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VALIDATION METHODOLOGY FOR THE DEVELOPMENT OF LOW EMISSION FUEL INJECTORS FOR AERO-ENGINES

Hassa, Christoph and Heinze, Johanes and Rackwitz, Leif and Dörr, Thomas (2006) VALIDATION METHODOLOGY FOR THE DEVELOPMENT OF LOW EMISSION FUEL INJECTORS FOR AERO-ENGINES. In: INTERNATIONAL CONGRESS OF AERONAUTICAL SCIENCES (25), 8.10.5.1-8.10.5.12. Optimage Ltd.. INTERNATIONAL CONGRESS OF AERONAUTICAL SCIENCES, 2006-9-3 - 2006-9-7, Hamburg. ISBN 0-9533991-7-6

Full text not available from this repository.

Official URL: http://www.optimage.co.uk/

Abstract

This contribution describes a newly derived development chain for the early design and validation phases of lean burning injectors allowing a faster and cheaper design process. It comprises an initial concept definition, design optimizations based on CFD and a design validation by qualitative fuel flow tests, followed by the application of laser diagnostic methods. Finally, emission and operability characteristics are determined at real operating conditions. The comprehensiveness of the applied development chain has been proved to significantly reduce NOx emissions of the lean burners and to generate validated design rules for the fuel injectors analyzed in this study.

Item URL in elib:https://elib.dlr.de/44691/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:VALIDATION METHODOLOGY FOR THE DEVELOPMENT OF LOW EMISSION FUEL INJECTORS FOR AERO-ENGINES
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hassa, ChristophUNSPECIFIEDUNSPECIFIED
Heinze, JohanesUNSPECIFIEDUNSPECIFIED
Rackwitz, LeifRolls-Royce DeutschlandUNSPECIFIED
Dörr, ThomasRolls-Royce DeutschlandUNSPECIFIED
Date:3 September 2006
Journal or Publication Title: INTERNATIONAL CONGRESS OF AERONAUTICAL SCIENCES
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:8.10.5.1-8.10.5.12
Editors:
EditorsEmail
Grant, IanUNSPECIFIED
Publisher:Optimage Ltd.
Series Name:Proceedings of the INTERNATIONAL CONGRESS OF AERONAUTICAL SCIENCES
ISBN:0-9533991-7-6
Status:Published
Keywords:aeroengine, Combustor, desgn method, measurement, optical diagnostics, CFD, Low emission
Event Title: INTERNATIONAL CONGRESS OF AERONAUTICAL SCIENCES
Event Location:Hamburg
Event Type:international Conference
Event Dates:2006-9-3 - 2006-9-7
Organizer:International Council of the Aeronautical Sciences (ICAS)
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Combustion Chamber Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Combustor
Deposited By: Hassa, Dr.-Ing. Christoph
Deposited On:18 Sep 2006
Last Modified:27 Apr 2009 13:04

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