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Home › Turbine blade cooling with a hollow airfoil configured to minimize a distance between a pin array section and the trailing edge of the air foil

Turbine blade cooling with a hollow airfoil configured to minimize a distance between a pin array section and the trailing edge of the air foil

US Patent 8231329 · Granted Jul 31, 2012

Estimated economic value: $23,457,000 ⓘ

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