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207results about How to "Minimized pressure drop" patented technology

Cooling device

A cooling device has a large number of closely spaced impinging jets, adjacent an impingement gap, with parallel return paths for supplying coolant flow for the impinging jets with the least possible pressure drop using an interdigitated, branched hierarchical manifold. Surface enhancement features spanning the impingement gap form U-shaped microchannels between single impinging jets and single outlets.
Owner:IBM CORP

Cooling apparatus, cooled electronic module and methods of fabrication thereof employing an integrated coolant inlet and outlet manifold

A cooling apparatus and method of fabrication are provided for facilitating removal of heat from a heat generating electronic device. The cooling apparatus includes an integrated coolant inlet and outlet manifold having a plurality of inlet orifices for injecting coolant onto a surface to be cooled, and a plurality of outlet openings for exhausting coolant after impinging on the surface to be cooled. The inlet orifices and the outlet openings are interspersed in a common surface of the integrated manifold. A plurality of exit openings are also provided on at least one edge surface of the manifold. These exit openings are in fluid communication through the manifold with the outlet openings to facilitate exhausting of coolant through the outlet openings and minimize pressure drop through the manifold. At least one surface plane projection of the at least one edge surface intersects a surface plane projection of the common surface.
Owner:GOOGLE LLC

Method and apparatus for actuating fuel trim valves in a gas turbine

The gas turbines of the present invention have multiple combustion chambers, and within each chamber are multiple fuel nozzles. Each nozzle has its own fuel control valve to control the fuel flowing to the nozzles. To minimize the pressure drop through the fuel control valves, multiple manifolds are employed. Each manifold supplies at least one fuel nozzle in multiple combustion chambers with fuel. The fuel control valves are mounted on the manifolds such that the weight of the fuel control valves and nozzles are carried by the manifolds, not the multiple combustion chambers. A plurality of thermocouples for measuring exhaust gas from said multiple combustion chambers are employed to sense gas exhaust temperature. In carrying out the methods of the present invention for tuning a gas turbine, it is essential to note that the most efficient gas turbine is one which has the least nitrous oxides, the least amount of unburned hydrocarbons, and the least amount of carbon monoxide for a specified energy output. In order to tune the gas turbine to accomplish these objectives, it is desirable that each combustion chamber in the gas turbine be well balanced relative to the remaining combustion chambers. It is an aim of the present invention to tune each of the multiple combustion chambers such that no specific combustion chamber is rich or lean, and all are operating within about 1% of the remaining combustion chambers.
Owner:GENERAL ELECTRIC CO
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