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US Patent 11686210 Component assembly for variable airfoil systems

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Current Assignee
General Electric
General Electric
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Date Filed
March 24, 2021
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Date of Patent
June 27, 2023
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Patent Applicant
General Electric
General Electric
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Patent Application Number
17210760
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Patent Citations
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US Patent 9546562 Seal segment
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US Patent 9593587 Turbine seal fin leakage flow rate control
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US Patent 9771942 Exhaust gas turbocharger having guiding screen rings that are rotatable relative to each other
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US Patent 10145336 Translating outer cowl flow modulation device and method
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US Patent 10301967 Incident tolerant turbine vane gap flow discouragement
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US Patent 10385728 Airfoil contour for low-loss on-boarding of cooling air through an articulating spindle
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US Patent 10458267 Seal assembly for counter rotating turbine assembly
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US Patent 10539020 Two spool gas turbine engine with interdigitated turbine section
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US Patent 10544734 Three spool gas turbine engine with interdigitated turbine section
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US Patent 10605168 Interdigitated turbine engine air bearing cooling structure and method of thermal management
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•••
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11686210
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Patent Primary Examiner
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J. Todd Newton
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CPC Code
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F01D 17/141
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F01D 17/148
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F01D 17/16
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F01D 9/023
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F01D 17/167
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F01D 1/24
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F01D 1/26
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F01D 17/162
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F01D 17/14
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