GAS-TURBINE BLADE PROVIDED WITH IMPROVED COOLING CIRCUITS

FIELD: blades for aircraft engines. ^ SUBSTANCE: proposed blade is provided with at least three cooling circuits. First cooling circuit has at least one cavity on concave end of blade feather stretched in radial direction close to concave surface of feather. Second cooling circuit is independent of...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	EHNO PATRIS, PIKO FILIPP, BURR'E IZABEL'
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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