Unmanned aerial vehicle comprehensive test platform
The utility model discloses an unmanned aerial vehicle comprehensive test platform comprising an external pedestal, an outer ring, an inner ring, a fixed support and a control device, the fixed support is used for being connected with an unmanned aerial vehicle, two ends of the fixed support are ins...
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| creator | LI BINGFENG WANG JINSHA ZHOU QI MO LIANGJUN HUANG XINSHEN ZHANG ZHENKUN WU ZHENG LI HAO FAN WENYAN LIANG MING |
| description | The utility model discloses an unmanned aerial vehicle comprehensive test platform comprising an external pedestal, an outer ring, an inner ring, a fixed support and a control device, the fixed support is used for being connected with an unmanned aerial vehicle, two ends of the fixed support are installed in the inner ring through a first rotating shaft, and two ends of the inner ring are installed in the outer ring through a second rotating shaft. The two ends of the outer ring are installed in the outer base through third rotating shafts, the fixing support can rotate around the first rotating shaft, the inner ring can rotate around the second rotating shaft, the outer ring can rotate around the third rotating shaft, and the first rotating shaft, the second rotating shaft and the third rotating shaft are in a three-axis orthogonal relation in space. Angle sensors are mounted on the first rotating shaft, the second rotating shaft and the third rotating shaft; and each angle sensor iselectrically connected wi |
| format | Patent |
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The two ends of the outer ring are installed in the outer base through third rotating shafts, the fixing support can rotate around the first rotating shaft, the inner ring can rotate around the second rotating shaft, the outer ring can rotate around the third rotating shaft, and the first rotating shaft, the second rotating shaft and the third rotating shaft are in a three-axis orthogonal relation in space. Angle sensors are mounted on the first rotating shaft, the second rotating shaft and the third rotating shaft; and each angle sensor iselectrically connected wi</description><language>chi ; eng</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2020</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=20201103&DB=EPODOC&CC=CN&NR=211844950U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20201103&DB=EPODOC&CC=CN&NR=211844950U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LI BINGFENG</creatorcontrib><creatorcontrib>WANG JINSHA</creatorcontrib><creatorcontrib>ZHOU QI</creatorcontrib><creatorcontrib>MO LIANGJUN</creatorcontrib><creatorcontrib>HUANG XINSHEN</creatorcontrib><creatorcontrib>ZHANG ZHENKUN</creatorcontrib><creatorcontrib>WU ZHENG</creatorcontrib><creatorcontrib>LI HAO</creatorcontrib><creatorcontrib>FAN WENYAN</creatorcontrib><creatorcontrib>LIANG MING</creatorcontrib><title>Unmanned aerial vehicle comprehensive test platform</title><description>The utility model discloses an unmanned aerial vehicle comprehensive test platform comprising an external pedestal, an outer ring, an inner ring, a fixed support and a control device, the fixed support is used for being connected with an unmanned aerial vehicle, two ends of the fixed support are installed in the inner ring through a first rotating shaft, and two ends of the inner ring are installed in the outer ring through a second rotating shaft. The two ends of the outer ring are installed in the outer base through third rotating shafts, the fixing support can rotate around the first rotating shaft, the inner ring can rotate around the second rotating shaft, the outer ring can rotate around the third rotating shaft, and the first rotating shaft, the second rotating shaft and the third rotating shaft are in a three-axis orthogonal relation in space. Angle sensors are mounted on the first rotating shaft, the second rotating shaft and the third rotating shaft; and each angle sensor iselectrically connected wi</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAOzctNzMtLTVFITC3KTMxRKEvNyEzOSVVIzs8tKErNSM0rzixLVShJLS5RKMhJLEnLL8rlYWBNS8wpTuWF0twMSm6uIc4euqkF-fGpxQWJyal5qSXxzn5GhoYWJiaWpgahocZEKQIAiuMtsw</recordid><startdate>20201103</startdate><enddate>20201103</enddate><creator>LI BINGFENG</creator><creator>WANG JINSHA</creator><creator>ZHOU QI</creator><creator>MO LIANGJUN</creator><creator>HUANG XINSHEN</creator><creator>ZHANG ZHENKUN</creator><creator>WU ZHENG</creator><creator>LI HAO</creator><creator>FAN WENYAN</creator><creator>LIANG MING</creator><scope>EVB</scope></search><sort><creationdate>20201103</creationdate><title>Unmanned aerial vehicle comprehensive test platform</title><author>LI BINGFENG ; WANG JINSHA ; ZHOU QI ; MO LIANGJUN ; HUANG XINSHEN ; ZHANG ZHENKUN ; WU ZHENG ; LI HAO ; FAN WENYAN ; LIANG MING</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN211844950UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2020</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>LI BINGFENG</creatorcontrib><creatorcontrib>WANG JINSHA</creatorcontrib><creatorcontrib>ZHOU QI</creatorcontrib><creatorcontrib>MO LIANGJUN</creatorcontrib><creatorcontrib>HUANG XINSHEN</creatorcontrib><creatorcontrib>ZHANG ZHENKUN</creatorcontrib><creatorcontrib>WU ZHENG</creatorcontrib><creatorcontrib>LI HAO</creatorcontrib><creatorcontrib>FAN WENYAN</creatorcontrib><creatorcontrib>LIANG MING</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LI BINGFENG</au><au>WANG JINSHA</au><au>ZHOU QI</au><au>MO LIANGJUN</au><au>HUANG XINSHEN</au><au>ZHANG ZHENKUN</au><au>WU ZHENG</au><au>LI HAO</au><au>FAN WENYAN</au><au>LIANG MING</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle comprehensive test platform</title><date>2020-11-03</date><risdate>2020</risdate><abstract>The utility model discloses an unmanned aerial vehicle comprehensive test platform comprising an external pedestal, an outer ring, an inner ring, a fixed support and a control device, the fixed support is used for being connected with an unmanned aerial vehicle, two ends of the fixed support are installed in the inner ring through a first rotating shaft, and two ends of the inner ring are installed in the outer ring through a second rotating shaft. The two ends of the outer ring are installed in the outer base through third rotating shafts, the fixing support can rotate around the first rotating shaft, the inner ring can rotate around the second rotating shaft, the outer ring can rotate around the third rotating shaft, and the first rotating shaft, the second rotating shaft and the third rotating shaft are in a three-axis orthogonal relation in space. Angle sensors are mounted on the first rotating shaft, the second rotating shaft and the third rotating shaft; and each angle sensor iselectrically connected wi</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS TRANSPORTING |
| title | Unmanned aerial vehicle comprehensive test platform |
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