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Research on Hot Stream Liners for Acoustic Damping at DLR

Bake, F. (2012) Research on Hot Stream Liners for Acoustic Damping at DLR. In: Proceedings of the ASME Turbo Expo 2012, Vol 5. ASME Turbo Expo 2012: Power for Land, Sea and Air; Panel Session on "Combustion Dynamics Integrated with Structures: Aero Excitations & Damping, 11.06. - 15.06.2012, Copenhagen, Denmark.

Full text not available from this repository.

Abstract

Thermoacoustic instabilities remain of great concern for the design of modern gas turbine combustors, especially due to the application of lean burn concepts, the need for fuel flexibility, and a wide operating range with respective safety margins. Combustor oscillations can cause severe damage to the combustor itself and adjacent components. Thus, gas turbine manufacturers – which includes both aero-engines and industrial gas turbines – have developed a range of concepts and devices in order to avoid, suppress, or reduce these instabilities. One of those concepts applicable for gas turbine combustors relies on the damping of the occurring pressure fluctuations in order to weaken the coupling with the unsteady heat release to suppress the instability growth. Since most of the current combustors need some dilution and cooling air somewhere downstream of the primary combustion zone, the feeding system for this secondary air could be designed in a way to provide appropriate damping for the pressure fluctuations as well. Here, the research activity of the s at the German Aerospace Center (DLR) in the field of damping liners, especially for hot stream application, is presented. The results of extensive experimental studies on the influence of the various liner parameters like for instance perforation ratio, bias flow and cavity design will be shown. Since the liner design for real engine application requires also the damping dependencies on pressure and temperature, the DLR Department of Engine Acoustics built up a new test facility, the Hot-Acoustic-Testrig (HAT). This testrig allows the investigation of damping characteristics and cooling performance of hot stream liner segments. The features of this test facility will be explained in detail.

Item URL in elib:https://elib.dlr.de/80198/
Document Type:Conference or Workshop Item (Speech)
Title:Research on Hot Stream Liners for Acoustic Damping at DLR
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Bake, F.UNSPECIFIEDUNSPECIFIED
Date:2012
Journal or Publication Title:Proceedings of the ASME Turbo Expo 2012, Vol 5
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Status:Published
Keywords:Acoustic damping, combustion noise, HAT, liner, bias flow liner
Event Title:ASME Turbo Expo 2012: Power for Land, Sea and Air; Panel Session on "Combustion Dynamics Integrated with Structures: Aero Excitations & Damping
Event Location:Copenhagen, Denmark
Event Type:international Conference
Event Dates:11.06. - 15.06.2012
HGF - Research field:Energy, Aeronautics, Space and Transport
HGF - Program:Efficient Energy Conversion and Use (old), Aeronautics
HGF - Program Themes:Power Plants (old), Propulsion Systems (old)
DLR - Research area:Energy, Aeronautics
DLR - Program:E VG - Combustion and Gas Turbine Technologies, L ER - Engine Research
DLR - Research theme (Project):E - Gasturbine (old), L - Combustion Chamber Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Kaur, Balbir
Deposited On:10 Jan 2013 11:54
Last Modified:27 Jun 2018 14:54

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