AIRCRAFT HEAT MANAGEMENT

A gas turbine engine includes an engine core with a combustor; a turbine including turbine blades; a compressor as a source of cooling air for the turbine blades; and an inducer to accelerate and direct the cooling air onto the turbine blades, and a modulating valve to allow or block cooling air flo...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BEMMENT, Craig W, MINELLI, Andrea, KEELER, Benjamin J, YATES, Martin K, MADDEN, Christopher P, SWANN, Peter
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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