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Developing advanced Engine Multi-disciplinary Optimization Simulations (DEMOS)

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€410 450
EU Contribution
€410 450
Project website
Project Acronym
DEMOS
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Deployment planning/Financing/Market roll-out
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP01-2014-01
Link to CORDIS
Objectives

The “Innovative Aircraft Architecture” technology stream of the Clean Sky 2 Airframe ITD focuses on advanced power-plant solutions (such as CROR and UHBR) that are able to deliver a significant gain in aircraft performance.

Project DEMOS will develop advanced predictive modelling and simulation capabilities for engine design space exploration and performance optimization of such novel propulsion systems.

The overall and detailed objectives of Project DEMOS may be summed up as follows:

  • Assess, adapt and further develop a set of reliable and robust models to simulate/optimise performance of UHBR propulsion system architectures
  • Identify, build and integrate simulation models of specific (novel) components which may be considered as enablers of the technology
  • Demonstrate and assess the effect and influence of these components on the propulsion system performance in terms of overall performance, increase in mass, effect on lifing characteristics of the propulsion system and on the operating/ maintenance cost
  • Develop a modular approach to enable integration and further development of main modules/models for preliminary design process
  • Facilitate complex integration requirements
  • Improve process efficiency through the development of advanced solvers and adequate numerical methods to address complex system simulations
  • Development of advanced simulation techniques to improve the monitoring of communication between integrated models, robustness and convergence
  • Enable complex propulsion system performance optimisation with constraint handling capability
  • Develop a suite of advanced solvers to enable extended transient capabilities and simulation of complex systems transients and control

The project will build on the established multi-disciplinary concept design tools and further develop and adapt them in terms of applicability to advanced technologies and multi-objective concept analysis and selection.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.4.

Partners

Lead Organisation
Organisation
Empresarios Agrupados Internacional Sa
Address
Calle Magallanes 3, 28015 Madrid, Spain
EU Contribution
€110 000
Partner Organisations
Organisation
National Technical University Of Athens
Address
Heroon Polytechniou 9 (polytechnic campus), 15780 ZOGRAFOS, Greece
Organisation website
EU Contribution
€139 663
Organisation
Cranfield Aerospace Limited
Address
Cranfield University Campus Hangar 2, Cranfield, MK43 0AL, United Kingdom
Organisation website
EU Contribution
€160 788

Technologies

Technology Theme
Aircraft propulsion
Technology
Ultra-high bypass ratio jet engine
Development phase
Research/Invention

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