Skip to main content
European Commission logo
TRIMIS

Surface Heat Exchangers For Aero Engines 2

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€1 343 120
EU Contribution
€1 335 887
Project Acronym
SHEFAE 2
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Decarbonisation
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-MG-2015_SingleStage-A
Link to CORDIS
Objectives

The Project aim is to develop and demonstrate lighter integrated heat exchanger systems for the turbofan engine. Currently in turbofan engines heat exchangers are used to cool the oil that is supplied to the bearing chambers and generators. They contribute to achieving the best engine performance by maintaining oil and fuel temperatures within defined limits.

In the future, extensive use of heat exchangers will be required in order to get the very lowest levels of fuel burn to meet the environmental challenges. Therefore development of compact, lightweight and low cost heat exchanger systems is required. In this context, research and development activities are foreseen, to assess, develop, design and manufacture: High Length to depth ratio Surface Air Cooled Oil Coolers; Utilisation of engine structural components for thermal cooling; Robust mounting systems to integrate the high length to depth Surface Air Cooled Oil Cooler on the turbofan engine; High efficiency Fuel Oil Heat Exchanger; High reliability Modulating Oil Bypass Valve that is integrated within the Fuel Oil Heat Exchanger. The heat exchanger systems will be tested on the rig and Rolls-Royce demonstrator engines to validate their performance and structural capabilities. The integration of the high length to depth ratio Surface Air Cooled Oil Coolers on the engine will require a robust mounting system to tolerate the induced stresses due to thermal and vibrational loads. Advanced manufacturing capability will be developed for the designs of the high length to depth ratio Surface Air Cooled Oil Coolers and the Fuel Oil Heat Exchanger with the integrated Modulating Oil Bypass Valve.

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
Rolls Royce Plc
Address
65 Buckingham gate, LONDON, SW1E 6AT, United Kingdom
Organisation website
EU Contribution
€617 887
Partner Organisations
Organisation
Brandenburgische Technische Universitat Cottbus
Address
UNIVERSITAETSPLATZ 3-4, 101344 COTTBUS, Germany
Organisation website
EU Contribution
€448 000
Organisation
Paulstra
Address
Marius Aufan 61, 92305 Levallois-Perret, France
Organisation website
EU Contribution
€270 000

Technologies

Technology Theme
Aircraft propulsion
Technology
New concepts for heat exchangers
Development phase
Research/Invention
Technology Theme
Aircraft propulsion
Technology
High performance lightweight High Pressure Compressor (HPC) guide vane and Cooled HPC exit cone
Development phase
Research/Invention

Contribute! Submit your project

Do you wish to submit a project or a programme? Head over to the Contribute page, login and follow the process!

Submit