Gas turbine engine thermal management

A method of controlling a cooled cooling air system of an aviation gas turbine engine is provided. The method includes receiving data indicative of an environmental condition of the aero-gas turbine engine, data indicative of a degradation parameter of the aero-gas turbine engine, data indicative of...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MARRINAN PATRICK MICHAEL, MCQUISTON ROBERT JON, MILLER BRANDON WAYNE, RAMBO JEFFREY DOUGLAS, FELDMANN KEVIN ROBERT
Format:	Patent
Sprache:	chi ; 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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