TURBOJET NACELLE COMPRISING AN INVERSER FLAP AND AN ADDITIONAL FLAP

L'invention concerne une nacelle (600) comportant un volet additionnel (602), un capot fixe et un capot mobile (207) mobile en translation, une fenêtre (210) délimitée par le capot fixe et le capot mobile (207), et ouverte entre une veine (202) et l'extérieur de la nacelle (600), un volet...

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Hauptverfasser: PIARD, Frédéric, PORTE, Alain, OBERLE, Patrick, BILLEROT, Vincent, LETAY, Benoit, OUNDJIAN, Franck, HARAMBURU, Eric, SURPLY, Thierry, SAUVALLE, Thomas
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creator PIARD, Frédéric
PORTE, Alain
OBERLE, Patrick
BILLEROT, Vincent
LETAY, Benoit
OUNDJIAN, Franck
HARAMBURU, Eric
SURPLY, Thierry
SAUVALLE, Thomas
description L'invention concerne une nacelle (600) comportant un volet additionnel (602), un capot fixe et un capot mobile (207) mobile en translation, une fenêtre (210) délimitée par le capot fixe et le capot mobile (207), et ouverte entre une veine (202) et l'extérieur de la nacelle (600), un volet inverseur (104) mobile en rotation entre une position fermée et une position ouverte, et un mécanisme d'entraînement coordonnant le passage de la position fermée à la position ouverte du volet inverseur (104) avec le passage de la position de fermeture à la position d'ouverture du capot mobile (207) et inversement. Le mécanisme d'entraînement assure, à partir de la position fermée: - une translation du capot mobile (207) vers la position d'ouverture, - puis une rotation (54) du volet inverseur (104) vers la position ouverte. A nacelle has a fixed cowl and a mobile cowl, which is movable along a translation path between closing and opening positions, a window delimited by the fixed cowl and the mobile cowl and open between an airflow and exterior of the nacelle, a reverser flap rotatably mounted to move between closed and open positions, and a drive mechanism configured to control passage of the reverser flap between the closed and open positions as the mobile cowl moves between the closed and open positions. From the closing/closed positions, the drive mechanism assures a translation of the mobile cowl and a rotation of the reverser flap toward their respective opening/open positions. From the open/opening positions, the drive mechanism assures a rotation of the reverser flap and a translation of the mobile cowl toward their respective closed/closing position. In some embodiments, the nacelle further includes an additional, or second, flap.
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Le mécanisme d'entraînement assure, à partir de la position fermée: - une translation du capot mobile (207) vers la position d'ouverture, - puis une rotation (54) du volet inverseur (104) vers la position ouverte. A nacelle has a fixed cowl and a mobile cowl, which is movable along a translation path between closing and opening positions, a window delimited by the fixed cowl and the mobile cowl and open between an airflow and exterior of the nacelle, a reverser flap rotatably mounted to move between closed and open positions, and a drive mechanism configured to control passage of the reverser flap between the closed and open positions as the mobile cowl moves between the closed and open positions. From the closing/closed positions, the drive mechanism assures a translation of the mobile cowl and a rotation of the reverser flap toward their respective opening/open positions. From the open/opening positions, the drive mechanism assures a rotation of the reverser flap and a translation of the mobile cowl toward their respective closed/closing position. In some embodiments, the nacelle further includes an additional, or second, flap.</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>2018</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=20180530&amp;DB=EPODOC&amp;CC=EP&amp;NR=3327274A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20180530&amp;DB=EPODOC&amp;CC=EP&amp;NR=3327274A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PIARD, Frédéric</creatorcontrib><creatorcontrib>PORTE, Alain</creatorcontrib><creatorcontrib>OBERLE, Patrick</creatorcontrib><creatorcontrib>BILLEROT, Vincent</creatorcontrib><creatorcontrib>LETAY, Benoit</creatorcontrib><creatorcontrib>OUNDJIAN, Franck</creatorcontrib><creatorcontrib>HARAMBURU, Eric</creatorcontrib><creatorcontrib>SURPLY, Thierry</creatorcontrib><creatorcontrib>SAUVALLE, Thomas</creatorcontrib><title>TURBOJET NACELLE COMPRISING AN INVERSER FLAP AND AN ADDITIONAL FLAP</title><description>L'invention concerne une nacelle (600) comportant un volet additionnel (602), un capot fixe et un capot mobile (207) mobile en translation, une fenêtre (210) délimitée par le capot fixe et le capot mobile (207), et ouverte entre une veine (202) et l'extérieur de la nacelle (600), un volet inverseur (104) mobile en rotation entre une position fermée et une position ouverte, et un mécanisme d'entraînement coordonnant le passage de la position fermée à la position ouverte du volet inverseur (104) avec le passage de la position de fermeture à la position d'ouverture du capot mobile (207) et inversement. 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From the open/opening positions, the drive mechanism assures a rotation of the reverser flap and a translation of the mobile cowl toward their respective closed/closing position. In some embodiments, the nacelle further includes an additional, or second, flap.</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAOCQ1y8vdyDVHwc3R29fFxVXD29w0I8gz29HNXcPRT8PQLcw0Kdg1ScPNxDAAKuIAEHV1cPEM8_f0cfcDCPAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXA2NjI3MjcxNHQmAglALxnKsY</recordid><startdate>20180530</startdate><enddate>20180530</enddate><creator>PIARD, Frédéric</creator><creator>PORTE, Alain</creator><creator>OBERLE, Patrick</creator><creator>BILLEROT, Vincent</creator><creator>LETAY, Benoit</creator><creator>OUNDJIAN, Franck</creator><creator>HARAMBURU, Eric</creator><creator>SURPLY, Thierry</creator><creator>SAUVALLE, Thomas</creator><scope>EVB</scope></search><sort><creationdate>20180530</creationdate><title>TURBOJET NACELLE COMPRISING AN INVERSER FLAP AND AN ADDITIONAL FLAP</title><author>PIARD, Frédéric ; PORTE, Alain ; OBERLE, Patrick ; BILLEROT, Vincent ; LETAY, Benoit ; OUNDJIAN, Franck ; HARAMBURU, Eric ; SURPLY, Thierry ; SAUVALLE, Thomas</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3327274A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</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>PIARD, Frédéric</creatorcontrib><creatorcontrib>PORTE, Alain</creatorcontrib><creatorcontrib>OBERLE, Patrick</creatorcontrib><creatorcontrib>BILLEROT, Vincent</creatorcontrib><creatorcontrib>LETAY, Benoit</creatorcontrib><creatorcontrib>OUNDJIAN, Franck</creatorcontrib><creatorcontrib>HARAMBURU, Eric</creatorcontrib><creatorcontrib>SURPLY, Thierry</creatorcontrib><creatorcontrib>SAUVALLE, Thomas</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PIARD, Frédéric</au><au>PORTE, Alain</au><au>OBERLE, Patrick</au><au>BILLEROT, Vincent</au><au>LETAY, Benoit</au><au>OUNDJIAN, Franck</au><au>HARAMBURU, Eric</au><au>SURPLY, Thierry</au><au>SAUVALLE, Thomas</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBOJET NACELLE COMPRISING AN INVERSER FLAP AND AN ADDITIONAL FLAP</title><date>2018-05-30</date><risdate>2018</risdate><abstract>L'invention concerne une nacelle (600) comportant un volet additionnel (602), un capot fixe et un capot mobile (207) mobile en translation, une fenêtre (210) délimitée par le capot fixe et le capot mobile (207), et ouverte entre une veine (202) et l'extérieur de la nacelle (600), un volet inverseur (104) mobile en rotation entre une position fermée et une position ouverte, et un mécanisme d'entraînement coordonnant le passage de la position fermée à la position ouverte du volet inverseur (104) avec le passage de la position de fermeture à la position d'ouverture du capot mobile (207) et inversement. Le mécanisme d'entraînement assure, à partir de la position fermée: - une translation du capot mobile (207) vers la position d'ouverture, - puis une rotation (54) du volet inverseur (104) vers la position ouverte. A nacelle has a fixed cowl and a mobile cowl, which is movable along a translation path between closing and opening positions, a window delimited by the fixed cowl and the mobile cowl and open between an airflow and exterior of the nacelle, a reverser flap rotatably mounted to move between closed and open positions, and a drive mechanism configured to control passage of the reverser flap between the closed and open positions as the mobile cowl moves between the closed and open positions. From the closing/closed positions, the drive mechanism assures a translation of the mobile cowl and a rotation of the reverser flap toward their respective opening/open positions. From the open/opening positions, the drive mechanism assures a rotation of the reverser flap and a translation of the mobile cowl toward their respective closed/closing position. In some embodiments, the nacelle further includes an additional, or second, flap.</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 TURBOJET NACELLE COMPRISING AN INVERSER FLAP AND AN ADDITIONAL FLAP
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