Foldable bionic flapping wing and aircraft

The invention provides a foldable bionic flapping wing which is characterized in that a folding mechanism comprises a first folding wing, a second folding wing, a third folding wing and a fourth folding wing, one end of the first folding wing is connected with one end of the fourth folding wing, the...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: SUN JIYU, LI PENGPENG, ZHANG JUNFENG, ZHAN YUCHAO, LIU CHAO, YAN YONGWEI, SONG ZELAI, SONG FA
Format: Patent
Sprache:chi ; 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 SUN JIYU
LI PENGPENG
ZHANG JUNFENG
ZHAN YUCHAO
LIU CHAO
YAN YONGWEI
SONG ZELAI
SONG FA
description The invention provides a foldable bionic flapping wing which is characterized in that a folding mechanism comprises a first folding wing, a second folding wing, a third folding wing and a fourth folding wing, one end of the first folding wing is connected with one end of the fourth folding wing, the other end of the fourth folding wing is connected to the third folding wing, one end of the third folding wing is connected with one end of the second folding wing, and the other end of the second folding wing is connected to the first folding wing; the first connecting point, the second connecting point, the third connecting point and the fourth connecting point are sequentially positioned at four vertexes of the parallelogram in the folding process of the flapping wing; one end of a first connecting rod is connected with the first flap, the other end of the first connecting rod is fixedly connected to the aircraft, one end of the pull rod is connected to the first flap, and the other end of the pull rod is slida
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN113148144A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN113148144A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN113148144A3</originalsourceid><addsrcrecordid>eNrjZNByy89JSUzKSVVIyszPy0xWSMtJLCjIzEtXKAcRiXkpComZRclFiWklPAysaYk5xam8UJqbQdHNNcTZQze1ID8-tbggMTk1L7Uk3tnP0NDY0MTC0MTE0ZgYNQARnyi5</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Foldable bionic flapping wing and aircraft</title><source>esp@cenet</source><creator>SUN JIYU ; LI PENGPENG ; ZHANG JUNFENG ; ZHAN YUCHAO ; LIU CHAO ; YAN YONGWEI ; SONG ZELAI ; SONG FA</creator><creatorcontrib>SUN JIYU ; LI PENGPENG ; ZHANG JUNFENG ; ZHAN YUCHAO ; LIU CHAO ; YAN YONGWEI ; SONG ZELAI ; SONG FA</creatorcontrib><description>The invention provides a foldable bionic flapping wing which is characterized in that a folding mechanism comprises a first folding wing, a second folding wing, a third folding wing and a fourth folding wing, one end of the first folding wing is connected with one end of the fourth folding wing, the other end of the fourth folding wing is connected to the third folding wing, one end of the third folding wing is connected with one end of the second folding wing, and the other end of the second folding wing is connected to the first folding wing; the first connecting point, the second connecting point, the third connecting point and the fourth connecting point are sequentially positioned at four vertexes of the parallelogram in the folding process of the flapping wing; one end of a first connecting rod is connected with the first flap, the other end of the first connecting rod is fixedly connected to the aircraft, one end of the pull rod is connected to the first flap, and the other end of the pull rod is slida</description><language>chi ; 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=20210723&amp;DB=EPODOC&amp;CC=CN&amp;NR=113148144A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20210723&amp;DB=EPODOC&amp;CC=CN&amp;NR=113148144A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SUN JIYU</creatorcontrib><creatorcontrib>LI PENGPENG</creatorcontrib><creatorcontrib>ZHANG JUNFENG</creatorcontrib><creatorcontrib>ZHAN YUCHAO</creatorcontrib><creatorcontrib>LIU CHAO</creatorcontrib><creatorcontrib>YAN YONGWEI</creatorcontrib><creatorcontrib>SONG ZELAI</creatorcontrib><creatorcontrib>SONG FA</creatorcontrib><title>Foldable bionic flapping wing and aircraft</title><description>The invention provides a foldable bionic flapping wing which is characterized in that a folding mechanism comprises a first folding wing, a second folding wing, a third folding wing and a fourth folding wing, one end of the first folding wing is connected with one end of the fourth folding wing, the other end of the fourth folding wing is connected to the third folding wing, one end of the third folding wing is connected with one end of the second folding wing, and the other end of the second folding wing is connected to the first folding wing; the first connecting point, the second connecting point, the third connecting point and the fourth connecting point are sequentially positioned at four vertexes of the parallelogram in the folding process of the flapping wing; one end of a first connecting rod is connected with the first flap, the other end of the first connecting rod is fixedly connected to the aircraft, one end of the pull rod is connected to the first flap, and the other end of the pull rod is slida</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>eNrjZNByy89JSUzKSVVIyszPy0xWSMtJLCjIzEtXKAcRiXkpComZRclFiWklPAysaYk5xam8UJqbQdHNNcTZQze1ID8-tbggMTk1L7Uk3tnP0NDY0MTC0MTE0ZgYNQARnyi5</recordid><startdate>20210723</startdate><enddate>20210723</enddate><creator>SUN JIYU</creator><creator>LI PENGPENG</creator><creator>ZHANG JUNFENG</creator><creator>ZHAN YUCHAO</creator><creator>LIU CHAO</creator><creator>YAN YONGWEI</creator><creator>SONG ZELAI</creator><creator>SONG FA</creator><scope>EVB</scope></search><sort><creationdate>20210723</creationdate><title>Foldable bionic flapping wing and aircraft</title><author>SUN JIYU ; LI PENGPENG ; ZHANG JUNFENG ; ZHAN YUCHAO ; LIU CHAO ; YAN YONGWEI ; SONG ZELAI ; SONG FA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN113148144A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; 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>SUN JIYU</creatorcontrib><creatorcontrib>LI PENGPENG</creatorcontrib><creatorcontrib>ZHANG JUNFENG</creatorcontrib><creatorcontrib>ZHAN YUCHAO</creatorcontrib><creatorcontrib>LIU CHAO</creatorcontrib><creatorcontrib>YAN YONGWEI</creatorcontrib><creatorcontrib>SONG ZELAI</creatorcontrib><creatorcontrib>SONG FA</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SUN JIYU</au><au>LI PENGPENG</au><au>ZHANG JUNFENG</au><au>ZHAN YUCHAO</au><au>LIU CHAO</au><au>YAN YONGWEI</au><au>SONG ZELAI</au><au>SONG FA</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Foldable bionic flapping wing and aircraft</title><date>2021-07-23</date><risdate>2021</risdate><abstract>The invention provides a foldable bionic flapping wing which is characterized in that a folding mechanism comprises a first folding wing, a second folding wing, a third folding wing and a fourth folding wing, one end of the first folding wing is connected with one end of the fourth folding wing, the other end of the fourth folding wing is connected to the third folding wing, one end of the third folding wing is connected with one end of the second folding wing, and the other end of the second folding wing is connected to the first folding wing; the first connecting point, the second connecting point, the third connecting point and the fourth connecting point are sequentially positioned at four vertexes of the parallelogram in the folding process of the flapping wing; one end of a first connecting rod is connected with the first flap, the other end of the first connecting rod is fixedly connected to the aircraft, one end of the pull rod is connected to the first flap, and the other end of the pull rod is slida</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN113148144A
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Foldable bionic flapping 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=2025-01-02T17%3A49%3A27IST&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=SUN%20JIYU&rft.date=2021-07-23&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN113148144A%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