Closure system for an orifice of an air-intake duct of a combustion chamber of a ramjet, as well as ramjet and missile comprising said system

The ramjet engine (2), designed for a missile (1) launched in a rocket mode with the ramjet taking over at a given speed, has its combustion chamber air intake ducts (7) closed by shutters (15) with glass plates (18). The plates have protective elastomer coverings, while on the inside of the ducts t...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: CARTON, LAURENT
Format: Patent
Sprache:eng ; fre ; ger
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 CARTON, LAURENT
description The ramjet engine (2), designed for a missile (1) launched in a rocket mode with the ramjet taking over at a given speed, has its combustion chamber air intake ducts (7) closed by shutters (15) with glass plates (18). The plates have protective elastomer coverings, while on the inside of the ducts there are components (17), e.g. operated pyrotechnically, that break the shutter plates when the missile is travelling at a given speed, enabling the ramjet mode of the engine to take over from the rocket mode.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP1367251B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP1367251B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP1367251B13</originalsourceid><addsrcrecordid>eNqNjT0OgkAQhWksjHqHOYAUSNRegrG0sCfDMquj-5edJcZDeGdFOIDVy_vyfubZuzJe-kggL0lkQfsI6MBH1qwIvB4ccszZJXwQdL1KPwrK27aXxN6BuqFtKY48or1TWgMKPMmYQUf0XerAsggbGtohsrC7giB30_0ym2k0QqtJFxkc60t1yin4hiSgIkepqc9FudtvtsWhKP-IfAAMBEx7</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Closure system for an orifice of an air-intake duct of a combustion chamber of a ramjet, as well as ramjet and missile comprising said system</title><source>esp@cenet</source><creator>CARTON, LAURENT</creator><creatorcontrib>CARTON, LAURENT</creatorcontrib><description>The ramjet engine (2), designed for a missile (1) launched in a rocket mode with the ramjet taking over at a given speed, has its combustion chamber air intake ducts (7) closed by shutters (15) with glass plates (18). The plates have protective elastomer coverings, while on the inside of the ducts there are components (17), e.g. operated pyrotechnically, that break the shutter plates when the missile is travelling at a given speed, enabling the ramjet mode of the engine to take over from the rocket mode.</description><language>eng ; fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2006</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=20061102&amp;DB=EPODOC&amp;CC=EP&amp;NR=1367251B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20061102&amp;DB=EPODOC&amp;CC=EP&amp;NR=1367251B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CARTON, LAURENT</creatorcontrib><title>Closure system for an orifice of an air-intake duct of a combustion chamber of a ramjet, as well as ramjet and missile comprising said system</title><description>The ramjet engine (2), designed for a missile (1) launched in a rocket mode with the ramjet taking over at a given speed, has its combustion chamber air intake ducts (7) closed by shutters (15) with glass plates (18). The plates have protective elastomer coverings, while on the inside of the ducts there are components (17), e.g. operated pyrotechnically, that break the shutter plates when the missile is travelling at a given speed, enabling the ramjet mode of the engine to take over from the rocket mode.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</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>2006</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjT0OgkAQhWksjHqHOYAUSNRegrG0sCfDMquj-5edJcZDeGdFOIDVy_vyfubZuzJe-kggL0lkQfsI6MBH1qwIvB4ccszZJXwQdL1KPwrK27aXxN6BuqFtKY48or1TWgMKPMmYQUf0XerAsggbGtohsrC7giB30_0ym2k0QqtJFxkc60t1yin4hiSgIkepqc9FudtvtsWhKP-IfAAMBEx7</recordid><startdate>20061102</startdate><enddate>20061102</enddate><creator>CARTON, LAURENT</creator><scope>EVB</scope></search><sort><creationdate>20061102</creationdate><title>Closure system for an orifice of an air-intake duct of a combustion chamber of a ramjet, as well as ramjet and missile comprising said system</title><author>CARTON, LAURENT</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP1367251B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2006</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</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>CARTON, LAURENT</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CARTON, LAURENT</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Closure system for an orifice of an air-intake duct of a combustion chamber of a ramjet, as well as ramjet and missile comprising said system</title><date>2006-11-02</date><risdate>2006</risdate><abstract>The ramjet engine (2), designed for a missile (1) launched in a rocket mode with the ramjet taking over at a given speed, has its combustion chamber air intake ducts (7) closed by shutters (15) with glass plates (18). The plates have protective elastomer coverings, while on the inside of the ducts there are components (17), e.g. operated pyrotechnically, that break the shutter plates when the missile is travelling at a given speed, enabling the ramjet mode of the engine to take over from the rocket mode.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP1367251B1
source esp@cenet
subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title Closure system for an orifice of an air-intake duct of a combustion chamber of a ramjet, as well as ramjet and missile comprising said system
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-18T02%3A44%3A35IST&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=CARTON,%20LAURENT&rft.date=2006-11-02&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP1367251B1%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