TURBINE ENGINE SEPARATE FLOW MIXER

TURBINE ENGINE SEPARATE FLOW MIXER

The invention relates to a turbine engine separate flow mixer centered on a longitudinal axis, comprising an exhaust housing, a shroud directly connected to the exhaust housing and intended to mix the flows originating in the turbine engine, said shroud comprising a metal sheet formed by a successio...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: VINCENT, Pierre, LAMBERT, Olivier, Arnaud, Fabien, TELMAN, Cyrille, AMOEDO, Simon, José, Pierre
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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 VINCENT, Pierre
LAMBERT, Olivier, Arnaud, Fabien
TELMAN, Cyrille
AMOEDO, Simon, José, Pierre
description The invention relates to a turbine engine separate flow mixer centered on a longitudinal axis, comprising an exhaust housing, a shroud directly connected to the exhaust housing and intended to mix the flows originating in the turbine engine, said shroud comprising a metal sheet formed by a succession of first and second longitudinal strips distributed circumferentially around the longitudinal axis of the mixer by circumferentially placing the second strips on either side of the first strips, the first and second strips being configured to form the shroud when at rest and grooves in the shroud when operating, the grooves being defined by an alternation of internal lobes and of external lobes.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3963196B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3963196B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3963196B13</originalsourceid><addsrcrecordid>eNrjZFAKCQ1y8vRzVXD1cwdRwa4BjkGOIa4Kbj7-4Qq-nhGuQTwMrGmJOcWpvFCam0HBzTXE2UM3tSA_PrW4IDE5NS-1JN41wNjSzNjQ0szJ0JgIJQD3ryIe</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>TURBINE ENGINE SEPARATE FLOW MIXER</title><source>esp@cenet</source><creator>VINCENT, Pierre ; LAMBERT, Olivier, Arnaud, Fabien ; TELMAN, Cyrille ; AMOEDO, Simon, José, Pierre</creator><creatorcontrib>VINCENT, Pierre ; LAMBERT, Olivier, Arnaud, Fabien ; TELMAN, Cyrille ; AMOEDO, Simon, José, Pierre</creatorcontrib><description>The invention relates to a turbine engine separate flow mixer centered on a longitudinal axis, comprising an exhaust housing, a shroud directly connected to the exhaust housing and intended to mix the flows originating in the turbine engine, said shroud comprising a metal sheet formed by a succession of first and second longitudinal strips distributed circumferentially around the longitudinal axis of the mixer by circumferentially placing the second strips on either side of the first strips, the first and second strips being configured to form the shroud when at rest and grooves in the shroud when operating, the grooves being defined by an alternation of internal lobes and of external lobes.</description><language>eng ; fre ; ger</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2023</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=20230712&amp;DB=EPODOC&amp;CC=EP&amp;NR=3963196B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20230712&amp;DB=EPODOC&amp;CC=EP&amp;NR=3963196B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>VINCENT, Pierre</creatorcontrib><creatorcontrib>LAMBERT, Olivier, Arnaud, Fabien</creatorcontrib><creatorcontrib>TELMAN, Cyrille</creatorcontrib><creatorcontrib>AMOEDO, Simon, José, Pierre</creatorcontrib><title>TURBINE ENGINE SEPARATE FLOW MIXER</title><description>The invention relates to a turbine engine separate flow mixer centered on a longitudinal axis, comprising an exhaust housing, a shroud directly connected to the exhaust housing and intended to mix the flows originating in the turbine engine, said shroud comprising a metal sheet formed by a succession of first and second longitudinal strips distributed circumferentially around the longitudinal axis of the mixer by circumferentially placing the second strips on either side of the first strips, the first and second strips being configured to form the shroud when at rest and grooves in the shroud when operating, the grooves being defined by an alternation of internal lobes and of external lobes.</description><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAKCQ1y8vRzVXD1cwdRwa4BjkGOIa4Kbj7-4Qq-nhGuQTwMrGmJOcWpvFCam0HBzTXE2UM3tSA_PrW4IDE5NS-1JN41wNjSzNjQ0szJ0JgIJQD3ryIe</recordid><startdate>20230712</startdate><enddate>20230712</enddate><creator>VINCENT, Pierre</creator><creator>LAMBERT, Olivier, Arnaud, Fabien</creator><creator>TELMAN, Cyrille</creator><creator>AMOEDO, Simon, José, Pierre</creator><scope>EVB</scope></search><sort><creationdate>20230712</creationdate><title>TURBINE ENGINE SEPARATE FLOW MIXER</title><author>VINCENT, Pierre ; LAMBERT, Olivier, Arnaud, Fabien ; TELMAN, Cyrille ; AMOEDO, Simon, José, Pierre</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3963196B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>VINCENT, Pierre</creatorcontrib><creatorcontrib>LAMBERT, Olivier, Arnaud, Fabien</creatorcontrib><creatorcontrib>TELMAN, Cyrille</creatorcontrib><creatorcontrib>AMOEDO, Simon, José, Pierre</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>VINCENT, Pierre</au><au>LAMBERT, Olivier, Arnaud, Fabien</au><au>TELMAN, Cyrille</au><au>AMOEDO, Simon, José, Pierre</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBINE ENGINE SEPARATE FLOW MIXER</title><date>2023-07-12</date><risdate>2023</risdate><abstract>The invention relates to a turbine engine separate flow mixer centered on a longitudinal axis, comprising an exhaust housing, a shroud directly connected to the exhaust housing and intended to mix the flows originating in the turbine engine, said shroud comprising a metal sheet formed by a succession of first and second longitudinal strips distributed circumferentially around the longitudinal axis of the mixer by circumferentially placing the second strips on either side of the first strips, the first and second strips being configured to form the shroud when at rest and grooves in the shroud when operating, the grooves being defined by an alternation of internal lobes and of external lobes.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3963196B1
source esp@cenet
subjects BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title TURBINE ENGINE SEPARATE FLOW MIXER
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-18T17%3A52%3A48IST&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=VINCENT,%20Pierre&rft.date=2023-07-12&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3963196B1%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