1. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 1 An Assessment of the Brayton Cycle for High Performance Power Plants R. Schleicher 1, A. R. Raffray 2, and C. P. Wong 1 1 General Atomics, P.O. Box 85608, San Diego, CA 92186, USA 2 University of California, San Diego, 460 EBU-II, La Jolla, CA 92093-0417, USA 14th Topical Meeting on the Technology of Fusion Energy Park City, Utah October 15-19, 2000

2. R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 2 Brayton Cycle Offers Best Near-Term Possibility of Power Conversion with High Efficiency Application of closed-cycle gas turbine (CCGT) technology to fusion power plants -Maximize potential gain from high-temperature fusion in-reactor operation -Compatible with in-reactor He coolant or other coolant through use of IHX -High efficiency translates in lower COE and lower heat load Identify key design parameters influencing cycle efficiency and their likely improvement based on near-term technology development - Estimate CCGT performance improvements for fusion power plant

3. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 3 A Brief CCGT History Indicates a Resurgence in Technology Development 1939 First fossil-fired CCGT plant commissioned in Switzerland. (Air as working fluid) 1978 Last of seven CCGTs, Oberhausen II plant, commissioned in Germany (helium as working fluid) – 50 MWe rating 1970’sStrong development program in U.S. and Germany for coupling direct helium CCGTs to high temperature gas-cooled reactors – work was discontinued due to lack of incentive with tubular recuperators (efficiency ~40%) 1980Work on German HHV CCGT nuclear prototype is discontinued due to oil bearing leaks. 1987Work at MIT demonstrates that high effectiveness plate-fin recuperators can elevate net efficiency of nuclear gas turbines to ~50% 1990sStrong U.S. DOE effort to design a 350MWe nuclear CCGT for new production reactor (NPR). Work was discontinued with close of NPR program. 2000Republic of South Africa and U.S./Russia engaged in well-funded design programs to design and construct nuclear CCGT prototypes.

4. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 4 350 MWE Nuclear CCGT (GT-MHR) Currently Being Designed by U.S./Russia Reactor Power Conversion Module Generator Turbine Recuperator Compressor Inter-Cooler Pre-Cooler Reactor

5. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 5 Ideal CCGT for Fusion Power Plant Multi-stage compression with inter-coolers to reduce compression work Split-shaft turbine to allow independent optimization of compressor and turbine aerodynamic performance

6. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 6 The Cycle Efficiency is Optimized by Setting System Parameters Under the Designer’s Control Compressor turbine inlet temperature, T in Recuperator effectiveness,  rec System fractional pressure drop,  P/P out Turbine and compressor adiabatic efficiencies,  T,ad and  C,ad Overall compression ratio,  C =P out /P in -  C also sets the in-reactor component or IHX return temperature, T out which is constrained by material limits The power conversion system (PCS) is likely to be a small fraction of the overall capital cost (~10-20%) -power cost optimization will be driven by efficiency gains over PCS component cost -for fusion we can assume that PCS component designs are limited mainly by technology.

7. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 7 Current and Near-Term Technology Values of CCGT Design Parameters and Corresponding Gross Cycle Efficiency IndependentCurrentNear- Term VariableValueValue T in 850 o C 1,200 o C *  rec 95% 96% (@ ~510 o C)(@ ~800 o C) P out 7 MPa15 MPa  T,ad 93%94%  C,ad 89%92%  P/P out 0.070.04  cycle 51%64% *10-20 years in the future Minimum He Temp. in cycle (heat sink) = 35°C

8. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 8 Sensitivity of CCGT Performance to Independent Parameters for the Case of Optimized  C Changing the turbine inlet temperature from 850°C to 1200°C has the major effect on increasing  cycle from 51% to ~60%. Changing the other parameters within the stated range play a lesser but still significant role, cumulatively pushing  cycle to 64%.

9. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 9 Ceramic Turbine Would Allow for High Temperature Operation  The major issues associated with large helium turbocompressors are: -Material limitations of high temperature blades and disks -Dynamic stability of large flexible rotor assemblies -Dynamic loading capability of magnetic bearings  High temperature turbine blades/disks limited by creep and fatigue crack growth -Uncooled turbine components made of cast mono-crystal nickel (e.g. IN-100) and special wrought materials -Projected useable lifetimes of 50-60,000 hrs at 850 ° C -Cooling of blades/disks with cold bypass helium -Higher inlet temperatures, but with diminishing improvements -Refractories and ceramics offers high potential gains in performance - Arc-cast molybdenum based refractories (e.g. TZM) could allow inlet temperatures as high as 1000 ° C -SiC f /SiC composites could allow inlet temperatures of up to 1150-1200 ° C -Advanced carbon-carbon materials exhibit acceptable strength at temperatures up to 1500 ° C in low oxidizing helium environments

10. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 10 High Adiabatic Efficiencies Can be Achieved with Split-Shaft and Larger-Size Compressor and Turbine Helium turbine and compressor adiabatic efficiencies dependent on volumetric flow and rotational speeds. -Common practice is to connect turbine and compressor through a common shaft to limit runaway speeds in the event of a loss-of-loads -This limits optimization of the compressor efficiency, which performs better at high rotational speeds to compensate for lower volumetric flows -Splitting the turbine and compressor into two shafts gives better compressor performances but requires development of fast-acting control techniques It is easier to achieve higher adiabatic efficiencies with larger turbine and compressor sizes (94 and 92%, respectively achievable for ~400 MWe). - Large helium turbocompressors tend to be long and flexible and operating speed will be well into the critical speed range -Operation of large turbines above critical speeds is only possible with magnetic bearings, which can actively control stiffness and damping characteristics to adjust the critical speed relative to the operating speed -Fusion rotors are estimated to weight ~100 tonnes and would require 4-6 radial bearings. -The largest rotor suspended to-date on magnetic bearings is 23 tonnes using 5 active magnetic radial bearings

11. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 11 High Recuperator Effectiveness Achievable Based on Near-Term Technology Development of plate-fin recuperators in last two decades was the most important advance for improving CCGT performance. -Until the early 1980’s, tubular designs limited large recuperator effectiveness to ~ 81-82%. -Development of manufacturing techniques for large plate-fin recuperators in the early 1980s by Allied Signal and others made possible designs of helium recuperators with  of up to 95%. -Presently, high temperature, high effectiveness recuperators are available from Allied Signal, Heatrix (U.K.) and IHI (Japan). -OKBM of Nizhny-Novgorad (Russia) recently constructed and tested a modular helium recuperator for nuclear CCGT service and demonstrated 95% effectiveness at a heat duty of 628 MWt, peak temperature of 508 o C and pressure differential of 45 atm.

12. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 12 Key Challenge for Advanced Helium CCGT Recuperator is Accommodation of Increased Temperature and Pressure Differential Maximum recuperator temperature -~590-600°C for medium priced heat exchanger materials (e.g. SS316) -~750-800°C for ~10x more expensive nickel based alloys (e.g. Alloy 800H) Use of ceramic materials for high effectiveness, high temperature, high pressure, fixed surface recuperator still needs to be demonstrated High heat flux porous media as heat exchanger configuration might also improve future recuperator performance and needs to be further studied Even based on metallic materials and conventional configurations, recuperator effectiveness of 96% at a temperature of 800 o C are projected for fusion reactors

13. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 13 High Pressure Operation Would Minimize Fractional Pressure Drop and Increase Cycle Efficiency Brayton cycle efficiency is dependent on the fractional pressure drop (  P/P) High pressure losses, as expected from high volume flow rates through fusion in- reactor elements, can be compensated by increase in the system pressure. The maximum pressure considered in nuclear design studies to-date is ~7 MPa, limited to the capability of large, uninsulated, high temperature pressure vessels. Internal insulation would increase the pressure capability Power conversion system should be able to achieve pressure capabilities of current nuclear pressure vessels and piping components (~15 MPa.) It is likely that He-cooled in-reactor components will establish the pressure limit  P/P of 0.04 seems achievable based on past studies

14. October 15-19, 2000 R. Schleicher, A. R. Raffray, and C. P. Wong, An Assessment of the Brayton Cycle…, TOFE 2000 14 Conclusions Helium closed-cycle gas turbines are a promising technology for future fusion plants. They can be coupled with fusion in-reactor components using the same He coolant but also using different coolants via an intermediate heat exchanger The overall compression ratio for given cycle parameters can be optimized for maximum cycle efficiency and acceptable in-reactor inlet temperature as required by material consideration Based on current technology, He CCGT can achieve a gross cycle efficiency of ~51% With technology developments related to turbine and recuperator materials and increases in turbine size, it seems reasonable to expect an increased gross thermal efficiency of up to ~64% on a time scale of ~10-20 years As the technology is applicable to both fusion and fission reactors, fusion will benefit from current developments and demonstrations in this area under fission programs