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US Patent 11421702 Impeller with chordwise vane thickness variation
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Patent
Current Assignee
Pratt & Whitney Canada
Date Filed
August 21, 2019
Date of Patent
August 23, 2022
Patent Applicant
Pratt & Whitney Canada
Patent Application Number
16546781
Patent Citations
US Patent 10006297 Turbine rotor blade
US Patent 10002209 Method for modelling a part, in particular a blading
US Patent 10253633 Rotor of an exhaust gas turbocharger
Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
11421702
Patent Primary Examiner
Sabbir Hasan
CPC Code
F04D 29/30
F04D 29/441
F04D 29/242
F05D 2240/304
F04D 29/324
F04D 29/284
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