Lpp Combustion, Llc.

World Energy Systems Corporation

Combustion Science & Engineering, Inc.

Ponnuthurai Gokulakrishnan

Michael S Klassen

Casey Fuller

Richard J Roby

Leo Eskin

Richard Joklik

Michael J Ramotowski

Glenn Gaines

Charles H Ware

John E Langdon

Andrew J Hamer

Andrew Trettel

Darin Viehe

Leo D Eskin

Richard G Joklik

Glenn C Gaines

Casey C Fuller

A method for implementing a modeling tool that generates optimized reduced kinetics models for given operating conditions and a numerical scheme to speed-up kinetics evaluation of turbulent-chemistry coupling during CFD simulations. The tool is capable of predicting ignition and flameholding phenomenon for most propulsion systems, including gas turbine applications. A lumped-parameterization based optimization scheme may generate multi-step quasi-global kinetics models using laminar flame speed as the target data. This scheme may be further extended to include optimization of emission predictions such as CO and NO.

Computationally efficient reduced kinetics methodologies for jet fuels

In one embodiment of a method for vaporizing liquids such as fuels, the liquid is sprayed into a chamber such that the spray does not impinge on any surface. The energy for vaporization is supplied through the injection of a hot diluent such as nitrogen or oxygen depleted air. Additional heat is added through the surface. In another embodiment, the liquid is sprayed onto a hot surface using a geometry such that the entire spray is intercepted by the surface. Heat is added through the surface to maintain an internal surface temperature above the boiling point of the least volatile component of the liquid. The liquid droplets impinging on the surface are thus flash vaporized. A carrier gas may also be flowed through the vaporizer to control the dew point of the resultant vapor phase mixture.

Method and apparatus for conditioning liquid hydrocarbon fuels

A downhole burner for a steam generator includes an injector and a cooling liner. Steam enters the burner through holes in the cooling liner. Combustion occurring within the cooling liner heats the steam and increases its quality and may superheat it. The heated, high-quality steam and combustion products exit the burner and enter an oil-bearing formation to upgrade and improve the mobility of heavy crude oils held in the formation. The injector includes a face plate, a cover plate, an oxidizer distribution manifold plate, and a fuel distribution manifold plate. The cooling liner has an effusion cooling section and effusion cooling and jet mixing section. The effusion cooling section includes effusion holes for injecting steam along the cooling liner surface to protect the liner. The effusion cooling and jet mixing section has both effusion holes and mixing holes for injecting steam further toward central portions of the burner.

System, method and apparatus for hydrogen-oxygen burner in downhole steam generator

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Columbia, MD, United States of America

Ponnuthurai Gokulakrishnan