PROCESS OF MAKING A LAYERED STRUCTURE AND AIRCRAFT EQUIPPED WITH SUCH A STRUCTURE
To produce a layered structure (1) which includes a panel (2) made of composite materials applied against at least one metal plate (3), the panel and the plate are stacked, then the stack is bored to produce a fastening borehole, and a fastening rod (8) is inserted into the borehole and the fastener...
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| creator | CABANAC, JEAN-PIERRE GUITTARD, DOMINIQUE ROGER, JANY |
| description | To produce a layered structure (1) which includes a panel (2) made of composite materials applied against at least one metal plate (3), the panel and the plate are stacked, then the stack is bored to produce a fastening borehole, and a fastening rod (8) is inserted into the borehole and the fastener is secured. In the invention, during boring, negative play is created between the bore diameter and the diameter of the fastener such that when the fastener is inserted, it is inserted from the metal plate. By doing so, it is shown that positive interference is caused, promoting the durability of the fastener.
Pour réaliser une structure (1) stratifiée qui comporte un panneau (2) en matériaux composites plaqué contre au moins une plaque (3) de métal, on présente le panneau et la plaque en empilement, on perce l'empilement pour former un alésage de fixation, on introduit une tige (8) de fixation dans l'alésage, et on fixe la fixation. Dans l'invention, lors du perçage, on réalise un jeu négatif entre un diamètre de l'alésage et un diamètre de la fixation, et lors de l'introduction de la fixation on l'introduit à partir de la plaque en métal. On montre qu'en agissant ainsi, on provoque une interférence positive favorable à la pérennité de la fixation. |
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Pour réaliser une structure (1) stratifiée qui comporte un panneau (2) en matériaux composites plaqué contre au moins une plaque (3) de métal, on présente le panneau et la plaque en empilement, on perce l'empilement pour former un alésage de fixation, on introduit une tige (8) de fixation dans l'alésage, et on fixe la fixation. Dans l'invention, lors du perçage, on réalise un jeu négatif entre un diamètre de l'alésage et un diamètre de la fixation, et lors de l'introduction de la fixation on l'introduit à partir de la plaque en métal. On montre qu'en agissant ainsi, on provoque une interférence positive favorable à la pérennité de la fixation.</description><language>eng ; fre</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 ; FORGE FURNACES ; FORGING ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HAMMERING ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL ; PERFORMING OPERATIONS ; PRESSING METAL ; PUNCHING METAL ; RIVETING ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2013</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=20131224&DB=EPODOC&CC=CA&NR=2486875C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20131224&DB=EPODOC&CC=CA&NR=2486875C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CABANAC, JEAN-PIERRE</creatorcontrib><creatorcontrib>GUITTARD, DOMINIQUE</creatorcontrib><creatorcontrib>ROGER, JANY</creatorcontrib><title>PROCESS OF MAKING A LAYERED STRUCTURE AND AIRCRAFT EQUIPPED WITH SUCH A STRUCTURE</title><description>To produce a layered structure (1) which includes a panel (2) made of composite materials applied against at least one metal plate (3), the panel and the plate are stacked, then the stack is bored to produce a fastening borehole, and a fastening rod (8) is inserted into the borehole and the fastener is secured. In the invention, during boring, negative play is created between the bore diameter and the diameter of the fastener such that when the fastener is inserted, it is inserted from the metal plate. By doing so, it is shown that positive interference is caused, promoting the durability of the fastener.
Pour réaliser une structure (1) stratifiée qui comporte un panneau (2) en matériaux composites plaqué contre au moins une plaque (3) de métal, on présente le panneau et la plaque en empilement, on perce l'empilement pour former un alésage de fixation, on introduit une tige (8) de fixation dans l'alésage, et on fixe la fixation. Dans l'invention, lors du perçage, on réalise un jeu négatif entre un diamètre de l'alésage et un diamètre de la fixation, et lors de l'introduction de la fixation on l'introduit à partir de la plaque en métal. On montre qu'en agissant ainsi, on provoque une interférence positive favorable à la pérennité de la fixation.</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>FORGE FURNACES</subject><subject>FORGING</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HAMMERING</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</subject><subject>PERFORMING OPERATIONS</subject><subject>PRESSING METAL</subject><subject>PUNCHING METAL</subject><subject>RIVETING</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAgMCPJ3dg0OVvB3U_B19Pb0c1dwVPBxjHQNcnVRCA4JCnUOCQ1yVXD0c1Fw9AxyDnJ0C1FwDQz1DAgAyod7hngoBIc6ewD1wNXyMLCmJeYUp_JCaW4GeTfXEGcP3dSC_PjU4oLE5NS81JJ4Z0cjEwszC3NTZ2PCKgDZhi5u</recordid><startdate>20131224</startdate><enddate>20131224</enddate><creator>CABANAC, JEAN-PIERRE</creator><creator>GUITTARD, DOMINIQUE</creator><creator>ROGER, JANY</creator><scope>EVB</scope></search><sort><creationdate>20131224</creationdate><title>PROCESS OF MAKING A LAYERED STRUCTURE AND AIRCRAFT EQUIPPED WITH SUCH A STRUCTURE</title><author>CABANAC, JEAN-PIERRE ; GUITTARD, DOMINIQUE ; ROGER, JANY</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2486875C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2013</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>FORGE FURNACES</topic><topic>FORGING</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HAMMERING</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</topic><topic>PERFORMING OPERATIONS</topic><topic>PRESSING METAL</topic><topic>PUNCHING METAL</topic><topic>RIVETING</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>CABANAC, JEAN-PIERRE</creatorcontrib><creatorcontrib>GUITTARD, DOMINIQUE</creatorcontrib><creatorcontrib>ROGER, JANY</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CABANAC, JEAN-PIERRE</au><au>GUITTARD, DOMINIQUE</au><au>ROGER, JANY</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PROCESS OF MAKING A LAYERED STRUCTURE AND AIRCRAFT EQUIPPED WITH SUCH A STRUCTURE</title><date>2013-12-24</date><risdate>2013</risdate><abstract>To produce a layered structure (1) which includes a panel (2) made of composite materials applied against at least one metal plate (3), the panel and the plate are stacked, then the stack is bored to produce a fastening borehole, and a fastening rod (8) is inserted into the borehole and the fastener is secured. In the invention, during boring, negative play is created between the bore diameter and the diameter of the fastener such that when the fastener is inserted, it is inserted from the metal plate. By doing so, it is shown that positive interference is caused, promoting the durability of the fastener.
Pour réaliser une structure (1) stratifiée qui comporte un panneau (2) en matériaux composites plaqué contre au moins une plaque (3) de métal, on présente le panneau et la plaque en empilement, on perce l'empilement pour former un alésage de fixation, on introduit une tige (8) de fixation dans l'alésage, et on fixe la fixation. Dans l'invention, lors du perçage, on réalise un jeu négatif entre un diamètre de l'alésage et un diamètre de la fixation, et lors de l'introduction de la fixation on l'introduit à partir de la plaque en métal. On montre qu'en agissant ainsi, on provoque une interférence positive favorable à la pérennité de la fixation.</abstract><oa>free_for_read</oa></addata></record> |
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| 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 FORGE FURNACES FORGING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HAMMERING HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL PERFORMING OPERATIONS PRESSING METAL PUNCHING METAL RIVETING THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | PROCESS OF MAKING A LAYERED STRUCTURE AND AIRCRAFT EQUIPPED WITH SUCH A STRUCTURE |
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