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Additive manufacturing optimized first stage vane
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Near wall leading edge cooling channel for airfoil
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Heat treatment process for additive manufactured components
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Flamesheet diffusion cartridge
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Nickel-base alloy for gas turbine applications
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Vane platform rail configuration for reduced airfoil stress
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Inlet bleed heat and power augmentation for a gas turbine engine
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Turbine static structure for reduced leakage air
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Gas turbine transition duct
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Airflow distribution to a low emissions combustor
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Flashback suppression system for a gas turbine combustor
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Seal for a gas turbine engine having improved flexibility
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Combustion liner with enhanced heat transfer
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Self-purging pilot fuel injection system
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Apparatus and method for reducing carbon monoxide emissions
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Apparatus and method for providing an off-gas to a combustion system
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Vane platform rail configuration for reduced airfoil stress
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Combustion liner seal with heat transfer augmentation
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US2005254944A1
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Fastened vane assembly
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Transition duct apparatus having reduced pressure loss
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