High overall pressure ratio (OPR) engine cycles for reduced NOx emissions will generate new aggravated requirements and boundary conditions by implementing low emission combustion technologies into advanced engine architectures. Lean burn combustion systems will have a significant impact on the temperature and velocity traverse at the combustor exit. With the transition to high-pressure engines, it is essential to fully understand and determine the high energetic interface between combustor and turbine to avoid excessive cooling. Spatially resolved temperatures were measured at different operating conditions using planar laser-induced fluorescence of OH (OH-PLIF) and filtered Rayleigh scattering (FRS), the latter being used in a combustor environment for the first time. Apart from a conventional signal detection arrangement, FRS was also applied with an endoscope for signal collection, to assess its feasibility for future application in a full annular combustor with restricted optical access. Both techniques are complementary in several respects, which justified their combined application. OH-PLIF allows instantaneous measurements and therefore enables local temperature statistics, but is limited to relatively high temperatures. On the other hand, FRS can also be applied at low temperatures, which makes it particularly attractive for measurements in cooling layers. However, FRS requires long sampling times and therefore can only provide temporal averages. When applied in combination, the accuracy of both techniques could be improved by each method helping to overcome the other's shortcomings.
Skip Nav Destination
Article navigation
February 2017
Research-Article
Temperature Measurements at the Outlet of a Lean Burn Single-Sector Combustor by Laser Optical Methods
Ulrich Doll,
Ulrich Doll
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Ulrich.Dolll@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Ulrich.Dolll@dlr.de
Search for other works by this author on:
Guido Stockhausen,
Guido Stockhausen
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Guido.Stockhausen@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Guido.Stockhausen@dlr.de
Search for other works by this author on:
Johannes Heinze,
Johannes Heinze
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Johannes.Heinze@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Johannes.Heinze@dlr.de
Search for other works by this author on:
Ulrich Meier,
Ulrich Meier
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Ulrich.Meier@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Ulrich.Meier@dlr.de
Search for other works by this author on:
Christoph Hassa,
Christoph Hassa
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Christoph.Hassa@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Christoph.Hassa@dlr.de
Search for other works by this author on:
Imon Bagchi
Imon Bagchi
Rolls-Royce Deutschland Ltd & Co KG,
Eschenweg 11, Dahlewitz,
Blankenfelde-Mahlow 15827, Germany
e-mail: Imon-Kalyan.Bagchi@rolls-royce.com
Eschenweg 11, Dahlewitz,
Blankenfelde-Mahlow 15827, Germany
e-mail: Imon-Kalyan.Bagchi@rolls-royce.com
Search for other works by this author on:
Ulrich Doll
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Ulrich.Dolll@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Ulrich.Dolll@dlr.de
Guido Stockhausen
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Guido.Stockhausen@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Guido.Stockhausen@dlr.de
Johannes Heinze
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Johannes.Heinze@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Johannes.Heinze@dlr.de
Ulrich Meier
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Ulrich.Meier@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Ulrich.Meier@dlr.de
Christoph Hassa
DLR—German Aerospace Center,
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Christoph.Hassa@dlr.de
Institute of Propulsion Technology,
Linder Hoehe,
Cologne 51147, Germany
e-mail: Christoph.Hassa@dlr.de
Imon Bagchi
Rolls-Royce Deutschland Ltd & Co KG,
Eschenweg 11, Dahlewitz,
Blankenfelde-Mahlow 15827, Germany
e-mail: Imon-Kalyan.Bagchi@rolls-royce.com
Eschenweg 11, Dahlewitz,
Blankenfelde-Mahlow 15827, Germany
e-mail: Imon-Kalyan.Bagchi@rolls-royce.com
1Corresponding author.
Contributed by the Combustion and Fuels Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received June 29, 2016; final manuscript received July 5, 2016; published online September 20, 2016. Editor: David Wisler.
J. Eng. Gas Turbines Power. Feb 2017, 139(2): 021507 (10 pages)
Published Online: September 20, 2016
Article history
Received:
June 29, 2016
Revised:
July 5, 2016
Citation
Doll, U., Stockhausen, G., Heinze, J., Meier, U., Hassa, C., and Bagchi, I. (September 20, 2016). "Temperature Measurements at the Outlet of a Lean Burn Single-Sector Combustor by Laser Optical Methods." ASME. J. Eng. Gas Turbines Power. February 2017; 139(2): 021507. https://doi.org/10.1115/1.4034355
Download citation file:
Get Email Alerts
An Adjustable Elastic Support Structure for Vibration Suppression of Rotating Machinery
J. Eng. Gas Turbines Power
Operation of a Compression Ignition Engine at Idling Load under Simulated Cold Weather Conditions
J. Eng. Gas Turbines Power
In-Cylinder Imaging and Emissions Measurements of Cold-Start Split Injection Strategies
J. Eng. Gas Turbines Power
Related Articles
Flow Field Characterization at the Outlet of a Lean Burn Single-Sector Combustor by Laser-Optical Methods
J. Eng. Gas Turbines Power (January,2017)
Inverse Analysis of In-Cylinder Gas-Wall Boundary Conditions: Investigation of a Yttria-Stabilized Zirconia Thermal Barrier Coating for Homogeneous Charge Compression Ignition
J. Eng. Gas Turbines Power (October,2017)
Wall Temperature Measurements in a Full-Scale Gas Turbine Combustor Test Rig With Fiber Coupled Phosphor Thermometry
J. Turbomach (January,2021)
The Effect of Liquid-Fuel Preparation on Gas Turbine Emissions
J. Eng. Gas Turbines Power (March,2008)
Related Proceedings Papers
Related Chapters
Physiology of Human Power Generation
Design of Human Powered Vehicles
Outlook
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