SYSTEM AND METHOD FOR COMBINING COMPRESSOR BLEED FLOW AND VENTILATION FLOW OF GAS TURBINE ENGINE

To provide a system and method for combining a compressor bleed flow and a ventilation flow of a gas turbine engine.SOLUTION: A flow combiner (12) is provided for a gas turbine engine (50). The flow combiner (12) includes an outlet duct (14), a compressor bleed inlet duct (16) coupled to the outlet...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	RAVINDER YERRAM, QUOC HOAI NGUYEN, MOHAMMAD MAHABUB, THO V NGUYEN
Format:	Patent
Sprache:	eng ; jpn
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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