Overview Presentation
|
|
- Lorin Cross
- 6 years ago
- Views:
Transcription
1 Overview Presentation Ralf v.d.bank (1), Nicolas Savary (2), Mark Linne (3), Marco Zedda (4), James Mc Guirk (5), Giuseppe Cinque (6) 1 Rolls-Royce Deutschland, Dahlewitz, Germany 2 Turbomeca, Pau, France 3 Lunds Universitet, Sweden 4 Rolls-Royce, Derby, United Kingdom 5 Loughborough University, United Kingdom 6 AVIO, Pomigliano d Arco, Italy
2 Consortium University of of Loughborough Department Chemical Engineering Cambridge SNECMA Villaroche CNRS-LCD Poitiers ONERA Palaiseau Turbomeca Pau Imperial College London Rolls-Royce Derby CERFACS Toulouse DLR Köln AVIO Napoli Combustion Physics Universitet Lunds Università di di Firenze Rolls-Royce Deutschland Dahlewitz // Berlin University of of Czestochowa Universität Bundeswehr München Engler-Bunte Institut Universität Karlsruhe
3 Budget * Efforts Status YE Review Meeting - Budget 2,6 MEUR 34 % Person Months 334 PM 41 % 14% WP6 Total Budget: 7,7 MEUR 17% EC Funding: 5,0 MEUR Ratio: 64,6 % Audit Cert.s 1% WP7 3% 15% 21% 4% WP1 28% 817 Person Months 68 Person Years Duration: 4 years 1 January December % WP2 WP5 1% 15% 17% 2% WP4 WP3 21% 13%
4 Targets Improving the environmental impact with regards to emissions EC Target: - reduction of NOx emissions by 80% in the LTO cycle relative to CEAP2 - achieving an NOx emission index of 5 g NOx per / kg fuel burnt ACARE A Vision for 2020 : - reduction of 50% CO 2 emissions (engine contribution 15-20%) - reducing NOx emissions by 80% Strengthening of competitiveness of European aero-engine manufacturers - reduce short & long term development costs by 20 and 50%, respectively - incorporate new technology faster into future products - project timescales to less than 2 years
5 Trades SFC - CO 2 NOx Influencing Physical Factors P30/T30 SFC CO 2 BPR SFC CO 2 BPR Nacelle & Fan Drag P30 NOx T30 T40 NOx BPR AFR T40 NOx Source: M. Plohr, R.v.d.Bank, T.Schilling, DGLR , Munich, Germany Note: Fan and nacelle drag and weight variations were not considered. Higher P30/T30 and higher BPR improve cycle / propulsive efficiency Reduction of fuel burn (SFC) and green house gas emissions (CO 2 ) Aggravated situation with respect to low NOx target / challenge
6 Challenges Operability: Combustion Efficiency Cold Start, Ignition Altitude Relight Hail & Rain Slam Deceleration Weak Extinction Sprays: Spray Break-Up Spray Vaporisation Droplet Diameters Pre-Diffuser: Pressure Loss Air Feeding SFC Injectors: Air Blast / MultiPoint LPP LP(P) LDI SC Fuel System: Fuel Coking Schedule Staging Control Fuel Types Aromatics Combustor design is highly complex Combustion Noise: Thermo-Acoustic Instabilities Combustion Driven Pressure Oscillations Mechanical Integrity LP(P) / LDI 50 to 80 % W30 General: Weight Length Part Count Complexity Emissions NOx SOOT CO UHC Cooling: Life Prediction / Technology Surface to Volume Ratio
7 Technology Objectives Improvement of ultra-low NOx combustion systems - lean flame stability / weak extinction, flash-back & auto-ignition - low power conditions & transient engines operation Lean burn combustion - lower combustion temperature - reduced flame stability - may lead at very weak conditions - to severe increase of CO emissions and - unburnt hydro carbon emissions right before flame-out Deterioration when - slam deceleration during maneuvering in inclement weather con.s which leads to hail or rain (tropical storm) ingestion - with further reduced compressor outlet temperature and - reduced chemical reaction rates (moisture is almost inert)
8 WP3 WP3 Ignition LUND Capability Lunds Universitet Work Programme Combustion WP4 RRD WP4 Stability & Extinction Rolls-Royce Deutschland Low NOx III WP2 WP2 - TM Knowledge Based Lean Combustor Turbomeca WP6 Technology Assessment Rolls-Royce United Kingdom LOPOCOTEP WP6 External WP6 Aerodynamics Loughborough University Air Distribution WP7 Combustor WP7 Cooling AVIO AVIO Exploitation & Dissemination
9 Advanced low NOx technologies being investigated 1 AVIO: CLEAN 2 SNECMA: DEM21 3 TM: LPP 4 RRD: LDI Combustion Technology
10 Adapting the input data: - Increasing Pressure and Temperature - Variation of the liner cooling design p 3, T 3 V CC, Z-ring number Database Effusion cooled combustor Z-ring cooled combustor
11 Advanced ultra-low NOx technologies being investigated Future combustors will require most of the airflow to go through the cowl and fuel injector New design methodologies are being developed, based on optimisation and CFD Parametric geometry and automatic mesh generation are relied on to let the optimiser search the design space An integrated design approach (OGV + prediffuser) has proven to bring about significant performance benefits (lower pressure loss, higher recovery) Simulation results confirmed by testing Parametric design and rapid meshing system design parameters optimiser datum geometry optimised geometry constraints boundary conditions and cell connectivity tool element collapsing multugridalgorithm multigridalgorithm CFD solver RR UK & Loughborough Uni: External Aerodynamics Optimization
12 flame front development and fluctuations of fuel distribution Pressure cycle OH PLIF single shot images at 200 Hz and 91 0 oscillation phase angle Equivalence ratio distribution and fluctuation 200 Hz forced oscillation, full cycle
13 Advanced ultra-low NOx technologies being investigated 1 CERFACS - Cooling Technology
14 Effusion Cooling CFD - Standard RANS Standard model k-ε improvements Anisotropic model
15 Main Results by End of Project - first building bricks for KBE systems - coupling of preliminary design tools to speed-up design processes - rules for the design of piloting devices within low NOx injectors - assessment of ignition and lean stability modelling with LES codes - extending ignition and lean stability limits / low NOx injectors / int. fuel staging - implication of stability and ignition on combustor architecture and operation - quantification of low NOx and operability trade-off - optimized 3D pre-diffuser design methodology - demonstration of coupling of CFD analysis with heat transfer calculations - better understanding of effusion cooling to improve current cooling devices
16
17 Organisation Contract Consortium Agreement Project Support Team SNECMA (Industrial RR Partners) TM AVIO European Commission Project Coordination Co-ordinator (WP1 WP1 Leader) RRD Steering Committee (All Consortium Partners) Project Management Committee TM LUND (WP RRD Leaders) RR LOUGH AVIO WP2 Leader TM WP3 Leader LUND WP4 Leader RRD WP5 Leader RR WP6 LOUGH Leader WP7 Leader AVIO TM RRD SNECMA WP2M RR Team ONERA CERFACS UBWM AVIO Task LUND RRD IC WP3M UC Team Task RRD UCAM RR WP4M Team DLR ONERA UC IC AVIO Task RR RRD AVIO WP5M Team Task LOUGH SNECMA RR WP6M RRD Team TM Task AVIO SNECMA UFLOR WP7M CNRS Team CERFACS EBI TM Task
Integrated Lean Low Emission Combustor Design Methodology
Integrated Lean Low Emission Combustor Design Methodology Presenter: Ralf von der Bank (Rolls-Royce Deutschland) Consortium University of of Loughborough Department Chemical Engineering Cambridge SNECMA
More informationSIXTH FRAMEWORK PROGRAMME PRIORITY 4 AERONAUTICS AND SPACE SPECIFIC TARGETED RESEARCH PROJECT TLC
SIXTH FRAMEWORK PROGRAMME PRIORITY 4 AERONAUTICS AND SPACE SPECIFIC TARGETED RESEARCH PROJECT TLC Towards Lean Combustion Start : 1st March 2005 / Budget : 7,5 Meuros EC Scientific Officer : Daniel Chiron
More information1 Rolls-Royce Deutschland, Dahlewitz, Germany 2 Turbomeca, Pau, France 3 SNECMA, Villaroche, France 4 Rolls-Royce, Derby, United Kingdom
Ralf v.d.bank (1), Claude Berat (2), Michel Cazalens (3), Stephen Harding (4) 1 Rolls-Royce Deutschland, Dahlewitz, Germany 2 Turbomeca, Pau, France 3 SNECMA, Villaroche, France 4 Rolls-Royce, Derby, United
More informationLOw POllutant COmbustor TEchnology Project
Aeronautics Days 2006 Vienna/ Austria, 19 21 June 2006 LOw POllutant COmbustor TEchnology Project Project funded by the European Community under the Competitive and Sustainable Growth Programme (1998-2002)
More informationMSFI TECHNOLOGY AT SAFRAN AIRCRAFT
MSFI TECHNOLOGY AT SAFRAN AIRCRAFT ENGINES S. BOURGOIS 08/03/2017 Ce document et les informations qu il contient sont la propriété de Safran. Ils ne doivent pas être copiés ni communiqués à un tiers sans
More informationPresenter: Sébastien Bourgois (SN)
Multi point i injection i system development at Snecma Presenter: Sébastien Bourgois (SN) Outline Overview of Multipoint Injection System development at SNECMA Tools used for conception An example: LEMCOTEC
More informationProject Periodic Report. -Publishable Summary-
Project Periodic Report -Publishable Summary- Grant Agreement Number: ACP1-GA-2011-283216 Project acronym: LEMCOTEC Project title: Low Emissions Core Engine Technologies Funding Scheme: Collaborative Project
More informationDave Bone. DREAM Project Coordinator
Validation of radical engine architecture systems the alternative solution for a cleaner future Dave Bone Rolls-Royce plc Dave Bone Rolls-Royce plc DREAM Project Coordinator DREAM Project Coordinator This
More informationLean Burn Technology at Rolls-Royce
Lean Burn Technology at Rolls-Royce June 2014 FORUM AE Technology Workshop Kenneth Young Chief of R&T Combustion Sub-System 2014 Rolls-Royce plc The information in this document is the property of Rolls-Royce
More informationNEWAC Overall Specification, Assessment and Concept Optimization
NEWAC Overall Specification, Assessment and Concept Optimization Andrew Rolt, Rolls-Royce plc. with contributions from: Konstantinos Kyprianidis, Cranfield University; Stefan Donnerhack and Wolfgang Sturm,
More informationPERM injection system Development. PERM injection system Validation
PERM injection system Development AVIO, Antonio Peschiulli KIT, Nikos Zarzalis PERM injection system Validation ENGINSOFT, Lorenzo Bucchieri ONERA, Isabel Da Costa DGA, Vincent Plana Index 1. Introduction
More informationWhole Engine Integration
Sub Project 1 Whole Engine Integration Andrew Rolt, Rolls-Royce plc. European Engine Technology Workshop Warsaw, SP1 Whole Engine Integration Introduction and Objectives Development of the four advanced
More informationENGINE Demonstration Programmes in Clean Sky & Clean Sky 2
ENGINE Demonstration Programmes in Clean Sky & Clean Sky 2 Jean-François BROUCKAERT SAGE & ENGINES ITD Project Officer Aerodays 2015, London, 20-23 October 2015 Innovation Takes Off Outline 1. Open-Rotor
More informationInnovation Takes Off. Not legally binding
Innovation Takes Off Not legally binding Clean Sky 2 Information Day dedicated to the 1 st Call for Proposals (CFP01) Innovation Takes Off Engine ITD François Mirville, SAFRAN/Snecma Keith Nurney, Rolls-Royce
More informationEngine Industry Management Group EIMG. The European Aero-engine Community. Riga, 20 April 2005
EIMG The European Aero-engine Community Riga, 20 April 2005 EIMG : The European aero-engine community Rolls-Royce UK Volvo Aero Alstom Techspace Aero Snecma Moteurs Turbomeca ITP Rolls-Royce D PBS MTU
More informationEnvironmentally friendly aero-engines for the 21st century Dr. Norbert Arndt, Managing Director Engineering Rolls-Royce Deutschland
Environmentally friendly aero-engines for the 21st century Dr. Norbert Arndt, Managing Director Engineering Rolls-Royce Deutschland CEAS Berlin, 12 th September 2007 Content ACARE goals & physical boundaries
More informationNew Aero Engine Core Concepts
The integrated Project New Aero Engine Core Concepts NEWAC Goals Project Structure New Core Concepts Technology Roadmap ACARE Goals Implications to Aero Engine The ACARE Goals 2020 Half current perceived
More informationPublishable Executive Summary
Publishable Executive Summary CONTRACT N o : AST3-CT-2003-502961 PROJECT N o : 502961 ACRONYM: TITLE: INTELLECT D.M. Integrated Lean Low Emission Combustor Design Methodology PROJECT CO-ORDINATOR: Rolls-Royce
More informationLOW EMISSIONS COMBUSTOR TECHNOLOGY DEVELOPMENTS IN THE EUROPEAN PROGRAMMES LOPOCOTEP AND TLC
25 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES LOW EMISSIONS COMBUSTOR TECHNOLOGY DEVELOPMENTS IN THE EUROPEAN PROGRAMMES LOPOCOTEP AND TLC Olivier PENANHOAT* *SNECMA Keywords: Lean Combustion,
More informationEmissions Mitigation Concepts
COORDINATION ACTION FP7 European coordination action ; GA 605506 ; 2013-2017 Emissions Mitigation Concepts Paul Madden, Denise Ahrens (RR) Olivier Penanhoat, Yoann Mery, Nicolas Tantot (Safran-AE) ECATS
More informationExperimental Verification of Low Emission Combustor Technology at DLR
www.dlr.de Chart 1 > FORUM-AE Non-CO2 mitigation technology Workshop> Hassa > 2.7.2014 Experimental Verification of Low Emission Combustor Technology at DLR Christoph Hassa Institute of Propulsion Technology
More informationXavier Vancassel (Onera) Introduction. FORUM-AE workshop - Sustainable Aviation Fuel Forum Madrid 21 st October 2014
Olivier Penanhoat (Snecma) Xavier Vancassel (Onera) Introduction workshop - Sustainable Aviation Fuel Forum Madrid 21 st October 2014 MAIN OBJECTIVES FORUM on Aviation and Emissions (& Environment) EU
More informationInnovation Takes Off. Not legally binding
Innovation Takes Off Not legally binding Clean Sky 2 Information Day Engines ITD Simon Weeks: Rolls-Royce Marius Goutines: SNECMA Jean Roch Cossa: SAFRAN Gerhard Ebenhoch: MTU Aero Engines Bonn, 20 th
More informationTP400-D6 Turboprop A European Collaboration Programme
TP400-D6 Turboprop A European Collaboration Programme Royal Aeronautical Society Lecture, 19 September 2006 Hamburg Content l Why a Turboprop? l The Engine Team l TP400-D6 Overview l TP400-D6 Validation
More informationDave Bone. DREAM Project Coordinator
Validation of radical engine architecture systems Andrew Bradley Rolls-Royce plc Dave Bone Rolls-Royce plc DREAM Project Chief Engineer DREAM Project Coordinator the alternative solution for a cleaner
More informationFuel Cell Application in a New Configured Aircraft PUBLISHABLE REPORT
Fuel Cell Application in a New Configured Aircraft PUBLISHABLE REPORT Document Reference CELINA Publishable Report Contract Nr. AST4-CT-2005-516126 Version/Date Version 1.3 January 2009 Issued by Airbus
More informationTECC-AE, Task 2.1 Spray ignition limitations and sub grid model for CFD for lean extinction and spark ignition
TECC-AE, Task 2.1 Spray ignition limitations and sub grid model for CFD for lean extinction and spark ignition Speaker s name & organisation: Prof. E. Mastorakos, University of Cambridge Speaker s role
More informationCorso di Motori Aeronautici
Corso di Motori Aeronautici Mauro Valorani Laurea Magistrale in Ingegneria Aeronautica (MAER) Sapienza, Università di Roma Anno Accademico 2011-12 Sett. 13: Conclusioni 1 FP7 Aero Engine Scenario ERS Strategy
More informationFlow Controlled Core Overview
Flow Controlled Core Overview Hanna Reiss, Snecma Safran Group Introduction High BPR and/or new architectures will require highly loaded, efficient and operable HPC (+20/25% vs. in-service compressor)
More informationOverview. Dr. Joerg Sieber, MTU Aero Engines
Overview Dr. Joerg Sieber, MTU Aero Engines Contents Future Requirements and EU Technology Projects Technical Approach NEWAC Program Subprograms Whole Engine Integration Intercooled Recuperated Core Intercooled
More informationAdaptive and Passive Flow Control for Fan Broadband Noise Reduction Selected final results
Adaptive and Passive Flow Control for Fan Broadband Noise Reduction Selected final results Lars Enghardt, DLR Berlin FLOCON project coordinator September 2008 August 2012 Introduction Motivation Air traffic
More informationFUEL BURN REDUCTION. Fuel consumption improvement 20 % 5 % 20 to 30% 1 Direction Technique YD 20 juin first generation
Environmental Constraints and Future Engine Architectures 0 Direction Technique YD 20 juin 2008 Jacques Renvier Senior VP System Engineering FUEL BURN REDUCTION B737-200 / JT8D first generation 20 % offers
More informationCFD Simulation of Dry Low Nox Turbogas Combustion System
CFD Simulation of Dry Low Nox Turbogas Combustion System L. Bucchieri - Engin Soft F. Turrini - Fiat Avio CFX Users Conference - Friedrichshafen June 1999 1 Objectives Develop a CFD model for turbogas
More informationCFM Technology. realizing the promise 50% LOWER NOX EMISSIONS. ANOTHER LEAP FORWARD FOR LEAP TECHNOLOGY.
50% LOWER NOX EMISSIONS. CFM Technology realizing the promise ANOTHER LEAP FORWARD FOR LEAP TECHNOLOGY. Bill Brown General Manger CFM Marketing June 2010 CFM International Proprietary Information The information
More informationIgnition of gas turbines. MUSAF-II, 19 September 2013
Ignition of gas turbines MUSAF-II, 19 September 2013 Epaminondas Mastorakos em257@eng.cam.ac.uk Department of Engineering 1 Acknowledgements Drs. S. Ahmed, C. Letty, A. Neophytou, A. Tyliszczak, J. Kariuki,
More informationDevelopments in Modern Aero-Engines to minimize the Impact of Bleed Air
Developments in Modern Aero-Engines to minimize the Impact of Bleed Air Dr. Dieter Peitsch Rolls-Royce Deutschland Ltd. & Co. KG Dahlewitz, Germany Contact: dieter.peitsch@rolls-royce.com Outline Why is
More informationAviation Alternative Fuels Towards sustainable air travel
June 3rd, 2009 Presented by Philippe FONTA Head of Sustainable Development Airbus Vice-chairman of the Aircraft Noise and Engine Emissions Committee - ICCAIA Aviation Alternative Fuels Towards sustainable
More informationNEMESIS 2 + (278138)
NEMESIS 2 + (278138) Programme Review Days 2012 Brussels, 28 & 29 November 2012 Stefan Martin German Aerospace Center/ Institute of Technical Thermodynamics 0. Project & Partnership description General
More informationObjectives. WP1: Systems for increased fuel flexibility
WP1: Systems for increased fuel flexibility Objectives To develop engines able to switch between fuels, whilst operating in the most cost effective way and complying with the regulations in all sailing
More informationROSAS Final Meeting ROSAS. Eric MAURY AIRBUS Engineering Future Projects. Main Achievements. 3rd March Presented by
ROSAS 3rd March 2005 Presented by Eric MAURY AIRBUS Engineering Future Projects ROSAS Final Meeting Main Achievements ROSAS Final Meeting: Overview of achievements WP1 Definition of Silent Aircraft concepts
More informationCrankcase scavenging.
Software for engine simulation and optimization www.diesel-rk.bmstu.ru The full cycle thermodynamic engine simulation software DIESEL-RK is designed for simulating and optimizing working processes of two-
More informationGas exchange and fuel-air mixing simulations in a turbocharged gasoline engine with high compression ratio and VVA system
Third Two-Day Meeting on Internal Combustion Engine Simulations Using the OpenFOAM technology, Milan 22 nd -23 rd February 2018. Gas exchange and fuel-air mixing simulations in a turbocharged gasoline
More informationDual-fuel combustion for the introduction of renewable alcohol fuels in heavy-duty diesel engines
KTH ROYAL INSTITUTE OF TECHNOLOGY Dual-fuel combustion for the introduction of renewable alcohol fuels in heavy-duty diesel engines Nicola Giramondi Prof. Anders Christiansen Erlandsson (KTH) Dr. Anders
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. EASA E.047 for RB211 Trent 800 series engines Type Certificate Holder 62 Buckingham Gate Westminster London SW1E 6AT United Kingdom For Models: RB211 Trent 895-17 RB211
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET EASA.E.060 for RB211 Trent 500 Series Engines Type Certificate Holder 62 Buckingham Gate Westminster London SW1E 6AT United Kingdom For Models: RB211 Trent 553-61 RB211 Trent
More informationASSESSMENT OF NEW AEROENGINE CORE CONCEPTS AND TECHNOLOGIES IN THE EU FRAMEWORK 6 NEWAC PROGRAMME
27 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES ASSESSMENT OF NEW AEROENGINE CORE CONCEPTS AND TECHNOLOGIES IN THE EU FRAMEWORK 6 NEWAC PROGRAMME Andrew M Rolt* and Konstantinos G Kyprianidis**
More informationThe HERCULES ( ) R&D program on 'green' engines for ships
Nikolaos Kyrtatos Page 1 HERCULES Programme The HERCULES (2004-2018) R&D program on 'green' engines for ships Prof. Nikolaos P. Kyrtatos, HERCULES Coordinator Presentation to CIMAC Circle at Norshipping
More informationTechnologies to Reduce GT Emissions
GE Power Systems Technologies to Reduce GT Emissions Rich Rapagnani Global Marketing & Development March 18, 2003 GE Power Systems Technologies to Reduce GT Emissions Dry Low NOx Combustion Systems Advanced
More informationPEM Fuel Cells Manufacturing - Stack
11 th October 2018 PEM Fuel Cells Manufacturing - Stack Richard Peart Head of Manufacturing Development 1 About Intelligent Energy A fuel cell engineering company focused on the development and commercialisation
More informationUltra Low NOx Gas Turbine Combustion Monday 16 - Friday 20 January 2017
Ultra Low NOx Gas Turbine Combustion Monday 16 - Friday 20 January 2017 Programme Monday 16 January 2017 Fundamentals of NOx Formation 08:00 Registration and coffee 08:30 Introduction & GT cycles for low
More informationTechnological Achievements
Open Rotor Technological Achievements François MIRVILLE SAFRAN/Snecma July 1, 2014 1/ SUMMARY Open Rotor Architectures and Aircraft Integration Main Technical Objectives Technologies involved Technology
More informationCORE. Chris Such, Ricardo
CORE CO 2 REduction for long distance transport Chris Such, Ricardo On behalf of CORE Project Coordinator Johan Engstrom, Volvo CORE Vision CO2RE focus is on highly efficient drivelines for long distance
More informationNumerical Investigation of the Influence of different Valve Seat Geometries on the In-Cylinder Flow and Combustion in Spark Ignition Engines
Institute for Combustion and Gas Dynamics Fluid Dynamics Numerical Investigation of the Influence of different Valve Seat Geometries on the In-Cylinder Flow and Combustion in Spark Ignition Engines Peter
More informationRéduction des impacts liés à l utilisation du carburant aéronautique
Réduction des impacts liés à l utilisation du carburant aéronautique Francis Couillard, Directeur des affaires environnementales de Snecma 1 Engine fuel consumption reduction Fuel burn Index 100% 90% 80%
More informationGeneration of an Advanced Helicopter Experimental Aerodynamic Database for CFD Code Validation (GOAHEAD)
Generation of an Advanced Helicopter Experimental Aerodynamic Database for CFD Code Validation (GOAHEAD) T. Schwarz, K. Pahlke DLR Braunschweig, Germany Folie 1 Outline Motivation The GOAHEAD project Wind
More information<PUBLISHABLE SUMMARY M1-M12>
Ver: 1 Date: 30/11/2007 Page 1 of 15 Project n 031236 RC2 Instrument: STREP SPECIFIC TARGETED RESEARCH OR INNOVATION PROJECT Thematic Priority: SUSTAINABLE DEVELOPMENT, GLOBAL CHANGE AND ECOSYSTEMS
More informationPaper No: 05-IAGT-1.1 INDUSTRIAL APPLICATION OF GAS TURBINES COMMITTEE
Paper No: 05-IAGT-1.1 INDUSTRIAL APPLICATION OF GAS TURBINES COMMITTEE Mercury 50 Field Evaluation and Product Introduction by David Teraji of Solar Turbines Incorporated San Diego, California, USA 1 AUTHORS
More informationMID TERM REPORT CONTRACT N : G4RD-CT PROJECT N : GRD ACRONYM: MUSCLES
` MID TERM REPORT CONTRACT N : G4RD-CT-2002-00644 PROJECT N : GRD1-2001-40198 ACRONYM: MUSCLES TITLE: Modelling of UnSteady Combustion in Low Emission Systems PROJECT CO-ORDINATOR: H. T. Brocklehurst,
More informationNew Integrated Combustion Engines for future Passenger Car Engines (NICE)
New Integrated Combustion Engines for future Passenger Car Engines (NICE) Background EUCAR SG P group, after consulting RTRAC,had submitted an Expression of interest on CCS for EC FWP6 programme in July
More informationIndia-EU and Member States Partnership for a Strategic Roadmap in Research and Innovation
India-EU and Member States Partnership for a Strategic Roadmap in Research and Innovation 1. Session D2 : Multilateral EU-India research and innovation initiatives R&D Teams from Europe visiting CSIR-NAL
More information1. FINAL EXECUTIVE SUMMARY
1. FINAL EXECUTIVE SUMMARY 1.1 Summary of Project Objectives The present project aims at the selection, test and assessment of a novel, fully integrated active aftertreatment system, aimed to allow compliance
More informationInternal Combustion Engines ERTRAC Workshop, 2 June Project title: CORE. Coordinator Johan Engström, Volvo. Status May 2015
Internal Combustion Engines ERTRAC Workshop, 2 June 2015 Project title: CORE CO 2 REduction for long distance transport Coordinator Johan Engström, Volvo Status May 2015 Project general information CORE
More informationThe company supplies some of the world s most advanced engine testing systems ranging from combustion analysis to fully automated test benches.
FEV is an internationally recognized leader in the design and development of internal combustion engines and supplier of advanced test and instrumentation systems. Founded in 1978, the company today employs
More informationOverview of the relationship between fuel properties and engine performance
Overview of the relationship between fuel properties and engine performance Nader Rizk Rolls-Royce Indianapolis, IN ICAO Workshop, Aviation & Alternative Fuels Montreal, Canada 10-12 February 2009 2009
More informationDual Fuel Engine Charge Motion & Combustion Study
Dual Fuel Engine Charge Motion & Combustion Study STAR-Global-Conference March 06-08, 2017 Berlin Kamlesh Ghael, Prof. Dr. Sebastian Kaiser (IVG-RF), M. Sc. Felix Rosenthal (IFKM-KIT) Introduction: Operation
More informationATELIER: SIMULATION NUMÉRIQUE POUR LES GROUPES MOTOPROPULSEURS 2 FÉVRIER 2017 SAINT-ETIENNE-DU-ROUVRAY
ATELIER: SIMULATION NUMÉRIQUE POUR LES GROUPES MOTOPROPULSEURS 2 FÉVRIER 2017 SAINT-ETIENNE-DU-ROUVRAY 1 ENGINE AND VEHICLE MODELING & SIMULATION SCIENTIFIC AND TECHNICAL CHALLENGES 2 CONTEXT Main drivers
More informationProject introduction. Document prepared by: Element Energy. A project co-funded by under the Grant Agreement n and n.
Project introduction Document prepared by: Element Energy A project co-funded by under the Grant Agreement n.671438 and n. 700350 H2ME initiative (2015 2022) Project overview HRS: Hydrogen Refuelling Station
More informationPh. NOVELLI, coordinator. ICAO Montréal, 18 October 2011
SWAFEA European Study for Alternative fuels in Aviation Main outcomes Ph. NOVELLI, coordinator ICAO Montréal, 18 October 2011 Sustainable Way for Alternative Fuel and Energy in Aviation A study funded
More informationClean Sky SAGE ITD. NEWAC Workshop Warsaw 3 June 2009 Mark Pacey
Clean Sky SAGE ITD NEWAC Workshop Warsaw 3 June 2009 Mark Pacey Clean Sky Introduction Largest ever EU aeronautics programme 1.6bn over 7 years Public-Private Partnership between the Community (represented
More informationLEAP-X Program Update
LEAP-X Program Update 29 Oct 09 NYC CFM International Proprietary Information The information in this document is CFM Proprietary Information and is disclosed in confidence. It is the property of CFM International
More informationClean Sky Programme. JTI Workshop, Vienna 3 rd of February, Helmut Schwarze, Project Officer CSJU Andrzej Podsadowski, Project Officer CSJU
Clean Sky Programme Helmut Schwarze, Project Officer CSJU Andrzej Podsadowski, Project Officer CSJU JTI Workshop, Vienna 3 rd of February, 2011 1 1 Clean Sky Programme Overview 2 2 Clean Sky Integrated
More informationComponent and System Level Modeling of a Two-Phase Cryogenic Propulsion System for Aerospace Applications
Component and System Level Modeling of a Two-Phase Cryogenic Propulsion System for Aerospace Applications J. LoRusso, B. Kalina, M. Van Benschoten, Roush Industries GT Users Conference November 9, 2015
More informationSimulating Gas-Air Mixture Formation for Dual-Fuel Applications
Simulating Gas-Air Mixture Formation for Dual-Fuel Applications Karri Keskinen, Ossi Kaario, Mika Nuutinen, Ville Vuorinen, Zaira Künsch and Martti Larmi Thermodynamics and Combustion Technology Research
More informationUsage Issues and Fischer-Tropsch Commercialization
Usage Issues and Fischer-Tropsch Commercialization Presentation at the CCTR Advisory Panel Meeting Terre Haute, Indiana June 1, 2006 Diesel Engine Research John Abraham (ME), Jim Caruthers (CHE) Gas Turbine
More informationHERCULES-2 Project. Deliverable: D8.8
HERCULES-2 Project Fuel Flexible, Near Zero Emissions, Adaptive Performance Marine Engine Deliverable: D8.8 Study an alternative urea decomposition and mixer / SCR configuration and / or study in extended
More informationNew Environmental Friendly Aero Engine Core Concepts
New Environmental Friendly Aero Engine Core Concepts Günter Wilfert, Joerg Sieber (MTU Aero Engines) Andrew Rolt, Nick Baker (Rolls-Royce) Armel Touyeras (Snecma), Salvatore Colantuoni (AVIO) Abstract
More informationAIRCRAFT AND TECHNOLOGY CONCEPTS FOR AN N+3 SUBSONIC TRANSPORT. Elena de la Rosa Blanco May 27, 2010
AIRCRAFT AND TECHNOLOGY CONCEPTS FOR AN N+3 SUBSONIC TRANSPORT MIT, Aurora Flights Science, and Pratt & Whitney Elena de la Rosa Blanco May 27, 2010 1 The information in this document should not be disclosed
More informationUne nouvelle génération de Moteurs Le LEAP Aviation et Environnement Pau 7 Février 2013
Une nouvelle génération de Moteurs Le LEAP Aviation et Environnement Pau 7 Février 2013 CFM, CFM56, LEAP and the CFM logo are trademarks of CFM International, a 5050 joint company between Snecma (Safran
More informationAutomatic CFD optimisation of biomass combustion plants. Ali Shiehnejadhesar
Automatic CFD optimisation of biomass combustion plants Ali Shiehnejadhesar IEA Bioenergy Task 32 workshop Thursday 6 th June 2013 Contents Scope of work Methodology CFD model for biomass grate furnaces
More informationTAKE OFF Informationsveranstaltung zu Ausschreibungen nationaler und europäischer Luftfahrtforschungsprogramme Clean Sky
TAKE OFF Informationsveranstaltung zu Ausschreibungen nationaler und europäischer Luftfahrtforschungsprogramme Clean Sky Eric Dautriat, Executive Director June 1st, 2010, Vienna Greenhouse effect Environment
More informationPOSIBILITIES TO IMPROVED HOMOGENEOUS CHARGE IN INTERNAL COMBUSTION ENGINES, USING C.F.D. PROGRAM
POSIBILITIES TO IMPROVED HOMOGENEOUS CHARGE IN INTERNAL COMBUSTION ENGINES, USING C.F.D. PROGRAM Alexandru-Bogdan Muntean *, Anghel,Chiru, Ruxandra-Cristina (Dica) Stanescu, Cristian Soimaru Transilvania
More informationROSANNE Results after 2 years of project duration Roland Spielhofer, AIT BUDAPEST, HUNGARY 2015
ROSANNE Results after 2 years of project duration Roland Spielhofer, AIT BUDAPEST, HUNGARY 2015 ROSANNE project Project overview What has been achieved so far? ROSANNE project FP7 Small Collaborative Research
More informationEFFECT OF INJECTION ORIENTATION ON EXHAUST EMISSIONS IN A DI DIESEL ENGINE: THROUGH CFD SIMULATION
EFFECT OF INJECTION ORIENTATION ON EXHAUST EMISSIONS IN A DI DIESEL ENGINE: THROUGH CFD SIMULATION *P. Manoj Kumar 1, V. Pandurangadu 2, V.V. Pratibha Bharathi 3 and V.V. Naga Deepthi 4 1 Department of
More informationSmartBatt Smart and Safe Integration of Batteries in Electric Vehicles. An EU funded project
SmartBatt Smart and Safe Integration of Batteries in Electric Vehicles An EU funded project SmartBatt EU funded under 7 th Framework Programme Objectives: - Development of an electric vehicle battery focusing
More informationEngine Technology Development to Address Local Air Quality Concerns
Engine Technology Development to Address Local Air Quality Concerns John Moran Corporate Specialist Combustion Rolls-Royce Associate Fellow - Combustion Overview This presentation summarizes material presented
More informationMORSE: MOdel-based Real-time Systems Engineering. Reducing physical testing in the calibration of diagnostic and driveabilty features
MORSE: MOdel-based Real-time Systems Engineering Reducing physical testing in the calibration of diagnostic and driveabilty features Mike Dempsey Claytex Future Powertrain Conference 2017 MORSE project
More informationTOWARD ACARE 2020: INNOVATIVE ENGINE ARCHITECTURES TO ACHIEVE THE ENVIRONMENTAL GOALS?
27 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES TOWARD ACARE 2020: INNOVATIVE ENGINE ARCHITECTURES TO ACHIEVE THE ENVIRONMENTAL GOALS? Lamine M BENGUE Snecma SAFRAN Group Keywords: Environment,
More informationThe European Tilt Rotor-Status of ERICA Design and Test Activities. Madrid, 31 March 2011
The European Tilt Rotor-Status of ERICA Design and Test Activities Alessandro Stabellini NICETRIP Project Manager TILTROTOR RESEARCH IN EUROPE Handling Qualities requirements background Flight Control
More informationCo-ordinated Action A E R O N E T. Aircraft Emissions and Reduction Technologies.
Co-ordinated Action A E R O N E T Aircraft Emissions and Reduction Technologies http://www.aero-net.org Currently funded by the European Community DG Research, Aeronautics under Contract No. ACA3-CT-2003-502882
More informationin ultra-low NOx lean combustion grid plate
CFD predictions of aerodynamics and mixing in ultra-low NOx lean combustion grid plate flame stabilizer JOSÉ RAMÓN QUIÑONEZ ARCE, DR. ALAN BURNS, PROF. GORDON E. ANDREW S. SCHOOL OF CHEMICAL AND PROCESS
More informationCombining Optimisation with Dymola to Calibrate a 2-zone Predictive Combustion Model.
Combining Optimisation with Dymola to Calibrate a 2-zone Predictive Combustion Model. Mike Dempsey Optimised Engineering Design Conference 2016 Claytex Services Limited Software, Consultancy, Training
More informationEuropean Workshop on New Aero Engine Concepts Munich, 30 June 1 July 2010
08 June 2010 1 Pulse Detonation Core Engine (from WP 2.3: Future Innovative Core Configuration A. Lundblahd, VOLVO Aero WP2.3.3: Innovative combustion F Giuliani, TU Graz) F. Giuliani, A. Lang, Graz University
More informationOPTIMATE. Platform overview. Adrien Atayi RTE. 2015/05/22 - Brussels. Co-funded by the Intelligent Energy Europe Programme of the European Union
OPTIMATE Platform overview Adrien Atayi RTE 2015/05/22 - Brussels Co-funded by the Intelligent Energy Europe Programme of the European Union Agenda Context OPTIMATE Platform Focus on reference equilibrium
More informationFoundations of Thermodynamics and Chemistry. 1 Introduction Preface Model-Building Simulation... 5 References...
Contents Part I Foundations of Thermodynamics and Chemistry 1 Introduction... 3 1.1 Preface.... 3 1.2 Model-Building... 3 1.3 Simulation... 5 References..... 8 2 Reciprocating Engines... 9 2.1 Energy Conversion...
More informationPlasma Assisted Combustion in Complex Flow Environments
High Fidelity Modeling and Simulation of Plasma Assisted Combustion in Complex Flow Environments Vigor Yang Daniel Guggenheim School of Aerospace Engineering Georgia Institute of Technology Atlanta, Georgia
More informationEngine encapsulation. A synergic approach to exterior noise and CO 2 emissions reduction. Brussels, 18th December 2012 Maurizio Mantovani - Autoneum
Engine encapsulation A synergic approach to exterior noise and CO 2 emissions reduction Brussels, 18th December 2012 Maurizio Mantovani - Autoneum Agenda 1. Who is Autoneum 2. Benefits of encapsulation
More informationVehicle Aerodynamics Subscription Development of Numerical Simulation Method of Flow Around Automobile Using Meshfree Method
Vehicle Aerodynamics Subscription 2005-01-0544 Development of Numerical Simulation Method of Flow Around Automobile Using Meshfree Method 2005-01-0545 A Downforce Optimization Study for a Racing Car Shape
More informationDecarbonising long range heavy-duty road transport
Decarbonising long range heavy-duty road transport A research and demostration funding perspective HyER/Great event 31/1/2018 Maurizio Maggiore DG RTD H2 Some EGCI statistics (1) 115 project running or
More informationDr. Chris Dudfield. Chief Technology Officer Intelligent Energy. Sponsors
Dr. Chris Dudfield Chief Technology Officer Intelligent Energy Sponsors 7 th September 2017 Creating the blueprint for advanced fuel cell manufacturing Dr Chris Dudfield Chief Technology Officer 2 The
More informationH2020 (ART ) CARTRE SCOUT
H2020 (ART-06-2016) CARTRE SCOUT Objective Advance deployment of connected and automated driving across Europe October 2016 September 2018 Coordination & Support Action 2 EU-funded Projects 36 consortium
More information