JOINT STRUCTURE AND ASSEMBLY METHOD FOR SAME
A joint structure (10) includes a connection member (5) provided between a reinforced member (1) and a reinforcing member (3) and connecting both of them to each other. The connection member (5) includes a first coupling portion (5a) and a second coupling portion (5b) that are coupled to one and ano...
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| creator | AKIMOTO, Toyoharu SHIGENARI, Yu OKUMURA, Ikuo HARADA, Takashi |
| description | A joint structure (10) includes a connection member (5) provided between a reinforced member (1) and a reinforcing member (3) and connecting both of them to each other. The connection member (5) includes a first coupling portion (5a) and a second coupling portion (5b) that are coupled to one and another of the reinforced member (1) and the reinforcing member (3), respectively. The first coupling portion (5a) is coupled to a joint portion (3a) of one of the reinforced member (1) and the reinforcing member (3) by an adhesive (9) or welding. The first coupling portion (5a) and the joint portion (3a) are shaped so as to be caught by each other in a joining direction (D3) in which the reinforced member (1) and the reinforcing member (3) are joined to each other. |
| format | Patent |
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The connection member (5) includes a first coupling portion (5a) and a second coupling portion (5b) that are coupled to one and another of the reinforced member (1) and the reinforcing member (3), respectively. The first coupling portion (5a) is coupled to a joint portion (3a) of one of the reinforced member (1) and the reinforcing member (3) by an adhesive (9) or welding. The first coupling portion (5a) and the joint portion (3a) are shaped so as to be caught by each other in a joining direction (D3) in which the reinforced member (1) and the reinforcing member (3) are joined to each other.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ; ENGINEERING ELEMENTS AND UNITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2022</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=20220216&DB=EPODOC&CC=EP&NR=3954907A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220216&DB=EPODOC&CC=EP&NR=3954907A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>AKIMOTO, Toyoharu</creatorcontrib><creatorcontrib>SHIGENARI, Yu</creatorcontrib><creatorcontrib>OKUMURA, Ikuo</creatorcontrib><creatorcontrib>HARADA, Takashi</creatorcontrib><title>JOINT STRUCTURE AND ASSEMBLY METHOD FOR SAME</title><description>A joint structure (10) includes a connection member (5) provided between a reinforced member (1) and a reinforcing member (3) and connecting both of them to each other. The connection member (5) includes a first coupling portion (5a) and a second coupling portion (5b) that are coupled to one and another of the reinforced member (1) and the reinforcing member (3), respectively. The first coupling portion (5a) is coupled to a joint portion (3a) of one of the reinforced member (1) and the reinforcing member (3) by an adhesive (9) or welding. The first coupling portion (5a) and the joint portion (3a) are shaped so as to be caught by each other in a joining direction (D3) in which the reinforced member (1) and the reinforcing member (3) are joined to each other.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNDx8vf0C1EIDgkKdQ4JDXJVcPRzUXAMDnb1dfKJVPB1DfHwd1Fw8w9SCHb0deVhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcaWpiaWBuaOhsZEKAEAV6ok2w</recordid><startdate>20220216</startdate><enddate>20220216</enddate><creator>AKIMOTO, Toyoharu</creator><creator>SHIGENARI, Yu</creator><creator>OKUMURA, Ikuo</creator><creator>HARADA, Takashi</creator><scope>EVB</scope></search><sort><creationdate>20220216</creationdate><title>JOINT STRUCTURE AND ASSEMBLY METHOD FOR SAME</title><author>AKIMOTO, Toyoharu ; SHIGENARI, Yu ; OKUMURA, Ikuo ; HARADA, Takashi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3954907A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>AKIMOTO, Toyoharu</creatorcontrib><creatorcontrib>SHIGENARI, Yu</creatorcontrib><creatorcontrib>OKUMURA, Ikuo</creatorcontrib><creatorcontrib>HARADA, Takashi</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>AKIMOTO, Toyoharu</au><au>SHIGENARI, Yu</au><au>OKUMURA, Ikuo</au><au>HARADA, Takashi</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>JOINT STRUCTURE AND ASSEMBLY METHOD FOR SAME</title><date>2022-02-16</date><risdate>2022</risdate><abstract>A joint structure (10) includes a connection member (5) provided between a reinforced member (1) and a reinforcing member (3) and connecting both of them to each other. The connection member (5) includes a first coupling portion (5a) and a second coupling portion (5b) that are coupled to one and another of the reinforced member (1) and the reinforcing member (3), respectively. The first coupling portion (5a) is coupled to a joint portion (3a) of one of the reinforced member (1) and the reinforcing member (3) by an adhesive (9) or welding. The first coupling portion (5a) and the joint portion (3a) are shaped so as to be caught by each other in a joining direction (D3) in which the reinforced member (1) and the reinforcing member (3) are joined to each other.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| source | esp@cenet |
| subjects | AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | JOINT STRUCTURE AND ASSEMBLY METHOD FOR SAME |
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