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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

0

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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.

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

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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