WING FOR AN AIRCRAFT
Disclosed is a wing (3) for an aircraft (1), comprising a main wing (5) and a slat assembly comprising a slat (7), and at least one connection assembly (9) comprising an elongate slat track (17), wherein the front end (21) of the slat track (17) is mounted to the slat (7), wherein the rear end (23)...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Patent |
Sprache: | eng ; fre ; ger |
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 | Schlipf, Bernhard Lorenz, Florian |
description | Disclosed is a wing (3) for an aircraft (1), comprising a main wing (5) and a slat assembly comprising a slat (7), and at least one connection assembly (9) comprising an elongate slat track (17), wherein the front end (21) of the slat track (17) is mounted to the slat (7), wherein the rear end (23) and/or the intermediate portion (25) of the slat track (17) are mounted to the main wing (5) by a roller or slide bearing (27) such that the slat track (17) is movable along the track longitudinal axis (19), wherein the connection assembly (9) comprises a drive unit (73) configured for driving the slat track (17). The object to provide a wing employing a simple, robust, and cost-efficient drive unit, is achieved in that the drive unit (73) comprises a rotary actuator (75) mounted to the main wing (5) and having at least one drive arm (77) rotatably driven about a rotation axis (79) and drivingly engaging the slat track (17), and in that one of the drive arm (77) and the slat track (17) comprises at least one groove (81) and the other one of the drive arm (77) and the slat track (17) comprises at least one spigot (83) drivingly engaging the groove (81). |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP4101754B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP4101754B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP4101754B13</originalsourceid><addsrcrecordid>eNrjZBAJ9_RzV3DzD1Jw9FNw9AxyDnJ0C-FhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuASaGBobmpiZOhsZEKAEAJCkd6A</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>WING FOR AN AIRCRAFT</title><source>esp@cenet</source><creator>Schlipf, Bernhard ; Lorenz, Florian</creator><creatorcontrib>Schlipf, Bernhard ; Lorenz, Florian</creatorcontrib><description>Disclosed is a wing (3) for an aircraft (1), comprising a main wing (5) and a slat assembly comprising a slat (7), and at least one connection assembly (9) comprising an elongate slat track (17), wherein the front end (21) of the slat track (17) is mounted to the slat (7), wherein the rear end (23) and/or the intermediate portion (25) of the slat track (17) are mounted to the main wing (5) by a roller or slide bearing (27) such that the slat track (17) is movable along the track longitudinal axis (19), wherein the connection assembly (9) comprises a drive unit (73) configured for driving the slat track (17). The object to provide a wing employing a simple, robust, and cost-efficient drive unit, is achieved in that the drive unit (73) comprises a rotary actuator (75) mounted to the main wing (5) and having at least one drive arm (77) rotatably driven about a rotation axis (79) and drivingly engaging the slat track (17), and in that one of the drive arm (77) and the slat track (17) comprises at least one groove (81) and the other one of the drive arm (77) and the slat track (17) comprises at least one spigot (83) drivingly engaging the groove (81).</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2024</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=20240828&DB=EPODOC&CC=EP&NR=4101754B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240828&DB=EPODOC&CC=EP&NR=4101754B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Schlipf, Bernhard</creatorcontrib><creatorcontrib>Lorenz, Florian</creatorcontrib><title>WING FOR AN AIRCRAFT</title><description>Disclosed is a wing (3) for an aircraft (1), comprising a main wing (5) and a slat assembly comprising a slat (7), and at least one connection assembly (9) comprising an elongate slat track (17), wherein the front end (21) of the slat track (17) is mounted to the slat (7), wherein the rear end (23) and/or the intermediate portion (25) of the slat track (17) are mounted to the main wing (5) by a roller or slide bearing (27) such that the slat track (17) is movable along the track longitudinal axis (19), wherein the connection assembly (9) comprises a drive unit (73) configured for driving the slat track (17). The object to provide a wing employing a simple, robust, and cost-efficient drive unit, is achieved in that the drive unit (73) comprises a rotary actuator (75) mounted to the main wing (5) and having at least one drive arm (77) rotatably driven about a rotation axis (79) and drivingly engaging the slat track (17), and in that one of the drive arm (77) and the slat track (17) comprises at least one groove (81) and the other one of the drive arm (77) and the slat track (17) comprises at least one spigot (83) drivingly engaging the groove (81).</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>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBAJ9_RzV3DzD1Jw9FNw9AxyDnJ0C-FhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuASaGBobmpiZOhsZEKAEAJCkd6A</recordid><startdate>20240828</startdate><enddate>20240828</enddate><creator>Schlipf, Bernhard</creator><creator>Lorenz, Florian</creator><scope>EVB</scope></search><sort><creationdate>20240828</creationdate><title>WING FOR AN AIRCRAFT</title><author>Schlipf, Bernhard ; Lorenz, Florian</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4101754B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</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>Schlipf, Bernhard</creatorcontrib><creatorcontrib>Lorenz, Florian</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Schlipf, Bernhard</au><au>Lorenz, Florian</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>WING FOR AN AIRCRAFT</title><date>2024-08-28</date><risdate>2024</risdate><abstract>Disclosed is a wing (3) for an aircraft (1), comprising a main wing (5) and a slat assembly comprising a slat (7), and at least one connection assembly (9) comprising an elongate slat track (17), wherein the front end (21) of the slat track (17) is mounted to the slat (7), wherein the rear end (23) and/or the intermediate portion (25) of the slat track (17) are mounted to the main wing (5) by a roller or slide bearing (27) such that the slat track (17) is movable along the track longitudinal axis (19), wherein the connection assembly (9) comprises a drive unit (73) configured for driving the slat track (17). The object to provide a wing employing a simple, robust, and cost-efficient drive unit, is achieved in that the drive unit (73) comprises a rotary actuator (75) mounted to the main wing (5) and having at least one drive arm (77) rotatably driven about a rotation axis (79) and drivingly engaging the slat track (17), and in that one of the drive arm (77) and the slat track (17) comprises at least one groove (81) and the other one of the drive arm (77) and the slat track (17) comprises at least one spigot (83) drivingly engaging the groove (81).</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng ; fre ; ger |
recordid | cdi_epo_espacenet_EP4101754B1 |
source | esp@cenet |
subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | WING FOR AN AIRCRAFT |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-22T16%3A59%3A06IST&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=Schlipf,%20Bernhard&rft.date=2024-08-28&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP4101754B1%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 |