SYSTEM FOR CONTROLLING VARIABLE GEOMETRY EQUIPMENT OF A GAS TURBINE ENGINE ESPECIALLY COMPRISING A GUIDING TRACK CONNECTION
The invention relates to a system for controlling at least two sets of variable geometry equipment (10, 110) of a gas turbine engine comprising at least one first body and a second body, the first set of equipment (10) being a stage of variable stator vanes of a compressor of the first body moving b...
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| creator | GAULLY, BRUNO ROBERT COLOTTE, BAPTISTE BENOIT |
| description | The invention relates to a system for controlling at least two sets of variable geometry equipment (10, 110) of a gas turbine engine comprising at least one first body and a second body, the first set of equipment (10) being a stage of variable stator vanes of a compressor of the first body moving between a closed position during idling and an open position at high speed, and the second set of equipment (110) being at least one bleed valve of a compressor of the second body moving between an open position during idling and a closed position at high speed. The system according to the invention is characterised in that it comprises an actuator (24) that actuates the two sets of equipment.
La présente invention porte sur un système de commande d'au moins deux équipements (10, 110) à géométrie variable d'un moteur à turbine à gaz comportant au moins un premier corps et un deuxième corps, le premier équipement (10) étant un étage d'aubes de stator à angle de calage variable d'un compresseur du premier corps évoluant entre une position fermée au ralenti et une position ouverte à fort régime, le second équipement (110) étant au moins une vanne de décharge d'un compresseur du deuxième corps évoluant entre une position ouverte au ralenti et une position fermée à fort régime; il est caractérisé par le fait qu'il comporte un actionneur (24) qui actionne les deux équipements. |
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La présente invention porte sur un système de commande d'au moins deux équipements (10, 110) à géométrie variable d'un moteur à turbine à gaz comportant au moins un premier corps et un deuxième corps, le premier équipement (10) étant un étage d'aubes de stator à angle de calage variable d'un compresseur du premier corps évoluant entre une position fermée au ralenti et une position ouverte à fort régime, le second équipement (110) étant au moins une vanne de décharge d'un compresseur du deuxième corps évoluant entre une position ouverte au ralenti et une position fermée à fort régime; il est caractérisé par le fait qu'il comporte un actionneur (24) qui actionne les deux équipements.</description><language>eng ; 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>2016</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=20160809&DB=EPODOC&CC=CA&NR=2738215C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160809&DB=EPODOC&CC=CA&NR=2738215C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GAULLY, BRUNO ROBERT</creatorcontrib><creatorcontrib>COLOTTE, BAPTISTE BENOIT</creatorcontrib><title>SYSTEM FOR CONTROLLING VARIABLE GEOMETRY EQUIPMENT OF A GAS TURBINE ENGINE ESPECIALLY COMPRISING A GUIDING TRACK CONNECTION</title><description>The invention relates to a system for controlling at least two sets of variable geometry equipment (10, 110) of a gas turbine engine comprising at least one first body and a second body, the first set of equipment (10) being a stage of variable stator vanes of a compressor of the first body moving between a closed position during idling and an open position at high speed, and the second set of equipment (110) being at least one bleed valve of a compressor of the second body moving between an open position during idling and a closed position at high speed. The system according to the invention is characterised in that it comprises an actuator (24) that actuates the two sets of equipment.
La présente invention porte sur un système de commande d'au moins deux équipements (10, 110) à géométrie variable d'un moteur à turbine à gaz comportant au moins un premier corps et un deuxième corps, le premier équipement (10) étant un étage d'aubes de stator à angle de calage variable d'un compresseur du premier corps évoluant entre une position fermée au ralenti et une position ouverte à fort régime, le second équipement (110) étant au moins une vanne de décharge d'un compresseur du deuxième corps évoluant entre une position ouverte au ralenti et une position fermée à fort régime; il est caractérisé par le fait qu'il comporte un actionneur (24) qui actionne les deux équipements.</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>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqFjbsOgkAQRWksjPoNzg9YCDHaLuuwTtwH7g4kVISYtTJKgp0_Lxh7q3OLk3PnyTs0gdFA4TxIZ9k7rckqqIUnkWsEhc4g-wbwUlFp0DK4AgQoEYArn5NFQKu-CCVKElo3Y8qUnsJUGtWKjtNiL-R5erEomZxdJrNbdx_i6sdFsi6Q5WkT-2cbh767xkd8tVKk--yQbncy-298AISNOhQ</recordid><startdate>20160809</startdate><enddate>20160809</enddate><creator>GAULLY, BRUNO ROBERT</creator><creator>COLOTTE, BAPTISTE BENOIT</creator><scope>EVB</scope></search><sort><creationdate>20160809</creationdate><title>SYSTEM FOR CONTROLLING VARIABLE GEOMETRY EQUIPMENT OF A GAS TURBINE ENGINE ESPECIALLY COMPRISING A GUIDING TRACK CONNECTION</title><author>GAULLY, BRUNO ROBERT ; COLOTTE, BAPTISTE BENOIT</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2738215C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2016</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>GAULLY, BRUNO ROBERT</creatorcontrib><creatorcontrib>COLOTTE, BAPTISTE BENOIT</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GAULLY, BRUNO ROBERT</au><au>COLOTTE, BAPTISTE BENOIT</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEM FOR CONTROLLING VARIABLE GEOMETRY EQUIPMENT OF A GAS TURBINE ENGINE ESPECIALLY COMPRISING A GUIDING TRACK CONNECTION</title><date>2016-08-09</date><risdate>2016</risdate><abstract>The invention relates to a system for controlling at least two sets of variable geometry equipment (10, 110) of a gas turbine engine comprising at least one first body and a second body, the first set of equipment (10) being a stage of variable stator vanes of a compressor of the first body moving between a closed position during idling and an open position at high speed, and the second set of equipment (110) being at least one bleed valve of a compressor of the second body moving between an open position during idling and a closed position at high speed. The system according to the invention is characterised in that it comprises an actuator (24) that actuates the two sets of equipment.
La présente invention porte sur un système de commande d'au moins deux équipements (10, 110) à géométrie variable d'un moteur à turbine à gaz comportant au moins un premier corps et un deuxième corps, le premier équipement (10) étant un étage d'aubes de stator à angle de calage variable d'un compresseur du premier corps évoluant entre une position fermée au ralenti et une position ouverte à fort régime, le second équipement (110) étant au moins une vanne de décharge d'un compresseur du deuxième corps évoluant entre une position ouverte au ralenti et une position fermée à fort régime; il est caractérisé par le fait qu'il comporte un actionneur (24) qui actionne les deux équipements.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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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 | SYSTEM FOR CONTROLLING VARIABLE GEOMETRY EQUIPMENT OF A GAS TURBINE ENGINE ESPECIALLY COMPRISING A GUIDING TRACK CONNECTION |
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