2006
DOI: 10.1016/j.energy.2005.01.014
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Part load performance analysis of recuperated gas turbines considering engine configuration and operation strategy

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Cited by 115 publications
(36 citation statements)
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“…This trend is due to the fixed turbine exit temperature, i.e., between 873.15 K and 923.15 K for the machines under consideration in Figure 5, and variable speed control to find the optimal operation line to achieve highest possible efficiency at full and part load. The optimal operation line is obtained by matching the compressor and turbine characteristic curves for a set of variables such as rotational speed, pressure ratio, inlet and outlet temperature, mass flow of air and fuel [24,35,36]. As most of the CHP machines operate either at full load or above 50% part load, the variation in the η em,gross , i.e., from the gross mechanical power output to the electrical power output, within this range is little owing to low frictional losses.…”
Section: Mgt Modelmentioning
confidence: 99%
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“…This trend is due to the fixed turbine exit temperature, i.e., between 873.15 K and 923.15 K for the machines under consideration in Figure 5, and variable speed control to find the optimal operation line to achieve highest possible efficiency at full and part load. The optimal operation line is obtained by matching the compressor and turbine characteristic curves for a set of variables such as rotational speed, pressure ratio, inlet and outlet temperature, mass flow of air and fuel [24,35,36]. As most of the CHP machines operate either at full load or above 50% part load, the variation in the η em,gross , i.e., from the gross mechanical power output to the electrical power output, within this range is little owing to low frictional losses.…”
Section: Mgt Modelmentioning
confidence: 99%
“…This configuration is typical for MGTs. More detailed information to MGTs can be found in [4,24,25].…”
Section: Introductionmentioning
confidence: 99%
“…The entire GT cycle is based on the compression of air by the compressor, which is then transferred to the combustion chamber. This compressed air is then mixed with fuel to produce high-temperature flue gas (Kim & Hwang, 2006). The power turbine, which is connected to the shaft of the generator for producing the electricity, receives this high-temperature flue gas.…”
Section: Introductionmentioning
confidence: 99%
“…The development of aero engines has been closely linked to the development of high temperature performance alloys such as Waspaloy® and Haynes® 282® [2] . In the alloy design, mechanical properties must be balanced with other properties such as weldability for successful application of the alloy.…”
Section: Introductionmentioning
confidence: 99%