System and method for thermal control in a gas turbine engine

A system includes a gas turbine engine (12) that includes a compressor section (16) configured to generate compressed air (24) and a combustor (18) coupled to the compressor section (16). The combustor (18) is configured to combust a first mixture comprising the compressed air (24) and a first fuel...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	THACKER, PRADEEP STANLEY, AVAGLIANO, AARON JOHN
Format:	Patent
Sprache:	eng ; fre ; ger
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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