ASSEMBLY FOR A TURBOMACHINE

The invention relates to an assembly for a turbomachine, comprising: -a nacelle comprising an inlet lip which defines an air inlet, and-a device for modifying the geometry of the air inlet, comprising: -a first spout, and-a second spout, the first spout and the second spout being translatably movabl...

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Hauptverfasser: TANTOT, Nicolas Jérôme Jean, MARTIN PLEGUEZUELO, Alejandro, CARBONNEAU, Xavier, GARCIA ROSA, Nicolas, SIRVIN, Nicolas Joseph, CHANEZ, Philippe Gérard
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creator TANTOT, Nicolas Jérôme Jean
MARTIN PLEGUEZUELO, Alejandro
CARBONNEAU, Xavier
GARCIA ROSA, Nicolas
SIRVIN, Nicolas Joseph
CHANEZ, Philippe Gérard
description The invention relates to an assembly for a turbomachine, comprising: -a nacelle comprising an inlet lip which defines an air inlet, and-a device for modifying the geometry of the air inlet, comprising: -a first spout, and-a second spout, the first spout and the second spout being translatably movable in relation the nacelle between: -a first configuration, in which the first spout forms the inlet lip and the second spout extends inside the nacelle, and-a second configuration, in which the first spout extends away from the inlet lip, and the second spout forms the inlet lip so as to define an air flow channel between a downstream surface of the first spout and an upstream surface of the second spout.
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AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2023</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=20231102&amp;DB=EPODOC&amp;CC=US&amp;NR=2023349323A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20231102&amp;DB=EPODOC&amp;CC=US&amp;NR=2023349323A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TANTOT, Nicolas Jérôme Jean</creatorcontrib><creatorcontrib>MARTIN PLEGUEZUELO, Alejandro</creatorcontrib><creatorcontrib>CARBONNEAU, Xavier</creatorcontrib><creatorcontrib>GARCIA ROSA, Nicolas</creatorcontrib><creatorcontrib>SIRVIN, Nicolas Joseph</creatorcontrib><creatorcontrib>CHANEZ, Philippe Gérard</creatorcontrib><title>ASSEMBLY FOR A TURBOMACHINE</title><description>The invention relates to an assembly for a turbomachine, comprising: -a nacelle comprising an inlet lip which defines an air inlet, and-a device for modifying the geometry of the air inlet, comprising: -a first spout, and-a second spout, the first spout and the second spout being translatably movable in relation the nacelle between: -a first configuration, in which the first spout forms the inlet lip and the second spout extends inside the nacelle, and-a second configuration, in which the first spout extends away from the inlet lip, and the second spout forms the inlet lip so as to define an air flow channel between a downstream surface of the first spout and an upstream surface of the second spout.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB2DA529XXyiVRw8w9ScFQICQ1y8vd1dPbw9HPlYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXxocFGBkbGxiaWxkbGjobGxKkCAMrYIV0</recordid><startdate>20231102</startdate><enddate>20231102</enddate><creator>TANTOT, Nicolas Jérôme Jean</creator><creator>MARTIN PLEGUEZUELO, Alejandro</creator><creator>CARBONNEAU, Xavier</creator><creator>GARCIA ROSA, Nicolas</creator><creator>SIRVIN, Nicolas Joseph</creator><creator>CHANEZ, Philippe Gérard</creator><scope>EVB</scope></search><sort><creationdate>20231102</creationdate><title>ASSEMBLY FOR A TURBOMACHINE</title><author>TANTOT, Nicolas Jérôme Jean ; 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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
WEAPONS
title ASSEMBLY FOR A TURBOMACHINE
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