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US Patent 10822987 Turbine stator outer shroud cooling fins

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Current Assignee
Pratt & Whitney Canada
Pratt & Whitney Canada
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Date Filed
April 16, 2019
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Date of Patent
November 3, 2020
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Patent Applicant
Pratt & Whitney Canada
Pratt & Whitney Canada
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Patent Application Number
16385428
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Patent Citations
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US Patent 10280762 Multi-chamber platform cooling structures
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US Patent 10280793 Insert and standoff design for a gas turbine engine vane
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US Patent 10323526 Blade with tip shroud
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US Patent 10294796 Blade or vane arrangement for a gas turbine engine
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US Patent 10012238 Electrostatic discharge prevention for a fan blade
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US Patent 10082033 Gas turbine blade with platform cooling
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US Patent 10113439 Internal shroud for a compressor of an axial-flow turbomachine
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US Patent 10184342 System for cooling seal rails of tip shroud of turbine blade
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US Patent 10202864 Chevron trip strip
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
10822987
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Patent Primary Examiner
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Michael Lebentritt
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