GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM

A thermal management system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a heat exchanger and a valve that controls an amount of a first fluid that is communicated through the heat exchanger A first sensor senses a first characteri...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PHILLIPS, KATHLEEN R, PAPA, FEDERICO, STEARNS, ETHAN K, HEISS, JUSTIN W, PHILLIPS, THOMAS G
Format:	Patent
Sprache:	eng ; fre
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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