Thrust orienting nozzle

Thrust orienting nozzle

The present invention relates to a thrust orienting nozzle, shaped in such a way as to divide a principal propulsion gas flow coming from at least one gas generator into a first flow and a second flow for an ejection in a first half-nozzle and in a second half-nozzle and comprising at least one of f...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: DARIS THOMAS, PAGE ALAIN, SCHENHER FREDERIC, DOUSSINAULT MARC, PROUTEAU JACKIE
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 DARIS THOMAS
PAGE ALAIN
SCHENHER FREDERIC
DOUSSINAULT MARC
PROUTEAU JACKIE
description The present invention relates to a thrust orienting nozzle, shaped in such a way as to divide a principal propulsion gas flow coming from at least one gas generator into a first flow and a second flow for an ejection in a first half-nozzle and in a second half-nozzle and comprising at least one of following two piloting means: a means of dividing the principal flow into each of the two half-nozzles, and a means of orienting the thrust vector produced by each of the two half-nozzles. The invention applies in particular to the yaw control of an aircraft without a vertical tail unit.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US7631486B2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US7631486B2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US7631486B23</originalsourceid><addsrcrecordid>eNrjZBAPySgqLS5RyC_KTM0rycxLV8jLr6rKSeVhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGhweZmxoYmFmZORsZEKAEAsbciEQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Thrust orienting nozzle</title><source>esp@cenet</source><creator>DARIS THOMAS ; PAGE ALAIN ; SCHENHER FREDERIC ; DOUSSINAULT MARC ; PROUTEAU JACKIE</creator><creatorcontrib>DARIS THOMAS ; PAGE ALAIN ; SCHENHER FREDERIC ; DOUSSINAULT MARC ; PROUTEAU JACKIE</creatorcontrib><description>The present invention relates to a thrust orienting nozzle, shaped in such a way as to divide a principal propulsion gas flow coming from at least one gas generator into a first flow and a second flow for an ejection in a first half-nozzle and in a second half-nozzle and comprising at least one of following two piloting means: a means of dividing the principal flow into each of the two half-nozzles, and a means of orienting the thrust vector produced by each of the two half-nozzles. The invention applies in particular to the yaw control of an aircraft without a vertical tail unit.</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>2009</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=20091215&amp;DB=EPODOC&amp;CC=US&amp;NR=7631486B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76418</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20091215&amp;DB=EPODOC&amp;CC=US&amp;NR=7631486B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DARIS THOMAS</creatorcontrib><creatorcontrib>PAGE ALAIN</creatorcontrib><creatorcontrib>SCHENHER FREDERIC</creatorcontrib><creatorcontrib>DOUSSINAULT MARC</creatorcontrib><creatorcontrib>PROUTEAU JACKIE</creatorcontrib><title>Thrust orienting nozzle</title><description>The present invention relates to a thrust orienting nozzle, shaped in such a way as to divide a principal propulsion gas flow coming from at least one gas generator into a first flow and a second flow for an ejection in a first half-nozzle and in a second half-nozzle and comprising at least one of following two piloting means: a means of dividing the principal flow into each of the two half-nozzles, and a means of orienting the thrust vector produced by each of the two half-nozzles. The invention applies in particular to the yaw control of an aircraft without a vertical tail unit.</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>2009</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBAPySgqLS5RyC_KTM0rycxLV8jLr6rKSeVhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGhweZmxoYmFmZORsZEKAEAsbciEQ</recordid><startdate>20091215</startdate><enddate>20091215</enddate><creator>DARIS THOMAS</creator><creator>PAGE ALAIN</creator><creator>SCHENHER FREDERIC</creator><creator>DOUSSINAULT MARC</creator><creator>PROUTEAU JACKIE</creator><scope>EVB</scope></search><sort><creationdate>20091215</creationdate><title>Thrust orienting nozzle</title><author>DARIS THOMAS ; PAGE ALAIN ; SCHENHER FREDERIC ; DOUSSINAULT MARC ; PROUTEAU JACKIE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US7631486B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2009</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>DARIS THOMAS</creatorcontrib><creatorcontrib>PAGE ALAIN</creatorcontrib><creatorcontrib>SCHENHER FREDERIC</creatorcontrib><creatorcontrib>DOUSSINAULT MARC</creatorcontrib><creatorcontrib>PROUTEAU JACKIE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DARIS THOMAS</au><au>PAGE ALAIN</au><au>SCHENHER FREDERIC</au><au>DOUSSINAULT MARC</au><au>PROUTEAU JACKIE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Thrust orienting nozzle</title><date>2009-12-15</date><risdate>2009</risdate><abstract>The present invention relates to a thrust orienting nozzle, shaped in such a way as to divide a principal propulsion gas flow coming from at least one gas generator into a first flow and a second flow for an ejection in a first half-nozzle and in a second half-nozzle and comprising at least one of following two piloting means: a means of dividing the principal flow into each of the two half-nozzles, and a means of orienting the thrust vector produced by each of the two half-nozzles. The invention applies in particular to the yaw control of an aircraft without a vertical tail unit.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_US7631486B2
source esp@cenet
subjects BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title Thrust orienting nozzle
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-08T22%3A58%3A11IST&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=DARIS%20THOMAS&rft.date=2009-12-15&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS7631486B2%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