Combustion Sensors: Gas Turbine Applications

By: Nasa, National Aeronautics and Space Adm

This report documents efforts to survey the current research directions in sensor technology for gas turbine systems. The work is driven by the current and future requirements on system performance and optimization. Accurate real time measurements of velocities, pressure, temperatures, and species concentrations will be required for objectives such as combustion instability attenuation, pollutant reduction, engine health management, exhaust profile control via active control, etc. Changing combustor conditions - engine aging, flow path slagging, or rapid maneuvering - will require adaptive responses; the effectiveness of such will be only as good as the dynamic information available for processing. All of these issues point toward the importance of continued sensor development. For adequate control of the combustion process, sensor data must include information about the above mentioned quantities along with equivalence ratios and radical concentrations, and also include both temporal and spatial velocity resolution. Ultimately these devices must transfer from the laboratory to field installations, and thus must become low weight and cost, reliable and maintainable. A primary conclusion from this study is that the optics-based sensor science will be the primary diagnostic in future gas turbine technologies.Human, MelAmes Research CenterCOMBUSTION; COMBUSTION STABILITY; GAS TURBINES; OPTICAL MEASURING INSTRUMENTS; TECHNOLOGY ASSESSMENT; RESEARCH; TEMPERATURE MEASUREMENT; VELOCITY MEASUREMENT; PRESSURE MEASUREMENT

• Format: Paperback
• Language: English
• ISBN: 1723713120
• ISBN13: 9781723713125
• Release Date: January 1
• Publisher: Independently Published
• Length: 34 Pages
• Weight: 0.23 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"