Hassa, Christoph and Magens, Eggert and Voigt, Lena and Diers, Olaf and Otterpohl, Ingo and Heinze, Johannes (2020) Soot Formation and Emission from JET A-1 and a 30 % HEFA blend in a multisector combustor at realistic operating conditions. In: ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020. ASME Turbo Expo 2020 Turbommachinery Technical Conference and Exposition, 21.-25.9.2020, virtuell. doi: 10.1115/GT2020-14462. ISBN 978-079188419-5.
Full text not available from this repository.
Abstract
The production and emission of soot from Kerosene JETA1 and a blend of a different JET-A1 and 30 % HEFA was investigated in a realistic multisector combustor of Rolls-Royce Deutschland. Soot concentration measurements were performed at the exit as well as in the optically accessible primary zone of the combustor. There, information of soot mass concentration is available from measurements using Laser induced incandescence and Laser extinction. At the exit of the combustor, soot particles were measured with a scanning mobility particle sizer. This resulted in particle size distributions from which soot number and mass concentrations were calculated. Within the pressurized combustor, low load points, scaled cruise and high load points were operated. For the investigated operating range which reaches to ~50 % of max pressure but preserves engine AFR, up to 75 % reduction of both soot particle mass and number EI were observed for the HEFA blend in part load and 50 % at the scaled high-power condition. However at the end of the primary zone, a reduction increasing with soot concentration and fuel load was recorded. This guides attention to the different oxidation characteristics for the fuels in the investigated combustor. Accordingly, larger particles were consistently measured at the exit for the HEFA blend.
Item URL in elib: | https://elib.dlr.de/136476/ | |||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Document Type: | Conference or Workshop Item (Other) | |||||||||||||||||||||
Title: | Soot Formation and Emission from JET A-1 and a 30 % HEFA blend in a multisector combustor at realistic operating conditions | |||||||||||||||||||||
Authors: |
| |||||||||||||||||||||
Date: | 21 September 2020 | |||||||||||||||||||||
Journal or Publication Title: | ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020 | |||||||||||||||||||||
Refereed publication: | Yes | |||||||||||||||||||||
Open Access: | No | |||||||||||||||||||||
Gold Open Access: | No | |||||||||||||||||||||
In SCOPUS: | Yes | |||||||||||||||||||||
In ISI Web of Science: | No | |||||||||||||||||||||
DOI: | 10.1115/GT2020-14462 | |||||||||||||||||||||
ISBN: | 978-079188419-5 | |||||||||||||||||||||
Status: | Published | |||||||||||||||||||||
Keywords: | HEFA blend, Aero-engine combustor, Particle measurement | |||||||||||||||||||||
Event Title: | ASME Turbo Expo 2020 Turbommachinery Technical Conference and Exposition | |||||||||||||||||||||
Event Location: | virtuell | |||||||||||||||||||||
Event Type: | international Conference | |||||||||||||||||||||
Event Dates: | 21.-25.9.2020 | |||||||||||||||||||||
Organizer: | American Society of Mechanical Engineers | |||||||||||||||||||||
HGF - Research field: | Aeronautics, Space and Transport | |||||||||||||||||||||
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 (old) | |||||||||||||||||||||
Location: | Köln-Porz | |||||||||||||||||||||
Institutes and Institutions: | Institute of Propulsion Technology > Combustor | |||||||||||||||||||||
Deposited By: | Hassa, Dr.-Ing. Christoph | |||||||||||||||||||||
Deposited On: | 10 Dec 2020 12:07 | |||||||||||||||||||||
Last Modified: | 08 Feb 2021 10:32 |
Repository Staff Only: item control page