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Proc. ASME. GT2017, Volume 6: Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy, V006T05A004, June 26–30, 2017

Paper No: GT2017-63413

DOI: https://doi.org/10.1115/GT2017-63413

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Topics: Combustion chambers, Gas turbines, Cooling, Aircraft engines, Combustion, Combustion technologies, Computer simulation, Emissions, Flames, Flow (Dynamics)

Journal Articles

Development and Test of Oxide/Oxide Ceramic Matrix Composites Combustor Liner Demonstrators for Aero-engines

Thomas Behrendt, Stefan Hackemann, Peter Mechnich, Yuan Shi, Sandrine Hönig, Severin Hofmann, Dietmar Koch

J. Eng. Gas Turbines Power. March 2017, 139(3): 031507.

Paper No: GTP-16-1275

DOI: https://doi.org/10.1115/1.4034515

Published Online: October 4, 2016

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Topics: Ceramic matrix composites, Combustion chambers, Cooling, Temperature, Stress, Design

Proceedings Papers

Effusion Cooled Combustor Liner Tiles With Modern Cooling Concepts: A Comparative Experimental Study

Thomas Jackowski, Achmed Schulz, Hans-Jörg Bauer, Miklós Gerendás, Thomas Behrendt

Proc. ASME. GT2016, Volume 5B: Heat Transfer, V05BT17A007, June 13–17, 2016

Paper No: GT2016-56598

DOI: https://doi.org/10.1115/GT2016-56598

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Topics: Combustion chambers, Cooling, Tiles, Pressure, Combustion, Coolants, Flow (Dynamics), Geometry, Temperature, Additive manufacturing

Proceedings Papers

Development and Test of Oxide/Oxide CMC Combustor Liner Demonstrators for Aero Engines

Thomas Behrendt, Stefan Hackemann, Peter Mechnich, Yuan Shi, Sandrine Hönig, Severin Hofmann, Dietmar Koch

Proc. ASME. GT2016, Volume 6: Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy, V006T02A004, June 13–17, 2016

Paper No: GT2016-57323

DOI: https://doi.org/10.1115/GT2016-57323

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Topics: Aircraft engines, Ceramic matrix composites, Combustion chambers, Design, Failure, Protective coatings, Alloys, Coating processes, Coatings, Computers

Proceedings Papers

Characterization of Advanced Combustor Cooling Concepts for Metallic Walls and Oxide Ceramic Matrix Composites in a Reacting Flow

Thomas Behrendt, Tim Richter, Anna-Samira Söhngen

Proc. ASME. GT2014, Volume 5C: Heat Transfer, V05CT18A014, June 16–20, 2014

Paper No: GT2014-26909

DOI: https://doi.org/10.1115/GT2014-26909

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Topics: Combustion chambers, Composite materials, Cooling, Flow (Dynamics), Oxide ceramics, Skin, Design, Manufacturing, Momentum, Additive manufacturing

Proceedings Papers

Experimental and Numerical Investigation of a Planar Combustor Sector at Realistic Operating Conditions

Thomas Behrendt, Martin Carl, Christian Fleing, Matthias Frodermann, Johannes Heinze, Christoph Hassa, Ulrich Meier, Dagmar Wolff-Gaßmann, Stefan Hohmann, Nikolaos Zarzalis

Proc. ASME. GT2000, Volume 2: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations, V002T02A043, May 8–11, 2000

Paper No: 2000-GT-0123

DOI: https://doi.org/10.1115/2000-GT-0123

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Topics: Combustion chambers, Computational fluid dynamics, Flow (Dynamics), Aerospace industry, Air jets, Chemiluminescence, Collaboration, Electromagnetic scattering, Engines, Light scattering

Proceedings Papers

Development and Validation of Oxide/Oxide CMC Combustors Within the HiPOC Program

Miklós Gerendás, Christian Wilhelmi, Thays Machry, Ralf Knoche, Erich Werth, Thomas Behrendt, Dietmar Koch, Severin Hofmann, Jürgen Göring, Kamen Tushtev, Eike Volkmann

Proc. ASME. GT2013, Volume 4: Ceramics; Concentrating Solar Power Plants; Controls, Diagnostics and Instrumentation; Education; Electric Power; Fans and Blowers, V004T02A003, June 3–7, 2013

Paper No: GT2013-94679

DOI: https://doi.org/10.1115/GT2013-94679

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Topics: Ceramic matrix composites, Combustion chambers, Design, Fibers, Combustion, Manufacturing, Oxide ceramics, Sealing (Process), Testing, Clearances (Engineering)

Proceedings Papers

Characterization of the Influence of Moderate Pressure Fluctuations on the Cooling Performance of Advanced Combustor Cooling Concepts in a Reacting Flow

Thomas Behrendt, Miklós Gerendás

Proc. ASME. GT2012, Volume 4: Heat Transfer, Parts A and B, 987-999, June 11–15, 2012

Paper No: GT2012-68845

DOI: https://doi.org/10.1115/GT2012-68845

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Topics: Combustion, Combustion chambers, Cooling, Flow (Dynamics), Fluctuations (Physics), Pressure

Proceedings Papers

Improvement of Oxide/Oxide CMC and Development of Combustor and Turbine Components in the HiPOC Program

Miklo´s Gerenda´s, Yannick Cadoret, Christian Wilhelmi, Thays Machry, Ralf Knoche, Thomas Behrendt, Thomas Aumeier, Sandrine Denis, Ju¨rgen Go¨ring, Dietmar Koch, Kamen Tushtev

Proc. ASME. GT2011, Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Wind Turbine Technology, 477-490, June 6–10, 2011

Paper No: GT2011-45460

DOI: https://doi.org/10.1115/GT2011-45460

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Topics: Ceramic matrix composites, Combustion chambers, Turbine components, Design, Coatings, Fibers, Oxide ceramics, Temperature, Turbines, Clearances (Engineering)

Proceedings Papers

In Situ Measurement and Validation of Gaseous Species Concentrations of a Gas Turbine Model Combustor by Tunable Diode Laser Absorption Spectroscopy (TDLAS)

Thomas Behrendt, Christoph Hassa, Ajmal Mohamed, Jean-Pierre Faleni

Proc. ASME. GT2008, Volume 2: Controls, Diagnostics and Instrumentation; Cycle Innovations; Electric Power, 273-282, June 9–13, 2008

Paper No: GT2008-51258

DOI: https://doi.org/10.1115/GT2008-51258

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Topics: Absorption spectroscopy, Combustion chambers, Emissions, Gas turbines, Lasers

Proceedings Papers

Characterization of Advanced Combustor Cooling Concepts Under Realistic Operating Conditions

Thomas Behrendt, Timea Lengyel, Christoph Hassa, Miklo´s Gerenda´s

Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 1801-1814, June 9–13, 2008

Paper No: GT2008-51191

DOI: https://doi.org/10.1115/GT2008-51191

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Topics: Combustion chambers, Cooling

Proceedings Papers

Experimental Investigation of a New LPP Injector Concept for Aero Engines at Elevated Pressures

Thomas Behrendt, Johannes Heinze, Christoph Hassa

Proc. ASME. GT2003, Volume 2: Turbo Expo 2003, 377-386, June 16–19, 2003

Paper No: GT2003-38444

DOI: https://doi.org/10.1115/GT2003-38444

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Topics: Aircraft engines, Ejectors, Emissions, Optical measurement, Temperature, Chemiluminescence, Combustion chambers, Design, Electromagnetic scattering, Evaporation

Journal citation

NARROW

Turbulent Flame Shape Switching at Conditions Relevant for Gas Turbines

Turbulent Flame Shape Switching at Conditions Relevant for Gas Turbines

Design and Application of a Multidisciplinary Predesign Process for Novel Engine Concepts

Quantitative CO PLIF Measurements in Aeroengine Gas Turbine Combustion Chambers Under Realistic Conditions

Development and Test of Oxide/Oxide Ceramic Matrix Composites Combustor Liner Demonstrators for Aero-engines

Effusion Cooled Combustor Liner Tiles With Modern Cooling Concepts: A Comparative Experimental Study

Development and Test of Oxide/Oxide CMC Combustor Liner Demonstrators for Aero Engines

Characterization of Advanced Combustor Cooling Concepts for Metallic Walls and Oxide Ceramic Matrix Composites in a Reacting Flow

Experimental and Numerical Investigation of a Planar Combustor Sector at Realistic Operating Conditions

Development and Validation of Oxide/Oxide CMC Combustors Within the HiPOC Program

Characterization of the Influence of Moderate Pressure Fluctuations on the Cooling Performance of Advanced Combustor Cooling Concepts in a Reacting Flow

Improvement of Oxide/Oxide CMC and Development of Combustor and Turbine Components in the HiPOC Program

In Situ Measurement and Validation of Gaseous Species Concentrations of a Gas Turbine Model Combustor by Tunable Diode Laser Absorption Spectroscopy (TDLAS)

Characterization of Advanced Combustor Cooling Concepts Under Realistic Operating Conditions

Experimental Investigation of a New LPP Injector Concept for Aero Engines at Elevated Pressures

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