INTERCHANGEABLE JOINT CONCEPT FOR AN AIRCRAFT REAR FUSELAGE CONE
Rear fuselage of an aircraft comprising a tail cone end and a rest of the real fuselage whereby the tail cone end is attached to the rest of the rear fuselage by means of an attachment system comprising a balancer fitting, three lugs and a waiting link. When there is a failure in one of the lugs, th...
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| creator | PINA LOPEZ JOSE MARIA SANZ MARTINEZ PABLO TIMOTEO |
| description | Rear fuselage of an aircraft comprising a tail cone end and a rest of the real fuselage whereby the tail cone end is attached to the rest of the rear fuselage by means of an attachment system comprising a balancer fitting, three lugs and a waiting link. When there is a failure in one of the lugs, the balancer fitting acts supporting loads in the transversal direction of the aircraft. The waiting link only acts if a failure in other link occurs. This waiting link is able to support loads in the longitudinal direction of the aircraft. |
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When there is a failure in one of the lugs, the balancer fitting acts supporting loads in the transversal direction of the aircraft. The waiting link only acts if a failure in other link occurs. This waiting link is able to support loads in the longitudinal direction of the aircraft.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COMBINED OPERATIONS ; COSMONAUTICS ; HELICOPTERS ; MACHINE TOOLS ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; OTHER WORKING OF METAL ; PERFORMING OPERATIONS ; TRANSPORTING ; UNIVERSAL MACHINE TOOLS</subject><creationdate>2012</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=20120412&DB=EPODOC&CC=US&NR=2012085866A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20120412&DB=EPODOC&CC=US&NR=2012085866A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PINA LOPEZ JOSE MARIA</creatorcontrib><creatorcontrib>SANZ MARTINEZ PABLO TIMOTEO</creatorcontrib><title>INTERCHANGEABLE JOINT CONCEPT FOR AN AIRCRAFT REAR FUSELAGE CONE</title><description>Rear fuselage of an aircraft comprising a tail cone end and a rest of the real fuselage whereby the tail cone end is attached to the rest of the rear fuselage by means of an attachment system comprising a balancer fitting, three lugs and a waiting link. 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This waiting link is able to support loads in the longitudinal direction of the aircraft.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COMBINED OPERATIONS</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>MACHINE TOOLS</subject><subject>METAL-WORKING NOT OTHERWISE PROVIDED FOR</subject><subject>OTHER WORKING OF METAL</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>UNIVERSAL MACHINE TOOLS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHDw9AtxDXL2cPRzd3V08nFV8PIHiig4-_s5uwaEKLj5Byk4-ik4egY5Bzm6hSgEuToGKbiFBrv6OLq7glS58jCwpiXmFKfyQmluBmU31xBnD93Ugvz41OKCxOTUvNSS-NBgIwNDIwMLUwszM0dDY-JUAQA1IitQ</recordid><startdate>20120412</startdate><enddate>20120412</enddate><creator>PINA LOPEZ JOSE MARIA</creator><creator>SANZ MARTINEZ PABLO TIMOTEO</creator><scope>EVB</scope></search><sort><creationdate>20120412</creationdate><title>INTERCHANGEABLE JOINT CONCEPT FOR AN AIRCRAFT REAR FUSELAGE CONE</title><author>PINA LOPEZ JOSE MARIA ; SANZ MARTINEZ PABLO TIMOTEO</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2012085866A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2012</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COMBINED OPERATIONS</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>MACHINE TOOLS</topic><topic>METAL-WORKING NOT OTHERWISE PROVIDED FOR</topic><topic>OTHER WORKING OF METAL</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>UNIVERSAL MACHINE TOOLS</topic><toplevel>online_resources</toplevel><creatorcontrib>PINA LOPEZ JOSE MARIA</creatorcontrib><creatorcontrib>SANZ MARTINEZ PABLO TIMOTEO</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PINA LOPEZ JOSE MARIA</au><au>SANZ MARTINEZ PABLO TIMOTEO</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>INTERCHANGEABLE JOINT CONCEPT FOR AN AIRCRAFT REAR FUSELAGE CONE</title><date>2012-04-12</date><risdate>2012</risdate><abstract>Rear fuselage of an aircraft comprising a tail cone end and a rest of the real fuselage whereby the tail cone end is attached to the rest of the rear fuselage by means of an attachment system comprising a balancer fitting, three lugs and a waiting link. When there is a failure in one of the lugs, the balancer fitting acts supporting loads in the transversal direction of the aircraft. The waiting link only acts if a failure in other link occurs. This waiting link is able to support loads in the longitudinal direction of the aircraft.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT AVIATION COMBINED OPERATIONS COSMONAUTICS HELICOPTERS MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR OTHER WORKING OF METAL PERFORMING OPERATIONS TRANSPORTING UNIVERSAL MACHINE TOOLS |
| title | INTERCHANGEABLE JOINT CONCEPT FOR AN AIRCRAFT REAR FUSELAGE CONE |
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