EJECTION CONE HAVING A FLEXIBLE AERODYNAMIC ATTACHMENT

EJECTION CONE HAVING A FLEXIBLE AERODYNAMIC ATTACHMENT

The invention relates to an assembly for an aircraft turbomachine, comprising a central element (1) for the ejection of gas, and a connecting flange (9) interposed between, upstream, a gas outlet (22a) made of metal for a turbomachine, and, at the downstream end, the central element (1). The connect...

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Hauptverfasser: CONETE, Eric, CARRERE, Benoit
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
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creator CONETE, Eric
CARRERE, Benoit
description The invention relates to an assembly for an aircraft turbomachine, comprising a central element (1) for the ejection of gas, and a connecting flange (9) interposed between, upstream, a gas outlet (22a) made of metal for a turbomachine, and, at the downstream end, the central element (1). The connecting flange comprises an annular portion (9a) and flexible tabs (11) having axially:a first end (111a) where the tab is connected to the said annular portion, anda second free end (111b), projecting radially inwardly with respect to the first end and to which said tab is attached with the central element (1).
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The connecting flange comprises an annular portion (9a) and flexible tabs (11) having axially:a first end (111a) where the tab is connected to the said annular portion, anda second free end (111b), projecting radially inwardly with respect to the first end and to which said tab is attached with the central element (1).</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>2022</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=20220713&amp;DB=EPODOC&amp;CC=EP&amp;NR=4025780A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25553,76306</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220713&amp;DB=EPODOC&amp;CC=EP&amp;NR=4025780A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CONETE, Eric</creatorcontrib><creatorcontrib>CARRERE, Benoit</creatorcontrib><title>EJECTION CONE HAVING A FLEXIBLE AERODYNAMIC ATTACHMENT</title><description>The invention relates to an assembly for an aircraft turbomachine, comprising a central element (1) for the ejection of gas, and a connecting flange (9) interposed between, upstream, a gas outlet (22a) made of metal for a turbomachine, and, at the downstream end, the central element (1). 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The connecting flange comprises an annular portion (9a) and flexible tabs (11) having axially:a first end (111a) where the tab is connected to the said annular portion, anda second free end (111b), projecting radially inwardly with respect to the first end and to which said tab is attached with the central element (1).</abstract><oa>free_for_read</oa></addata></record>
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subjects BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title EJECTION CONE HAVING A FLEXIBLE AERODYNAMIC ATTACHMENT
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