High fogging is a power augmentation device where water is sprayed upstream of the compressor inlet with higher mass flow than that which would be needed to saturate the intake air. The main focus of this paper is on applications of high fogging on the ALSTOM gas turbine engines of the family GT24/GT26. Engine operation and performance are illustrated based on test results obtained from four different engines that have meanwhile accumulated more than 12,000 operating hours (OH) in commercial operation with ALSTOM’s ALFog® high fogging system. The effect of internal cooling (water evaporation inside the compressor) is investigated considering actual compressor boundaries matched within the complete engine. Changes in the secondary air system (SAS) and corresponding movement of the engine operating line have been taken into account. Power output gain as high as 7.1% was experimentally demonstrated for injected water mass fraction equal to 1% and considering internal cooling effects only. Higher figures can be obtained for operation at low ambient relative humidity and partial evaporation upstream of the compressor inlet.
Skip Nav Destination
e-mail: giovanni.cataldi@power.alstom.com
Article navigation
January 2006
Technical Papers
Influence of High Fogging Systems on Gas Turbine Engine Operation and Performance
Giovanni Cataldi,
e-mail: giovanni.cataldi@power.alstom.com
Giovanni Cataldi
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Search for other works by this author on:
Harald Güntner,
Harald Güntner
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Search for other works by this author on:
Charles Matz,
Charles Matz
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Search for other works by this author on:
Tom McKay,
Tom McKay
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Search for other works by this author on:
Jürgen Hoffmann,
Jürgen Hoffmann
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Search for other works by this author on:
Anton Nemet,
Anton Nemet
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Search for other works by this author on:
Stefan Lecheler,
Stefan Lecheler
Universität der Bundeswehr München
, Werner-Heisenberg-Weg 39, D-85577 Neubiberg, Germany
Search for other works by this author on:
Jost Braun
Jost Braun
Kempten University of Applied Sciences
, Bahnhofstrasse 61-63, D-87435 Kempten, Germany
Search for other works by this author on:
Giovanni Cataldi
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerlande-mail: giovanni.cataldi@power.alstom.com
Harald Güntner
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Charles Matz
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Tom McKay
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Jürgen Hoffmann
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Anton Nemet
ALSTOM (Switzerland) Ltd.
, Brown Boveri Strasse 7, CH-5401 Baden, Switzerland
Stefan Lecheler
Universität der Bundeswehr München
, Werner-Heisenberg-Weg 39, D-85577 Neubiberg, Germany
Jost Braun
Kempten University of Applied Sciences
, Bahnhofstrasse 61-63, D-87435 Kempten, GermanyJ. Eng. Gas Turbines Power. Jan 2006, 128(1): 135-143 (9 pages)
Published Online: March 1, 2004
Article history
Received:
October 1, 2003
Revised:
March 1, 2004
Citation
Cataldi, G., Güntner, H., Matz, C., McKay, T., Hoffmann, J., Nemet, A., Lecheler, S., and Braun, J. (March 1, 2004). "Influence of High Fogging Systems on Gas Turbine Engine Operation and Performance." ASME. J. Eng. Gas Turbines Power. January 2006; 128(1): 135–143. https://doi.org/10.1115/1.1926313
Download citation file:
Get Email Alerts
Temperature Dependence of Aerated Turbine Lubricating Oil Degradation from a Lab-Scale Test Rig
J. Eng. Gas Turbines Power
Multi-Disciplinary Surrogate-Based Optimization of a Compressor Rotor Blade Considering Ice Impact
J. Eng. Gas Turbines Power
Experimental Investigations on Carbon Segmented Seals With Smooth and Pocketed Pads
J. Eng. Gas Turbines Power
Related Articles
Overspray and Interstage Fog Cooling in Gas Turbine Compressor Using Stage-Stacking Scheme—Part I: Development of Theory and Algorithm
J. Thermal Sci. Eng. Appl (September,2010)
Investigation of Cooling Effectiveness of Gas Turbine Inlet Fogging Location Relative to the Silencer
J. Eng. Gas Turbines Power (February,2012)
Siemens Westinghouse Advanced Turbine Systems Program Final Summary
J. Eng. Gas Turbines Power (July,2004)
Overspray and Interstage Fog Cooling in Gas Turbine Compressor Using Stage-Stacking Scheme—Part II: Case Study
J. Thermal Sci. Eng. Appl (September,2010)
Related Proceedings Papers
Related Chapters
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Thermodynamic Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Alternative Systems
Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students