BLADE

The blade for a gas turbine includes a root, a platform and an airfoil. The blade further has a cooling channel with an inlet located at the root or platform and outlets. The outlets are located at the platform.

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Bibliographic Details
Main Authors NAIK Shailendra, LUKETIC Ivan
Format Patent
LanguageEnglish
Published 10.11.2016
Subjects
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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Summary:The blade for a gas turbine includes a root, a platform and an airfoil. The blade further has a cooling channel with an inlet located at the root or platform and outlets. The outlets are located at the platform.
Bibliography:Application Number: US201615148756