Guided missile supporting and fixing mechanism with variable diameter and variable supporting spacing
The invention relates to a missile supporting and fixing mechanism with the variable diameter and the variable supporting distance, in particular to a missile supporting and fixing mechanism capable of being self-adaptive to different diameters and different supporting distances. A missile supportin...
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| creator | YUAN SUJIAO WANG WU WU KUNYING CHEN MINGFAN XIONG ZHIYAN LI YONGGUAN LI XINWU SUN YONGDUO FANG YUAN ZHANG YI ZHANG HONGYU LIU CHAOHONG ZHANG WEI PI WENBIAO ZOU ZHIQIANG |
| description | The invention relates to a missile supporting and fixing mechanism with the variable diameter and the variable supporting distance, in particular to a missile supporting and fixing mechanism capable of being self-adaptive to different diameters and different supporting distances. A missile supporting and fixing mechanism with the variable diameter and the variable supporting distance comprises a supporting distance adjusting unit and a supporting diameter changing unit. The support spacing adjusting unit comprises a guide rail, a bracket and a locking part; the supporting diameter changing unit comprises a supporting part and a telescopic adjusting part; the telescopic adjusting part is mounted on the bracket; during use, the relative position of the telescopic adjusting part and the bracket is adjusted, and then the relative distance between the two supporting blocks is changed. The invention has the following advantages: 1, guided missiles with different diameters are supported and fixed; 2, guided missiles |
| format | Patent |
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A missile supporting and fixing mechanism with the variable diameter and the variable supporting distance comprises a supporting distance adjusting unit and a supporting diameter changing unit. The support spacing adjusting unit comprises a guide rail, a bracket and a locking part; the supporting diameter changing unit comprises a supporting part and a telescopic adjusting part; the telescopic adjusting part is mounted on the bracket; during use, the relative position of the telescopic adjusting part and the bracket is adjusted, and then the relative distance between the two supporting blocks is changed. 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A missile supporting and fixing mechanism with the variable diameter and the variable supporting distance comprises a supporting distance adjusting unit and a supporting diameter changing unit. The support spacing adjusting unit comprises a guide rail, a bracket and a locking part; the supporting diameter changing unit comprises a supporting part and a telescopic adjusting part; the telescopic adjusting part is mounted on the bracket; during use, the relative position of the telescopic adjusting part and the bracket is adjusted, and then the relative distance between the two supporting blocks is changed. The invention has the following advantages: 1, guided missiles with different diameters are supported and fixed; 2, guided missiles</description><subject>AMMUNITION</subject><subject>BLASTING</subject><subject>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZEh1L81MSU1RyM0sLs7MSVUoLi0oyC8qycxLV0jMS1FIy6wAMXNTkzMS8zKLcxXKM0syFMoSizITk4CqUzITc1NLUovAauGiSGYUFyQmA2keBta0xJziVF4ozc2g6OYa4uyhm1qQH58KUpSal1oS7-xnaGhqYGZgaGTqaEyMGgB_qz_M</recordid><startdate>20220916</startdate><enddate>20220916</enddate><creator>YUAN SUJIAO</creator><creator>WANG WU</creator><creator>WU KUNYING</creator><creator>CHEN MINGFAN</creator><creator>XIONG ZHIYAN</creator><creator>LI YONGGUAN</creator><creator>LI XINWU</creator><creator>SUN YONGDUO</creator><creator>FANG YUAN</creator><creator>ZHANG YI</creator><creator>ZHANG HONGYU</creator><creator>LIU CHAOHONG</creator><creator>ZHANG WEI</creator><creator>PI WENBIAO</creator><creator>ZOU ZHIQIANG</creator><scope>EVB</scope></search><sort><creationdate>20220916</creationdate><title>Guided missile supporting and fixing mechanism with variable diameter and variable supporting spacing</title><author>YUAN SUJIAO ; WANG WU ; WU KUNYING ; CHEN MINGFAN ; XIONG ZHIYAN ; LI YONGGUAN ; LI XINWU ; SUN YONGDUO ; FANG YUAN ; ZHANG YI ; ZHANG HONGYU ; LIU CHAOHONG ; ZHANG WEI ; PI WENBIAO ; ZOU ZHIQIANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN115060125A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>AMMUNITION</topic><topic>BLASTING</topic><topic>EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>YUAN SUJIAO</creatorcontrib><creatorcontrib>WANG WU</creatorcontrib><creatorcontrib>WU KUNYING</creatorcontrib><creatorcontrib>CHEN MINGFAN</creatorcontrib><creatorcontrib>XIONG ZHIYAN</creatorcontrib><creatorcontrib>LI YONGGUAN</creatorcontrib><creatorcontrib>LI XINWU</creatorcontrib><creatorcontrib>SUN YONGDUO</creatorcontrib><creatorcontrib>FANG YUAN</creatorcontrib><creatorcontrib>ZHANG YI</creatorcontrib><creatorcontrib>ZHANG HONGYU</creatorcontrib><creatorcontrib>LIU CHAOHONG</creatorcontrib><creatorcontrib>ZHANG WEI</creatorcontrib><creatorcontrib>PI WENBIAO</creatorcontrib><creatorcontrib>ZOU ZHIQIANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YUAN SUJIAO</au><au>WANG WU</au><au>WU KUNYING</au><au>CHEN MINGFAN</au><au>XIONG ZHIYAN</au><au>LI YONGGUAN</au><au>LI XINWU</au><au>SUN YONGDUO</au><au>FANG YUAN</au><au>ZHANG YI</au><au>ZHANG HONGYU</au><au>LIU CHAOHONG</au><au>ZHANG WEI</au><au>PI WENBIAO</au><au>ZOU ZHIQIANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Guided missile supporting and fixing mechanism with variable diameter and variable supporting spacing</title><date>2022-09-16</date><risdate>2022</risdate><abstract>The invention relates to a missile supporting and fixing mechanism with the variable diameter and the variable supporting distance, in particular to a missile supporting and fixing mechanism capable of being self-adaptive to different diameters and different supporting distances. A missile supporting and fixing mechanism with the variable diameter and the variable supporting distance comprises a supporting distance adjusting unit and a supporting diameter changing unit. The support spacing adjusting unit comprises a guide rail, a bracket and a locking part; the supporting diameter changing unit comprises a supporting part and a telescopic adjusting part; the telescopic adjusting part is mounted on the bracket; during use, the relative position of the telescopic adjusting part and the bracket is adjusted, and then the relative distance between the two supporting blocks is changed. The invention has the following advantages: 1, guided missiles with different diameters are supported and fixed; 2, guided missiles</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | Guided missile supporting and fixing mechanism with variable diameter and variable supporting spacing |
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