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US Patent 11852036 Airfoil skin passageway cooling enhancement

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Date Filed
April 19, 2023
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Date of Patent
December 26, 2023
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Patent Applicant
Raytheon Technologies
Raytheon Technologies
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Patent Application Number
18136567
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Patent Citations
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US Patent 10533427 Turbine airfoil having flow displacement feature with partially sealed radial passages
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US Patent 10731474 Airfoil with varying wall thickness
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US Patent 11286793 Airfoil with ribs having connector arms and apertures defining a cooling circuit
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US Patent 11480059 Airfoil with rib having connector arms
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US Patent 7625178 High effectiveness cooled turbine blade
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US Patent 9115590 Gas turbine engine airfoil cooling circuit
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US Patent 9988913 Using inserts to balance heat transfer and stress in high temperature alloys
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US Patent 10252328 Ceramic and refractory metal core assembly
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Patent Inventor Names
Brandon W. Spangler
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11852036
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Patent Primary Examiner
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Eldon T Brockman
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CPC Code
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F05D 2230/211
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F05D 2260/22141
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F01D 5/187
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B22F 5/04
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F05D 2230/21
0

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