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TRIMIS

Advanced Steady and unsTeady distORtion sImulAtor

PROJECTS
Funding
European
European Union
Duration
-
Status
Ongoing
Geo-spatial type
Other
Total project cost
€2 378 125
EU Contribution
€2 200 000
Project Acronym
ASTORIA
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Other specified
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP09-2018-02
Link to CORDIS
Objectives

Fully answering the requirements of topic JTI-CS2-2018-CfP09-LPA-01-59, the ASTORIA project aims at developing a demonstrated set of tools and methodologies in order to design and test devices replicating complex, steady and unsteady, total pressure and swirl combined distortion profiles with high fidelity in a test rig environment.

Software and methodologies will be developed that will enable the definition of tailored multi-component devices, based on extensive exploitation of CFD, reduced-order models and optimization, harnessing the potential offered by rapid prototyping. Steady and unsteady patterns design methodologies will be validated through extensive experimental reduced-scale testing in precisely controlled conditions.

The software toolset will be highly modular and flexible. The objective is to combine into a new multi-component distortion generator generic total pressure distortion generating screens and aerodynamic turning vanes assemblies, with limitless possibilities in vane shapes, distribution and size for complex swirl pattern replication.

Several assembly solutions are envisaged, which will allow to jointly rotate parts (swirl frame and base distortion) or, conversely, preserve a fixed baseline steady distortion pattern and limit periodic position variation to a subset of turning vanes and/or screen. The integrated toolset will provide an unprecedented capability for combined arbitrarily complex total pressure and swirl distortion simulation, including the minimization of the undesirable influence of the device and directly integrating mechanical and manufacturability into the design intent. It will also seamlessly allow to integrate the potential effect of the fan.

ASTORIA is specifically linked with LPA-IADP-WP1.1.3.6, will directly be applicable for specific fan designs to be tested within the SA²FIR rig and will serve the “DX2 Boundary Layer Ingestion” demonstrator, paving the way for new robust integrated engine/airframe design practices.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.1. - IADP Large Passenger Aircraft
Other Programme
JTI-CS2-2018-CfP09-LPA-01-59 - Fan inlet advanced distortion simulator

Partners

Lead Organisation
Organisation
Centre De Recherche En Aéronautique
Address
Avenue Jean Mermoz 30, Bât. Mermoz 1, / GOSSELIES, Belgium
Organisation website
EU Contribution
€700 000
Partner Organisations
Organisation
Institut Von Karman De Dynamique Des Fluides
Address
Chaussee De Waterloo 72, 1640 Rhode Saint Genese, Belgium
EU Contribution
€1 100 000
Organisation
Numerical Mechanics Applications International Sa
Address
CHAUSSEE DE LA HULPE 187-189, 1170 BRUXELLES, Belgium
Organisation website
EU Contribution
€400 000

Technologies

Technology Theme
Aircraft propulsion
Technology
Optimum turbofan engine design
Development phase
Research/Invention

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