Closed cycle gas turbine plant control system: load following for gas turbine operating with gas cooled reactor on a closed cycle
Patent
·
OSTI ID:4352401
A closed cycle gas turbine power plant is described which consists of a gas compressor means, a heat source, gas turbine means, a recuperator and a heat rejection gas cooler, a high pressure flowpath for gas serially interconnecting the compressor means outlet, the heat receiving side of the recuperator, the heat source and the gas turbine means inlet, a low pressure flowpath for gas serially interconnecting the gas turbine means outlet, the heat yieldling side of the recuperator, and the gas cooler and the compressor means inlet. The high pressure side of the flowpath has two bypass ducts each arranged to bypass a controlled fraction of the total gas flow around one or more components in the flowpath with the effect of lowering the gas temperature at the heat source inlet and at the gas turbine means inlet. (UK)
- Research Organization:
- Originating Research Org. not identified
- NSA Number:
- NSA-29-014614
- OSTI ID:
- 4352401
- Report Number(s):
- GB 6014471
- Country of Publication:
- CEC
- Language:
- English
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