Internal cooling of the case of a low pressure turbine

A low pressure turbine casing (10) has a conical annular shell (12) circumscribed about a centerline (14). A forward flange (16) depends from a forward end (18) of the annular shell (12) and a forward hook (22) extends aftwardly from the forward flange (16). First and second rails (23, 25) having fi...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZEGARSKI, FREDERICK J, THOMPSON, JAMES EDWARD, HILDEBRAND, KURT THOMAS, ANDERSON, JR., HENRY CALVIN, BOSEL, TOD KENNETH
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 ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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