System and method for producing hydrogen rich fuel
a gas turbine and hydrogen rich technology, applied in the direction of engines, machines/engines, mechanical apparatus, etc., can solve the problems of high temperature exhaust, affecting the operation of the system, and requiring an external source of steam which may not be readily availabl
Inactive Publication Date: 2012-03-08
GENERAL ELECTRIC CO
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Benefits of technology
[0004]Aspects and advantages of the invention are set forth below in the following description, or may be obvious from the description, or may be learned through practice of the invention.
Problems solved by technology
However, a leaner fuel-air mixture introduces flame instability in the combustor, increasing the chance of a lean blow out (LBO) event that might interrupt service provided by the gas turbine.
In general, these reformers expose a catalyst, such as nickel, to a fuel, such as natural gas, in a high temperature and pressure environment to produce pure hydrogen, and the exothermic catalytic reaction produces a very high temperature exhaust that can present a problem for valves, seals, and other system components.
In addition, SMR reformers typically require an external source of steam which may not be readily available.
Method used
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[0012]Reference will now be made in detail to present embodiments of the invention, one or more examples of which are illustrated in the accompanying drawings. The detailed description uses numerical and letter designations to refer to features in the drawings. Like or similar designations in the drawings and description have been used to refer to like or similar parts of the invention.
[0013]Each example is provided by way of explanation of the invention, not limitation of the invention. In fact, it will be apparent to those skilled in the art that modifications and variations can be made in the present invention without departing from the scope or spirit thereof. For instance, features illustrated or described as part of one embodiment may be used on another embodiment to yield a still further embodiment. Thus, it is intended that the present invention covers such modifications and variations as come within the scope of the appended claims and their equivalents.
[0014]Various embodi...
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A system for providing hydrogen enriched fuel includes first and second gas turbines. The second gas turbine receives a portion of compressed working fluid from the first gas turbine and produces a reformed fuel, and a fuel skid provides fluid communication between a turbine in the second gas turbine and a combustor in the first gas turbine. A method for providing hydrogen enriched fuel includes diverting a portion of a first compressed working fluid from a first compressor to a second compressor and providing a second compressed working fluid from the second compressor. The method further includes mixing a fuel with the second compressed working fluid in a reformer to produce a reformed fuel, flowing the reformed fuel through a second turbine to cool the reformed fuel, and connecting the second turbine to the second compressor so that the second turbine drives the second compressor.
Description
FIELD OF THE INVENTION[0001]The present invention relates generally to an integrated gas turbine system that produces hydrogen rich fuel for subsequent combustion or distribution.BACKGROUND OF THE INVENTION[0002]Gas turbines are widely used in industrial and power generation operations. A typical gas turbine includes an axial compressor at the front, one or more combustors around the middle, and a turbine at the rear. Ambient air enters the compressor, and rotating blades and stationary vanes in the compressor progressively impart kinetic energy to the working fluid (air) to produce a compressed working fluid at a highly energized state. The compressed working fluid exits the compressor and flows to the combustors where it mixes with fuel and ignites to generate combustion gases having a high temperature, pressure, and velocity. The combustion gases expand in the turbine to produce work. For example, expansion of the combustion gases in the turbine may rotate a shaft connected to a ...
Claims
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Patent Timeline
Login to View More IPC IPC(8): F02C3/20F02C3/28
CPCF02C3/28F02C6/00F02C3/34
Inventor BERRY, JONATHAN DWIGHTHUGHES, MICHAEL JOHN
Owner GENERAL ELECTRIC CO