GET ON COOLED TURBINE BLADE (VARIANTS)

FIELD: engines and pumps. ^ SUBSTANCE: turbine blade contains tail designed to fix the blade in a turbine disk slot. The blade also is equipped with an inside contour of air cooling; the said contour includes component for air inlet located from that blade tail side that faces the slot and an air ou...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	KULON SIL'VI, BALLAN MORGAN LIONEL
Format:	Patent
Sprache:	eng ; rus
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	FIELD: engines and pumps. ^ SUBSTANCE: turbine blade contains tail designed to fix the blade in a turbine disk slot. The blade also is equipped with an inside contour of air cooling; the said contour includes component for air inlet located from that blade tail side that faces the slot and an air outlet component. The said side of the blade tail is equipped with a deflector to eliminate vortex flows containing at least one or two ribs arranged on one or both sides of the line along which holes for cooling air supply are drilled. ^ EFFECT: increased cooling efficiency. ^ 14 cl, 12 dwg