Rocket launching unmanned aerial vehicle thrust line measuring device
The utility model relates to an unmanned aerial vehicle measuring device, in particular to a rocket launching unmanned aerial vehicle thrust line measuring device. The technical problems that an existing rocket launching unmanned aerial vehicle thrust line measuring device is inconvenient to measure...
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| creator | LI DAJIAN LI DEGENG LI ZECHEN FENG YANGJIAN WANG QIANG WANG GUOFEI HUANG CHI |
| description | The utility model relates to an unmanned aerial vehicle measuring device, in particular to a rocket launching unmanned aerial vehicle thrust line measuring device. The technical problems that an existing rocket launching unmanned aerial vehicle thrust line measuring device is inconvenient to measure and low in measuring efficiency and measuring precision are solved. The technical solution of the utility model is as follows: the technical solution of the utility model is as follows; the utility model discloses a rocket launching unmanned aerial vehicle thrust line measuring device. Upper steelwire rope, the thrust bearing connecting rod is axially and fixedly connected with the upper steel wire rope; the thrust bearing connecting sleeve is sleeved outside the thrust bearing connecting rod;the thrust bearing is arranged between the thrust bearing connecting rod and the thrust bearing connecting sleeve; wherein one end of the lower steel wire rope is connected with the thrust bearing connecting sleeve, the other |
| format | Patent |
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The technical problems that an existing rocket launching unmanned aerial vehicle thrust line measuring device is inconvenient to measure and low in measuring efficiency and measuring precision are solved. The technical solution of the utility model is as follows: the technical solution of the utility model is as follows; the utility model discloses a rocket launching unmanned aerial vehicle thrust line measuring device. Upper steelwire rope, the thrust bearing connecting rod is axially and fixedly connected with the upper steel wire rope; the thrust bearing connecting sleeve is sleeved outside the thrust bearing connecting rod;the thrust bearing is arranged between the thrust bearing connecting rod and the thrust bearing connecting sleeve; wherein one end of the lower steel wire rope is connected with the thrust bearing connecting sleeve, the other</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>2019</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=20191112&DB=EPODOC&CC=CN&NR=209617539U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191112&DB=EPODOC&CC=CN&NR=209617539U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LI DAJIAN</creatorcontrib><creatorcontrib>LI DEGENG</creatorcontrib><creatorcontrib>LI ZECHEN</creatorcontrib><creatorcontrib>FENG YANGJIAN</creatorcontrib><creatorcontrib>WANG QIANG</creatorcontrib><creatorcontrib>WANG GUOFEI</creatorcontrib><creatorcontrib>HUANG CHI</creatorcontrib><title>Rocket launching unmanned aerial vehicle thrust line measuring device</title><description>The utility model relates to an unmanned aerial vehicle measuring device, in particular to a rocket launching unmanned aerial vehicle thrust line measuring device. 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Upper steelwire rope, the thrust bearing connecting rod is axially and fixedly connected with the upper steel wire rope; the thrust bearing connecting sleeve is sleeved outside the thrust bearing connecting rod;the thrust bearing is arranged between the thrust bearing connecting rod and the thrust bearing connecting sleeve; wherein one end of the lower steel wire rope is connected with the thrust bearing connecting sleeve, the other</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyj0KwkAQBtBtLES9w2AvqEEldYhYWYipwzD5dBc3k7A_Ob8KHsDqNW9u6tsgLyTynFWs0ydl7VkVHTGCY08TrBMPSjbk-IlOQT045vDdHSYnWJrZg33E6ufCrM_1vbpsMA4t4sgCRWqr635bHnenQ1E2TfFXegOHzzRm</recordid><startdate>20191112</startdate><enddate>20191112</enddate><creator>LI DAJIAN</creator><creator>LI DEGENG</creator><creator>LI ZECHEN</creator><creator>FENG YANGJIAN</creator><creator>WANG QIANG</creator><creator>WANG GUOFEI</creator><creator>HUANG CHI</creator><scope>EVB</scope></search><sort><creationdate>20191112</creationdate><title>Rocket launching unmanned aerial vehicle thrust line measuring device</title><author>LI DAJIAN ; LI DEGENG ; LI ZECHEN ; FENG YANGJIAN ; WANG QIANG ; WANG GUOFEI ; HUANG CHI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN209617539UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2019</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 DAJIAN</creatorcontrib><creatorcontrib>LI DEGENG</creatorcontrib><creatorcontrib>LI ZECHEN</creatorcontrib><creatorcontrib>FENG YANGJIAN</creatorcontrib><creatorcontrib>WANG QIANG</creatorcontrib><creatorcontrib>WANG GUOFEI</creatorcontrib><creatorcontrib>HUANG CHI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LI DAJIAN</au><au>LI DEGENG</au><au>LI ZECHEN</au><au>FENG YANGJIAN</au><au>WANG QIANG</au><au>WANG GUOFEI</au><au>HUANG CHI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Rocket launching unmanned aerial vehicle thrust line measuring device</title><date>2019-11-12</date><risdate>2019</risdate><abstract>The utility model relates to an unmanned aerial vehicle measuring device, in particular to a rocket launching unmanned aerial vehicle thrust line measuring device. The technical problems that an existing rocket launching unmanned aerial vehicle thrust line measuring device is inconvenient to measure and low in measuring efficiency and measuring precision are solved. The technical solution of the utility model is as follows: the technical solution of the utility model is as follows; the utility model discloses a rocket launching unmanned aerial vehicle thrust line measuring device. Upper steelwire rope, the thrust bearing connecting rod is axially and fixedly connected with the upper steel wire rope; the thrust bearing connecting sleeve is sleeved outside the thrust bearing connecting rod;the thrust bearing is arranged between the thrust bearing connecting rod and the thrust bearing connecting sleeve; wherein one end of the lower steel wire rope is connected with the thrust bearing connecting sleeve, the other</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 | Rocket launching unmanned aerial vehicle thrust line measuring device |
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