Monolithic Wing to Side Body Upper Chord Assembly for Aircraft

Monolithic Wing to Side Body Upper Chord Assembly for Aircraft

A monolithic joint system for a fuselage to wing joint in an aircraft is provided. The joint system comprises a first vertical flange, a base plate, a second vertical flange, and damage containment features associated with at least one of these components. The first vertical flange is configured to...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Koung, Tony, Fletcher, Daniel Harvey, Medlang, Jacob Richard, Rush, Michael Robert
Format: Patent
Sprache:eng
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 Koung, Tony
Fletcher, Daniel Harvey
Medlang, Jacob Richard
Rush, Michael Robert
description A monolithic joint system for a fuselage to wing joint in an aircraft is provided. The joint system comprises a first vertical flange, a base plate, a second vertical flange, and damage containment features associated with at least one of these components. The first vertical flange is configured to connect to a fuselage section of the aircraft and the second vertical flange is configured to connect to a rib web of a wing, while the base plate attaches outboard wing to inboard wing box. The first vertical flange, the base plate, and the second vertical flange are formed from a continuous piece of material. The damage containment features are configured to slow propagation of an active crack tip in the joint system during operation of the aircraft. Thus, the illustrative embodiments provide a one-piece joint system for the fuselage to wing joint of an aircraft.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2021291958A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2021291958A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2021291958A13</originalsourceid><addsrcrecordid>eNrjZLDzzc_Lz8ksychMVgjPzEtXKMlXCM5MSVVwyk-pVAgtKEgtUnDOyC9KUXAsLk7NTcqpVEjLL1JwzCxKLkpMK-FhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfGhwUYGRoZGloaWphaOhsbEqQIApbowlw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Monolithic Wing to Side Body Upper Chord Assembly for Aircraft</title><source>esp@cenet</source><creator>Koung, Tony ; Fletcher, Daniel Harvey ; Medlang, Jacob Richard ; Rush, Michael Robert</creator><creatorcontrib>Koung, Tony ; Fletcher, Daniel Harvey ; Medlang, Jacob Richard ; Rush, Michael Robert</creatorcontrib><description>A monolithic joint system for a fuselage to wing joint in an aircraft is provided. The joint system comprises a first vertical flange, a base plate, a second vertical flange, and damage containment features associated with at least one of these components. The first vertical flange is configured to connect to a fuselage section of the aircraft and the second vertical flange is configured to connect to a rib web of a wing, while the base plate attaches outboard wing to inboard wing box. The first vertical flange, the base plate, and the second vertical flange are formed from a continuous piece of material. The damage containment features are configured to slow propagation of an active crack tip in the joint system during operation of the aircraft. Thus, the illustrative embodiments provide a one-piece joint system for the fuselage to wing joint of an aircraft.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2021</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=20210923&amp;DB=EPODOC&amp;CC=US&amp;NR=2021291958A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20210923&amp;DB=EPODOC&amp;CC=US&amp;NR=2021291958A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Koung, Tony</creatorcontrib><creatorcontrib>Fletcher, Daniel Harvey</creatorcontrib><creatorcontrib>Medlang, Jacob Richard</creatorcontrib><creatorcontrib>Rush, Michael Robert</creatorcontrib><title>Monolithic Wing to Side Body Upper Chord Assembly for Aircraft</title><description>A monolithic joint system for a fuselage to wing joint in an aircraft is provided. The joint system comprises a first vertical flange, a base plate, a second vertical flange, and damage containment features associated with at least one of these components. The first vertical flange is configured to connect to a fuselage section of the aircraft and the second vertical flange is configured to connect to a rib web of a wing, while the base plate attaches outboard wing to inboard wing box. The first vertical flange, the base plate, and the second vertical flange are formed from a continuous piece of material. The damage containment features are configured to slow propagation of an active crack tip in the joint system during operation of the aircraft. Thus, the illustrative embodiments provide a one-piece joint system for the fuselage to wing joint of an aircraft.</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>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLDzzc_Lz8ksychMVgjPzEtXKMlXCM5MSVVwyk-pVAgtKEgtUnDOyC9KUXAsLk7NTcqpVEjLL1JwzCxKLkpMK-FhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfGhwUYGRoZGloaWphaOhsbEqQIApbowlw</recordid><startdate>20210923</startdate><enddate>20210923</enddate><creator>Koung, Tony</creator><creator>Fletcher, Daniel Harvey</creator><creator>Medlang, Jacob Richard</creator><creator>Rush, Michael Robert</creator><scope>EVB</scope></search><sort><creationdate>20210923</creationdate><title>Monolithic Wing to Side Body Upper Chord Assembly for Aircraft</title><author>Koung, Tony ; Fletcher, Daniel Harvey ; Medlang, Jacob Richard ; Rush, Michael Robert</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2021291958A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2021</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>Koung, Tony</creatorcontrib><creatorcontrib>Fletcher, Daniel Harvey</creatorcontrib><creatorcontrib>Medlang, Jacob Richard</creatorcontrib><creatorcontrib>Rush, Michael Robert</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Koung, Tony</au><au>Fletcher, Daniel Harvey</au><au>Medlang, Jacob Richard</au><au>Rush, Michael Robert</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Monolithic Wing to Side Body Upper Chord Assembly for Aircraft</title><date>2021-09-23</date><risdate>2021</risdate><abstract>A monolithic joint system for a fuselage to wing joint in an aircraft is provided. The joint system comprises a first vertical flange, a base plate, a second vertical flange, and damage containment features associated with at least one of these components. The first vertical flange is configured to connect to a fuselage section of the aircraft and the second vertical flange is configured to connect to a rib web of a wing, while the base plate attaches outboard wing to inboard wing box. The first vertical flange, the base plate, and the second vertical flange are formed from a continuous piece of material. The damage containment features are configured to slow propagation of an active crack tip in the joint system during operation of the aircraft. Thus, the illustrative embodiments provide a one-piece joint system for the fuselage to wing joint of an aircraft.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_US2021291958A1
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Monolithic Wing to Side Body Upper Chord Assembly for Aircraft
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-24T20%3A47%3A34IST&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=Koung,%20Tony&rft.date=2021-09-23&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2021291958A1%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