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2016
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Invention
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Fuel injection locations based on combustor flow path. Systems and methods for dual-fuel operatio... |
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Invention
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Gas turbine fuel components. Gas turbine combustion systems and fuel cartridge assemblies are pro... |
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2015
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Invention
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Leading edge cooling channel for airfoil. Methods and systems of cooling airfoils are provided. T... |
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Invention
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Tapered cooling channel for airfoil. The present invention includes systems and methods for provi... |
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Invention
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Flow control device for rotating flow supply system. This disclosure describes a removable flow c... |
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Invention
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Automated extended turndown of a gas turbine engine combined with incremental tuning to maintain ... |
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2014
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Invention
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Flamesheet combustor contoured liner. The present invention discloses a novel apparatus and way f... |
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Invention
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Sealing device for a gas turbine combustor. The present invention discloses a novel apparatus and... |
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Invention
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Combustor dome damper system. The present invention discloses a novel apparatus and way for contr... |
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Invention
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Axially staged gas turbine combustor with interstage premixer. The present invention discloses a ... |
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Invention
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Combustion liner with bias effusion cooling. A system and method for improving the cooling to a p... |
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Invention
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Dynamic and automatic tuning of a gas turbine engine using exhaust temperature and inlet guide va... |
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Invention
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Dynamic tuning of a gas turbine engine to detect and prevent lean blowout. A method for tuning a ... |
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Invention
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Turbine blade tip repair using dual fusion welding. A method for repairing a blade tip of a turbi... |
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Invention
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Ensuring non-excessive variation of gradients in auto-tuning a gas turbine engine. Methods are pr... |
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Invention
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Stabilizing a gas turbine engine via incremental tuning during transients. Methods and systems ar... |
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Invention
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Compressor airfoil. Aspects of the present invention relate to systems and methods of a vane desi... |
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Invention
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Anti-rotation lug and splitline jumper. The present invention relates to a system and method for ... |
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Invention
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Method of repairing a transition duct side seal. The present invention discloses various methods ... |
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2013
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Invention
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Axial retention of a platform seal. A gas turbine engine component has an axial seal pin assembly... |
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Invention
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Thermally free liner retention mechanism. The present invention discloses a novel and improved de... |
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Invention
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Flamesheet combustor dome. The present invention discloses a novel apparatus and way for controll... |
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Invention
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Detecting flashback by monitoring engine-dynamic spikes. A tuning process is provided for dynamic... |
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2012
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Invention
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Compressor blade. A compressor component having an improved airfoil profile so as to eliminate pr... |
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Invention
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Turbine blade having improved flutter capability and increased turbine stage output. A turbine bl... |
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2011
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Invention
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Employing fuel properties to auto-tune a gas turbine engine. A tuning process is provided for mon... |
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Invention
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Selecting and applying to fuel-flow splits bias values to correct for elevated inlet air humidity... |
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Invention
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Turbine blade platform undercut. A system and method of extending the useable life of a gas turbi... |
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Invention
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Dynamically auto-tuning a gas turbine engine. Tuning processes implemented by an auto-tune contro... |
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2010
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Invention
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Extending useful life of a cobalt-based gas turbine component. A method of extending the useable ... |
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Invention
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Stabilizing a gas turbine engine via incremental tuning. An auto-tune controller and tuning proce... |
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2009
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Invention
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Compressor vane diaphragm. A compressor diaphragm for a gas turbine engine having improved wear c... |
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Invention
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Gas turbine transition duct profile. A transition duct having a panel assembly with an inlet end ... |
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2008
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Invention
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Cooled gas turbine vane assembly. A gas turbine vane to improve vane performance by addressing kn... |
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Invention
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Axial retention of a platform seal. A gas turbine engine component having an axial pin stop assem... |
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Invention
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Shaped cooling holes for reduced stress. A gas turbine engine component having shaped cooling hol... |
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Invention
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Utilizing inlet bleed heat to improve mixing and engine turndown. An improved inlet bleed heat sy... |
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2007
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Invention
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Stator damper shim. A system and method for reducing vibration and wear to adjacent platform surf... |
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2006
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Invention
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Turbine static structure for reduced leakage air. A turbine static structure having reduced leaka... |
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Invention
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Nickel-base alloy for gas turbine applications. A nickel-based alloy suitable for casting gas tur... |
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Invention
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Gas turbine transition duct. A transition duct having a panel assembly with an inlet end of gener... |
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2005
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Invention
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Flashback suppression system for a gas turbine combustor. A gas turbine combustor having improved... |
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Invention
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Seal for a gas turbine engine having improved flexibility. A seal extending between adjacent slot... |
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Invention
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Shroud block with enhanced cooling. A shroud for surrounding a portion of a turbine flow path hav... |
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Invention
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Combustion liner with enhanced heat transfer. A combustion liner having enhanced heat transfer ov... |
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Invention
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Counter swirl shear mixer. The present invention provides a mixer for a gas turbine combustor com... |
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Invention
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Apparatus and method for reducing carbon monoxide emissions. The present invention discloses an a... |
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2004
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Invention
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Apparatus and method for providing an off-gas to a combustion system. A fuel supply system and me... |
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Invention
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Tornado torch igniter. An ignition system having improved reliability for a gas turbine combustor... |
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Invention
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Combustion liner seal with heat transfer augmentation. A gas turbine combustion liner is disclose... |
