Impact of Methane and Hydrogen-Enriched Methane Pilot Injection on the Surface Temperature of a Scaled-Down Burner Nozzle Measured Using Phosphor Thermometry

Author:

Feuk HenrikORCID,Pignatelli FrancescoORCID,Subash ArmanORCID,Bi RuikeORCID,Szász Robert-Zoltán,Bai Xue-Song,Lörstad Daniel,Richter Mattias

Abstract

The surface temperature of a burner nozzle using three different pilot hardware configurations was measured using lifetime phosphor thermometry with the ZnS:Ag phosphor in a gas turbine model combustor designed to mimic the Siemens DLE (Dry Low Emission) burner. The three pilot hardware configurations included a non-premixed pilot injection setup and two partially premixed pilot injections where one had a relatively higher degree of premixing. For each pilot hardware configuration, the combustor was operated with either methane or hydrogen-enriched methane (H2/CH4: 50/50 in volume %). The local heating from pilot flames was much more significant for hydrogen-enriched methane compared with pure methane due to the pilot flames being in general more closely attached to the pilot nozzles with hydrogen-enriched methane. For the methane fuel, the average surface temperature of the burner nozzle was approximately 40 K higher for the partially premixed pilot injection configuration with a lower degree of mixing as compared to the non-premixed pilot injection configuration. In contrast, with the hydrogen-enriched methane fuel, the differences in surface temperature between the different pilot injection hardware configurations were much smaller due to the close-to-nozzle frame structure.

Funder

Swedish Research Council

Siemens Energy AB

Publisher

MDPI AG

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering

Reference44 articles.

1. Schefer, R. (2002, January 6–10). Reduced Turbine Emissions Using Hydrogen-Enriched Fuels. Proceedings of the 2002 US DOE Hydrogen Program Review, Golden, CO, USA.

2. Combustion of hydrogen-enriched methane in a lean premixed swirl-stabilized burner;Proc. Combust. Inst.,2002

3. Fuel Composition Effects on the Velocity Field in a Lean Premixed Swirl-Stabilized Combustor;Turbo Expo: Power Land Sea Air,2003

4. Dynamics of swirling flames;Annu. Rev. Fluid Mech.,2014

5. Gupta, A.K., Syred, N., and Lilley, D.G. (1984). Swirl Flows, Taylor & Francis.

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