Bassam Sabry Mohammad
Bassam Sabry Mohammad Abdelnabi, Guilderland, NY US
Patent application number | Description | Published |
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20130255261 | SWIRLER FOR COMBUSTION CHAMBERS - A combustion swirler is provided. The combustion swirler includes multiple vanes axially extending from an annular first body portion of the combustion swirler. The combustion swirler also includes an annular second body portion enclosing the multiple vanes for directing a flow of combustion fluid. Each of the vanes comprises an aerodynamic blade body comprising a leading edge with a plurality of first tubercles and a trailing edge with a plurality of second tubercles. | 10-03-2013 |
Bassam Sabry Mohammad Abd El-Nabi, Niskayuna, NY US
Patent application number | Description | Published |
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20130196270 | JET MICRO-INDUCED FLOW REVERSALS COMBUSTOR - A jet micro-induced flow reversals combustor is used to reduce NO | 08-01-2013 |
Bassam Sabry Mohammad Abd El-Nabi, Guilderland, NY US
Patent application number | Description | Published |
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20140144142 | FUEL NOZZLE FOR USE IN A TURBINE ENGINE AND METHOD OF ASSEMBLY - A fuel nozzle for use in a turbine engine is provided. The fuel nozzle includes at least one premixer tube including a tube wall and a plurality of perforations defined therein and extending through the tube wall. The plurality of perforations are configured to channel a flow of air therethrough. The fuel nozzle also includes a liquid fuel plenum positioned upstream from the premixer tube, and at least one fuel injector coupled in flow communication with the liquid fuel plenum and the at least one premixer tube. The at least one fuel injector is configured to channel a flow of liquid fuel from the liquid fuel plenum into the premixer tube. | 05-29-2014 |
20140144150 | FUEL NOZZLE FOR USE IN A TURBINE ENGINE AND METHOD OF ASSEMBLY - A fuel nozzle for use in a turbine engine is provided. The fuel nozzle includes a fuel injector configured to discharge a flow of fuel therefrom and a premixer tube coupled in flow communication with the fuel injector. The premixer tube is configured to receive the fuel flow and a flow of air at an upstream end of the premixer tube, wherein the fuel and air are progressively mixed as the fuel and air are channeled through the length of the premixer tube. | 05-29-2014 |