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

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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