AIR OUTLET FOR AN AIRCRAFT TURBOJET ENGINE NACELLE COMPRISING A STRAIGHTENING DEVICE FOR SUPPORTING A REVERSE THRUST PHASE
Disclosed is an air outlet of a nacelle for an aircraft turbojet engine, the nacelle forming a solid of revolution about a longitudinal axis, the air outlet having a straightening device having a plurality of flaps mounted circumferentially and protruding, each flap being mounted pivoting around a p...
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| creator | MINCU, Daniel-Ciprian CHANEZ, Philippe Gérard |
| description | Disclosed is an air outlet of a nacelle for an aircraft turbojet engine, the nacelle forming a solid of revolution about a longitudinal axis, the air outlet having a straightening device having a plurality of flaps mounted circumferentially and protruding, each flap being mounted pivoting around a pivot axis, forming, with respect to the longitudinal axis, an angle of convergence in a radial plane, between a closed position, in which each flap extends along the pivot axis in the aerodynamic prolongation of the trailing edge in order to support a thrust phase and a deployed position, in which each flap extends in a deployed plane forming an angle of deployment with respect to the closed position about the pivot axis, so as to support a reverse thrust phase. |
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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&date=20221214&DB=EPODOC&CC=EP&NR=4100638A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221214&DB=EPODOC&CC=EP&NR=4100638A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MINCU, Daniel-Ciprian</creatorcontrib><creatorcontrib>CHANEZ, Philippe Gérard</creatorcontrib><title>AIR OUTLET FOR AN AIRCRAFT TURBOJET ENGINE NACELLE COMPRISING A STRAIGHTENING DEVICE FOR SUPPORTING A REVERSE THRUST PHASE</title><description>Disclosed is an air outlet of a nacelle for an aircraft turbojet engine, the nacelle forming a solid of revolution about a longitudinal axis, the air outlet having a straightening device having a plurality of flaps mounted circumferentially and protruding, each flap being mounted pivoting around a pivot axis, forming, with respect to the longitudinal axis, an angle of convergence in a radial plane, between a closed position, in which each flap extends along the pivot axis in the aerodynamic prolongation of the trailing edge in order to support a thrust phase and a deployed position, in which each flap extends in a deployed plane forming an angle of deployment with respect to the closed position about the pivot axis, so as to support a reverse thrust phase.</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjE0KwjAQhbtxIeod5gJCS0XcjnHaRGoSJpNuS5G4Ei3Ulae3_hzA1eO97-PNsycaBhelIYHKMaCFaVGMlYBE3rvjBMjWxhJYVNQ0BMqdPJtgbA0IQRhNrYXsux-oNYo-TyF671i-FlNLHAhEcwwCXmOgZTa79NcxrX65yKAiUXqdhnuXxqE_p1t6dOQ3RZ5vyx0W5R_KC5IZOiY</recordid><startdate>20221214</startdate><enddate>20221214</enddate><creator>MINCU, Daniel-Ciprian</creator><creator>CHANEZ, Philippe Gérard</creator><scope>EVB</scope></search><sort><creationdate>20221214</creationdate><title>AIR OUTLET FOR AN AIRCRAFT TURBOJET ENGINE NACELLE COMPRISING A STRAIGHTENING DEVICE FOR SUPPORTING A REVERSE THRUST PHASE</title><author>MINCU, Daniel-Ciprian ; CHANEZ, Philippe Gérard</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4100638A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</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>MINCU, Daniel-Ciprian</creatorcontrib><creatorcontrib>CHANEZ, Philippe Gérard</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MINCU, Daniel-Ciprian</au><au>CHANEZ, Philippe Gérard</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIR OUTLET FOR AN AIRCRAFT TURBOJET ENGINE NACELLE COMPRISING A STRAIGHTENING DEVICE FOR SUPPORTING A REVERSE THRUST PHASE</title><date>2022-12-14</date><risdate>2022</risdate><abstract>Disclosed is an air outlet of a nacelle for an aircraft turbojet engine, the nacelle forming a solid of revolution about a longitudinal axis, the air outlet having a straightening device having a plurality of flaps mounted circumferentially and protruding, each flap being mounted pivoting around a pivot axis, forming, with respect to the longitudinal axis, an angle of convergence in a radial plane, between a closed position, in which each flap extends along the pivot axis in the aerodynamic prolongation of the trailing edge in order to support a thrust phase and a deployed position, in which each flap extends in a deployed plane forming an angle of deployment with respect to the closed position about the pivot axis, so as to support a reverse thrust phase.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP4100638A1 |
| source | esp@cenet |
| subjects | BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | AIR OUTLET FOR AN AIRCRAFT TURBOJET ENGINE NACELLE COMPRISING A STRAIGHTENING DEVICE FOR SUPPORTING A REVERSE THRUST PHASE |
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