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3DFlameGT SIGNED

Evaluation of three-dimensional velocity field, mixing field, and flame-front in a model gas turbinecombustor

Total Cost €

EC-Contrib. €

Partnership

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3DFlameGT project word cloud

Explore the words cloud of the 3DFlameGT project. It provides you a very rough idea of what is the project "3DFlameGT" about.

mode dominant images point conversion researcher numerical resolution recorded radical air flames velocimetry engine speed gas flame front yag complementary diversify stabilized parallel database fellow fuel generate trl training pressure model lasers mimic stereoscopic bunsen indispensable nd slices planar turbine academic sheets assembled skill evaluation burner intrusive particle separated 3d 2d play ch2o fluorescence correlated topology validated swirl energy technique generation models instantaneous traces competitiveness laser head becomes diagnostics automotive experimental noted mixing volume cluster readiness nature as cameras combustor temporal network combustion interaction ensures turbulent space pulse deduce instability concentration reconstruct flow image scanning

Project "3DFlameGT" data sheet

The following table provides information about the project.

Coordinator	IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE Organization address address: SOUTH KENSINGTON CAMPUS EXHIBITION ROAD city: LONDON postcode: SW7 2AZ website: http://www.imperial.ac.uk/ contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	United Kingdom [UK]
Total cost	183˙454 €
EC max contribution	183˙454 € (100%)
Programme	1. H2020-EU.1.3.2. (Nurturing excellence by means of cross-border and cross-sector mobility)
Code Call	H2020-MSCA-IF-2016
Funding Scheme	MSCA-IF-EF-ST
Starting year	2018
Duration (year-month-day)	from 2018-03-19 to 2020-03-18

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE Organization address address: SOUTH KENSINGTON CAMPUS EXHIBITION ROAD city: LONDON postcode: SW7 2AZ website: http://www.imperial.ac.uk/ contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (LONDON)	coordinator	183˙454.00

Map

Project objective

As noted by European turbine network, gas turbine is and will remain dominant mode of energy conversion. An advanced experimental study of a model gas turbine combustor is proposed. The lasers play indispensable role in the experimental combustion research due to the associated non-intrusive nature. The laser diagnostics have evolved from a point measurement to planar measurement (2D) over the years. The objective of the present work is to develop novel laser diagnostics to deduce instantaneous 3D fields of the flow, air/fuel mixing, and flame-front topology in a 'volume'. The proposed technique will be applied to a model gas turbine combustor operating with and without combustion instability. A scanning stereoscopic Particle Image Velocimetry (flow field) and Laser Induced Fluorescence of CH2O radical (flame-front) and of fuel concentration will be assembled correlated with pressure traces. A 4 head Nd:YAG laser cluster will generate 4 parallel laser sheets separated in space and images will be recorded by high speed cameras. The novel use of laser cluster ensures high pulse energy and temporal resolution. Image processing will be developed to reconstruct the 3D fields from the planar slices. The approach will be validated in a Bunsen burner before applying it to swirl stabilized flames that mimic a typical gas turbine combustor. The technology readiness level (TRL) of the research will reach between TRL 3 to 4. The proposed research will diversify the skill set of the researcher and associated complementary training will ensure that the fellow becomes an established academic researcher. The impact of this work is the generation of a unique 3D flame database, which is of great importance for the understanding of turbulent flame-flow interaction and the evaluation of advanced numerical combustion models. Thus, the proposed research will enhance European competitiveness in gas turbine design and can have an impact on automotive engine development.

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The information about "3DFLAMEGT" are provided by the European Opendata Portal: CORDIS opendata.