GAS TURBINE BLADE COMPRISING WINGLETS TO COMPENSATE CENTRIFUGAL FORCES
A rotating blade for a gas turbine (5) is provided with: ¢ a root (17) configured to be coupled to a disc of the gas turbine (5) which rotates about an axis (A) of the gas turbine (5); a platform (20) coupled to the root (17); ¢ an airfoil (18) extending from the platform (20) and provided with a...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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