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Development and Manufacturing of an All-Oxide Inter Turbine Duct for Aeroengines

Objective

The objective of the proposal is the development of an all-oxide Ceramic Matrix Composites (CMC) inter turbine duct for testing of the component in a demonstrator engine.
The development steps include:
- Designing the parts including the attachment to the metallic support structure
- Defining design rules how to work with oxide CMCs for engine parts
- Simulation of the parts behavior under engine loads
- Assessment of the lifetime and reliability of the material in operation to translate the specimen behavior onto the component level
- Optimizing the performance of the parts w.r.t. manufacturing parameters e.g. fiber orientation
- Characterizing the material properties needed for the design process on specimen level. This includes the material development for example to improve the matrix system for prepreg technology
- Manufacturing of the demonstrator parts
- Develop a concept for fining qualification steps
- Develop a concept for non-destructive testing
- Validating simulation results with engine data resulting from engine tests
For manufacturing oxide CMCs specimen and parts the following manufacturing techniques are included in the proposed project:
- Winding
- Prepreg technology (as automated as possible)
- Braiding
The path to final manufacture and validation will be documented and coordinated in close collaboration with the consortium partners and the topic manager.
This proposal answers the CfP in “Work Package 4 – Advanced Geared Engine Configuration (HPC-LPT)” of the Engine Integrated Technology Demonstrators in Clean Sky 2. It utilizes the low specific weight of oxide CMCs to save weight and its inherent oxidation and temperature resistant nature to save cooling air. It therefore, contributes to the key objectives of the work package: improvement of efficiencies and innovative lightweight and temperature resistant materials.

Fields of science (EuroSciVoc)

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Programme(s)

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Topic(s)

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Funding Scheme

Funding scheme (or “Type of Action”) inside a programme with common features. It specifies: the scope of what is funded; the reimbursement rate; specific evaluation criteria to qualify for funding; and the use of simplified forms of costs like lump sums.

CS2-RIA - Research and Innovation action

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Call for proposal

Procedure for inviting applicants to submit project proposals, with the aim of receiving EU funding.

(opens in new window) H2020-CS2-CFP01-2014-01

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Coordinator

DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Net EU contribution

Net EU financial contribution. The sum of money that the participant receives, deducted by the EU contribution to its linked third party. It considers the distribution of the EU financial contribution between direct beneficiaries of the project and other types of participants, like third-party participants.

€ 1 685 095,00
Address
Linder Hoehe
51147 Koeln
Germany

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Region
Nordrhein-Westfalen Köln Bonn, Kreisfreie Stadt
Activity type
Research Organisations
Links
Total cost

The total costs incurred by this organisation to participate in the project, including direct and indirect costs. This amount is a subset of the overall project budget.

€ 1 685 095,00

Participants (2)

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