ADVANCED MICROTURBINE SYSTEMS Final Report for Tasks 1 Through 4 and Task 6

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ADVANCED MICROTURBINE SYSTEMS Final Report for Tasks 1 Through 4 and Task 6 ( advanced-microturbine-systems-final-report-tasks-1-through-4 )

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APPENDIX Preliminary Design of Ceramic Components for the ST5+ Advanced Microturbine Engine Jun Shi, Venkata R. Vedula, John Holowczak, Connie E. Bird, S. Scott Ochs, Luca Bertuccioli and David J. Bombara United Technologies Research Center, East Hartford, CT ABSTRACT Progress in the preliminary design of an axial vane ring and axial turbine rotor composed of silicon nitride structural ceramics is presented. The silicon nitride components allow for significantly increased turbine inlet temperature in the ST5+, an advanced version of the Pratt & Whitney Canada's ST5, which powers the DTE Technologies ENT400 Distributed Energy Generator. Preliminary aerodynamic and mechanical design, steady state thermal and stress analysis, and life prediction results will be reviewed. Foreign object damage resistance will be compared between ceramic versions of the baseline rotor blade geometry and that developed for the ST5+ engine. INTRODUCTION The demands for fast installation of power generators and easy upgrade of power output have spurred the development of microturbines in the last few years. The California power crisis heightened such demand when power shortages and blackouts disrupted normal business operations and everyday life. The power crisis shook public confidence in electric utilities and forced consumers to rethink alternative, reliable sources of power, such as microturbines. In response to market demand, Pratt & Whitney Canada (P&WC) has teamed up with DTE Energy Technologies to develop and produce a 400 kW microturbine system, the ENT400. The ST5 microturbine is based on P&WC’s PW207 helicopter engine with modifications to suit the needs of industrial power generation. With funding from the US Department of Energy, United Technologies Research Center (UTRC) has been working closely with P&WC to improve major ENT400 performance parameters: electrical efficiency from 30% to 40% or higher and NOx emission from 9ppm to 7ppm or less on natural gas. The efficiency gain comes from a bottoming Organic Rankine Cycle (ORC) and from the use of ceramic components in the engine hot gas path. The ORC makes use of the exhaust gas to heat a low boiling point liquid that drives a second generator and thus recovers some of the energy that is otherwise lost through the stack. By using high-temperature resistant ceramic components, the engine cycle can run hotter with reduced cooling requirements, both contributing to increased cycle efficiency. Figure 1 Baseline ST5 microturbine engine The ST5 (see Figure 1) is a twin shaft engine with separate compressor and power turbine stages. ST5’s single stage radial compressor has a nominal compression ratio of 8:1 and the single stage axial compressor rotor speed is nominally 51,000 rpm. The compressor turbine vane ring and compressor turbine rotor blades are made of single crystal materials to withstand the high temperature gas exiting from the combustor transition duct. The high-temperature combustion gas requires the vane ring to be cooled by compressor discharge air. Although the compressor turbine blades are uncooled, they operate close to their temperature limit. Therefore, an uncooled ceramic vane ring and ceramic turbine rotor could offer substantial cycle benefits. The ST5+ turbine inlet temperature is approximately 1150oC, a substantial increase over that of the baseline ST5 engine. Cycle studies show that an approximate 3% gain in electrical efficiency can be obtained by using ceramic materials [1]. Proceedings of: ASME TURBOEXPO 2002 June 3-6, 2002, Amsterdam, The Netherlands 2002-GT-30547 99 Copyright © 2002 by ASME

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