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US Patent 12123317 Aeronautical propulsion system

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Date Filed
December 15, 2023
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Date of Patent
October 22, 2024
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Patent Application Number
18541060
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Patent Citations
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US Patent 8720526 Process for forming a long gas turbine engine blade having a main wall with a thin portion near a tip
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US Patent 10260352 Gas turbine blade with corrugated tip wall
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US Patent 11396817 Gas turbine blade and method for producing such blade
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Patent Inventor Names
Clémentine Charlotte Marie Mouton
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Baptiste Dorian Lawniczek
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Didier René André Escure
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
12123317
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Patent Primary Examiner
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Eric J Zamora Alvarez
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CPC Code
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F01D 5/141
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F01D 5/147
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F01D 5/02
0
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F01D 25/24
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F01D 5/06
0
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F01D 5/20
0
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F01D 1/02
0
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F01D 11/08
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F01D 5/026
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F01D 5/18
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