COOLED WALL

The disclosure pertains to a cooled wall (1, 2) for separating a hot gas flow path of a gas turbine from a cooling flow (14) comprising at least one turbulator rib (5) extending from the wall into the cooling flow (4), and having a height (h), a width (w) for providing heat transfer enhancement for...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MARMILIC, ROBERT, SHCHUKIN, SERGEY
Format:	Patent
Sprache:	eng ; fre
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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