Cooling circuit for a turbine rotor blade and corresponding cooling method

A cooling circuit for a turbine bucket (10) having a shank (14), a platform (18) and an airfoil (12). The cooling circuit includes a first cooling passage (38) extending from an inlet (20) located at a radially inward end of the shank (14) and adapted to communicate with a turbine wheel-space, the f...

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Bibliographische Detailangaben
1. Verfasser: SEELY, MELISSA ANN
Format: Patent
Sprache:eng ; fre ; ger
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