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Turbine airfoil cooling system with nonlinear trailing edge exit slots
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Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles
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Flow control insert in cooling passage for turbine vane
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Integrated TBC and cooling flow metering plate in turbine vane
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Ceramic casting core having an integral vane internal core and shroud backside shell for vane segment casting
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Investment casting method for gas turbine engine vane segment
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Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements
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Multi-wall gas turbine airfoil cast using a ceramic core formed with a fugitive insert and method of manufacturing same
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Vane outer support ring with no forward hook in a compressor section of a gas turbine engine
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Outer vane support ring including a strong back plate in a compressor section of a gas turbine engine
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Cooling system in a turbine airfoil assembly including zigzag cooling passages interconnected with radial passageways
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US2014205441A1
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Seal assembly including grooves in a radially outwardly facing side of a platform in a gas turbine engine
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Aft outer rim seal arrangement
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Cooling passage including turbulator system in a turbine engine component
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US2014321980A1
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Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly
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US2014234076A1
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Outer rim seal assembly in a turbine engine
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US2014227103A1
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Turbine blade with contoured chamfered squealer tip
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US2013156579A1
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Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling
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US2014219811A1
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Twisted gas turbine engine airfoil having a twisted rib
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US2014219809A1
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Casting core for twisted gas turbine engine airfoil having a twisted rib
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