
TURBOMECA
TURBOMECA
5 Projects, page 1 of 1
assignment_turned_in ProjectFrom 2007Partners:UNIVERSITE DE PARIS XI [PARIS- SUD], TURBOMECA, OFFICE NATIONAL DETUDES ET DE RECHERCHES AEROSPATIALES [ONERA] CENTRE DETUDES ET DE RECHERCHES DE TOULOUSE, ASTRIUM SAS, Commissariat à l'Energie atomique et aux Energies Alternatives +6 partnersUNIVERSITE DE PARIS XI [PARIS- SUD],TURBOMECA,OFFICE NATIONAL DETUDES ET DE RECHERCHES AEROSPATIALES [ONERA] CENTRE DETUDES ET DE RECHERCHES DE TOULOUSE,ASTRIUM SAS,Commissariat à l'Energie atomique et aux Energies Alternatives,OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES (ONERA) Centre de TOULOUSE,Grenoble INP - UGA,AIRBUS OPERATIONS,ESTEREL,SAGEM DEFENSE SECURITE,UNIVERSITE GRENOBLE I [Joseph Fourier]Funder: French National Research Agency (ANR) Project Code: ANR-07-TLOG-0019Funder Contribution: 1,135,500 EURmore_vert assignment_turned_in ProjectFrom 2008Partners:SOCIETE CIVILE CERFACS CENTRE EUROPEEN DE RECHERCHE ET DEFORMATION AVANCEE EN CALCUL SCIENTIFIQUE, TURBOMECA, INSTITUT NATIONAL DES SCIENCES APPLIQUEES DE ROUEN, SNECMA, CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE - DELEGATION REGIONALE ILE-DE-FRANCE SECTEUR OUEST ET NORDSOCIETE CIVILE CERFACS CENTRE EUROPEEN DE RECHERCHE ET DEFORMATION AVANCEE EN CALCUL SCIENTIFIQUE,TURBOMECA,INSTITUT NATIONAL DES SCIENCES APPLIQUEES DE ROUEN,SNECMA,CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE - DELEGATION REGIONALE ILE-DE-FRANCE SECTEUR OUEST ET NORDFunder: French National Research Agency (ANR) Project Code: ANR-07-CIS7-0008Funder Contribution: 521,055 EURmore_vert assignment_turned_in ProjectFrom 2007Partners:ARMINES, SNECMA, CEA, ONERA (O.N.E.R.A.) CENTRE CHATILLON, AUBERT&DUVAL +3 partnersARMINES,SNECMA,CEA,ONERA (O.N.E.R.A.) CENTRE CHATILLON,AUBERT&DUVAL,CNRS - DR CENTRE POITOU-CHARENTES,TURBOMECA,ONERA - CENTRE CHATILLONFunder: French National Research Agency (ANR) Project Code: ANR-06-MAPR-0015Funder Contribution: 1,121,090 EURmore_vert assignment_turned_in ProjectFrom 2009Partners:EDF RECHERCHE ET DEVELOPPEMENT - SITE CHATOU, Institut National des Sciences Appliquées de Lyon - Laboratoire dIngénierie des Matériaux Polymères, ECOLE CENTRALE DE NANTES, TURBOMECA, EDF RECHERCHE & DEVELOPPEMENTEDF RECHERCHE ET DEVELOPPEMENT - SITE CHATOU,Institut National des Sciences Appliquées de Lyon - Laboratoire dIngénierie des Matériaux Polymères,ECOLE CENTRALE DE NANTES,TURBOMECA,EDF RECHERCHE & DEVELOPPEMENTFunder: French National Research Agency (ANR) Project Code: ANR-09-COSI-0008Funder Contribution: 727,875 EURmore_vert assignment_turned_in ProjectFrom 2014Partners:Centre national de la recherche scientifique Institut de Combustion Aérothermique Réactivité et Environnement, TURBOMECA, Laboratoire Pluridisciplinaire de Recherche en Ingénierie des Systèmes, Mécanique, Energétique de lUniversité dOrléans, Institut de Mécanique des Fluides de Toulouse, Laboratoire Pluridisciplinaire de Recherche en Ingénierie, Systèmes Mécanique et EnergieCentre national de la recherche scientifique Institut de Combustion Aérothermique Réactivité et Environnement,TURBOMECA,Laboratoire Pluridisciplinaire de Recherche en Ingénierie des Systèmes, Mécanique, Energétique de lUniversité dOrléans,Institut de Mécanique des Fluides de Toulouse,Laboratoire Pluridisciplinaire de Recherche en Ingénierie, Systèmes Mécanique et EnergieFunder: French National Research Agency (ANR) Project Code: ANR-13-ASTR-0013Funder Contribution: 288,600 EURWith the forthcoming depletion of fossil fuels, engine manufacturers and research institutes from aeronautics are working to find alternative solutions. To face this problem, the initial step consists of improving the combustion process in aeronautic chamber as well as developing new chamber designs for civil and military aircrafts. This work needs the use of computer codes able to simulate all the processes involved. The models need to be as predictive as possible. Another possibility is the use of non-fossil fuels. There are two families for these aeronautic alternative fuels: synthetic fuels and renewable fuels or biofuels. Despite the various physical and chemical properties of these different fuels, their use must be transparent for the user of the aeronautic engine in terms of performances, pollutant emissions and reliability. To face the diversity of the potential fuels, a tremendous effort is required to be sure these alternative fuels match the kinetics and the flame dynamics of the reference fuels. IDYLLE project aims at achieving a better understanding for a better modeling of the kinetic and the flame dynamic of aeronautic alternative fuels. Joint experimental and numerical approaches will be performed. This objective of this project is double: develop a reduced kinetic scheme for a synthetic aeronautic fuel and provide an improved turbulent combustion model. These two deliverables will allow a better simulation of the heat release as well as the stability and extinction limits. These improvements will also allow the design of new combustion chambers.
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