Behrendt, Thomas and Richter, Tim and Söhngen, Anna-Samira (2014) Characterization of Advanced Combustor Cooling Concepts for Metallic and Oxide Ceramic Matrix Composites in a Reacting Flow. In: Proceedings of the ASME Turbo Expo: Turbine Technical Conference and Exposition, 2014, Vol 1A, p. 26909. ASME. ASME Turbo Expo 2014, 2014-06-16 - 2014-06-20, Düsseldorf, Deutschland.
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Abstract
Effusion cooling is a promising approach to cool especially the walls of lean combustors where the cooling air consumption is to be reduced significantly. Due to the velocity distribution and cooling air pressure drop in a combustor the effectiveness can be further increased by reducing the cooling air momentum. Double skin designs like impingement effusion cooling provide a significant improvement but at the drawback of a complex and expensive manufacturing process. Different advanced cooling concepts offering a similar reduction of the cooling air jet momentum in a single skin design for metal and ceramic walls are characterized under realistic conditions. Lateral trenches as well as effusion holes with 90° turns are used. Their total cooling effectiveness is compared to a plain single skin effusion cooling concept. The metallic samples are manufactured using additive manufacturing offering additional degrees of freedom in the cooling design in comparison to conventional manufacturing techniques.
Item URL in elib: | https://elib.dlr.de/89593/ | ||||||||||||||||
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Document Type: | Conference or Workshop Item (Speech, Other) | ||||||||||||||||
Title: | Characterization of Advanced Combustor Cooling Concepts for Metallic and Oxide Ceramic Matrix Composites in a Reacting Flow | ||||||||||||||||
Authors: |
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Date: | 2014 | ||||||||||||||||
Journal or Publication Title: | Proceedings of the ASME Turbo Expo: Turbine Technical Conference and Exposition, 2014, Vol 1A | ||||||||||||||||
Refereed publication: | Yes | ||||||||||||||||
Open Access: | No | ||||||||||||||||
Gold Open Access: | No | ||||||||||||||||
In SCOPUS: | No | ||||||||||||||||
In ISI Web of Science: | Yes | ||||||||||||||||
Page Range: | p. 26909 | ||||||||||||||||
Publisher: | ASME | ||||||||||||||||
Status: | Published | ||||||||||||||||
Keywords: | Combustor cooling, single skin effusion cooling, combustion instabilities, infrared thermography, ceramic matrix composites, additive manufacturing | ||||||||||||||||
Event Title: | ASME Turbo Expo 2014 | ||||||||||||||||
Event Location: | Düsseldorf, Deutschland | ||||||||||||||||
Event Type: | international Conference | ||||||||||||||||
Event Start Date: | 16 June 2014 | ||||||||||||||||
Event End Date: | 20 June 2014 | ||||||||||||||||
Organizer: | ASME IGTI | ||||||||||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||
HGF - Program: | Aeronautics | ||||||||||||||||
HGF - Program Themes: | propulsion systems | ||||||||||||||||
DLR - Research area: | Aeronautics | ||||||||||||||||
DLR - Program: | L ER - Engine Research | ||||||||||||||||
DLR - Research theme (Project): | L - Combusion Chamber Technologies (old) | ||||||||||||||||
Location: | Köln-Porz | ||||||||||||||||
Institutes and Institutions: | Institute of Propulsion Technology > Combustor Technical Infrastructure | ||||||||||||||||
Deposited By: | Behrendt, Dr.-Ing. Thomas | ||||||||||||||||
Deposited On: | 30 Jun 2014 10:44 | ||||||||||||||||
Last Modified: | 24 Apr 2024 19:55 |
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