Skin hedging compression experiment device for aeronautical part test
The utility model relates to the technical field of aeronautical part experiments, in particular to a skin hedging compression experiment device for aeronautical part tests, which comprises a base and a fixing device, an impact testing device is mounted at the upper end of the base, a supporting pla...
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| creator | FENG BINGKANG ZHAO XIAOYAN WANG LIN |
| description | The utility model relates to the technical field of aeronautical part experiments, in particular to a skin hedging compression experiment device for aeronautical part tests, which comprises a base and a fixing device, an impact testing device is mounted at the upper end of the base, a supporting platform is fixedly connected to the upper end of the base, limiting grooves are formed in two ends of the supporting platform, and the fixing device is fixedly connected with the supporting platform. A connecting block is arranged in the limiting groove, the fixing device comprises a mounting plate, the mounting plate is fixedly connected to the end, located on the outer side of the limiting groove, of the connecting block, and a threaded column is arranged at the upper end of the mounting plate, so that the elastic self-adaptive force of the contact surface of one side of a limiting baffle and the skin is increased, and the buffering performance on the surface of the skin is increased; and then the threaded column i |
| format | Patent |
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A connecting block is arranged in the limiting groove, the fixing device comprises a mounting plate, the mounting plate is fixedly connected to the end, located on the outer side of the limiting groove, of the connecting block, and a threaded column is arranged at the upper end of the mounting plate, so that the elastic self-adaptive force of the contact surface of one side of a limiting baffle and the skin is increased, and the buffering performance on the surface of the skin is increased; and then the threaded column i</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 ; INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES ; MEASURING ; PERFORMING OPERATIONS ; PHYSICS ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR ; 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=20230714&DB=EPODOC&CC=CN&NR=219348130U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230714&DB=EPODOC&CC=CN&NR=219348130U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>FENG BINGKANG</creatorcontrib><creatorcontrib>ZHAO XIAOYAN</creatorcontrib><creatorcontrib>WANG LIN</creatorcontrib><title>Skin hedging compression experiment device for aeronautical part test</title><description>The utility model relates to the technical field of aeronautical part experiments, in particular to a skin hedging compression experiment device for aeronautical part tests, which comprises a base and a fixing device, an impact testing device is mounted at the upper end of the base, a supporting platform is fixedly connected to the upper end of the base, limiting grooves are formed in two ends of the supporting platform, and the fixing device is fixedly connected with the supporting platform. A connecting block is arranged in the limiting groove, the fixing device comprises a mounting plate, the mounting plate is fixedly connected to the end, located on the outer side of the limiting groove, of the connecting block, and a threaded column is arranged at the upper end of the mounting plate, so that the elastic self-adaptive force of the contact surface of one side of a limiting baffle and the skin is increased, and the buffering performance on the surface of the skin is increased; and then the threaded column i</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>INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES</subject><subject>MEASURING</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>TESTING</subject><subject>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</subject><subject>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyjEOgkAQBVAaC6PeYWJvIq6F1gRjZaPUZLJ8YCLMbnZH4_FtPIDVa96yqO9PURrRDaID-TDHhJwlKOETkWSGGnV4iwf1IREjBeWXieeJIicjQ7Z1seh5ytj8XBXbS_2orjvE0CJH9lBYW90O5dkdT6XbN437K30BnZI0gg</recordid><startdate>20230714</startdate><enddate>20230714</enddate><creator>FENG BINGKANG</creator><creator>ZHAO XIAOYAN</creator><creator>WANG LIN</creator><scope>EVB</scope></search><sort><creationdate>20230714</creationdate><title>Skin hedging compression experiment device for aeronautical part test</title><author>FENG BINGKANG ; ZHAO XIAOYAN ; WANG LIN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN219348130UU3</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>INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES</topic><topic>MEASURING</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>TESTING</topic><topic>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</topic><topic>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>FENG BINGKANG</creatorcontrib><creatorcontrib>ZHAO XIAOYAN</creatorcontrib><creatorcontrib>WANG LIN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>FENG BINGKANG</au><au>ZHAO XIAOYAN</au><au>WANG LIN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Skin hedging compression experiment device for aeronautical part test</title><date>2023-07-14</date><risdate>2023</risdate><abstract>The utility model relates to the technical field of aeronautical part experiments, in particular to a skin hedging compression experiment device for aeronautical part tests, which comprises a base and a fixing device, an impact testing device is mounted at the upper end of the base, a supporting platform is fixedly connected to the upper end of the base, limiting grooves are formed in two ends of the supporting platform, and the fixing device is fixedly connected with the supporting platform. A connecting block is arranged in the limiting groove, the fixing device comprises a mounting plate, the mounting plate is fixedly connected to the end, located on the outer side of the limiting groove, of the connecting block, and a threaded column is arranged at the upper end of the mounting plate, so that the elastic self-adaptive force of the contact surface of one side of a limiting baffle and the skin is increased, and the buffering performance on the surface of the skin is increased; and then the threaded column i</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 INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES MEASURING PERFORMING OPERATIONS PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR TRANSPORTING |
| title | Skin hedging compression experiment device for aeronautical part test |
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