Flapping wing aircraft and rolling flight method thereof

The invention relates to the technical field of aircrafts, aims to solve the problem that wings of an existing ornithopter cannot be directly controlled to generate rolling torque, and provides an ornithopter and a rolling flight method thereof.The ornithopter comprises an ornithopter body, the wing...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: HE JIAN, YANG YIN, XU XIN, LIU DAWEI, WANG RUIBO, SU LEI, CHEN YANRU, YANG KEPENG, ZHENG PIANPIAN, LI QIANG
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 HE JIAN
YANG YIN
XU XIN
LIU DAWEI
WANG RUIBO
SU LEI
CHEN YANRU
YANG KEPENG
ZHENG PIANPIAN
LI QIANG
description The invention relates to the technical field of aircrafts, aims to solve the problem that wings of an existing ornithopter cannot be directly controlled to generate rolling torque, and provides an ornithopter and a rolling flight method thereof.The ornithopter comprises an ornithopter body, the wings are symmetrically installed on the two sides of the ornithopter body, and transverse straight beams and skins are arranged on the wings; one end of the transverse straight beam is connected with the fuselage, and the skin is connected between the transverse straight beam and the fuselage and covers the wings; the transverse straight beam is divided into a first beam and a second beam, one end of the first beam is connected with the machine body, and the other end of the first beam is hinged to the second beam; a plurality of supporting rods are connected to the skin, one end of each supporting rod is connected to the hinge point of the first cross beam and the second cross beam, and all the supporting rods are un
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN115636086A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN115636086A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN115636086A3</originalsourceid><addsrcrecordid>eNrjZLBwy0ksKMjMS1coBxGJmUXJRYlpJQqJeSkKRfk5OSDBtJzM9IwShdzUkoz8FIWSjNSi1Pw0HgbWtMSc4lReKM3NoOjmGuLsoZtakB-fWlyQmJyal1oS7-xnaGhqZmxmYGHmaEyMGgAGVy5P</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Flapping wing aircraft and rolling flight method thereof</title><source>esp@cenet</source><creator>HE JIAN ; YANG YIN ; XU XIN ; LIU DAWEI ; WANG RUIBO ; SU LEI ; CHEN YANRU ; YANG KEPENG ; ZHENG PIANPIAN ; LI QIANG</creator><creatorcontrib>HE JIAN ; YANG YIN ; XU XIN ; LIU DAWEI ; WANG RUIBO ; SU LEI ; CHEN YANRU ; YANG KEPENG ; ZHENG PIANPIAN ; LI QIANG</creatorcontrib><description>The invention relates to the technical field of aircrafts, aims to solve the problem that wings of an existing ornithopter cannot be directly controlled to generate rolling torque, and provides an ornithopter and a rolling flight method thereof.The ornithopter comprises an ornithopter body, the wings are symmetrically installed on the two sides of the ornithopter body, and transverse straight beams and skins are arranged on the wings; one end of the transverse straight beam is connected with the fuselage, and the skin is connected between the transverse straight beam and the fuselage and covers the wings; the transverse straight beam is divided into a first beam and a second beam, one end of the first beam is connected with the machine body, and the other end of the first beam is hinged to the second beam; a plurality of supporting rods are connected to the skin, one end of each supporting rod is connected to the hinge point of the first cross beam and the second cross beam, and all the supporting rods are un</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2023</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=20230124&amp;DB=EPODOC&amp;CC=CN&amp;NR=115636086A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20230124&amp;DB=EPODOC&amp;CC=CN&amp;NR=115636086A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HE JIAN</creatorcontrib><creatorcontrib>YANG YIN</creatorcontrib><creatorcontrib>XU XIN</creatorcontrib><creatorcontrib>LIU DAWEI</creatorcontrib><creatorcontrib>WANG RUIBO</creatorcontrib><creatorcontrib>SU LEI</creatorcontrib><creatorcontrib>CHEN YANRU</creatorcontrib><creatorcontrib>YANG KEPENG</creatorcontrib><creatorcontrib>ZHENG PIANPIAN</creatorcontrib><creatorcontrib>LI QIANG</creatorcontrib><title>Flapping wing aircraft and rolling flight method thereof</title><description>The invention relates to the technical field of aircrafts, aims to solve the problem that wings of an existing ornithopter cannot be directly controlled to generate rolling torque, and provides an ornithopter and a rolling flight method thereof.The ornithopter comprises an ornithopter body, the wings are symmetrically installed on the two sides of the ornithopter body, and transverse straight beams and skins are arranged on the wings; one end of the transverse straight beam is connected with the fuselage, and the skin is connected between the transverse straight beam and the fuselage and covers the wings; the transverse straight beam is divided into a first beam and a second beam, one end of the first beam is connected with the machine body, and the other end of the first beam is hinged to the second beam; a plurality of supporting rods are connected to the skin, one end of each supporting rod is connected to the hinge point of the first cross beam and the second cross beam, and all the supporting rods are un</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>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLBwy0ksKMjMS1coBxGJmUXJRYlpJQqJeSkKRfk5OSDBtJzM9IwShdzUkoz8FIWSjNSi1Pw0HgbWtMSc4lReKM3NoOjmGuLsoZtakB-fWlyQmJyal1oS7-xnaGhqZmxmYGHmaEyMGgAGVy5P</recordid><startdate>20230124</startdate><enddate>20230124</enddate><creator>HE JIAN</creator><creator>YANG YIN</creator><creator>XU XIN</creator><creator>LIU DAWEI</creator><creator>WANG RUIBO</creator><creator>SU LEI</creator><creator>CHEN YANRU</creator><creator>YANG KEPENG</creator><creator>ZHENG PIANPIAN</creator><creator>LI QIANG</creator><scope>EVB</scope></search><sort><creationdate>20230124</creationdate><title>Flapping wing aircraft and rolling flight method thereof</title><author>HE JIAN ; YANG YIN ; XU XIN ; LIU DAWEI ; WANG RUIBO ; SU LEI ; CHEN YANRU ; YANG KEPENG ; ZHENG PIANPIAN ; LI QIANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN115636086A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</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>HE JIAN</creatorcontrib><creatorcontrib>YANG YIN</creatorcontrib><creatorcontrib>XU XIN</creatorcontrib><creatorcontrib>LIU DAWEI</creatorcontrib><creatorcontrib>WANG RUIBO</creatorcontrib><creatorcontrib>SU LEI</creatorcontrib><creatorcontrib>CHEN YANRU</creatorcontrib><creatorcontrib>YANG KEPENG</creatorcontrib><creatorcontrib>ZHENG PIANPIAN</creatorcontrib><creatorcontrib>LI QIANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HE JIAN</au><au>YANG YIN</au><au>XU XIN</au><au>LIU DAWEI</au><au>WANG RUIBO</au><au>SU LEI</au><au>CHEN YANRU</au><au>YANG KEPENG</au><au>ZHENG PIANPIAN</au><au>LI QIANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Flapping wing aircraft and rolling flight method thereof</title><date>2023-01-24</date><risdate>2023</risdate><abstract>The invention relates to the technical field of aircrafts, aims to solve the problem that wings of an existing ornithopter cannot be directly controlled to generate rolling torque, and provides an ornithopter and a rolling flight method thereof.The ornithopter comprises an ornithopter body, the wings are symmetrically installed on the two sides of the ornithopter body, and transverse straight beams and skins are arranged on the wings; one end of the transverse straight beam is connected with the fuselage, and the skin is connected between the transverse straight beam and the fuselage and covers the wings; the transverse straight beam is divided into a first beam and a second beam, one end of the first beam is connected with the machine body, and the other end of the first beam is hinged to the second beam; a plurality of supporting rods are connected to the skin, one end of each supporting rod is connected to the hinge point of the first cross beam and the second cross beam, and all the supporting rods are un</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN115636086A
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Flapping wing aircraft and rolling flight method thereof
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-24T13%3A49%3A38IST&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=HE%20JIAN&rft.date=2023-01-24&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN115636086A%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