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2015
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Invention
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Small arrayed swirler system for reduced emissions and noise.
A combustor assembly employs an ej... |
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Invention
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Gas turbine engine package and corresponding method. A gas turbine engine unit (110) for use in a... |
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2014
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Invention
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Two-branch mixing passage and method to control combustor pulsations. A gas turbine engine combus... |
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Invention
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Capacity control of turbine by the use of a reheat combustor in multishaft engine. One example of... |
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Invention
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Capacity control of turbine by the use of a reheat combustor in multi shaft engine. One example o... |
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2013
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Invention
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Lean azimuthal flame combustor. A combustion chamber may include a first surface and a second sur... |
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Invention
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Cogen heat load matching through reheat and capacity match. One example of a gas turbine engine m... |
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Invention
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Lean azimuthal flame combustor. A combustion chamber may include a first surface (102) and a seco... |
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2012
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Invention
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Radial staging method and configuration of a liquid injection system for power plants. A turbine ... |
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2008
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Invention
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Gas turbine engine mixing duct and method to start the engine. A combustion chamber device having... |
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2007
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Invention
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Method and apparatus for isolating inactive fuel passages. One aspect relates to an apparatus hav... |
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Invention
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Fuel injector. An apparatus and method for minimizing and/or preventing thermal degradation of fu... |
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Invention
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Components for a gas turbine engine. An aerofoil assembly including an aerofoil and a spray eleme... |
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Invention
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Gas turbine engine combustion systems. One embodiment is a unique gas turbine engine combustion c... |
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Invention
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Component for fuel supply. A joint for a gas turbine fuel injector, the joint comprises a housing... |
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Invention
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Bleed off valve system. A gas turbine engine system including a plurality of bleed off doors form... |
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2006
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Invention
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Airfoil for a second stage nozzle guide vane. The present invention provides an airfoil a second ... |
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Invention
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Airfoil for a first stage nozzle guide vane. The present invention provides an airfoil for a firs... |
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Invention
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First stage turbine airfoil. The present invention provides an airfoil for a first stage turbine ... |
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Invention
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Second stage turbine airfoil. The present invention provides an airfoil for a second stage turbin... |
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Invention
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Airfoil for a third stage nozzle guide vane. The present invention provides an airfoil for a thir... |
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Invention
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Third stage turbine airfoil. The present invention provides an airfoil for a third stage blade ha... |
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Invention
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Gas turbine engine premix injectors. One embodiment is a gas turbine engine premix injector inclu... |
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Invention
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Controlling a gas turbine engine with a transient load. A technique is provided for operating a g... |
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Invention
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Determination of a signal indicative of shaft power. A gas turbine engine provides mechanical sha... |
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Invention
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Gas turbine exhaust diffuser. A gas turbine including an exhaust diffuser with a flow splitter lo... |
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Invention
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Fuel injection. In order to allow dual fuel operation, that is to say gas and liquid fuel, a fuel... |
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2005
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Invention
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System and method for controlling the working line position in a gas turbine engine compressor. A... |
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Invention
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Two-branch mixing passage and method to control combustor pulsations.
A gas turbine engine combu... |
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2004
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Invention
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Method and system for controlling fuel supply in a combustion turbine engine. In order to regulat... |
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2003
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Invention
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Combustion chamber. A three-stage lean burn combustion chamber (28) comprises a primary combustio... |
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2000
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Invention
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Combustion chamber. A three stage lean burn combustion chamber (28) comprises a primary combustio... |
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1999
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Invention
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Combustion chamber comprising mixing ducts with fuel injectors varying in number and cross-sectio... |
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Invention
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Combustion chamber assembly having a transition duct damping member. A combustion chamber assembl... |
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1996
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Invention
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Turbine engine control system. A fuel control system for a premixed lean burn combustor in a comb... |
