AIRCRAFT HEAT MANAGEMENT

A method of operating a gas turbine engine including an engine core and turbine, a compressor, a combustor arranged to combust a fuel, and a core shaft connecting the turbine to the compressor; a fan located upstream of the engine core; a fan shaft; a main gearbox that receives an input from the cor...

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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