METHOD OF ASSEMBLY OF FLYING VEHICLE STRUCTURAL MEMBERS
FIELD: aviation; methods of assembly of wing outer panels. SUBSTANCE: simultaneously at pressing off the upper skin by means of pressing-off devices 4, members of longitudinal framework 6 secured on this skin and sealed up at joint area are pressed off. EFFECT: reduction of time required for assembl...
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; rus |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | Tsvetkov E.A Sedov A.D Mishin V.I |
| description | FIELD: aviation; methods of assembly of wing outer panels. SUBSTANCE: simultaneously at pressing off the upper skin by means of pressing-off devices 4, members of longitudinal framework 6 secured on this skin and sealed up at joint area are pressed off. EFFECT: reduction of time required for assembly; facilitated procedure and improved quality of coupling jobs. 1 dwg
Изобретение относится к области авиации, а более конкретно к способам сборки консольных частей крыла летательного аппарата. Цель изобретения - сокращение времени, повышение технологичности и качества стыковочных работ. Для этого одновременно с отжатием верхней обшивки с помощью отжимных приспособлений 4 осуществляют отжатие элементов прикрепленного продольного набора 6, закрепленных и загерметизированных на ней в зоне стыка. 1 ил. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_SU1718527A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>SU1718527A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_SU1718527A13</originalsourceid><addsrcrecordid>eNrjZDD3dQ3x8HdR8HdTcAwOdvV18okEsd18Ij393BXCXD08nX1cFYJDgkKdQ0KDHH0UfIFqXIOCeRhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJfHCoobmhhamRuaOhMRFKAPI3KAI</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>METHOD OF ASSEMBLY OF FLYING VEHICLE STRUCTURAL MEMBERS</title><source>esp@cenet</source><creator>Tsvetkov E.A ; Sedov A.D ; Mishin V.I</creator><creatorcontrib>Tsvetkov E.A ; Sedov A.D ; Mishin V.I</creatorcontrib><description>FIELD: aviation; methods of assembly of wing outer panels. SUBSTANCE: simultaneously at pressing off the upper skin by means of pressing-off devices 4, members of longitudinal framework 6 secured on this skin and sealed up at joint area are pressed off. EFFECT: reduction of time required for assembly; facilitated procedure and improved quality of coupling jobs. 1 dwg
Изобретение относится к области авиации, а более конкретно к способам сборки консольных частей крыла летательного аппарата. Цель изобретения - сокращение времени, повышение технологичности и качества стыковочных работ. Для этого одновременно с отжатием верхней обшивки с помощью отжимных приспособлений 4 осуществляют отжатие элементов прикрепленного продольного набора 6, закрепленных и загерметизированных на ней в зоне стыка. 1 ил.</description><language>eng ; rus</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>1997</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=19970120&DB=EPODOC&CC=SU&NR=1718527A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19970120&DB=EPODOC&CC=SU&NR=1718527A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Tsvetkov E.A</creatorcontrib><creatorcontrib>Sedov A.D</creatorcontrib><creatorcontrib>Mishin V.I</creatorcontrib><title>METHOD OF ASSEMBLY OF FLYING VEHICLE STRUCTURAL MEMBERS</title><description>FIELD: aviation; methods of assembly of wing outer panels. SUBSTANCE: simultaneously at pressing off the upper skin by means of pressing-off devices 4, members of longitudinal framework 6 secured on this skin and sealed up at joint area are pressed off. EFFECT: reduction of time required for assembly; facilitated procedure and improved quality of coupling jobs. 1 dwg
Изобретение относится к области авиации, а более конкретно к способам сборки консольных частей крыла летательного аппарата. Цель изобретения - сокращение времени, повышение технологичности и качества стыковочных работ. Для этого одновременно с отжатием верхней обшивки с помощью отжимных приспособлений 4 осуществляют отжатие элементов прикрепленного продольного набора 6, закрепленных и загерметизированных на ней в зоне стыка. 1 ил.</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>1997</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDD3dQ3x8HdR8HdTcAwOdvV18okEsd18Ij393BXCXD08nX1cFYJDgkKdQ0KDHH0UfIFqXIOCeRhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJfHCoobmhhamRuaOhMRFKAPI3KAI</recordid><startdate>19970120</startdate><enddate>19970120</enddate><creator>Tsvetkov E.A</creator><creator>Sedov A.D</creator><creator>Mishin V.I</creator><scope>EVB</scope></search><sort><creationdate>19970120</creationdate><title>METHOD OF ASSEMBLY OF FLYING VEHICLE STRUCTURAL MEMBERS</title><author>Tsvetkov E.A ; Sedov A.D ; Mishin V.I</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_SU1718527A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; rus</language><creationdate>1997</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>Tsvetkov E.A</creatorcontrib><creatorcontrib>Sedov A.D</creatorcontrib><creatorcontrib>Mishin V.I</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Tsvetkov E.A</au><au>Sedov A.D</au><au>Mishin V.I</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD OF ASSEMBLY OF FLYING VEHICLE STRUCTURAL MEMBERS</title><date>1997-01-20</date><risdate>1997</risdate><abstract>FIELD: aviation; methods of assembly of wing outer panels. SUBSTANCE: simultaneously at pressing off the upper skin by means of pressing-off devices 4, members of longitudinal framework 6 secured on this skin and sealed up at joint area are pressed off. EFFECT: reduction of time required for assembly; facilitated procedure and improved quality of coupling jobs. 1 dwg
Изобретение относится к области авиации, а более конкретно к способам сборки консольных частей крыла летательного аппарата. Цель изобретения - сокращение времени, повышение технологичности и качества стыковочных работ. Для этого одновременно с отжатием верхней обшивки с помощью отжимных приспособлений 4 осуществляют отжатие элементов прикрепленного продольного набора 6, закрепленных и загерметизированных на ней в зоне стыка. 1 ил.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; rus |
| recordid | cdi_epo_espacenet_SU1718527A1 |
| source | esp@cenet |
| 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 | METHOD OF ASSEMBLY OF FLYING VEHICLE STRUCTURAL MEMBERS |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-13T06%3A24%3A01IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Tsvetkov%20E.A&rft.date=1997-01-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ESU1718527A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |