascal</creator><creator>Kafyeke, Fassi</creator><scope>EVB</scope></search><sort><creationdate>20201224</creationdate><title>WING TO FUSE JUNCTION SHAPING, AND ASSOCIATED SYSTEMS AND METHODS</title><author>Mokhtarian, Farzad ; Pepin, François ; Bochud, Pascal ; Kafyeke, Fassi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2020398970A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2020</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Mokhtarian, Farzad</creatorcontrib><creatorcontrib>Pepin, François</creatorcontrib><creatorcontrib>Bochud, Pascal</creatorcontrib><creatorcontrib>Kafyeke, Fassi</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Mokhtarian, Farzad</au><au>Pepin, François</au><au>Bochud, Pascal</au><au>Kafyeke, Fassi</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>WING TO FUSE JUNCTION SHAPING, AND ASSOCIATED SYSTEMS AND METHODS</title><date>2020-12-24</date><risdate>2020</risdate><abstract>Wing to fuse junction shaping, and associated systems and methods are disclosed herein. An aircraft includes: a fuselage, a wing, and a fairing that covers a junction between the wing and the fuselage. The fairing is configured to receive an inboard section of the wing. An outer surface of the fairing includes an upstream bump proximate to a leading edge of the wing, a midsection sculpting, and a downstream bump proximate to a trailing edge of the wing.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_US2020398970A1
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR
GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT
HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title WING TO FUSE JUNCTION SHAPING, AND ASSOCIATED SYSTEMS AND METHODS
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%3A50%3A35IST&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=Mokhtarian,%20Farzad&rft.date=2020-12-24&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2020398970A1%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