Método de fabricación de una junta con forma de anillo para una aeronave
La invención se refiere a un método para fabricar una junta anular (1) para una aeronave, que comprende los siguientes pasos: proporcionar una varilla (2) de material compuesto preimpregnado; proporcionar un molde (3) que tiene una parte hembra (4) y una parte macho (5), teniendo al menos una de las...
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| creator | NUNEZ DELGADO, Julio JIMENEZ VIVAS, Antonio PEREZ PASTOR, Augusto CANO CEDIEL, Jose David DIAZ VAZQUEZ, Juan Pedro |
| description | La invención se refiere a un método para fabricar una junta anular (1) para una aeronave, que comprende los siguientes pasos: proporcionar una varilla (2) de material compuesto preimpregnado; proporcionar un molde (3) que tiene una parte hembra (4) y una parte macho (5), teniendo al menos una de las partes (4, 5) una ranura (6) con la configuración en forma de anillo deseada; colocar la varilla (2) sobre la parte hembra (4) y colocar la parte macho (5) sobre la varilla anular para obtener una preforma anular (7); aplicar vacío para reducir el volumen de la preforma en forma de anillo (7); curar la preforma en forma de anillo (7) para obtener una preforma curada en forma de anillo (9); y desmoldar la preforma curada anular (9) para obtener así una junta anular (1). (Traducción automática con Google Translate, sin valor legal)
The invention refers to a method for manufacturing a ring-shaped gasket (1) for an aircraft, comprising the following steps: providing a rod (2) made of prepreg composite material; providing a mold (3) having a female part (4) and a male part (5), at least one of the parts (4, 5) having a groove (6) with the ring-shaped desired configuration; placing the rod (2) onto the female part (4) and set the male part (5) over the ring-shaped rod to obtain a ring-shaped preform (7); applying vacuum to debulk the ring-shaped preform (7); curing the ring-shaped preform (7) to obtain a ring-shaped cured preform (9); and demolding the ring-shaped cured preform (9) to thus obtain a ring-shaped gasket (1). |
| format | Patent |
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The invention refers to a method for manufacturing a ring-shaped gasket (1) for an aircraft, comprising the following steps: providing a rod (2) made of prepreg composite material; providing a mold (3) having a female part (4) and a male part (5), at least one of the parts (4, 5) having a groove (6) with the ring-shaped desired configuration; placing the rod (2) onto the female part (4) and set the male part (5) over the ring-shaped rod to obtain a ring-shaped preform (7); applying vacuum to debulk the ring-shaped preform (7); curing the ring-shaped preform (7) to obtain a ring-shaped cured preform (9); and demolding the ring-shaped cured preform (9) to thus obtain a ring-shaped gasket (1).</description><language>spa</language><subject>AEROPLANES ; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; CYLINDERS ; ENGINEERING ELEMENTS AND UNITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HELICOPTERS ; INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES ; INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; PISTONS ; PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE ; SEALINGS ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS ; 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=20230410&DB=EPODOC&CC=ES&NR=2938388T3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230410&DB=EPODOC&CC=ES&NR=2938388T3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NUNEZ DELGADO, Julio</creatorcontrib><creatorcontrib>JIMENEZ VIVAS, Antonio</creatorcontrib><creatorcontrib>PEREZ PASTOR, Augusto</creatorcontrib><creatorcontrib>CANO CEDIEL, Jose David</creatorcontrib><creatorcontrib>DIAZ VAZQUEZ, Juan Pedro</creatorcontrib><title>Método de fabricación de una junta con forma de anillo para una aeronave</title><description>La invención se refiere a un método para fabricar una junta anular (1) para una aeronave, que comprende los siguientes pasos: proporcionar una varilla (2) de material compuesto preimpregnado; proporcionar un molde (3) que tiene una parte hembra (4) y una parte macho (5), teniendo al menos una de las partes (4, 5) una ranura (6) con la configuración en forma de anillo deseada; colocar la varilla (2) sobre la parte hembra (4) y colocar la parte macho (5) sobre la varilla anular para obtener una preforma anular (7); aplicar vacío para reducir el volumen de la preforma en forma de anillo (7); curar la preforma en forma de anillo (7) para obtener una preforma curada en forma de anillo (9); y desmoldar la preforma curada anular (9) para obtener así una junta anular (1). (Traducción automática con Google Translate, sin valor legal)
The invention refers to a method for manufacturing a ring-shaped gasket (1) for an aircraft, comprising the following steps: providing a rod (2) made of prepreg composite material; providing a mold (3) having a female part (4) and a male part (5), at least one of the parts (4, 5) having a groove (6) with the ring-shaped desired configuration; placing the rod (2) onto the female part (4) and set the male part (5) over the ring-shaped rod to obtain a ring-shaped preform (7); applying vacuum to debulk the ring-shaped preform (7); curing the ring-shaped preform (7) to obtain a ring-shaped cured preform (9); and demolding the ring-shaped cured preform (9) to thus obtain a ring-shaped gasket (1).</description><subject>AEROPLANES</subject><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>CYLINDERS</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>INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES</subject><subject>INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>PISTONS</subject><subject>PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE</subject><subject>SEALINGS</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</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>eNrjZPDyPbyyJD8lXyElVSEtMakoMzkxOfPw5jwQvzQvUSGrNK8kUSE5P08hLb8oNxEknJiXmZOTr1CQWJQIVpKYWpSfl1iWysPAmpaYU5zKC6W5GRTdXEOcPXRTC_LjU4sLEpNT81JL4l2DjSyNLYwtLEJCjI2JUQMAdnc1-g</recordid><startdate>20230410</startdate><enddate>20230410</enddate><creator>NUNEZ DELGADO, Julio</creator><creator>JIMENEZ VIVAS, Antonio</creator><creator>PEREZ PASTOR, Augusto</creator><creator>CANO CEDIEL, Jose David</creator><creator>DIAZ VAZQUEZ, Juan Pedro</creator><scope>EVB</scope></search><sort><creationdate>20230410</creationdate><title>Método de fabricación de una junta con forma de anillo para una aeronave</title><author>NUNEZ DELGADO, Julio ; JIMENEZ VIVAS, Antonio ; PEREZ PASTOR, Augusto ; CANO CEDIEL, Jose David ; DIAZ VAZQUEZ, Juan Pedro</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_ES2938388TT33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>spa</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>BLASTING</topic><topic>COSMONAUTICS</topic><topic>CYLINDERS</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>INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES</topic><topic>INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>PISTONS</topic><topic>PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE</topic><topic>SEALINGS</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>NUNEZ DELGADO, Julio</creatorcontrib><creatorcontrib>JIMENEZ VIVAS, Antonio</creatorcontrib><creatorcontrib>PEREZ PASTOR, Augusto</creatorcontrib><creatorcontrib>CANO CEDIEL, Jose David</creatorcontrib><creatorcontrib>DIAZ VAZQUEZ, Juan Pedro</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NUNEZ DELGADO, Julio</au><au>JIMENEZ VIVAS, Antonio</au><au>PEREZ PASTOR, Augusto</au><au>CANO CEDIEL, Jose David</au><au>DIAZ VAZQUEZ, Juan Pedro</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Método de fabricación de una junta con forma de anillo para una aeronave</title><date>2023-04-10</date><risdate>2023</risdate><abstract>La invención se refiere a un método para fabricar una junta anular (1) para una aeronave, que comprende los siguientes pasos: proporcionar una varilla (2) de material compuesto preimpregnado; proporcionar un molde (3) que tiene una parte hembra (4) y una parte macho (5), teniendo al menos una de las partes (4, 5) una ranura (6) con la configuración en forma de anillo deseada; colocar la varilla (2) sobre la parte hembra (4) y colocar la parte macho (5) sobre la varilla anular para obtener una preforma anular (7); aplicar vacío para reducir el volumen de la preforma en forma de anillo (7); curar la preforma en forma de anillo (7) para obtener una preforma curada en forma de anillo (9); y desmoldar la preforma curada anular (9) para obtener así una junta anular (1). (Traducción automática con Google Translate, sin valor legal)
The invention refers to a method for manufacturing a ring-shaped gasket (1) for an aircraft, comprising the following steps: providing a rod (2) made of prepreg composite material; providing a mold (3) having a female part (4) and a male part (5), at least one of the parts (4, 5) having a groove (6) with the ring-shaped desired configuration; placing the rod (2) onto the female part (4) and set the male part (5) over the ring-shaped rod to obtain a ring-shaped preform (7); applying vacuum to debulk the ring-shaped preform (7); curing the ring-shaped preform (7) to obtain a ring-shaped cured preform (9); and demolding the ring-shaped cured preform (9) to thus obtain a ring-shaped gasket (1).</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION BLASTING COSMONAUTICS CYLINDERS ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS PISTONS PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE SEALINGS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
| title | Método de fabricación de una junta con forma de anillo para una aeronave |
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