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US Patent 11371359 Turbine blade for a gas turbine engine

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Current Assignee
Pratt & Whitney Canada
Pratt & Whitney Canada
Date Filed
November 26, 2020
Date of Patent
June 28, 2022
Patent Applicant
Pratt & Whitney Canada
Pratt & Whitney Canada
Patent Application Number
17105583
Patent Citations
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US Patent 10184342 System for cooling seal rails of tip shroud of turbine blade
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US Patent 10190418 Gas turbine engine and turbine blade
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US Patent 10253637 Method and system for improving turbine blade performance
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US Patent 10287900 Incident tolerant turbine vane cooling
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US Patent 10301943 Turbomachine rotor blade
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US Patent 10301945 Interior cooling configurations in turbine rotor blades
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US Patent 10350684 Additive manufacturing method for making complex film holes
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US Patent 10677066 Turbine blade with airfoil tip vortex control
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US Patent 10487664 Additive manufacturing method for making holes bounded by thin walls in turbine components
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US Patent 10012089 Airfoil tip pocket with augmentation features
•••
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11371359
Patent Primary Examiner
‌
Eric J Zamora Alvarez
CPC Code
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F01D 5/147
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F01D 5/18
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F01D 5/186
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F01D 5/187
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F05D 2220/32
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F01D 5/20
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F05D 2260/202
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F05D 2240/301
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F05D 2240/305
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F05D 2240/307
•••

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