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TRIMIS

Ultra Low emission Technology Innovations for Mid-century Aircraft Turbine Engines

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€3 138 122
EU Contribution
€3 138 122
Project Acronym
ULTIMATE
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Environmental/Emissions aspects,
Decarbonisation
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-MG-2014_TwoStages
Link to CORDIS
Objectives

With the ULTIMATE project five experienced research groups and four major European engine manufacturers will develop innovative propulsion systems to fulfil the SRIA 2050 key challenges. One of the most challenging targets is the 75% reduction in energy consumption and CO2-emissions. Technologies currently at TRL 3-5, cannot achieve this aim. It is estimated that around a 30% reduction must come from radical innovations now being at lower TRL. Thus, European industry needs synergetic breakthrough technologies for every part of the air transport system, including the airframe, propulsion and power.

 

The ULTIMATE project singles out the major loss sources in a state of the art turbofan (combustor irreversibility, core exhaust heat, bypass exhaust kinetic energy). These are then used to categorize breakthrough technologies (e.g. piston topping, intercooling & exhaust heat exchangers, and advanced propulsor & integration concepts). This classification approach gives a structured way to combine and explore synergies between the technologies in the search for ultralow CO2, NOx and noise emissions. The most promising combinations of radical technologies will then be developed for a short range European and a long range intercontinental advanced tube and wing aircraft.

 

Through the EU projects VITAL, NEWAC, DREAM, LEMCOTEC, E-BREAK and ENOVAL, the ULTIMATE partners have gained the most comprehensive experience in Europe on conception and evaluation of advanced aero engine architectures. Existing tools, knowledge and models will be used to perform optimization and evaluation against the SRIA targets to mature the technologies to TRL 2. Road maps will be set up to outline the steps to develop the technologies into products and bring them onto the market. These road maps will also provide a way forward for future European propulsion and aviation research.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.

Partners

Lead Organisation
Organisation
Chalmers Tekniska Hoegskola Ab
Address
41296 GOTHENBURG, Sweden
Organisation website
EU Contribution
€650 000
Partner Organisations
Organisation
Safran Aircraft Engines
Address
2 Bvd Du General Martial-Valin, 75724 Paris, France
EU Contribution
€99 844
Organisation
Aristotelio Panepistimio Thessalonikis
Address
KEDEA BUILDING, TRITIS SEPTEMVRIOU, ARISTOTLE UNIV CAMPUS, 54636 THESSALONIKI, Greece
Organisation website
EU Contribution
€380 000
Organisation
Institut Superieur De L'aeronautique Et De L'espace
Address
AVENUE EDOUARD BELIN 10, 31055 TOULOUSE, France
Organisation website
EU Contribution
€400 000
Organisation
Bauhaus Luftfahrt Ev
Address
Boltzmannstraße, 85748 Garching Near Munich, Germany
EU Contribution
€420 000
Organisation
Arttic
Address
58A rue du Dessous des Berges, 75013 PARIS, France
Organisation website
EU Contribution
€187 578
Organisation
Gkn Aerospace Sweden Ab
Address
46181 Trollhaettan, Sweden
EU Contribution
€150 000
Organisation
Cranfield Aerospace Limited
Address
Cranfield University Campus Hangar 2, Cranfield, MK43 0AL, United Kingdom
Organisation website
EU Contribution
€550 700
Organisation
Rolls Royce Plc
Address
65 Buckingham gate, LONDON, SW1E 6AT, United Kingdom
Organisation website
EU Contribution
€100 000
Organisation
Mtu Aero Engines
Address
Dachauer Strasse 665, 80995 MUENCHEN, Germany
Organisation website
EU Contribution
€200 000

Technologies

Technology Theme
Aircraft propulsion
Technology
Optimum turbofan engine design
TRL
TRL 5
Development phase
Demonstration/prototyping/Pilot Production

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