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Thermoelectric generator for engine control system

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€1 015 318
EU Contribution
€474 971
Project Acronym
THETAGEN
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Environmental/Emissions aspects
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
SP1-JTI-CS-2009-01
Link to CORDIS
Objectives

ThetaGen aimed to scavenge energy from a turboshaft and convert it into electrical power to feed the engine control unit. It defined and specified such a power block, benchmarks potential technologies, developed a demonstrator and proved the concept through actual measurements on an engine. It gathers companies over four European countries: an aircraft manufacturer, two research labs, an expert in thermoelectric devices, a thermal expert and a power block manufacturer.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
JTI-CS - Joint Technology Initiatives - Clean Sky
Other Programme
JTI-CS-2009-1-SAGE-05-001 Development of a thermoelectricity generator for the supply of the engine control system

Results

Executive Summary:

ThetaGen aimed to scavenge thermal energy from a helicopter turboshaft and convert it into electrical power to feed the engine control unit.

It defined and specified such a power block, benchmarks potential technologies, aimed to develop a demonstrator and prove the concept through actual measurements on an engine.

It gathered companies over four European countries: an aircraft manufacturer (EVEKTOR, Czech republic) , a research lab (CNRS, France), an expert in thermoelectric devices (TERMOGEN AB, Sweden), a thermal expert (EPSILON, France) and a power block manufacturer (TRONICO, France).

The project failed to design the expected demonstrator because:

1. A current turboshaft is not a friendly environment for a thermo generator. It has not been designed for, and it does not fit with any evolution. No practical solution could be found with the current design;

2. In future turbo shafts, several evolutions have to be considered: anchoring devices on the combustion chamber and/or the compressors, cooling the fuel circuit and/or the fuel tank, improve the oil circuit.

3. A wide range of temperature is definitely not practical at system level. To narrow the temperature domain in all flight conditions it should be nice to use the combustion chamber as a hot source (more or less stable) and the oil circuit as a cool source (temperature controlled for other reasons). The fuel circuit can also be a nice cool source if properly refreshed.

 

Partners

Lead Organisation
Organisation
Electronique Industrielle De L'ouest - Tronico Sas
Address
Rue du bocage 26, 85660 Saint Philbert de Bouaine, France
Organisation website
EU Contribution
€192 000
Partner Organisations
Organisation
Epsilon Ingenierie
Address
RUE TARFAYA BATIMENT B612, 31400 TOULOUSE, France
Organisation website
EU Contribution
€70 728
Organisation
Evektor Spol. S R.o.
Address
Letecka 1008, 68604 KUNOVICE, Czechia
Organisation website
EU Contribution
€71 487
Organisation
Termo-Gen Ab
Address
Hangvar Olarve 609, SE624 54 Lärbro, Sweden
EU Contribution
€121 256
Organisation
Centre National De La Recherche Scientifique
Address
3 rue Michel-Ange, 75794 PARIS, France
Organisation website
EU Contribution
€19 500

Technologies

Technology Theme
Energy efficiency
Technology
Waste heat recovery system
Development phase
Research/Invention

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