Unmanned aerial vehicle rocket booster capable of adjusting thrust
The utility model discloses an unmanned aerial vehicle rocket booster capable of adjusting thrust, which comprises a combustion chamber main body, a head part arranged at one end of the combustion chamber main body, a connecting table arranged on the head part, a tail part arranged at the other end...
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| creator | YIN WEIBIN LIU MAOJIN |
| description | The utility model discloses an unmanned aerial vehicle rocket booster capable of adjusting thrust, which comprises a combustion chamber main body, a head part arranged at one end of the combustion chamber main body, a connecting table arranged on the head part, a tail part arranged at the other end of the combustion chamber main body and a spray pipe arranged on the tail part, the head part is connected with the connecting end through a first connecting part, the tail part is connected with the connecting end through a second connecting part, and threaded connecting mechanisms matched with the head part, the tail part and the connecting end are arranged in the first connecting part and the second connecting part. The connecting end, the head portion and the tail portion can be conveniently mounted and dismounted, then propellant grains in the combustion chamber body can be conveniently mounted and dismounted, the propellant grains located on the same radius can be conveniently and integrally dismounted throug |
| format | Patent |
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The connecting end, the head portion and the tail portion can be conveniently mounted and dismounted, then propellant grains in the combustion chamber body can be conveniently mounted and dismounted, the propellant grains located on the same radius can be conveniently and integrally dismounted throug</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>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=20230630&DB=EPODOC&CC=CN&NR=219277836U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230630&DB=EPODOC&CC=CN&NR=219277836U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YIN WEIBIN</creatorcontrib><creatorcontrib>LIU MAOJIN</creatorcontrib><title>Unmanned aerial vehicle rocket booster capable of adjusting thrust</title><description>The utility model discloses an unmanned aerial vehicle rocket booster capable of adjusting thrust, which comprises a combustion chamber main body, a head part arranged at one end of the combustion chamber main body, a connecting table arranged on the head part, a tail part arranged at the other end of the combustion chamber main body and a spray pipe arranged on the tail part, the head part is connected with the connecting end through a first connecting part, the tail part is connected with the connecting end through a second connecting part, and threaded connecting mechanisms matched with the head part, the tail part and the connecting end are arranged in the first connecting part and the second connecting part. The connecting end, the head portion and the tail portion can be conveniently mounted and dismounted, then propellant grains in the combustion chamber body can be conveniently mounted and dismounted, the propellant grains located on the same radius can be conveniently and integrally dismounted throug</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>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAKzctNzMtLTVFITC3KTMxRKEvNyEzOSVUoyk_OTi1RSMrPLy5JLVJITixITAIK56cpJKZklRaXZOalK5RkFAFZPAysaYk5xam8UJqbQcnNNcTZQze1ID8-tbggMTk1L7Uk3tnPyNDSyNzcwtgsNNSYKEUAwYIzMQ</recordid><startdate>20230630</startdate><enddate>20230630</enddate><creator>YIN WEIBIN</creator><creator>LIU MAOJIN</creator><scope>EVB</scope></search><sort><creationdate>20230630</creationdate><title>Unmanned aerial vehicle rocket booster capable of adjusting thrust</title><author>YIN WEIBIN ; LIU MAOJIN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN219277836UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</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>YIN WEIBIN</creatorcontrib><creatorcontrib>LIU MAOJIN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YIN WEIBIN</au><au>LIU MAOJIN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Unmanned aerial vehicle rocket booster capable of adjusting thrust</title><date>2023-06-30</date><risdate>2023</risdate><abstract>The utility model discloses an unmanned aerial vehicle rocket booster capable of adjusting thrust, which comprises a combustion chamber main body, a head part arranged at one end of the combustion chamber main body, a connecting table arranged on the head part, a tail part arranged at the other end of the combustion chamber main body and a spray pipe arranged on the tail part, the head part is connected with the connecting end through a first connecting part, the tail part is connected with the connecting end through a second connecting part, and threaded connecting mechanisms matched with the head part, the tail part and the connecting end are arranged in the first connecting part and the second connecting part. The connecting end, the head portion and the tail portion can be conveniently mounted and dismounted, then propellant grains in the combustion chamber body can be conveniently mounted and dismounted, the propellant grains located on the same radius can be conveniently and integrally dismounted throug</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 rocket booster capable of adjusting thrust |
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