Loading unmanned aerial vehicle
The invention belongs to the technical field of unmanned aerial vehicle equipment, particularly relates to a loading unmanned aerial vehicle, and aims to solve the problems that an existing unmanned aerial vehicle cannot clamp an object during loading, so that the object shakes in the flying process...
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| creator | LU RUNTIAN CHI YANCAO YU DENGXIU |
| description | The invention belongs to the technical field of unmanned aerial vehicle equipment, particularly relates to a loading unmanned aerial vehicle, and aims to solve the problems that an existing unmanned aerial vehicle cannot clamp an object during loading, so that the object shakes in the flying process of the unmanned aerial vehicle, and due to the fact that the mass of the object is relatively heavy, when the unmanned aerial vehicle falls, if the ground is not level, the vehicle easily rolls over and damages. In order to solve the problem, the following scheme is provided that the unmanned aerial vehicle comprises a vehicle body, two symmetrically-arranged take-off devices are fixedly installed on the two sides of the vehicle body a loading box is fixedly installed at the bottom of the fuselage, and a fixing cavity is formed in the loading box; and the two symmetrically-arranged fixing grooves are formed in the inner wall of the bottom of the fixing cavity, the same fixing rod is fixedly mounted on the inner wa |
| format | Patent |
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In order to solve the problem, the following scheme is provided that the unmanned aerial vehicle comprises a vehicle body, two symmetrically-arranged take-off devices are fixedly installed on the two sides of the vehicle body a loading box is fixedly installed at the bottom of the fuselage, and a fixing cavity is formed in the loading box; and the two symmetrically-arranged fixing grooves are formed in the inner wall of the bottom of the fixing cavity, the same fixing rod is fixedly mounted on the inner wa</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; PARACHUTES ; 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&date=20210514&DB=EPODOC&CC=CN&NR=112793791A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210514&DB=EPODOC&CC=CN&NR=112793791A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LU RUNTIAN</creatorcontrib><creatorcontrib>CHI YANCAO</creatorcontrib><creatorcontrib>YU DENGXIU</creatorcontrib><title>Loading unmanned aerial vehicle</title><description>The invention belongs to the technical field of unmanned aerial vehicle equipment, particularly relates to a loading unmanned aerial vehicle, and aims to solve the problems that an existing unmanned aerial vehicle cannot clamp an object during loading, so that the object shakes in the flying process of the unmanned aerial vehicle, and due to the fact that the mass of the object is relatively heavy, when the unmanned aerial vehicle falls, if the ground is not level, the vehicle easily rolls over and damages. In order to solve the problem, the following scheme is provided that the unmanned aerial vehicle comprises a vehicle body, two symmetrically-arranged take-off devices are fixedly installed on the two sides of the vehicle body a loading box is fixedly installed at the bottom of the fuselage, and a fixing cavity is formed in the loading box; and the two symmetrically-arranged fixing grooves are formed in the inner wall of the bottom of the fixing cavity, the same fixing rod is fixedly mounted on the inner wa</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJD3yU9MycxLVyjNy03My0tNUUhMLcpMzFEoS83ITM5J5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hoZG5pbG5paGjsbEqAEAHf8k2A</recordid><startdate>20210514</startdate><enddate>20210514</enddate><creator>LU RUNTIAN</creator><creator>CHI YANCAO</creator><creator>YU DENGXIU</creator><scope>EVB</scope></search><sort><creationdate>20210514</creationdate><title>Loading unmanned aerial vehicle</title><author>LU RUNTIAN ; CHI YANCAO ; YU DENGXIU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112793791A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>LU RUNTIAN</creatorcontrib><creatorcontrib>CHI YANCAO</creatorcontrib><creatorcontrib>YU DENGXIU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LU RUNTIAN</au><au>CHI YANCAO</au><au>YU DENGXIU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Loading unmanned aerial vehicle</title><date>2021-05-14</date><risdate>2021</risdate><abstract>The invention belongs to the technical field of unmanned aerial vehicle equipment, particularly relates to a loading unmanned aerial vehicle, and aims to solve the problems that an existing unmanned aerial vehicle cannot clamp an object during loading, so that the object shakes in the flying process of the unmanned aerial vehicle, and due to the fact that the mass of the object is relatively heavy, when the unmanned aerial vehicle falls, if the ground is not level, the vehicle easily rolls over and damages. In order to solve the problem, the following scheme is provided that the unmanned aerial vehicle comprises a vehicle body, two symmetrically-arranged take-off devices are fixedly installed on the two sides of the vehicle body a loading box is fixedly installed at the bottom of the fuselage, and a fixing cavity is formed in the loading box; and the two symmetrically-arranged fixing grooves are formed in the inner wall of the bottom of the fixing cavity, the same fixing rod is fixedly mounted on the inner wa</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | Loading unmanned aerial vehicle |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-30T04%3A30%3A00IST&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=LU%20RUNTIAN&rft.date=2021-05-14&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN112793791A%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 |