THRUST REVERSER COMPRISING A SINGLE ACTUATOR FOR CONTROLLING A MOBILE COWLING
The invention relates to a thrust reverser (20) for an aircraft propulsion assembly, this reverser (20) comprising a mobile annular external structure (22), a single actuator (25) for controlling the position of this mobile external structure (22) and a device for guiding (40) the mobile external st...
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| creator | BRAVIN, Fabien CHAPELAIN, Loïc CHARLIAC, Fabien CARUEL, Pierre |
| description | The invention relates to a thrust reverser (20) for an aircraft propulsion assembly, this reverser (20) comprising a mobile annular external structure (22), a single actuator (25) for controlling the position of this mobile external structure (22) and a device for guiding (40) the mobile external structure (22) when changing its position. The actuator (25) and the guiding device (40) are housed in a fairing of a pylon of the propulsion assembly to a wing or fuselage of the aircraft.
L'invention se rapporte à un inverseur de poussée (20) pour ensemble propulsif d'aéronef, cet inverseur (20) comprenant une structure externe mobile (22) annulaire, un unique vérin (25) de commande de la position de cette structure externe mobile (22) et un dispositif de guidage (40) de la structure externe mobile (22) lors de son changement de position. Le vérin (25) et le dispositif de guidage (40) sont logés dans un carénage d'un mât d'accrochage de l'ensemble propulsif à une voilure ou un fuselage de l'aéronef. |
| format | Patent |
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L'invention se rapporte à un inverseur de poussée (20) pour ensemble propulsif d'aéronef, cet inverseur (20) comprenant une structure externe mobile (22) annulaire, un unique vérin (25) de commande de la position de cette structure externe mobile (22) et un dispositif de guidage (40) de la structure externe mobile (22) lors de son changement de position. Le vérin (25) et le dispositif de guidage (40) sont logés dans un carénage d'un mât d'accrochage de l'ensemble propulsif à une voilure ou un fuselage de l'aéronef.</description><language>eng ; fre</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2021</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=20210311&DB=EPODOC&CC=WO&NR=2021044096A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210311&DB=EPODOC&CC=WO&NR=2021044096A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BRAVIN, Fabien</creatorcontrib><creatorcontrib>CHAPELAIN, Loïc</creatorcontrib><creatorcontrib>CHARLIAC, Fabien</creatorcontrib><creatorcontrib>CARUEL, Pierre</creatorcontrib><title>THRUST REVERSER COMPRISING A SINGLE ACTUATOR FOR CONTROLLING A MOBILE COWLING</title><description>The invention relates to a thrust reverser (20) for an aircraft propulsion assembly, this reverser (20) comprising a mobile annular external structure (22), a single actuator (25) for controlling the position of this mobile external structure (22) and a device for guiding (40) the mobile external structure (22) when changing its position. The actuator (25) and the guiding device (40) are housed in a fairing of a pylon of the propulsion assembly to a wing or fuselage of the aircraft.
L'invention se rapporte à un inverseur de poussée (20) pour ensemble propulsif d'aéronef, cet inverseur (20) comprenant une structure externe mobile (22) annulaire, un unique vérin (25) de commande de la position de cette structure externe mobile (22) et un dispositif de guidage (40) de la structure externe mobile (22) lors de son changement de position. Le vérin (25) et le dispositif de guidage (40) sont logés dans un carénage d'un mât d'accrochage de l'ensemble propulsif à une voilure ou un fuselage de l'aéronef.</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>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPAN8QgKDQ5RCHINcw0Kdg1ScPb3DQjyDPb0c1dwVABRPq4Kjs4hoY4h_kEKbv4gBX4hQf4-PhAVvv5OnkAVzv7hIAEeBta0xJziVF4ozc2g7OYa4uyhm1qQH59aXJCYnJqXWhIf7m9kYGRoYGJiYGnmaGhMnCoAxj4vUw</recordid><startdate>20210311</startdate><enddate>20210311</enddate><creator>BRAVIN, Fabien</creator><creator>CHAPELAIN, Loïc</creator><creator>CHARLIAC, Fabien</creator><creator>CARUEL, Pierre</creator><scope>EVB</scope></search><sort><creationdate>20210311</creationdate><title>THRUST REVERSER COMPRISING A SINGLE ACTUATOR FOR CONTROLLING A MOBILE COWLING</title><author>BRAVIN, Fabien ; CHAPELAIN, Loïc ; CHARLIAC, Fabien ; CARUEL, Pierre</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2021044096A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2021</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>BRAVIN, Fabien</creatorcontrib><creatorcontrib>CHAPELAIN, Loïc</creatorcontrib><creatorcontrib>CHARLIAC, Fabien</creatorcontrib><creatorcontrib>CARUEL, Pierre</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BRAVIN, Fabien</au><au>CHAPELAIN, Loïc</au><au>CHARLIAC, Fabien</au><au>CARUEL, Pierre</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>THRUST REVERSER COMPRISING A SINGLE ACTUATOR FOR CONTROLLING A MOBILE COWLING</title><date>2021-03-11</date><risdate>2021</risdate><abstract>The invention relates to a thrust reverser (20) for an aircraft propulsion assembly, this reverser (20) comprising a mobile annular external structure (22), a single actuator (25) for controlling the position of this mobile external structure (22) and a device for guiding (40) the mobile external structure (22) when changing its position. The actuator (25) and the guiding device (40) are housed in a fairing of a pylon of the propulsion assembly to a wing or fuselage of the aircraft.
L'invention se rapporte à un inverseur de poussée (20) pour ensemble propulsif d'aéronef, cet inverseur (20) comprenant une structure externe mobile (22) annulaire, un unique vérin (25) de commande de la position de cette structure externe mobile (22) et un dispositif de guidage (40) de la structure externe mobile (22) lors de son changement de position. Le vérin (25) et le dispositif de guidage (40) sont logés dans un carénage d'un mât d'accrochage de l'ensemble propulsif à une voilure ou un fuselage de l'aéronef.</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 | THRUST REVERSER COMPRISING A SINGLE ACTUATOR FOR CONTROLLING A MOBILE COWLING |
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