BLADE

The blade (1) for a gas turbine comprises a root (2), a platform (3) and an airfoil (4). The blade (1) further has a cooling channel (5) with an inlet (6) located at the root (2) or platform (3) and outlets (7). The outlets (7) are located at the platform (3).

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Bibliographic Details
Main Authors LUKETIC, IVAN, NAIK, SHAILENDRA
Format Patent
LanguageEnglish
French
German
Published 09.11.2016
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS
INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:The blade (1) for a gas turbine comprises a root (2), a platform (3) and an airfoil (4). The blade (1) further has a cooling channel (5) with an inlet (6) located at the root (2) or platform (3) and outlets (7). The outlets (7) are located at the platform (3).
Bibliography:Application Number: EP20150166685