DISTRIBUTEUR D'UNE TURBINE RADIALE DE TURBOMACHINE, TURBOMACHINE COMPRENANT UN TEL DISTRIBUTEUR ET SYSTEME DE CONDITIONNEMENT D'AIR COMPRENANT UNE TELLE TURBOMACHINE
The invention relates to an air conditioning system for an aircraft comprising a turbine engine comprising at least one radial turbine and a compressor, said radial turbine extending along a central axis (10) and comprising a wheel (20) equipped with vanes (21) mounted so as to be able to rotate abo...
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| creator | ROUMEAS, MATHIEU LAURIAU, PIERRE-THOMAS FOURAGNAN, JAMES CROS, SANDRINE BINDER, NICOLAS |
| description | The invention relates to an air conditioning system for an aircraft comprising a turbine engine comprising at least one radial turbine and a compressor, said radial turbine extending along a central axis (10) and comprising a wheel (20) equipped with vanes (21) mounted so as to be able to rotate about said central axis (10), a nozzle (30) arranged at the periphery of said wheel (20) comprising a plurality of variable-pitch blades (31) arranged around said central axis (10), and a volute (12) comprising an air inlet (12a) and an air outlet (12b) opening onto said plurality of variable-pitch blades (31), characterized in that said variable-pitch blades (31) are arranged around said central axis (10) between two nozzle casing walls (11a, 11b) delimiting an air passage section of said nozzle between them, each variable-pitch blade (31) further comprising means for axial displacement of the blade between the two casing walls (11a, 11b). |
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LAURIAU, PIERRE-THOMAS ; FOURAGNAN, JAMES ; CROS, SANDRINE ; BINDER, NICOLAS</creatorcontrib><description>The invention relates to an air conditioning system for an aircraft comprising a turbine engine comprising at least one radial turbine and a compressor, said radial turbine extending along a central axis (10) and comprising a wheel (20) equipped with vanes (21) mounted so as to be able to rotate about said central axis (10), a nozzle (30) arranged at the periphery of said wheel (20) comprising a plurality of variable-pitch blades (31) arranged around said central axis (10), and a volute (12) comprising an air inlet (12a) and an air outlet (12b) opening onto said plurality of variable-pitch blades (31), characterized in that said variable-pitch blades (31) are arranged around said central axis (10) between two nozzle casing walls (11a, 11b) delimiting an air passage section of said nozzle between them, each variable-pitch blade (31) further comprising means for axial displacement of the blade between the two casing walls (11a, 11b).</description><language>fre</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; 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=20220729&DB=EPODOC&CC=FR&NR=3082563B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220729&DB=EPODOC&CC=FR&NR=3082563B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ROUMEAS, MATHIEU</creatorcontrib><creatorcontrib>LAURIAU, PIERRE-THOMAS</creatorcontrib><creatorcontrib>FOURAGNAN, JAMES</creatorcontrib><creatorcontrib>CROS, SANDRINE</creatorcontrib><creatorcontrib>BINDER, NICOLAS</creatorcontrib><title>DISTRIBUTEUR D'UNE TURBINE RADIALE DE TURBOMACHINE, TURBOMACHINE COMPRENANT UN TEL DISTRIBUTEUR ET SYSTEME DE CONDITIONNEMENT D'AIR COMPRENANT UNE TELLE TURBOMACHINE</title><description>The invention relates to an air conditioning system for an aircraft comprising a turbine engine comprising at least one radial turbine and a compressor, said radial turbine extending along a central axis (10) and comprising a wheel (20) equipped with vanes (21) mounted so as to be able to rotate about said central axis (10), a nozzle (30) arranged at the periphery of said wheel (20) comprising a plurality of variable-pitch blades (31) arranged around said central axis (10), and a volute (12) comprising an air inlet (12a) and an air outlet (12b) opening onto said plurality of variable-pitch blades (31), characterized in that said variable-pitch blades (31) are arranged around said central axis (10) between two nozzle casing walls (11a, 11b) delimiting an air passage section of said nozzle between them, each variable-pitch blade (31) further comprising means for axial displacement of the blade between the two casing walls (11a, 11b).</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjb0KwjAUhbs4iPoOd-uioBbFNU1uaaC9keRmcCpF4iRaqK_kexp_lmxOh_Nx73em2VNpx1aXntFbULknBPa21DGtUFo0COqLTCtkHfkyaSBNe7RIghg8AWMDiRIZ3Mkxth-PNKQ0a0MUQfxQudA2VeDb0aST82xy6a9jWPxylkGFLOtVGO5dGIf-HG7h0VW2WB-2u31Rboo_Tl6IJ0ZJ</recordid><startdate>20220729</startdate><enddate>20220729</enddate><creator>ROUMEAS, MATHIEU</creator><creator>LAURIAU, PIERRE-THOMAS</creator><creator>FOURAGNAN, JAMES</creator><creator>CROS, SANDRINE</creator><creator>BINDER, NICOLAS</creator><scope>EVB</scope></search><sort><creationdate>20220729</creationdate><title>DISTRIBUTEUR D'UNE TURBINE RADIALE DE TURBOMACHINE, TURBOMACHINE COMPRENANT UN TEL DISTRIBUTEUR ET SYSTEME DE CONDITIONNEMENT D'AIR COMPRENANT UNE TELLE TURBOMACHINE</title><author>ROUMEAS, MATHIEU ; 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| recordid | cdi_epo_espacenet_FR3082563B1 |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | DISTRIBUTEUR D'UNE TURBINE RADIALE DE TURBOMACHINE, TURBOMACHINE COMPRENANT UN TEL DISTRIBUTEUR ET SYSTEME DE CONDITIONNEMENT D'AIR COMPRENANT UNE TELLE TURBOMACHINE |
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