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Bathina

Mahesh Bathina, Bangalore IN

Patent application numberDescriptionPublished
20110083444LOW BTU FUEL INJECTION SYSTEM - A system includes a gas turbine compressor including multiple radial protrusions disposed about a circumference of the gas turbine compressor. Each radial protrusion includes multiple gaseous fuel injection orifices configured to inject gaseous fuel into the gas turbine compressor.04-14-2011

Mahesh Bathina, Ongole IN

Patent application numberDescriptionPublished
20100107641METHOD AND APPARATUS FOR AFFECTING A RECIRCULATION ZONE IN A CROSS FLOW - Disclosed is a cross flow apparatus including a surface and at least one outlet located at the surface. The cross flow apparatus further includes at least one guide at the surface configured to direct an intersecting flow flowing across the surface and increase a velocity of a cross flow being expelled from the at least one outlet downstream from the at least one outlet.05-06-2010
20100172746METHOD AND APPARATUS FOR COOLING A TRANSITION PIECE - Disclosed is a compressor discharge can including a transition piece and a flow redirector located about the transition piece, defining an airflow space therebetween, the flow redirector configured to reduce recirculation of flow in the airflow space.07-08-2010
20100300102METHOD AND APPARATUS FOR AIR AND FUEL INJECTION IN A TURBINE - A method includes receiving fuel and air into a cup of a turbine fuel nozzle. The method also includes mixing the fuel and air at least partially within the cup. In addition, the method includes directing a fuel air mixture toward a turbine combustor. The method also includes shielding an inner wall of the cup with a blanket of a protective fluid flow to reduce the possibility of flame holding along the inner wall. The protective fluid flow excludes a combustible mixture of fuel and air.12-02-2010

Mahesh Bathina, Bangalore Karnataka IN

Patent application numberDescriptionPublished
20100287938CROSS FLOW VANE - The present application provides a cross flow vane for a turbine. The cross flow vane may include a number of jets positioned therein and a divider positioned within one or more of the jets so as to form a number of fuel slots therein.11-18-2010

Mahesh Bathina, Andhra Pradesh IN

Patent application numberDescriptionPublished
20100199675FUEL INJECTION FOR GAS TURBINE COMBUSTORS - An injector includes a surface and an injector hole formed in the surface. The injector also includes a groove formed in the surface, the groove surrounding the injector hole.08-12-2010