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...

Ausführliche Beschreibung

Bibliographische Detailangaben

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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!