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3DFlameGT SIGNED

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

Total Cost €

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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.

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

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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