Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise

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:	HUBER JEROME, JOURNADE FREDERIC, JOURNADE JEROME
Format:	Patent
Sprache:	eng
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	HUBER JEROME JOURNADE FREDERIC JOURNADE JEROME
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_US8516824B2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US8516824B2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US8516824B23</originalsourceid><addsrcrecordid>eNqNzDsOwjAQRdE0FAjYw2yAgvBRahCfHqijwRknEzljYztEdCydEFgA1Sve0R0nryMGoJpUZCugrBBo6wEFkL3yqCPE1t9sTRHo3rJzVEDHsQKEgh6svr4kIY-RpRx4a0j6h_sKOM8N-idoYzsw3PCgPj2xHGiajDSaQLPfThI47C-705yczSk4VH065tdztl5ssnS1TZd_kDd9nEjf</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise</title><source>esp@cenet</source><creator>HUBER JEROME ; JOURNADE FREDERIC ; JOURNADE JEROME</creator><creatorcontrib>HUBER JEROME ; JOURNADE FREDERIC ; JOURNADE JEROME</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</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2013</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=20130827&DB=EPODOC&CC=US&NR=8516824B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20130827&DB=EPODOC&CC=US&NR=8516824B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HUBER JEROME</creatorcontrib><creatorcontrib>JOURNADE FREDERIC</creatorcontrib><creatorcontrib>JOURNADE JEROME</creatorcontrib><title>Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise</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>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNzDsOwjAQRdE0FAjYw2yAgvBRahCfHqijwRknEzljYztEdCydEFgA1Sve0R0nryMGoJpUZCugrBBo6wEFkL3yqCPE1t9sTRHo3rJzVEDHsQKEgh6svr4kIY-RpRx4a0j6h_sKOM8N-idoYzsw3PCgPj2xHGiajDSaQLPfThI47C-705yczSk4VH065tdztl5ssnS1TZd_kDd9nEjf</recordid><startdate>20130827</startdate><enddate>20130827</enddate><creator>HUBER JEROME</creator><creator>JOURNADE FREDERIC</creator><creator>JOURNADE JEROME</creator><scope>EVB</scope></search><sort><creationdate>20130827</creationdate><title>Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise</title><author>HUBER JEROME ; JOURNADE FREDERIC ; JOURNADE JEROME</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US8516824B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2013</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>HUBER JEROME</creatorcontrib><creatorcontrib>JOURNADE FREDERIC</creatorcontrib><creatorcontrib>JOURNADE JEROME</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HUBER JEROME</au><au>JOURNADE FREDERIC</au><au>JOURNADE JEROME</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise</title><date>2013-08-27</date><risdate>2013</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
recordid	cdi_epo_espacenet_US8516824B2
source	esp@cenet
subjects	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
title	Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise
url	https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-26T18%3A20%3A57IST&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=HUBER%20JEROME&rft.date=2013-08-27&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS8516824B2%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