Skip to main content
European Commission logo
TRIMIS

Development of a composite sleeve for spatial separation of rotor and stator in an electric motor

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete with results
Geo-spatial type
Other
Total project cost
€297 809
EU Contribution
€193 375
Project Acronym
COMPOSLEEVE
STRIA Roadmaps
Transport electrification (ELT)
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues,
Safety/Security
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
SP1-JTI-CS-2013-03
Link to CORDIS
Objectives

The Project COMPOSLEEVE aimed to find out a way to produce a stator sleeve for stator/rotor separation in electrical motor, which need to be cooled with aggressive fluids such as Skydrol, with high internal pressure and a temperature range that goes above 200ºC. For this application possible materials were composites with high Tg resins, such as BMI or Cyanate ester, reinforced with non conductive fibres.

Production method needs to be researched but Filament Winding seems to be the right candidate process. In particular the design and manufacturing of sleeve component was targeted. Thus the project looked for a cost effective way of producing these sleeve components in these composites material while ensuring to withstand with requirements. The aim was to get a cost effective way of manufacturing.

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-2013-3-SGO-02-085 Development of a composite sleeve for spatial separation of rotor and stator of an electrical motor

Results

Executive Summary:

Due to electrical systems increase, in example landing gear, in future Aircraft, the need for more electrical power on board was envisioned. But, the weight associated to electrical rotating machine increase can be a drawback for More Electric Aircraft (MEA) architectures. Consequently, the rotating electrical machine manufacturers were looking for solutions to reduce the mass of these assemblies.

For these reason, the objectives of COMPOSLEEVE projects were:

  • To find out the right materials and techniques for manufacturing a slim composite sleeve which is compliant with the constraints and requirements concerning pressure, temperature and chemical stability
  • To carry out design activities (included material characterization) to get a design compliant with main constraints
  • To manufacture between 5 to 10 sleeves for testing (some of them by the consortia, some of them by Topic Manager in a further motor assembly)
  • To test the resulting sleeve, alone against the requirements: pressure, heat
  • In a further stage the Topic Manager will test the sleeve in a corresponding motor prototype to see the behaviour under more integral operational, environmental and failure conditions.

The following main constraints and requirements were considered:

  • Material shall be able to resist a temperature > 150°
  • Material shall be non-conductive
  • Composite sleeve shall be able to resist a pressure of 350 bar
  • Wall thickness shall be not more than 2.5mm
  • The composite sleeve shall withstand a stator temperature of 200°C, at teeth level, without ductile deformation or any other damages.
  • Because of the build in situation at the motor there are a lot of supporting points around the contour of the sleeve which are able to absorb the pressure force.
  • The sleeve will be designed, manufactured and prototype tested (pressure, heat)
  • It will also be optimized the construction and technique of the sleeve for industrial manufacturing and the cost will be analysed for a serial production.

To accomplish the project objectives, the consortium assumes the responsibility for:

  • The selection of the materials for the composite sleeve (resin, fibre ...)
  • The selection of the detailed manufacturing process
  • The Composite sleeve design
  • The development of a manufacturing process for the sleeve
  • The manufacturing of 5 to 10 for test some of them by the consortia and some of them in motor test at Topic Manager further development
  • The performing of test concerning the requirements: temp., pressure, fatigue
  • The proposal of optimization of design, materials and manufacturing process concerning quality and cost
  • An estimative cost analysis (RC / NRC) concerning serial production

At the end of the project the COMPOSLEEVE had fully achieved its objectives. During the project the following foreground was generated.

  • Design of sleeve for an electrical motor in composite
  • Testing of sleeve in a pressure test bench as well as in testing machines

The expected impact of COMPOSLEEVE was a considerable weight saving by achieving taking into account the replacement of a complex assembly of metal/plastic part with a density in the range of 8 g/cm3 vs 1,5 g/cmm3 of the proposed composite sleeve.

As well as an innovative design and manufacturing alternative for composite tubes combining advanced polymer with nonconductive fibre and liner.

Partners

Lead Organisation
Organisation
Fundacio Eurecat
Address
AVENIDA UNIVERSITAT AUTONOMA 23, 08290 CERDANYOLA DEL VALLES (BARCELONA), Spain
Organisation website
EU Contribution
€53 508
Partner Organisations
Organisation
Universitat De Girona
Address
PLACA SANT DOMENEC 3, 17004 GIRONA, Spain
Organisation website
EU Contribution
€1 499 073
Organisation
Universitat De Girona
Address
PLACA SANT DOMENEC 3, 17004 GIRONA, Spain
Organisation website
EU Contribution
€44 708
Organisation
Fundacio Privada Ascamm
Address
AVENIDA UNIVERSITAT AUTONOMA , PARC TECNOLOGIC DEL VALLES 23, 08290 CERDANYOLA DEL VALLES, Spain
Organisation website
EU Contribution
€35 198
Organisation
Airborne Composites Automation Bv
Address
LAAN VAN YPENBURG 70, 2497 GB S GRAVENHAGE, Netherlands
EU Contribution
€59 962

Technologies

Technology Theme
Composite materials
Technology
Composite materials for structural purposes in the aircraft
Development phase
Validation

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