ACOUSTIC PANEL FOR AN AIRCRAFT TURBOMACHINE
An acoustic panel for an aircraft turbomachine has a sandwich structure. The sandwich structure includes a cell structure with a plurality of acoustic cells, a perforated acoustic structure, and a porous acoustic structure attached to the perforated acoustic structure. The perforated acoustic struct...
Gespeichert in:
Hauptverfasser: | , , , , |
---|---|
Format: | Patent |
Sprache: | eng |
Schlagworte: | |
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 | CARUEL, Pierre Charles DESJOYEAUX, Bertrand Léon Marie CLUZEAU, Geneviève PREAU, Mathieu François Eric VERSAEVEL, Marc |
description | An acoustic panel for an aircraft turbomachine has a sandwich structure. The sandwich structure includes a cell structure with a plurality of acoustic cells, a perforated acoustic structure, and a porous acoustic structure attached to the perforated acoustic structure. The perforated acoustic structure is arranged between the cell structure and the porous acoustic structure. The porous acoustic structure is multi-layered and has a first woven textile layer and a second woven textile layer connected to the first layer. The second layer is arranged between the first layer and the perforated acoustic structure. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2024351699A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2024351699A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2024351699A13</originalsourceid><addsrcrecordid>eNrjZNB2dPYPDQ7xdFYIcPRz9VFw8w9ScPRTcPQMcg5ydAtRCAkNcvL3dXT28PRz5WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgZGJsamhmaWlo6GxsSpAgD35iXG</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>ACOUSTIC PANEL FOR AN AIRCRAFT TURBOMACHINE</title><source>esp@cenet</source><creator>CARUEL, Pierre Charles ; DESJOYEAUX, Bertrand Léon Marie ; CLUZEAU, Geneviève ; PREAU, Mathieu François Eric ; VERSAEVEL, Marc</creator><creatorcontrib>CARUEL, Pierre Charles ; DESJOYEAUX, Bertrand Léon Marie ; CLUZEAU, Geneviève ; PREAU, Mathieu François Eric ; VERSAEVEL, Marc</creatorcontrib><description>An acoustic panel for an aircraft turbomachine has a sandwich structure. The sandwich structure includes a cell structure with a plurality of acoustic cells, a perforated acoustic structure, and a porous acoustic structure attached to the perforated acoustic structure. The perforated acoustic structure is arranged between the cell structure and the porous acoustic structure. The porous acoustic structure is multi-layered and has a first woven textile layer and a second woven textile layer connected to the first layer. The second layer is arranged between the first layer and the perforated acoustic structure.</description><language>eng</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>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=20241024&DB=EPODOC&CC=US&NR=2024351699A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20241024&DB=EPODOC&CC=US&NR=2024351699A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CARUEL, Pierre Charles</creatorcontrib><creatorcontrib>DESJOYEAUX, Bertrand Léon Marie</creatorcontrib><creatorcontrib>CLUZEAU, Geneviève</creatorcontrib><creatorcontrib>PREAU, Mathieu François Eric</creatorcontrib><creatorcontrib>VERSAEVEL, Marc</creatorcontrib><title>ACOUSTIC PANEL FOR AN AIRCRAFT TURBOMACHINE</title><description>An acoustic panel for an aircraft turbomachine has a sandwich structure. The sandwich structure includes a cell structure with a plurality of acoustic cells, a perforated acoustic structure, and a porous acoustic structure attached to the perforated acoustic structure. The perforated acoustic structure is arranged between the cell structure and the porous acoustic structure. The porous acoustic structure is multi-layered and has a first woven textile layer and a second woven textile layer connected to the first layer. The second layer is arranged between the first layer and the perforated acoustic structure.</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>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB2dPYPDQ7xdFYIcPRz9VFw8w9ScPRTcPQMcg5ydAtRCAkNcvL3dXT28PRz5WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgZGJsamhmaWlo6GxsSpAgD35iXG</recordid><startdate>20241024</startdate><enddate>20241024</enddate><creator>CARUEL, Pierre Charles</creator><creator>DESJOYEAUX, Bertrand Léon Marie</creator><creator>CLUZEAU, Geneviève</creator><creator>PREAU, Mathieu François Eric</creator><creator>VERSAEVEL, Marc</creator><scope>EVB</scope></search><sort><creationdate>20241024</creationdate><title>ACOUSTIC PANEL FOR AN AIRCRAFT TURBOMACHINE</title><author>CARUEL, Pierre Charles ; DESJOYEAUX, Bertrand Léon Marie ; CLUZEAU, Geneviève ; PREAU, Mathieu François Eric ; VERSAEVEL, Marc</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2024351699A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2024</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>CARUEL, Pierre Charles</creatorcontrib><creatorcontrib>DESJOYEAUX, Bertrand Léon Marie</creatorcontrib><creatorcontrib>CLUZEAU, Geneviève</creatorcontrib><creatorcontrib>PREAU, Mathieu François Eric</creatorcontrib><creatorcontrib>VERSAEVEL, Marc</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CARUEL, Pierre Charles</au><au>DESJOYEAUX, Bertrand Léon Marie</au><au>CLUZEAU, Geneviève</au><au>PREAU, Mathieu François Eric</au><au>VERSAEVEL, Marc</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ACOUSTIC PANEL FOR AN AIRCRAFT TURBOMACHINE</title><date>2024-10-24</date><risdate>2024</risdate><abstract>An acoustic panel for an aircraft turbomachine has a sandwich structure. The sandwich structure includes a cell structure with a plurality of acoustic cells, a perforated acoustic structure, and a porous acoustic structure attached to the perforated acoustic structure. The perforated acoustic structure is arranged between the cell structure and the porous acoustic structure. The porous acoustic structure is multi-layered and has a first woven textile layer and a second woven textile layer connected to the first layer. The second layer is arranged between the first layer and the perforated acoustic structure.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_US2024351699A1 |
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 | ACOUSTIC PANEL FOR AN AIRCRAFT TURBOMACHINE |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T06%3A17%3A33IST&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=CARUEL,%20Pierre%20Charles&rft.date=2024-10-24&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2024351699A1%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 |