Amphibious vertical take-off and landing aircraft structure
The utility model relates to the technical field of flight, in particular to an amphibious vertical take-off and landing aircraft structure which comprises a fuselage, a front wing and an empennage, the fuselage adopts a double-hull structure and is provided with a mounting frame, and a plurality of...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| 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 | XIE ENLI |
| description | The utility model relates to the technical field of flight, in particular to an amphibious vertical take-off and landing aircraft structure which comprises a fuselage, a front wing and an empennage, the fuselage adopts a double-hull structure and is provided with a mounting frame, and a plurality of rotor wing mechanisms are mounted on the mounting frame; the rotor wing mechanism comprises a rotor wing and a driving motor; and the rotor wings are obliquely mounted on the mounting frame in the advancing direction of the aircraft. The aircraft not only can take off and land on the water surface, but also can take off and land so as to adapt to multi-scene application. In the whole flight process of the aircraft, the multiple rotor mechanisms on the aircraft are always in a running state and are both vertical take-off and landing lift power and cruise flight thrust power, and compared with a traditional aircraft with a lift and thrust layout, the aircraft is simpler and safer to operate and control flight, and t |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN218519846UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN218519846UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN218519846UU3</originalsourceid><addsrcrecordid>eNrjZLB2zC3IyEzKzC8tVihLLSrJTE7MUShJzE7VzU9LU0jMS1HIARKZeekKiZlFyUWJaSUKxSVFpcklpUWpPAysaYk5xam8UJqbQcnNNcTZQze1ID8-tbggMTk1L7Uk3tnPyNDC1NDSwsQsNNSYKEUALoswkw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Amphibious vertical take-off and landing aircraft structure</title><source>esp@cenet</source><creator>XIE ENLI</creator><creatorcontrib>XIE ENLI</creatorcontrib><description>The utility model relates to the technical field of flight, in particular to an amphibious vertical take-off and landing aircraft structure which comprises a fuselage, a front wing and an empennage, the fuselage adopts a double-hull structure and is provided with a mounting frame, and a plurality of rotor wing mechanisms are mounted on the mounting frame; the rotor wing mechanism comprises a rotor wing and a driving motor; and the rotor wings are obliquely mounted on the mounting frame in the advancing direction of the aircraft. The aircraft not only can take off and land on the water surface, but also can take off and land so as to adapt to multi-scene application. In the whole flight process of the aircraft, the multiple rotor mechanisms on the aircraft are always in a running state and are both vertical take-off and landing lift power and cruise flight thrust power, and compared with a traditional aircraft with a lift and thrust layout, the aircraft is simpler and safer to operate and control flight, and t</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&date=20230224&DB=EPODOC&CC=CN&NR=218519846U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230224&DB=EPODOC&CC=CN&NR=218519846U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>XIE ENLI</creatorcontrib><title>Amphibious vertical take-off and landing aircraft structure</title><description>The utility model relates to the technical field of flight, in particular to an amphibious vertical take-off and landing aircraft structure which comprises a fuselage, a front wing and an empennage, the fuselage adopts a double-hull structure and is provided with a mounting frame, and a plurality of rotor wing mechanisms are mounted on the mounting frame; the rotor wing mechanism comprises a rotor wing and a driving motor; and the rotor wings are obliquely mounted on the mounting frame in the advancing direction of the aircraft. The aircraft not only can take off and land on the water surface, but also can take off and land so as to adapt to multi-scene application. In the whole flight process of the aircraft, the multiple rotor mechanisms on the aircraft are always in a running state and are both vertical take-off and landing lift power and cruise flight thrust power, and compared with a traditional aircraft with a lift and thrust layout, the aircraft is simpler and safer to operate and control flight, and t</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>eNrjZLB2zC3IyEzKzC8tVihLLSrJTE7MUShJzE7VzU9LU0jMS1HIARKZeekKiZlFyUWJaSUKxSVFpcklpUWpPAysaYk5xam8UJqbQcnNNcTZQze1ID8-tbggMTk1L7Uk3tnPyNDC1NDSwsQsNNSYKEUALoswkw</recordid><startdate>20230224</startdate><enddate>20230224</enddate><creator>XIE ENLI</creator><scope>EVB</scope></search><sort><creationdate>20230224</creationdate><title>Amphibious vertical take-off and landing aircraft structure</title><author>XIE ENLI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN218519846UU3</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>XIE ENLI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>XIE ENLI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Amphibious vertical take-off and landing aircraft structure</title><date>2023-02-24</date><risdate>2023</risdate><abstract>The utility model relates to the technical field of flight, in particular to an amphibious vertical take-off and landing aircraft structure which comprises a fuselage, a front wing and an empennage, the fuselage adopts a double-hull structure and is provided with a mounting frame, and a plurality of rotor wing mechanisms are mounted on the mounting frame; the rotor wing mechanism comprises a rotor wing and a driving motor; and the rotor wings are obliquely mounted on the mounting frame in the advancing direction of the aircraft. The aircraft not only can take off and land on the water surface, but also can take off and land so as to adapt to multi-scene application. In the whole flight process of the aircraft, the multiple rotor mechanisms on the aircraft are always in a running state and are both vertical take-off and landing lift power and cruise flight thrust power, and compared with a traditional aircraft with a lift and thrust layout, the aircraft is simpler and safer to operate and control flight, and t</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN218519846UU |
| source | esp@cenet |
| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | Amphibious vertical take-off and landing aircraft structure |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-29T15%3A53%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=XIE%20ENLI&rft.date=2023-02-24&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN218519846UU%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 |