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US Patent 10174627 Gas turbine engine thin wall composite vane airfoil

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Patent abstract

An airfoil for a gas turbine engine has a first layer forming a cavity having transitioning from a first thickness to a second thickness through a ply drop region. A second layer is secured to the first layer.

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Infobox
Is a
Patent
Patent
0
Patent Applicant
United Technologies
United Technologies
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
101746270
Date of Patent
January 8, 2019
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Patent Application Number
147675120
Date Filed
February 5, 2014
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Patent Citations Received
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US Patent 10605103 CMC airfoil assembly
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US Patent 10767493 Turbine vane assembly with ceramic matrix composite vanes
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US Patent 10767497 Turbine vane assembly with ceramic matrix composite components
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US Patent 10830063 Turbine vane assembly with ceramic matrix composite components
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US Patent 10859268 Ceramic matrix composite turbine vanes and vane ring assemblies
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US Patent 10883376 Turbine vane assembly with ceramic matrix composite vanes
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US Patent 10890076 Turbine vane assembly having ceramic matrix composite components with expandable spar support
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US Patent 10890077 Anti-fret liner
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US Patent 10954802 Turbine section assembly with ceramic matrix composite vane
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US Patent 10961857 Turbine section of a gas turbine engine with ceramic matrix composite vanes
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US Patent 10975708 Turbine section assembly with ceramic matrix composite vane
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US Patent 11008880 Turbine section assembly with ceramic matrix composite vane
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US Patent 11008888 Turbine vane assembly with ceramic matrix composite components
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US Patent 11047247 Turbine section of a gas turbine engine with ceramic matrix composite vanes
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US Patent 11319822 Hybrid vane segment with ceramic matrix composite airfoils
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US Patent 11384646 Method for forming hollow ceramic matrix composite article using a mandrel
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US Patent 11519279 Ceramic matrix composite turbine vane and method for making
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US Patent 11560799 Ceramic matrix composite vane assembly with shaped load transfer features
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Patent Primary Examiner
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Mark Laurenzi
0
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US Patent 11560799 Ceramic matrix composite vane assembly with shaped load transfer features
0
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US Patent 11519279 Ceramic matrix composite turbine vane and method for making
0
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Infobox
Patent Citations Received
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US Patent 10605103 CMC airfoil assembly
0
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