Behrendt, Thomas und Richter, Tim und 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, Seite 26909. ASME. ASME Turbo Expo 2014, 2014-06-16 - 2014-06-20, Düsseldorf, Deutschland.
Dieses Archiv kann nicht den Volltext zur Verfügung stellen.
Kurzfassung
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.
elib-URL des Eintrags: | https://elib.dlr.de/89593/ | ||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Dokumentart: | Konferenzbeitrag (Vortrag, Anderer) | ||||||||||||||||
Titel: | Characterization of Advanced Combustor Cooling Concepts for Metallic and Oxide Ceramic Matrix Composites in a Reacting Flow | ||||||||||||||||
Autoren: |
| ||||||||||||||||
Datum: | 2014 | ||||||||||||||||
Erschienen in: | Proceedings of the ASME Turbo Expo: Turbine Technical Conference and Exposition, 2014, Vol 1A | ||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||
Open Access: | Nein | ||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||
In ISI Web of Science: | Ja | ||||||||||||||||
Seitenbereich: | Seite 26909 | ||||||||||||||||
Verlag: | ASME | ||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||
Stichwörter: | Combustor cooling, single skin effusion cooling, combustion instabilities, infrared thermography, ceramic matrix composites, additive manufacturing | ||||||||||||||||
Veranstaltungstitel: | ASME Turbo Expo 2014 | ||||||||||||||||
Veranstaltungsort: | Düsseldorf, Deutschland | ||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||
Veranstaltungsbeginn: | 16 Juni 2014 | ||||||||||||||||
Veranstaltungsende: | 20 Juni 2014 | ||||||||||||||||
Veranstalter : | ASME IGTI | ||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||
HGF - Programmthema: | Antriebssysteme | ||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||
DLR - Forschungsgebiet: | L ER - Engine Research | ||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Brennkammertechnologien (alt) | ||||||||||||||||
Standort: | Köln-Porz | ||||||||||||||||
Institute & Einrichtungen: | Institut für Antriebstechnik > Brennkammer Technische Infrastruktur | ||||||||||||||||
Hinterlegt von: | Behrendt, Dr.-Ing. Thomas | ||||||||||||||||
Hinterlegt am: | 30 Jun 2014 10:44 | ||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:55 |
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags