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(70) Therefore, the risk of sulphuric acid dew point attack ... - DTI Home

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The world’s first operational steam cooled gas turbine, built by MHI, was<br />

commissioned in Japan in 1998 and installed in Unit 4 at <strong>the</strong> Higashi Niigata<br />

Power Station. In <strong>the</strong> United States, it was not until early 2001 that Siemens-<br />

Westinghouse achieved commercial operation with a 360 MWe power plant<br />

located in Massachusetts followed immediately by a second 249 MWe plant in<br />

Florida. The gas turbine installed in <strong>the</strong> American plants is considered<br />

“partially” steam cooled, with just <strong>the</strong> first stage vanes being incorporated<br />

within a closed loop. Whilst specific teething problems were found during<br />

start up conditions <strong>of</strong> <strong>the</strong> W105G gas turbine, a cycle efficiency <strong>of</strong> ~58%<br />

(LHV) was achieved with this technology.<br />

More recently General Electric installed <strong>the</strong>ir first H-class unit at <strong>the</strong> Baglan<br />

Energy Park in South Wales. This unit, which features steam-cooled rotor and<br />

stator vanes, is currently under commissioning tests with engineers aiming to<br />

break <strong>the</strong> 60% (LHV) cycle efficiency barrier.<br />

4.3.2 Fuel Heating<br />

In <strong>the</strong> late 90’s methods <strong>of</strong> heating fuel prior to combustion in <strong>the</strong> gas turbine<br />

were being introduced to <strong>the</strong> combined cycle in order to enhance efficiency.<br />

Preheating <strong>of</strong> <strong>the</strong> fuel results in a reduction in <strong>the</strong> amount <strong>of</strong> fuel needed to<br />

achieve a given firing temperature in <strong>the</strong> gas turbine. However, whilst <strong>the</strong><br />

efficiency <strong>of</strong> <strong>the</strong> cycle improves, <strong>the</strong> plant power output is found to reduce<br />

slightly. This originates from <strong>the</strong> fact that when a gas turbine is fed warmer<br />

fuel, it requires less mass flow <strong>of</strong> that fuel to obtain <strong>the</strong> previous cold-fuel<br />

firing temperatures, thus <strong>the</strong> exhaust mass flow and water vapour content <strong>of</strong><br />

<strong>the</strong> combustion products is lower. Less power is <strong>the</strong>refore obtained from <strong>the</strong><br />

combustion gas expansion through <strong>the</strong> turbine. Fur<strong>the</strong>rmore <strong>the</strong> HRSG<br />

generates a little less steam from <strong>the</strong> decline in gas turbine exhaust mass flow<br />

and hence a drop in steam turbine power also occurs. However, <strong>the</strong> overall<br />

improvement in <strong>the</strong> cycle efficiency results from <strong>the</strong> fact that <strong>the</strong> energy<br />

diverted from producing steam power is <strong>of</strong> relatively low grade, and is better<br />

employed as a heating medium for <strong>the</strong> fuel.<br />

The fuel heating source may be ei<strong>the</strong>r steam or water. For <strong>the</strong> case <strong>of</strong> steam<br />

this can originate from <strong>the</strong> steam turbine bleed or directly from one <strong>of</strong> <strong>the</strong><br />

HRSG pressure level circuits. For <strong>the</strong> case <strong>of</strong> water heating, <strong>the</strong> hot water is<br />

drawn from <strong>the</strong> HRSG economisers.<br />

There is a threshold at which <strong>the</strong> benefits associated with <strong>the</strong> increase in<br />

efficiency are found to be at <strong>the</strong> expense <strong>of</strong> <strong>the</strong> level <strong>of</strong> electrical power<br />

produced [62] . For example fuel heating to around 200°C from an intermediate<br />

pressure economiser exit water source on a typical three pressure reheat<br />

combined cycle, results in a net heat rate gain <strong>of</strong> about 0.6% with a<br />

corresponding net power loss <strong>of</strong> about 0.3%. If <strong>the</strong> temperature <strong>of</strong> <strong>the</strong> fuel<br />

was raised to around 300°C by a high pressure economiser exit water source,<br />

<strong>the</strong> loss <strong>of</strong> power becomes more evident at 0.75% whereas <strong>the</strong> noted increase<br />

in <strong>the</strong> heat rate gain is less apparent as it only rises to 0.8%.<br />

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