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US Patent 11655718 Blade with tip rail, cooling

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Current Assignee
General Electric
General Electric
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Date Filed
May 10, 2021
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Date of Patent
May 23, 2023
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Patent Applicant
General Electric
General Electric
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Patent Application Number
17316026
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Patent Citations
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US Patent 8079811 Turbine blade with multi-impingement cooled squealer tip
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US Patent 7118342 Fluted tip turbine blade
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US Patent 9249670 Components with microchannel cooling
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US Patent 9297262 Cooling structures in the tips of turbine rotor blades
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US Patent 8100654 Turbine blade with impingement cooling
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US Patent 8469666 Turbine blade tip portion with trenched cooling holes
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US Patent 9085988 Gas turbine engine flow path member
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US Patent 9188012 Cooling structures in the tips of turbine rotor blades
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11655718
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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 5/18
0
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F01D 25/12
0
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F01D 5/087
0
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F01D 5/141
0
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F01D 5/20
0
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F01D 5/3007
0
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F05D 2220/323
0
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F05D 2240/307
0
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F05D 2250/185
0
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F05D 2260/201
0
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