Behrendt, Thomas and Hassa, Christoph (2008) A test rig for investigations of gas turbine combustor cooling concepts under realistic operating conditions. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 222, pp. 169-177. Professional Engineering Publishing. DOI: 10.1243/09544100JAERO288. ISSN 0954-4100.
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In the current paper, a new test rig for the characterization of advanced combustor cooling concepts for gas turbine combustors is presented. The test rig is designed to allow investigations at elevated pressures and temperatures representing realistic operating conditions of future lean low emission combustors. The features and capabilities of the test rig in comparison to existing rigs are described. The properties of the hot gas flow are measured in order to provide the necessary data for a detailed analysis of the measured cooling effectivity of combustor wall test samples. Results of the characterization of the velocity and temperature distribution in the hot gas flow at the leading edge of the test sample at pressures up to p<=10 bar and near wall hot gas temperatures up to TF<= 1800 K are presented.
|Title:||A test rig for investigations of gas turbine combustor cooling concepts under realistic operating conditions|
|Journal or Publication Title:||Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 169-177|
|Publisher:||Professional Engineering Publishing|
|Keywords:||gas turbine, combustor cooling, test facility|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Propulsion Systems|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ER - Engine Research|
|DLR - Research theme (Project):||L - Combustion Chamber Technologies|
|Institutes and Institutions:||Institute of Propulsion Technology > Combustor|
|Deposited By:||Dr.-Ing. Thomas Behrendt|
|Deposited On:||14 Apr 2008|
|Last Modified:||27 Apr 2009 14:53|
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