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3DFlameGT SIGNED

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

Total Cost €

0

EC-Contrib. €

0

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.

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

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 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.

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