Gas exhaust cone for an aircraft turbojet, corresponding turbojet and engine plant

A gas ejection cone for an aircraft turbojet, the cone including a hollow main body defining, on the outside, a radially inner skin of an annular primary flow channel, and a device generating turbulence in the primary flow limiting jet noise, mounted so as to move on the main body so as to be able t...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	JOURNADE, FRÉDÉRIC, JOURNADE, JÉRÔME, HUBER, JÉRÔME
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	JOURNADE, FRÉDÉRIC JOURNADE, JÉRÔME HUBER, JÉRÔME
description	A gas ejection cone for an aircraft turbojet, the cone including a hollow main body defining, on the outside, a radially inner skin of an annular primary flow channel, and a device generating turbulence in the primary flow limiting jet noise, mounted so as to move on the main body so as to be able to be displaced from an extracted position in which the device projects toward downstream in relation to a downstream end of the hollow main body, and a retracted position in which the device is retracted into the hollow main body, and vice versa. Further, the device includes a cylindrical support body having an axis parallel to an axis of the ejection cone, and at least one fin supported by the body.
format	Patent
fullrecord	<record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2191124B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2191124B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2191124B13</originalsourceid><addsrcrecordid>eNrjZAhyTyxWSK3ISCwtLlFIzs9LVUjLL1JIzFNIzCxKLkpMK1EoKS1Kys9KLdEBShcVpRYX5OelZOalw8WBilMUUvPSM4F6C3IS80p4GFjTEnOKU3mhNDeDgptriLOHbmpBfjxQf2Jyal5qSbxrgJGhpaGhkYmToTERSgCd8Dee</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Gas exhaust cone for an aircraft turbojet, corresponding turbojet and engine plant</title><source>esp@cenet</source><creator>JOURNADE, FRÉDÉRIC ; JOURNADE, JÉRÔME ; HUBER, JÉRÔME</creator><creatorcontrib>JOURNADE, FRÉDÉRIC ; JOURNADE, JÉRÔME ; HUBER, JÉRÔME</creatorcontrib><description>A gas ejection cone for an aircraft turbojet, the cone including a hollow main body defining, on the outside, a radially inner skin of an annular primary flow channel, and a device generating turbulence in the primary flow limiting jet noise, mounted so as to move on the main body so as to be able to be displaced from an extracted position in which the device projects toward downstream in relation to a downstream end of the hollow main body, and a retracted position in which the device is retracted into the hollow main body, and vice versa. Further, the device includes a cylindrical support body having an axis parallel to an axis of the ejection cone, and at least one fin supported by the body.</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>2015</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=20151007&DB=EPODOC&CC=EP&NR=2191124B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20151007&DB=EPODOC&CC=EP&NR=2191124B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JOURNADE, FRÉDÉRIC</creatorcontrib><creatorcontrib>JOURNADE, JÉRÔME</creatorcontrib><creatorcontrib>HUBER, JÉRÔME</creatorcontrib><title>Gas exhaust cone for an aircraft turbojet, corresponding turbojet and engine plant</title><description>A gas ejection cone for an aircraft turbojet, the cone including a hollow main body defining, on the outside, a radially inner skin of an annular primary flow channel, and a device generating turbulence in the primary flow limiting jet noise, mounted so as to move on the main body so as to be able to be displaced from an extracted position in which the device projects toward downstream in relation to a downstream end of the hollow main body, and a retracted position in which the device is retracted into the hollow main body, and vice versa. Further, the device includes a cylindrical support body having an axis parallel to an axis of the ejection cone, and at least one fin supported by the body.</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAhyTyxWSK3ISCwtLlFIzs9LVUjLL1JIzFNIzCxKLkpMK1EoKS1Kys9KLdEBShcVpRYX5OelZOalw8WBilMUUvPSM4F6C3IS80p4GFjTEnOKU3mhNDeDgptriLOHbmpBfjxQf2Jyal5qSbxrgJGhpaGhkYmToTERSgCd8Dee</recordid><startdate>20151007</startdate><enddate>20151007</enddate><creator>JOURNADE, FRÉDÉRIC</creator><creator>JOURNADE, JÉRÔME</creator><creator>HUBER, JÉRÔME</creator><scope>EVB</scope></search><sort><creationdate>20151007</creationdate><title>Gas exhaust cone for an aircraft turbojet, corresponding turbojet and engine plant</title><author>JOURNADE, FRÉDÉRIC ; JOURNADE, JÉRÔME ; HUBER, JÉRÔME</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2191124B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2015</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>JOURNADE, FRÉDÉRIC</creatorcontrib><creatorcontrib>JOURNADE, JÉRÔME</creatorcontrib><creatorcontrib>HUBER, JÉRÔME</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JOURNADE, FRÉDÉRIC</au><au>JOURNADE, JÉRÔME</au><au>HUBER, JÉRÔME</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Gas exhaust cone for an aircraft turbojet, corresponding turbojet and engine plant</title><date>2015-10-07</date><risdate>2015</risdate><abstract>A gas ejection cone for an aircraft turbojet, the cone including a hollow main body defining, on the outside, a radially inner skin of an annular primary flow channel, and a device generating turbulence in the primary flow limiting jet noise, mounted so as to move on the main body so as to be able to be displaced from an extracted position in which the device projects toward downstream in relation to a downstream end of the hollow main body, and a retracted position in which the device is retracted into the hollow main body, and vice versa. Further, the device includes a cylindrical support body having an axis parallel to an axis of the ejection cone, and at least one fin supported by the body.</abstract><oa>free_for_read</oa></addata></record>
fulltext	fulltext_linktorsrc
identifier
ispartof
issn
language	eng ; fre ; ger
recordid	cdi_epo_espacenet_EP2191124B1
source	esp@cenet
subjects	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
title	Gas exhaust cone for an aircraft turbojet, corresponding turbojet and engine plant
url	https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-26T06%3A06%3A26IST&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=JOURNADE,%20FR%C3%89D%C3%89RIC&rft.date=2015-10-07&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2191124B1%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