Single-duct aircraft based on Magnus effect

Single-duct aircraft based on Magnus effect

The single-duct aircraft based on the Magnus effect comprises a rack, a duct, a power device, an airflow adjusting device, a steering engine device and a control circuit, the power device and the airflow adjusting device are arranged in the duct, the steering engine device comprises a plurality of s...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: LI ZONGXIN, HAN RUIBIN, FU KAIHUA, CHEN HONG, YUAN JUN, WANG HAOXIANG, XIE WENFENG, GONG WEIJIE, HUANG RUNGUANG, GUO TING, ZHENG ZETING, WANG ZIJIAN
Format: Patent
Sprache:chi ; 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 LI ZONGXIN
HAN RUIBIN
FU KAIHUA
CHEN HONG
YUAN JUN
WANG HAOXIANG
XIE WENFENG
GONG WEIJIE
HUANG RUNGUANG
GUO TING
ZHENG ZETING
WANG ZIJIAN
description The single-duct aircraft based on the Magnus effect comprises a rack, a duct, a power device, an airflow adjusting device, a steering engine device and a control circuit, the power device and the airflow adjusting device are arranged in the duct, the steering engine device comprises a plurality of steering engine units, the steering engine units are installed on the rack and arranged below the duct, and the control circuit is arranged on the rack. The blades are circumferentially and uniformly distributed around the axis of the duct; the steering engine unit comprises a steering engine and a Magnus rudder sheet; the Magnus rudder sheet comprises a rudder sheet, a Magnus cylinder and a cylinder driving motor; the steering engine is installed on the rack, the rudder sheet is connected with a rudder disc of the steering engine, and the Magnus cylinder is rotatably installed above the top of the rudder sheet and is driven by the cylinder driving motor installed on the rudder sheet; the axis of the Magnus cylinder
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN117799827A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN117799827A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN117799827A3</originalsourceid><addsrcrecordid>eNrjZNAOzsxLz0nVTSlNLlFIzCxKLkpMK1FISixOTVHIz1PwTUzPKy1WSE1LS00u4WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hobm5paWFkbmjsbEqAEANMcpFw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Single-duct aircraft based on Magnus effect</title><source>esp@cenet</source><creator>LI ZONGXIN ; HAN RUIBIN ; FU KAIHUA ; CHEN HONG ; YUAN JUN ; WANG HAOXIANG ; XIE WENFENG ; GONG WEIJIE ; HUANG RUNGUANG ; GUO TING ; ZHENG ZETING ; WANG ZIJIAN</creator><creatorcontrib>LI ZONGXIN ; HAN RUIBIN ; FU KAIHUA ; CHEN HONG ; YUAN JUN ; WANG HAOXIANG ; XIE WENFENG ; GONG WEIJIE ; HUANG RUNGUANG ; GUO TING ; ZHENG ZETING ; WANG ZIJIAN</creatorcontrib><description>The single-duct aircraft based on the Magnus effect comprises a rack, a duct, a power device, an airflow adjusting device, a steering engine device and a control circuit, the power device and the airflow adjusting device are arranged in the duct, the steering engine device comprises a plurality of steering engine units, the steering engine units are installed on the rack and arranged below the duct, and the control circuit is arranged on the rack. The blades are circumferentially and uniformly distributed around the axis of the duct; the steering engine unit comprises a steering engine and a Magnus rudder sheet; the Magnus rudder sheet comprises a rudder sheet, a Magnus cylinder and a cylinder driving motor; the steering engine is installed on the rack, the rudder sheet is connected with a rudder disc of the steering engine, and the Magnus cylinder is rotatably installed above the top of the rudder sheet and is driven by the cylinder driving motor installed on the rudder sheet; the axis of the Magnus cylinder</description><language>chi ; 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&amp;date=20240402&amp;DB=EPODOC&amp;CC=CN&amp;NR=117799827A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240402&amp;DB=EPODOC&amp;CC=CN&amp;NR=117799827A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LI ZONGXIN</creatorcontrib><creatorcontrib>HAN RUIBIN</creatorcontrib><creatorcontrib>FU KAIHUA</creatorcontrib><creatorcontrib>CHEN HONG</creatorcontrib><creatorcontrib>YUAN JUN</creatorcontrib><creatorcontrib>WANG HAOXIANG</creatorcontrib><creatorcontrib>XIE WENFENG</creatorcontrib><creatorcontrib>GONG WEIJIE</creatorcontrib><creatorcontrib>HUANG RUNGUANG</creatorcontrib><creatorcontrib>GUO TING</creatorcontrib><creatorcontrib>ZHENG ZETING</creatorcontrib><creatorcontrib>WANG ZIJIAN</creatorcontrib><title>Single-duct aircraft based on Magnus effect</title><description>The single-duct aircraft based on the Magnus effect comprises a rack, a duct, a power device, an airflow adjusting device, a steering engine device and a control circuit, the power device and the airflow adjusting device are arranged in the duct, the steering engine device comprises a plurality of steering engine units, the steering engine units are installed on the rack and arranged below the duct, and the control circuit is arranged on the rack. The blades are circumferentially and uniformly distributed around the axis of the duct; the steering engine unit comprises a steering engine and a Magnus rudder sheet; the Magnus rudder sheet comprises a rudder sheet, a Magnus cylinder and a cylinder driving motor; the steering engine is installed on the rack, the rudder sheet is connected with a rudder disc of the steering engine, and the Magnus cylinder is rotatably installed above the top of the rudder sheet and is driven by the cylinder driving motor installed on the rudder sheet; the axis of the Magnus cylinder</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>eNrjZNAOzsxLz0nVTSlNLlFIzCxKLkpMK1FISixOTVHIz1PwTUzPKy1WSE1LS00u4WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hobm5paWFkbmjsbEqAEANMcpFw</recordid><startdate>20240402</startdate><enddate>20240402</enddate><creator>LI ZONGXIN</creator><creator>HAN RUIBIN</creator><creator>FU KAIHUA</creator><creator>CHEN HONG</creator><creator>YUAN JUN</creator><creator>WANG HAOXIANG</creator><creator>XIE WENFENG</creator><creator>GONG WEIJIE</creator><creator>HUANG RUNGUANG</creator><creator>GUO TING</creator><creator>ZHENG ZETING</creator><creator>WANG ZIJIAN</creator><scope>EVB</scope></search><sort><creationdate>20240402</creationdate><title>Single-duct aircraft based on Magnus effect</title><author>LI ZONGXIN ; HAN RUIBIN ; FU KAIHUA ; CHEN HONG ; YUAN JUN ; WANG HAOXIANG ; XIE WENFENG ; GONG WEIJIE ; HUANG RUNGUANG ; GUO TING ; ZHENG ZETING ; WANG ZIJIAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN117799827A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; 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>LI ZONGXIN</creatorcontrib><creatorcontrib>HAN RUIBIN</creatorcontrib><creatorcontrib>FU KAIHUA</creatorcontrib><creatorcontrib>CHEN HONG</creatorcontrib><creatorcontrib>YUAN JUN</creatorcontrib><creatorcontrib>WANG HAOXIANG</creatorcontrib><creatorcontrib>XIE WENFENG</creatorcontrib><creatorcontrib>GONG WEIJIE</creatorcontrib><creatorcontrib>HUANG RUNGUANG</creatorcontrib><creatorcontrib>GUO TING</creatorcontrib><creatorcontrib>ZHENG ZETING</creatorcontrib><creatorcontrib>WANG ZIJIAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LI ZONGXIN</au><au>HAN RUIBIN</au><au>FU KAIHUA</au><au>CHEN HONG</au><au>YUAN JUN</au><au>WANG HAOXIANG</au><au>XIE WENFENG</au><au>GONG WEIJIE</au><au>HUANG RUNGUANG</au><au>GUO TING</au><au>ZHENG ZETING</au><au>WANG ZIJIAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Single-duct aircraft based on Magnus effect</title><date>2024-04-02</date><risdate>2024</risdate><abstract>The single-duct aircraft based on the Magnus effect comprises a rack, a duct, a power device, an airflow adjusting device, a steering engine device and a control circuit, the power device and the airflow adjusting device are arranged in the duct, the steering engine device comprises a plurality of steering engine units, the steering engine units are installed on the rack and arranged below the duct, and the control circuit is arranged on the rack. The blades are circumferentially and uniformly distributed around the axis of the duct; the steering engine unit comprises a steering engine and a Magnus rudder sheet; the Magnus rudder sheet comprises a rudder sheet, a Magnus cylinder and a cylinder driving motor; the steering engine is installed on the rack, the rudder sheet is connected with a rudder disc of the steering engine, and the Magnus cylinder is rotatably installed above the top of the rudder sheet and is driven by the cylinder driving motor installed on the rudder sheet; the axis of the Magnus cylinder</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN117799827A
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Single-duct aircraft based on Magnus effect
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-17T15%3A54%3A01IST&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=LI%20ZONGXIN&rft.date=2024-04-02&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN117799827A%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