elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

Application of endoscopic OH* chemiluminescence measurements at a full-scale high-pressure gas turbine combustion test rig

Witzel, Benjamin and Heinze, Johannes and Kock, Boris F. and Stockhausen, Guido and Streb, Holger and van Kampen, Jaap and Schulz, Christof and Willert, Christian and Fleing, Christian (2012) Application of endoscopic OH* chemiluminescence measurements at a full-scale high-pressure gas turbine combustion test rig. In: Proceedings of ASME Turbo Expo 2012 (GT2012-68965). ASME Turbo Expo 2012, 11-15 June 2012, Kopenhagen, Denmark.

Full text not available from this repository.

Abstract

Single burner combustion tests play a key role in the Siemens gas turbine combustion system development process. The main scope of these tests is to assess the performance of combustor design variants in terms emissions or combustion stability at gas turbine relevant operation conditions. Both emissions and combustion stability strongly depend on the flame front and flame position. A pragmatic approach to investigate the flame is to detect the chemiluminescence signal of the combustion intermediate species OH*. Thus, the OH*-chemiluminescence signal was recorded at high-pressure combustion tests to get more insight in the complex interactions between combustor design, operation conditions and combustion performance. To minimize the impact of the measurement system on the combustion behavior, the optical access to the test rig was realized by using a water-cooled probe with an UV-transparent endoscope. The probe was located in the test rig side-wall, downstream of the burner outlet, viewing towards the burner with a 90° angle relative to the endoscope orientation. The experimental setup was completed by a combination of bandpass filters and an ICCD camera. During the experiments acoustic pressure oscillations inside the combustion chamber were recorded simultaneously to the chemiluminescence images to allow for phase-sorting of the recorded images during the image post-processing. The postprocessed images then were correlated with the pressure oscillations to investigate the relationship of the heat release to the pressure oscillations. The measurements were carried out during single burner gas turbine combustion tests at realistic gas turbine operation conditions at a scaled pressure of 9 bar. This paper presents selected test results and discusses how they give new insight in the complex combustion processes at full-scale high-pressure gas turbine combustion tests.

Document Type:Conference or Workshop Item (Paper)
Title:Application of endoscopic OH* chemiluminescence measurements at a full-scale high-pressure gas turbine combustion test rig
Authors:
AuthorsInstitution or Email of Authors
Witzel, BenjaminSiemens AG
Heinze, Johannesjohannes.heinze@dlr.de
Kock, Boris F.Siemens AG
Stockhausen, Guidoguido.stockhausen@dlr.de
Streb, HolgerSiemens AG
van Kampen, JaapSiemens AG
Schulz, ChristofUni Duisburg-Essen
Willert, Christianchris.willert@dlr.de
Fleing, Christianchristian.fleing@dlr.de
Date:June 2012
Journal or Publication Title:Proceedings of ASME Turbo Expo 2012
Refereed publication:Yes
In ISI Web of Science:No
Status:Published
Keywords:OH* chemiluminescence, endoscope, fiberscope, phase-averaging, phase-sorting
Event Title:ASME Turbo Expo 2012
Event Location:Kopenhagen, Denmark
Event Type:international Conference
Event Dates:11-15 June 2012
Organizer:ASME
HGF - Research field:Energy
HGF - Program:Efficient Energy Conversion (old)
HGF - Program Themes:E VG - Combustion and Gas Turbine Technologies (old)
DLR - Research area:Energy
DLR - Program:E VG - Combustion and Gas Turbine Technologies
DLR - Research theme (Project):E - Verbrennungs- und Kraftwerkssysteme (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Engine Measurement Systems
Deposited By: Dr.phil. Christian Willert
Deposited On:22 Aug 2012 11:18
Last Modified:22 Aug 2012 11:18

Repository Staff Only: item control page

Browse
Search
Help & Contact
Informationen
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.