AIR INTAKE OF AN AIRCRAFT NACELLE INCLUDING A REINFORCED LIP WITH A JOULE EFFECT DE-ICING SYSTEM

AIR INTAKE OF AN AIRCRAFT NACELLE INCLUDING A REINFORCED LIP WITH A JOULE EFFECT DE-ICING SYSTEM

The intake (40) has a first alveolar structure (60.1) that is made of a material for conducting the heat, where the heat is flattened against an inside surface of a wall (52) and provided between the wall and a defrosting system (58). A second alveolar structure (60.2) is made of composite material...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: PORTE, ALAIN, CHELIN, FRÉDÉRIC
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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 PORTE, ALAIN
CHELIN, FRÉDÉRIC
description The intake (40) has a first alveolar structure (60.1) that is made of a material for conducting the heat, where the heat is flattened against an inside surface of a wall (52) and provided between the wall and a defrosting system (58). A second alveolar structure (60.2) is made of composite material that is adjacent to the first alveolar structure, where the second alveolar structure is flattened against the inside surface of the wall, with the defrosting system and inserted between the second alveolar structure and the wall. The alveolar structures are made of aluminum alloy. An independent claim is also included for an aircraft nacelle.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2535271B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2535271B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2535271B13</originalsourceid><addsrcrecordid>eNqNykEKwjAQheFuXIh6h7lAF20pruNkYkdjUtIp4qoWiSvRQr0_RvAArh7871tmV8UB2Ik6EngDykEKGJQRcArJWkov2l6z24OCQOyMD0gaLLdwZmlSPfg-OTKGUEBTzvjV3aUTOq2zxX18zHHz21UGhgSbPE6vIc7TeIvP-B6oLeuqLrfFrqj-IB-TxjIR</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AIR INTAKE OF AN AIRCRAFT NACELLE INCLUDING A REINFORCED LIP WITH A JOULE EFFECT DE-ICING SYSTEM</title><source>esp@cenet</source><creator>PORTE, ALAIN ; CHELIN, FRÉDÉRIC</creator><creatorcontrib>PORTE, ALAIN ; CHELIN, FRÉDÉRIC</creatorcontrib><description>The intake (40) has a first alveolar structure (60.1) that is made of a material for conducting the heat, where the heat is flattened against an inside surface of a wall (52) and provided between the wall and a defrosting system (58). A second alveolar structure (60.2) is made of composite material that is adjacent to the first alveolar structure, where the second alveolar structure is flattened against the inside surface of the wall, with the defrosting system and inserted between the second alveolar structure and the wall. The alveolar structures are made of aluminum alloy. An independent claim is also included for an aircraft nacelle.</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2016</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&amp;date=20160810&amp;DB=EPODOC&amp;CC=EP&amp;NR=2535271B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20160810&amp;DB=EPODOC&amp;CC=EP&amp;NR=2535271B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PORTE, ALAIN</creatorcontrib><creatorcontrib>CHELIN, FRÉDÉRIC</creatorcontrib><title>AIR INTAKE OF AN AIRCRAFT NACELLE INCLUDING A REINFORCED LIP WITH A JOULE EFFECT DE-ICING SYSTEM</title><description>The intake (40) has a first alveolar structure (60.1) that is made of a material for conducting the heat, where the heat is flattened against an inside surface of a wall (52) and provided between the wall and a defrosting system (58). A second alveolar structure (60.2) is made of composite material that is adjacent to the first alveolar structure, where the second alveolar structure is flattened against the inside surface of the wall, with the defrosting system and inserted between the second alveolar structure and the wall. The alveolar structures are made of aluminum alloy. An independent claim is also included for an aircraft nacelle.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNykEKwjAQheFuXIh6h7lAF20pruNkYkdjUtIp4qoWiSvRQr0_RvAArh7871tmV8UB2Ik6EngDykEKGJQRcArJWkov2l6z24OCQOyMD0gaLLdwZmlSPfg-OTKGUEBTzvjV3aUTOq2zxX18zHHz21UGhgSbPE6vIc7TeIvP-B6oLeuqLrfFrqj-IB-TxjIR</recordid><startdate>20160810</startdate><enddate>20160810</enddate><creator>PORTE, ALAIN</creator><creator>CHELIN, FRÉDÉRIC</creator><scope>EVB</scope></search><sort><creationdate>20160810</creationdate><title>AIR INTAKE OF AN AIRCRAFT NACELLE INCLUDING A REINFORCED LIP WITH A JOULE EFFECT DE-ICING SYSTEM</title><author>PORTE, ALAIN ; CHELIN, FRÉDÉRIC</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2535271B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2016</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>PORTE, ALAIN</creatorcontrib><creatorcontrib>CHELIN, FRÉDÉRIC</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PORTE, ALAIN</au><au>CHELIN, FRÉDÉRIC</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIR INTAKE OF AN AIRCRAFT NACELLE INCLUDING A REINFORCED LIP WITH A JOULE EFFECT DE-ICING SYSTEM</title><date>2016-08-10</date><risdate>2016</risdate><abstract>The intake (40) has a first alveolar structure (60.1) that is made of a material for conducting the heat, where the heat is flattened against an inside surface of a wall (52) and provided between the wall and a defrosting system (58). A second alveolar structure (60.2) is made of composite material that is adjacent to the first alveolar structure, where the second alveolar structure is flattened against the inside surface of the wall, with the defrosting system and inserted between the second alveolar structure and the wall. The alveolar structures are made of aluminum alloy. An independent claim is also included for an aircraft nacelle.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP2535271B1
source esp@cenet
subjects AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
title AIR INTAKE OF AN AIRCRAFT NACELLE INCLUDING A REINFORCED LIP WITH A JOULE EFFECT DE-ICING SYSTEM
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-29T14%3A53%3A07IST&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=PORTE,%20ALAIN&rft.date=2016-08-10&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2535271B1%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