LEADING-EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFT
A leading-edge high-lift device according to an embodiment of the present invention is a leading-edge high-lift device that is deployable and retractable from/into a fixed leading edge of a main wing of an aircraft and includes: a leading edge portion; a trailing edge portion that forms a gap betwee...
Gespeichert in:
Hauptverfasser: | , , , , , , , |
---|---|
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 | ISOTANI, Kazuhide UENO, Yosuke YOKOKAWA, Yuzuru KOHZAI, Masataka YAMAMOTO, Kazuomi MURAYAMA, Mitsuhiro HAYASHI, Kensuke HAYAMA, Kenji |
description | A leading-edge high-lift device according to an embodiment of the present invention is a leading-edge high-lift device that is deployable and retractable from/into a fixed leading edge of a main wing of an aircraft and includes: a leading edge portion; a trailing edge portion that forms a gap between a trailing edge portion and the main wing during deployment; a cusp portion formed at a lower edge of the leading edge portion; a lower surface portion formed between the cusp portion and the trailing edge portion; and a curved hump portion that is locally provided on a surface of the lower surface portion and protrudes toward the main wing in a cross-sectional shape perpendicular to a wing span direction of the main wing. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2024246657A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2024246657A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2024246657A13</originalsourceid><addsrcrecordid>eNrjZDD0cXV08fRz13V1cXdV8PB099D18XQLUXBxDfN0dtVRCAfK6Sg4-rkoOHoGOQc5uoXwMLCmJeYUp_JCaW4GZTfXEGcP3dSC_PjU4oLE5NS81JL40GAjAyMTIxMzM1NzR0Nj4lQBAJXYJsY</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>LEADING-EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFT</title><source>esp@cenet</source><creator>ISOTANI, Kazuhide ; UENO, Yosuke ; YOKOKAWA, Yuzuru ; KOHZAI, Masataka ; YAMAMOTO, Kazuomi ; MURAYAMA, Mitsuhiro ; HAYASHI, Kensuke ; HAYAMA, Kenji</creator><creatorcontrib>ISOTANI, Kazuhide ; UENO, Yosuke ; YOKOKAWA, Yuzuru ; KOHZAI, Masataka ; YAMAMOTO, Kazuomi ; MURAYAMA, Mitsuhiro ; HAYASHI, Kensuke ; HAYAMA, Kenji</creatorcontrib><description>A leading-edge high-lift device according to an embodiment of the present invention is a leading-edge high-lift device that is deployable and retractable from/into a fixed leading edge of a main wing of an aircraft and includes: a leading edge portion; a trailing edge portion that forms a gap between a trailing edge portion and the main wing during deployment; a cusp portion formed at a lower edge of the leading edge portion; a lower surface portion formed between the cusp portion and the trailing edge portion; and a curved hump portion that is locally provided on a surface of the lower surface portion and protrudes toward the main wing in a cross-sectional shape perpendicular to a wing span direction of the main wing.</description><language>eng</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=20240725&DB=EPODOC&CC=US&NR=2024246657A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240725&DB=EPODOC&CC=US&NR=2024246657A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ISOTANI, Kazuhide</creatorcontrib><creatorcontrib>UENO, Yosuke</creatorcontrib><creatorcontrib>YOKOKAWA, Yuzuru</creatorcontrib><creatorcontrib>KOHZAI, Masataka</creatorcontrib><creatorcontrib>YAMAMOTO, Kazuomi</creatorcontrib><creatorcontrib>MURAYAMA, Mitsuhiro</creatorcontrib><creatorcontrib>HAYASHI, Kensuke</creatorcontrib><creatorcontrib>HAYAMA, Kenji</creatorcontrib><title>LEADING-EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFT</title><description>A leading-edge high-lift device according to an embodiment of the present invention is a leading-edge high-lift device that is deployable and retractable from/into a fixed leading edge of a main wing of an aircraft and includes: a leading edge portion; a trailing edge portion that forms a gap between a trailing edge portion and the main wing during deployment; a cusp portion formed at a lower edge of the leading edge portion; a lower surface portion formed between the cusp portion and the trailing edge portion; and a curved hump portion that is locally provided on a surface of the lower surface portion and protrudes toward the main wing in a cross-sectional shape perpendicular to a wing span direction of the main 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>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDD0cXV08fRz13V1cXdV8PB099D18XQLUXBxDfN0dtVRCAfK6Sg4-rkoOHoGOQc5uoXwMLCmJeYUp_JCaW4GZTfXEGcP3dSC_PjU4oLE5NS81JL40GAjAyMTIxMzM1NzR0Nj4lQBAJXYJsY</recordid><startdate>20240725</startdate><enddate>20240725</enddate><creator>ISOTANI, Kazuhide</creator><creator>UENO, Yosuke</creator><creator>YOKOKAWA, Yuzuru</creator><creator>KOHZAI, Masataka</creator><creator>YAMAMOTO, Kazuomi</creator><creator>MURAYAMA, Mitsuhiro</creator><creator>HAYASHI, Kensuke</creator><creator>HAYAMA, Kenji</creator><scope>EVB</scope></search><sort><creationdate>20240725</creationdate><title>LEADING-EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFT</title><author>ISOTANI, Kazuhide ; UENO, Yosuke ; YOKOKAWA, Yuzuru ; KOHZAI, Masataka ; YAMAMOTO, Kazuomi ; MURAYAMA, Mitsuhiro ; HAYASHI, Kensuke ; HAYAMA, Kenji</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2024246657A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</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>ISOTANI, Kazuhide</creatorcontrib><creatorcontrib>UENO, Yosuke</creatorcontrib><creatorcontrib>YOKOKAWA, Yuzuru</creatorcontrib><creatorcontrib>KOHZAI, Masataka</creatorcontrib><creatorcontrib>YAMAMOTO, Kazuomi</creatorcontrib><creatorcontrib>MURAYAMA, Mitsuhiro</creatorcontrib><creatorcontrib>HAYASHI, Kensuke</creatorcontrib><creatorcontrib>HAYAMA, Kenji</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ISOTANI, Kazuhide</au><au>UENO, Yosuke</au><au>YOKOKAWA, Yuzuru</au><au>KOHZAI, Masataka</au><au>YAMAMOTO, Kazuomi</au><au>MURAYAMA, Mitsuhiro</au><au>HAYASHI, Kensuke</au><au>HAYAMA, Kenji</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>LEADING-EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFT</title><date>2024-07-25</date><risdate>2024</risdate><abstract>A leading-edge high-lift device according to an embodiment of the present invention is a leading-edge high-lift device that is deployable and retractable from/into a fixed leading edge of a main wing of an aircraft and includes: a leading edge portion; a trailing edge portion that forms a gap between a trailing edge portion and the main wing during deployment; a cusp portion formed at a lower edge of the leading edge portion; a lower surface portion formed between the cusp portion and the trailing edge portion; and a curved hump portion that is locally provided on a surface of the lower surface portion and protrudes toward the main wing in a cross-sectional shape perpendicular to a wing span direction of the main wing.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_US2024246657A1 |
source | esp@cenet |
subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | LEADING-EDGE HIGH-LIFT DEVICE, WING, AND AIRCRAFT |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-26T16%3A37%3A29IST&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=ISOTANI,%20Kazuhide&rft.date=2024-07-25&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2024246657A1%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 |