A novel cooling and power cycle has been proposed that combines a semi-closed cycle gas turbine called the High Pressure Regenerative Turbine Engine (HPRTE) with a vapor absorption refrigeration system (VARS). The refrigeration cycle (VARS) interacts with the power cycle (HPRTE) solely through heat transfer in the generator and the evaporator. Waste heat from the recirculated combustion gas of the HPRTE is used to power the absorption refrigeration unit, which cools the high-pressure compressor inlet of the HPRTE to below ambient conditions and also produces excess refrigeration, in an amount which depends on ambient conditions. Water produced as a product of combustion is intentionally condensed in the evaporator of the VARS, which is designed to provide sufficient cooling for three purposes: chilling the inlet air to the high pressure compressor, water extraction, and for an external cooling load. In a previous study, the combined cycle was modeled using zero-dimensional steady-state thermodynamics, with the specified values of efficiencies and pressure drops for the turbo-machinery and heat exchangers. The model predicts that the combined cycle with steam blade cooling for a medium-sized engine will have a thermal efficiency of 49%, in addition to the external refrigeration load generated in the cycle which is 13% of the net work output. It also produces about 1.4 kg of water for each kg of fuel (propane) consumed. A small experimental unit demonstrating the HPRTE/VARS combined cycle has been constructed and is currently being tested in the Energy & Gas-dynamic Systems Laboratory at the University of Florida. A 45 HP Rover 1S-60 engine is integrated with a NH3/H2O vapor absorption refrigeration unit having a capacity of 19 Ton Refrigeration. The engine flow-path has been significantly modified to include partial recirculation of exhaust products, turbocharging, and recuperation, thus implementing the HPRTE concept. In addition, a significant modeling effort has been undertaken to simulate the combined cycle operation under design and off-design conditions. Initial experimental results show good agreement with the model predictions, including overall efficiency and water extraction rates.
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ASME 2006 International Mechanical Engineering Congress and
Exposition
November 5–10, 2006
Chicago, Illinois, USA
Conference Sponsors:
- Advanced Energy Systems Division
ISBN:
0-7918-4764-0
PROCEEDINGS PAPER
Testing and Modeling of a Semi-Closed Gas Turbine Cycle Integrated With a Vapor Absorption Refrigeration System
J. F. Crittenden,
J. F. Crittenden
Triad Research Corporation
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P. L. Meitner
P. L. Meitner
U.S. Army Research Laboratory
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J. R. Khan
University of Florida
W. E. Lear
University of Florida
S. A. Sherif
University of Florida
E. B. Howell
University of Florida
J. F. Crittenden
Triad Research Corporation
P. L. Meitner
U.S. Army Research Laboratory
Paper No:
IMECE2006-15403, pp. 137-148; 12 pages
Published Online:
December 14, 2007
Citation
Khan, JR, Lear, WE, Sherif, SA, Howell, EB, Crittenden, JF, & Meitner, PL. "Testing and Modeling of a Semi-Closed Gas Turbine Cycle Integrated With a Vapor Absorption Refrigeration System." Proceedings of the ASME 2006 International Mechanical Engineering Congress and Exposition. Advanced Energy Systems. Chicago, Illinois, USA. November 5–10, 2006. pp. 137-148. ASME. https://doi.org/10.1115/IMECE2006-15403
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