GAS TURBINE ENGINE WITH HIGHER LOW SPOOL TORQUE-TO-THRUST RATIO

A gas turbine engine (20) includes a fan drive turbine driving a low pressure compressor (44), and driving a gear reduction to in turn drive a fan rotor (42) at a speed slower than the fan drive turbine. The turbine section (28) further includes a high pressure turbine (54) driving the high pressure...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HASEL, Karl L, PIXTON, Stephen G
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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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