GAS TURBINE ENGINE COMPONENT WITH INTEGRAL HEAT EXCHANGER

An assembly is provided for a gas turbine engine (20). This engine assembly includes a vane array (76) and a heat exchanger (74) integrated with the vane array (76). The vane array (76) includes an inner platform (80), an outer platform (82) and a plurality of vanes (84, 86). The inner platform (80)...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	Durocher, Eric S
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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