COMPOSITE VANE FOR AN AIRCRAFT TURBINE ENGINE
Blower vane (1) for an aircraft turbine engine, the vane comprising a blade (13) connected to a root (11), the vane being made of a woven fibre-based composite material embedded in a polymeric resin, the vane further comprising a medium (2) for identifying the vane, which is a radio-identification m...
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| creator | LAMOUCHE, Damien Bruno LHOMMEAU, Tony Alain Roger Joël FAIVRE D'ARCIER, Pierre Jean MINERVINO, Matteo |
| description | Blower vane (1) for an aircraft turbine engine, the vane comprising a blade (13) connected to a root (11), the vane being made of a woven fibre-based composite material embedded in a polymeric resin, the vane further comprising a medium (2) for identifying the vane, which is a radio-identification medium, the blower vane being characterised in that it comprises at least a first portion (30, 32) the fibres of which are only electrically conductive fibres, and at least a second portion (34) the fibres of which are formed by a mixture of electrically conductive fibres and non-electrically conductive fibres, and in that the identification medium is located in or on the second portion (34).
Aube de soufflante (1) pour une turbomachine d'aéronef, l'aube comportant une pale (13) reliée à un pied (11), l'aube étant réalisée en matériau composite à base de fibres tissées et noyées dans une résine polymérique, l'aube comprenant en outre un support (2) d'identification de l'aube, qui est du type radio-identification, caractérisée en ce qu'elle comprend au moins une première portion (30, 32) dont les fibres sont uniquement des fibres électroconductrices et au moins une seconde portion (34) dont les fibres sont formées par un mélange de fibres électroconductrices et de fibres non électroconductrices, et en ce que le support d'identification est situé dans ou sur ladite seconde portion (34). |
| format | Patent |
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Aube de soufflante (1) pour une turbomachine d'aéronef, l'aube comportant une pale (13) reliée à un pied (11), l'aube étant réalisée en matériau composite à base de fibres tissées et noyées dans une résine polymérique, l'aube comprenant en outre un support (2) d'identification de l'aube, qui est du type radio-identification, caractérisée en ce qu'elle comprend au moins une première portion (30, 32) dont les fibres sont uniquement des fibres électroconductrices et au moins une seconde portion (34) dont les fibres sont formées par un mélange de fibres électroconductrices et de fibres non électroconductrices, et en ce que le support d'identification est situé dans ou sur ladite seconde portion (34).</description><language>eng ; fre</language><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; BLASTING ; CALCULATING ; COMPUTING ; COUNTING ; ENGINE PLANTS IN GENERAL ; HANDLING RECORD CARRIERS ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; PHYSICS ; PRESENTATION OF DATA ; PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE ; RECOGNITION OF DATA ; RECORD CARRIERS ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; STEAM ENGINES ; TRANSPORTING ; WEAPONS ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>2022</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=20220224&DB=EPODOC&CC=WO&NR=2022038323A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220224&DB=EPODOC&CC=WO&NR=2022038323A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LAMOUCHE, Damien Bruno</creatorcontrib><creatorcontrib>LHOMMEAU, Tony Alain Roger Joël</creatorcontrib><creatorcontrib>FAIVRE D'ARCIER, Pierre Jean</creatorcontrib><creatorcontrib>MINERVINO, Matteo</creatorcontrib><title>COMPOSITE VANE FOR AN AIRCRAFT TURBINE ENGINE</title><description>Blower vane (1) for an aircraft turbine engine, the vane comprising a blade (13) connected to a root (11), the vane being made of a woven fibre-based composite material embedded in a polymeric resin, the vane further comprising a medium (2) for identifying the vane, which is a radio-identification medium, the blower vane being characterised in that it comprises at least a first portion (30, 32) the fibres of which are only electrically conductive fibres, and at least a second portion (34) the fibres of which are formed by a mixture of electrically conductive fibres and non-electrically conductive fibres, and in that the identification medium is located in or on the second portion (34).
Aube de soufflante (1) pour une turbomachine d'aéronef, l'aube comportant une pale (13) reliée à un pied (11), l'aube étant réalisée en matériau composite à base de fibres tissées et noyées dans une résine polymérique, l'aube comprenant en outre un support (2) d'identification de l'aube, qui est du type radio-identification, caractérisée en ce qu'elle comprend au moins une première portion (30, 32) dont les fibres sont uniquement des fibres électroconductrices et au moins une seconde portion (34) dont les fibres sont formées par un mélange de fibres électroconductrices et de fibres non électroconductrices, et en ce que le support d'identification est situé dans ou sur ladite seconde portion (34).</description><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>BLASTING</subject><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COUNTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HANDLING RECORD CARRIERS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>PRESENTATION OF DATA</subject><subject>PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE</subject><subject>RECOGNITION OF DATA</subject><subject>RECORD CARRIERS</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>STEAM ENGINES</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB19vcN8A_2DHFVCHP0c1Vw8w9ScPRTcPQMcg5ydAtRCAkNcvIEirv6uQMpHgbWtMSc4lReKM3NoOzmGuLsoZtakB-fWlyQmJyal1oSH-5vZGBkZGBsYWxk7GhoTJwqAD4MJiQ</recordid><startdate>20220224</startdate><enddate>20220224</enddate><creator>LAMOUCHE, Damien Bruno</creator><creator>LHOMMEAU, Tony Alain Roger Joël</creator><creator>FAIVRE D'ARCIER, Pierre Jean</creator><creator>MINERVINO, Matteo</creator><scope>EVB</scope></search><sort><creationdate>20220224</creationdate><title>COMPOSITE VANE FOR AN AIRCRAFT TURBINE ENGINE</title><author>LAMOUCHE, Damien Bruno ; LHOMMEAU, Tony Alain Roger Joël ; FAIVRE D'ARCIER, Pierre Jean ; MINERVINO, Matteo</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2022038323A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2022</creationdate><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>BLASTING</topic><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>COUNTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HANDLING RECORD CARRIERS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>PRESENTATION OF DATA</topic><topic>PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE</topic><topic>RECOGNITION OF DATA</topic><topic>RECORD CARRIERS</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>STEAM ENGINES</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>LAMOUCHE, Damien Bruno</creatorcontrib><creatorcontrib>LHOMMEAU, Tony Alain Roger Joël</creatorcontrib><creatorcontrib>FAIVRE D'ARCIER, Pierre Jean</creatorcontrib><creatorcontrib>MINERVINO, Matteo</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LAMOUCHE, Damien Bruno</au><au>LHOMMEAU, Tony Alain Roger Joël</au><au>FAIVRE D'ARCIER, Pierre Jean</au><au>MINERVINO, Matteo</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMPOSITE VANE FOR AN AIRCRAFT TURBINE ENGINE</title><date>2022-02-24</date><risdate>2022</risdate><abstract>Blower vane (1) for an aircraft turbine engine, the vane comprising a blade (13) connected to a root (11), the vane being made of a woven fibre-based composite material embedded in a polymeric resin, the vane further comprising a medium (2) for identifying the vane, which is a radio-identification medium, the blower vane being characterised in that it comprises at least a first portion (30, 32) the fibres of which are only electrically conductive fibres, and at least a second portion (34) the fibres of which are formed by a mixture of electrically conductive fibres and non-electrically conductive fibres, and in that the identification medium is located in or on the second portion (34).
Aube de soufflante (1) pour une turbomachine d'aéronef, l'aube comportant une pale (13) reliée à un pied (11), l'aube étant réalisée en matériau composite à base de fibres tissées et noyées dans une résine polymérique, l'aube comprenant en outre un support (2) d'identification de l'aube, qui est du type radio-identification, caractérisée en ce qu'elle comprend au moins une première portion (30, 32) dont les fibres sont uniquement des fibres électroconductrices et au moins une seconde portion (34) dont les fibres sont formées par un mélange de fibres électroconductrices et de fibres non électroconductrices, et en ce que le support d'identification est situé dans ou sur ladite seconde portion (34).</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING BLASTING CALCULATING COMPUTING COUNTING ENGINE PLANTS IN GENERAL HANDLING RECORD CARRIERS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS PHYSICS PRESENTATION OF DATA PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE RECOGNITION OF DATA RECORD CARRIERS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS STEAM ENGINES TRANSPORTING WEAPONS WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
| title | COMPOSITE VANE FOR AN AIRCRAFT TURBINE ENGINE |
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