Abstract

The potential for high turbine entry temperature (TETs) turbines for nuclear power plants (NPPs) requires improved materials and sophisticated cooling. Cooling is critical for maintaining mechanical integrity of the turbine for temperatures >1000 °C. Increasing TET is one of the solutions for improving efficiency after cycle optimum pressure ratios have been achieved but cooling as a percentage of mass flow will have to increase, resulting in cycle efficiency penalties. To limit this effect, it is necessary to know the maximum allowable blade metal temperature to ensure that the minimum cooling fraction is used. The main objective of this study is to analyze the thermal efficiencies of four cycles in the 300–700 MW class for generation IV NPPs, using two different turbines with optimum cooling for TETs between 950 and 1200 °C. The cycles analyzed are simple cycle (SC), simple cycle recuperated (SCR), intercooled cycle (IC), and intercooled cycle recuperated (ICR). Although results showed that deterioration of cycle performance is lower when using improved turbine material, the justification to use optimum cooling improves the cycle significantly when a recuperator is used. Furthermore, optimized cooling flow and the introduction of an intercooler improve cycle efficiency by >3%, which is >1% more than previous studies. Finally, the study highlights the potential of cycle performance beyond 1200 °C for IC. This is based on the IC showing the least performance deterioration. The analyses intend to aid development of cycles for deployment in gas-cooled fast reactors (GFRs) and very high-temperature reactors (VHTRs).

Highlights

  • Generation IV reactor performance is key to the design of Nuclear Power Plants (NPPs), with one of the key aspects being the improvement of cycle thermal efficiency in comparison to the incumbent designs [1]

  • Due to the reactor thermal power being fixed for a given Core Outlet Temperature (COT), the precooler alone will not yield the specific work required for the NPP, which devalues the economics of the plant

  • Prerequisites to calculate the cooling flow from the Effects of Turbine Cooling on Efficiency and Specific compressor exit, which is required for the cycle are the Figure 7 shows the effect on cycle efficiency for Simple Recuperated Cycle (SCR) and

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Summary

Institutional Repository Cover Sheet

ASME Paper Title: A review of the turbine cooling fraction for very high turbine entry temperature helium gas turbine cycles for generation IV reactor power plants. Increasing TET is one of the solutions for improving efficiency after cycle optimum pressure ratios have been achieved but cooling as a percentage of mass flow will have to increase, resulting in cycle efficiency penalties. To limit this effect, it is necessary to know the maximum allowable blade metal temperature to ensure the minimum cooling fraction is used. Results showed that deterioration of cycle performance is lower when using improved turbine material, the justification to use optimum cooling improves the cycle significantly when a recuperator is used.

Power for Electrical Conversion
Introduction
Turbine Cooling
Simulation Tool
Precooler and Intercooler
Modular Helium Reactor
Cooling Calculations
Increasing TET and Optimising Turbine Cooling Fraction for SC and IC
Optimum DP line for the various TETs
Optimum DP
Blade B for higher TETs
Future Technology
Conclusion
Findings
The authors wish to thank the Gas Turbine Engineering
Full Text
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