GAS TURBINE WITH MULTIPLE PARTICLE SEPARATORS

The present disclosure generally relates to separating solid particles from an airflow in a gas turbine engine. A system for separating debris includes a first separation device (88) in fluid communication with an inlet flow path of a compressor and a second separation device (340) in fluid communic...

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Hauptverfasser:	WILLIAMS, Christopher, Robert, MANTEIGA, John, Alan, WILSON, Gregg, Hunt, MOOK, Joshua, Tyler, WAYMEYER, Stephen, Joseph
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	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
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creator	WILLIAMS, Christopher, Robert MANTEIGA, John, Alan WILSON, Gregg, Hunt MOOK, Joshua, Tyler WAYMEYER, Stephen, Joseph
description	The present disclosure generally relates to separating solid particles from an airflow in a gas turbine engine. A system for separating debris includes a first separation device (88) in fluid communication with an inlet flow path of a compressor and a second separation device (340) in fluid communication with an outlet flow path of the compressor and an inlet flow path of a combustor. The first separation device is adapted to remove coarse particles from the airflow. The second separation device is adapted to remove fine particles from the airflow. The course particles have a larger mean particle diameter than the fine particles. La présente invention concerne généralement la séparation de particules solides d'un flux d'air dans un moteur à turbine à gaz. Le système de séparation de débris comprend un premier dispositif de séparation (88) en communication fluidique avec un trajet d'écoulement d'entrée d'un compresseur et un second dispositif de séparation (340) en communication fluidique avec un trajet d'écoulement de sortie du compresseur et un trajet d'écoulement d'entrée d'une chambre de combustion. Le premier dispositif de séparation est conçu pour éliminer les particules grossières du flux d'air. Le second dispositif de séparation est conçu pour éliminer les particules fines du flux d'air. Les particules grossières ont un diamètre de particule moyen supérieur à celui des particules fines.
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A system for separating debris includes a first separation device (88) in fluid communication with an inlet flow path of a compressor and a second separation device (340) in fluid communication with an outlet flow path of the compressor and an inlet flow path of a combustor. The first separation device is adapted to remove coarse particles from the airflow. The second separation device is adapted to remove fine particles from the airflow. The course particles have a larger mean particle diameter than the fine particles. La présente invention concerne généralement la séparation de particules solides d'un flux d'air dans un moteur à turbine à gaz. Le système de séparation de débris comprend un premier dispositif de séparation (88) en communication fluidique avec un trajet d'écoulement d'entrée d'un compresseur et un second dispositif de séparation (340) en communication fluidique avec un trajet d'écoulement de sortie du compresseur et un trajet d'écoulement d'entrée d'une chambre de combustion. Le premier dispositif de séparation est conçu pour éliminer les particules grossières du flux d'air. Le second dispositif de séparation est conçu pour éliminer les particules fines du flux d'air. 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A system for separating debris includes a first separation device (88) in fluid communication with an inlet flow path of a compressor and a second separation device (340) in fluid communication with an outlet flow path of the compressor and an inlet flow path of a combustor. The first separation device is adapted to remove coarse particles from the airflow. The second separation device is adapted to remove fine particles from the airflow. The course particles have a larger mean particle diameter than the fine particles. La présente invention concerne généralement la séparation de particules solides d'un flux d'air dans un moteur à turbine à gaz. Le système de séparation de débris comprend un premier dispositif de séparation (88) en communication fluidique avec un trajet d'écoulement d'entrée d'un compresseur et un second dispositif de séparation (340) en communication fluidique avec un trajet d'écoulement de sortie du compresseur et un trajet d'écoulement d'entrée d'une chambre de combustion. Le premier dispositif de séparation est conçu pour éliminer les particules grossières du flux d'air. Le second dispositif de séparation est conçu pour éliminer les particules fines du flux d'air. 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A system for separating debris includes a first separation device (88) in fluid communication with an inlet flow path of a compressor and a second separation device (340) in fluid communication with an outlet flow path of the compressor and an inlet flow path of a combustor. The first separation device is adapted to remove coarse particles from the airflow. The second separation device is adapted to remove fine particles from the airflow. The course particles have a larger mean particle diameter than the fine particles. La présente invention concerne généralement la séparation de particules solides d'un flux d'air dans un moteur à turbine à gaz. Le système de séparation de débris comprend un premier dispositif de séparation (88) en communication fluidique avec un trajet d'écoulement d'entrée d'un compresseur et un second dispositif de séparation (340) en communication fluidique avec un trajet d'écoulement de sortie du compresseur et un trajet d'écoulement d'entrée d'une chambre de combustion. Le premier dispositif de séparation est conçu pour éliminer les particules grossières du flux d'air. Le second dispositif de séparation est conçu pour éliminer les particules fines du flux d'air. Les particules grossières ont un diamètre de particule moyen supérieur à celui des particules fines.</abstract><oa>free_for_read</oa></addata></record>
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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	GAS TURBINE WITH MULTIPLE PARTICLE SEPARATORS
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