METHOD FOR MANUFACTURING A MULTI-SPAR BOX WITH A CONTINUOUS SKIN UPPER SHELL OF A TAIL CONE SECTION FOR A REAR END OF AN AIRCRAFT AND A COMPOSITE ASSEMBLY
Examples herein relate to a method for manufacturing a composite assembly with a continuous skin for a rear end of an aircraft by obtaining an upper part (405) of the rear end by composite tooling. The upper part comprises a multi-spar vertical tail plane. The spars (410) of the vertical tail plane...
Gespeichert in:
| Hauptverfasser: | , , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre ; ger |
| 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 | CANAS RIOS, Maria, Almudena GARCIA NIETO, Carlos INIESTA LOZANO, Fernando MARTINO-GONZALEZ, Esteban VAZQUEZ CASTRO, Jesus Javier SANCHEZ PEREZ, Melania MENARD, Edouard ARANA HIDALGO, Alberto |
| description | Examples herein relate to a method for manufacturing a composite assembly with a continuous skin for a rear end of an aircraft by obtaining an upper part (405) of the rear end by composite tooling. The upper part comprises a multi-spar vertical tail plane. The spars (410) of the vertical tail plane comprise widening roots that form an upper shell of the rear end and an upper skin (425). Furthermore, a lower part (415) comprises a lower shell of the rear end including semi-complete frames (420) and stringers and a lower skin (430). The upper and lower parts are assembled with a joining procedure. The upper and lower skins are joined to obtain the composite assembly with the continuous skin. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3584152B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3584152B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3584152B13</originalsourceid><addsrcrecordid>eNqNzD0KAkEMhuFtLES9Qy5g4R_YZmczbnD-mMmgViIyVqKCnsbTui4ewCof4eEdVm9L0voGtI9g0WWNSnJktwEEm43wNAWMUPs97Fja7qu8E3bZ5wRpyw5yCBQhtWQMeN0BQTZfRZBICXvXxxEidSFyTa8cIEcVUUu3mz5rg08sBJgS2docxtXgcro-y-R3RxVoEtVOy-N-LM_H6Vxu5XWksFitl7PVvJ4t_iAfz6JB3g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>METHOD FOR MANUFACTURING A MULTI-SPAR BOX WITH A CONTINUOUS SKIN UPPER SHELL OF A TAIL CONE SECTION FOR A REAR END OF AN AIRCRAFT AND A COMPOSITE ASSEMBLY</title><source>esp@cenet</source><creator>CANAS RIOS, Maria, Almudena ; GARCIA NIETO, Carlos ; INIESTA LOZANO, Fernando ; MARTINO-GONZALEZ, Esteban ; VAZQUEZ CASTRO, Jesus Javier ; SANCHEZ PEREZ, Melania ; MENARD, Edouard ; ARANA HIDALGO, Alberto</creator><creatorcontrib>CANAS RIOS, Maria, Almudena ; GARCIA NIETO, Carlos ; INIESTA LOZANO, Fernando ; MARTINO-GONZALEZ, Esteban ; VAZQUEZ CASTRO, Jesus Javier ; SANCHEZ PEREZ, Melania ; MENARD, Edouard ; ARANA HIDALGO, Alberto</creatorcontrib><description>Examples herein relate to a method for manufacturing a composite assembly with a continuous skin for a rear end of an aircraft by obtaining an upper part (405) of the rear end by composite tooling. The upper part comprises a multi-spar vertical tail plane. The spars (410) of the vertical tail plane comprise widening roots that form an upper shell of the rear end and an upper skin (425). Furthermore, a lower part (415) comprises a lower shell of the rear end including semi-complete frames (420) and stringers and a lower skin (430). The upper and lower parts are assembled with a joining procedure. The upper and lower skins are joined to obtain the composite assembly with the continuous skin.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; 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 ; HELICOPTERS ; PERFORMING OPERATIONS ; PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; TRANSPORTING ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</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=20230607&DB=EPODOC&CC=EP&NR=3584152B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230607&DB=EPODOC&CC=EP&NR=3584152B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CANAS RIOS, Maria, Almudena</creatorcontrib><creatorcontrib>GARCIA NIETO, Carlos</creatorcontrib><creatorcontrib>INIESTA LOZANO, Fernando</creatorcontrib><creatorcontrib>MARTINO-GONZALEZ, Esteban</creatorcontrib><creatorcontrib>VAZQUEZ CASTRO, Jesus Javier</creatorcontrib><creatorcontrib>SANCHEZ PEREZ, Melania</creatorcontrib><creatorcontrib>MENARD, Edouard</creatorcontrib><creatorcontrib>ARANA HIDALGO, Alberto</creatorcontrib><title>METHOD FOR MANUFACTURING A MULTI-SPAR BOX WITH A CONTINUOUS SKIN UPPER SHELL OF A TAIL CONE SECTION FOR A REAR END OF AN AIRCRAFT AND A COMPOSITE ASSEMBLY</title><description>Examples herein relate to a method for manufacturing a composite assembly with a continuous skin for a rear end of an aircraft by obtaining an upper part (405) of the rear end by composite tooling. The upper part comprises a multi-spar vertical tail plane. The spars (410) of the vertical tail plane comprise widening roots that form an upper shell of the rear end and an upper skin (425). Furthermore, a lower part (415) comprises a lower shell of the rear end including semi-complete frames (420) and stringers and a lower skin (430). The upper and lower parts are assembled with a joining procedure. The upper and lower skins are joined to obtain the composite assembly with the continuous skin.</description><subject>AEROPLANES</subject><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><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>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>TRANSPORTING</subject><subject>WORKING OF PLASTICS</subject><subject>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNzD0KAkEMhuFtLES9Qy5g4R_YZmczbnD-mMmgViIyVqKCnsbTui4ewCof4eEdVm9L0voGtI9g0WWNSnJktwEEm43wNAWMUPs97Fja7qu8E3bZ5wRpyw5yCBQhtWQMeN0BQTZfRZBICXvXxxEidSFyTa8cIEcVUUu3mz5rg08sBJgS2docxtXgcro-y-R3RxVoEtVOy-N-LM_H6Vxu5XWksFitl7PVvJ4t_iAfz6JB3g</recordid><startdate>20230607</startdate><enddate>20230607</enddate><creator>CANAS RIOS, Maria, Almudena</creator><creator>GARCIA NIETO, Carlos</creator><creator>INIESTA LOZANO, Fernando</creator><creator>MARTINO-GONZALEZ, Esteban</creator><creator>VAZQUEZ CASTRO, Jesus Javier</creator><creator>SANCHEZ PEREZ, Melania</creator><creator>MENARD, Edouard</creator><creator>ARANA HIDALGO, Alberto</creator><scope>EVB</scope></search><sort><creationdate>20230607</creationdate><title>METHOD FOR MANUFACTURING A MULTI-SPAR BOX WITH A CONTINUOUS SKIN UPPER SHELL OF A TAIL CONE SECTION FOR A REAR END OF AN AIRCRAFT AND A COMPOSITE ASSEMBLY</title><author>CANAS RIOS, Maria, Almudena ; GARCIA NIETO, Carlos ; INIESTA LOZANO, Fernando ; MARTINO-GONZALEZ, Esteban ; VAZQUEZ CASTRO, Jesus Javier ; SANCHEZ PEREZ, Melania ; MENARD, Edouard ; ARANA HIDALGO, Alberto</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3584152B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><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>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>TRANSPORTING</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>CANAS RIOS, Maria, Almudena</creatorcontrib><creatorcontrib>GARCIA NIETO, Carlos</creatorcontrib><creatorcontrib>INIESTA LOZANO, Fernando</creatorcontrib><creatorcontrib>MARTINO-GONZALEZ, Esteban</creatorcontrib><creatorcontrib>VAZQUEZ CASTRO, Jesus Javier</creatorcontrib><creatorcontrib>SANCHEZ PEREZ, Melania</creatorcontrib><creatorcontrib>MENARD, Edouard</creatorcontrib><creatorcontrib>ARANA HIDALGO, Alberto</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CANAS RIOS, Maria, Almudena</au><au>GARCIA NIETO, Carlos</au><au>INIESTA LOZANO, Fernando</au><au>MARTINO-GONZALEZ, Esteban</au><au>VAZQUEZ CASTRO, Jesus Javier</au><au>SANCHEZ PEREZ, Melania</au><au>MENARD, Edouard</au><au>ARANA HIDALGO, Alberto</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD FOR MANUFACTURING A MULTI-SPAR BOX WITH A CONTINUOUS SKIN UPPER SHELL OF A TAIL CONE SECTION FOR A REAR END OF AN AIRCRAFT AND A COMPOSITE ASSEMBLY</title><date>2023-06-07</date><risdate>2023</risdate><abstract>Examples herein relate to a method for manufacturing a composite assembly with a continuous skin for a rear end of an aircraft by obtaining an upper part (405) of the rear end by composite tooling. The upper part comprises a multi-spar vertical tail plane. The spars (410) of the vertical tail plane comprise widening roots that form an upper shell of the rear end and an upper skin (425). Furthermore, a lower part (415) comprises a lower shell of the rear end including semi-complete frames (420) and stringers and a lower skin (430). The upper and lower parts are assembled with a joining procedure. The upper and lower skins are joined to obtain the composite assembly with the continuous skin.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP3584152B1 |
| source | esp@cenet |
| subjects | AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING 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 HELICOPTERS PERFORMING OPERATIONS PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
| title | METHOD FOR MANUFACTURING A MULTI-SPAR BOX WITH A CONTINUOUS SKIN UPPER SHELL OF A TAIL CONE SECTION FOR A REAR END OF AN AIRCRAFT AND A COMPOSITE ASSEMBLY |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-25T06%3A47%3A55IST&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=CANAS%20RIOS,%20Maria,%20Almudena&rft.date=2023-06-07&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3584152B1%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 |