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US Patent 12123318 Turbomachine blade with improved cooling holes
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Is a
Patent
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Date Filed
August 30, 2018
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Date of Patent
October 22, 2024
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Patent Application Number
16117359
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Patent Citations
US Patent 7255534 Gas turbine vane with integral cooling system
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US Patent 7789625 Turbine airfoil with enhanced cooling
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US Patent 8052378 Film-cooling augmentation device and turbine airfoil incorporating the same
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US Patent 8057182 Metered cooling slots for turbine blades
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US Patent 8777571 Turbine airfoil with curved diffusion film cooling slot
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US Patent 8245519 Laser shaped film cooling hole
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US Patent 8870536 Airfoil
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US Patent 7186085 Multiform film cooling holes
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US Patent 7249934 Pattern cooled turbine airfoil
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Patent Inventor Names
Guillaume Klein
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Julien Jerome Mathieu Reingpach
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Marine Laeticia Camille Chevalier
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
12123318
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Patent Primary Examiner
Brian P Wolcott
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CPC Code
F05D 2260/20
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F05D 2250/52
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F05D 2240/30
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F01D 5/187
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F01D 5/186
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F05D 2220/323
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F05D 2250/10
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