AIRCRAFT TYRE CARCASS REINFORCEMENTS
The present invention relates to a radial tyre for an aircraft, comprising at least one carcass ply (51) comprising reinforcing elements, each carcass ply (51) having a first main portion (52) which connects one bead wire to the other and is connected at the ends thereof to two other portions or tur...
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| creator | FERIGO, Hervé |
| description | The present invention relates to a radial tyre for an aircraft, comprising at least one carcass ply (51) comprising reinforcing elements, each carcass ply (51) having a first main portion (52) which connects one bead wire to the other and is connected at the ends thereof to two other portions or turn-ups (53) each having a free end (531). The free ends (531) of the two turn-ups (53) of at least one carcass ply (52) are positioned axially so as to form an overlay (6) between the two axially outer walls (2112) of the two axially outermost grooves (211) of the tread, each overlay having an axial width (L) of less than one third of the axial width (L1) of the crown reinforcement.
La présente invention a pour objet un pneumatique radial pour avion, comportant au moins une couche de carcasse (51) comportant des éléments de renfort, chaque couche de carcasse (51) ayant une première partie (52) principale reliant une tringle à l'autre et reliée à ses extrémités à deux autres parties ou retournements (53) ayant chacun une extrémité libre (531). Les extrémités libres (531) des deux retournements (53) d'au moins une couche de carcasse (52) sont positionnées axialement de manière à former un recouvrement (6) entre les deux parois axialement extérieures (2112) des deux sillons (211) les plus axialement extérieurs de la bande de roulement, chaque recouvrement ayant une largeur axiale (L) inférieure à un tiers de la largeur axiale (L1) de l'armature de sommet. |
| format | Patent |
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La présente invention a pour objet un pneumatique radial pour avion, comportant au moins une couche de carcasse (51) comportant des éléments de renfort, chaque couche de carcasse (51) ayant une première partie (52) principale reliant une tringle à l'autre et reliée à ses extrémités à deux autres parties ou retournements (53) ayant chacun une extrémité libre (531). Les extrémités libres (531) des deux retournements (53) d'au moins une couche de carcasse (52) sont positionnées axialement de manière à former un recouvrement (6) entre les deux parois axialement extérieures (2112) des deux sillons (211) les plus axialement extérieurs de la bande de roulement, chaque recouvrement ayant une largeur axiale (L) inférieure à un tiers de la largeur axiale (L1) de l'armature de sommet.</description><language>eng ; fre</language><subject>DEVICES OR ARRANGEMENTS RELATED TO TYRES ; PERFORMING OPERATIONS ; REPAIRING, OR CONNECTING VALVES TO, INFLATABLE ELASTIC BODIESIN GENERAL ; TRANSPORTING ; TYRE CHANGING OR REPAIRING ; TYRE INFLATION ; VEHICLE TYRES ; VEHICLES IN GENERAL</subject><creationdate>2024</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=20241003&DB=EPODOC&CC=WO&NR=2024200361A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20241003&DB=EPODOC&CC=WO&NR=2024200361A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>FERIGO, Hervé</creatorcontrib><title>AIRCRAFT TYRE CARCASS REINFORCEMENTS</title><description>The present invention relates to a radial tyre for an aircraft, comprising at least one carcass ply (51) comprising reinforcing elements, each carcass ply (51) having a first main portion (52) which connects one bead wire to the other and is connected at the ends thereof to two other portions or turn-ups (53) each having a free end (531). The free ends (531) of the two turn-ups (53) of at least one carcass ply (52) are positioned axially so as to form an overlay (6) between the two axially outer walls (2112) of the two axially outermost grooves (211) of the tread, each overlay having an axial width (L) of less than one third of the axial width (L1) of the crown reinforcement.
La présente invention a pour objet un pneumatique radial pour avion, comportant au moins une couche de carcasse (51) comportant des éléments de renfort, chaque couche de carcasse (51) ayant une première partie (52) principale reliant une tringle à l'autre et reliée à ses extrémités à deux autres parties ou retournements (53) ayant chacun une extrémité libre (531). Les extrémités libres (531) des deux retournements (53) d'au moins une couche de carcasse (52) sont positionnées axialement de manière à former un recouvrement (6) entre les deux parois axialement extérieures (2112) des deux sillons (211) les plus axialement extérieurs de la bande de roulement, chaque recouvrement ayant une largeur axiale (L) inférieure à un tiers de la largeur axiale (L1) de l'armature de sommet.</description><subject>DEVICES OR ARRANGEMENTS RELATED TO TYRES</subject><subject>PERFORMING OPERATIONS</subject><subject>REPAIRING, OR CONNECTING VALVES TO, INFLATABLE ELASTIC BODIESIN GENERAL</subject><subject>TRANSPORTING</subject><subject>TYRE CHANGING OR REPAIRING</subject><subject>TYRE INFLATION</subject><subject>VEHICLE TYRES</subject><subject>VEHICLES IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFBx9AxyDnJ0C1EIiQxyVXB2DHJ2DA5WCHL19HPzD3J29XX1CwnmYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXx4f5GBkYmRgYGxmaGjobGxKkCABNaI_c</recordid><startdate>20241003</startdate><enddate>20241003</enddate><creator>FERIGO, Hervé</creator><scope>EVB</scope></search><sort><creationdate>20241003</creationdate><title>AIRCRAFT TYRE CARCASS REINFORCEMENTS</title><author>FERIGO, Hervé</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2024200361A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2024</creationdate><topic>DEVICES OR ARRANGEMENTS RELATED TO TYRES</topic><topic>PERFORMING OPERATIONS</topic><topic>REPAIRING, OR CONNECTING VALVES TO, INFLATABLE ELASTIC BODIESIN GENERAL</topic><topic>TRANSPORTING</topic><topic>TYRE CHANGING OR REPAIRING</topic><topic>TYRE INFLATION</topic><topic>VEHICLE TYRES</topic><topic>VEHICLES IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>FERIGO, Hervé</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>FERIGO, Hervé</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT TYRE CARCASS REINFORCEMENTS</title><date>2024-10-03</date><risdate>2024</risdate><abstract>The present invention relates to a radial tyre for an aircraft, comprising at least one carcass ply (51) comprising reinforcing elements, each carcass ply (51) having a first main portion (52) which connects one bead wire to the other and is connected at the ends thereof to two other portions or turn-ups (53) each having a free end (531). The free ends (531) of the two turn-ups (53) of at least one carcass ply (52) are positioned axially so as to form an overlay (6) between the two axially outer walls (2112) of the two axially outermost grooves (211) of the tread, each overlay having an axial width (L) of less than one third of the axial width (L1) of the crown reinforcement.
La présente invention a pour objet un pneumatique radial pour avion, comportant au moins une couche de carcasse (51) comportant des éléments de renfort, chaque couche de carcasse (51) ayant une première partie (52) principale reliant une tringle à l'autre et reliée à ses extrémités à deux autres parties ou retournements (53) ayant chacun une extrémité libre (531). Les extrémités libres (531) des deux retournements (53) d'au moins une couche de carcasse (52) sont positionnées axialement de manière à former un recouvrement (6) entre les deux parois axialement extérieures (2112) des deux sillons (211) les plus axialement extérieurs de la bande de roulement, chaque recouvrement ayant une largeur axiale (L) inférieure à un tiers de la largeur axiale (L1) de l'armature de sommet.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | DEVICES OR ARRANGEMENTS RELATED TO TYRES PERFORMING OPERATIONS REPAIRING, OR CONNECTING VALVES TO, INFLATABLE ELASTIC BODIESIN GENERAL TRANSPORTING TYRE CHANGING OR REPAIRING TYRE INFLATION VEHICLE TYRES VEHICLES IN GENERAL |
| title | AIRCRAFT TYRE CARCASS REINFORCEMENTS |
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