Opendata, web and dolomites

SUBLIME SIGNED

Supporting Understanding of Boundary Layer Ingesting Model Experiment

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

 SUBLIME project word cloud

Explore the words cloud of the SUBLIME project. It provides you a very rough idea of what is the project "SUBLIME" about.

asking    performance    propulsor    ing    installation    skills    cranfield    passenger    suitable    equipped    engines    cycle    introduction    ingestion    bli    612    tested    designed    fuselage    subsequently    experiment    36    inlet    tools    responsible    position    cooperation    distortion    chalmers    university    savings    aircraftpropulsors    podded    theoretical    fan    model    aircrafts    power    flexible    fidelity    aviation    optimized    regarding    propulsors    supporting    bookkeeping    flow    grant    installed    500    saving    transonic    maximizes    layer    wind    manufactured    consistently    appropriate    architectures    distortions    months    dependencies    ara    propulsive    simulations    rear    accurate    aircraft    shape    manager    full    compliance    close    facilities    force    delivered    mainly    experimental    hit09    universities    complementary    releasing    distorted    corresponding    fed    pattern    cfd    poses    configurations    industry    minimizes    sme    conventional    tunnel    boundary    sublime    predict    engine   

Project "SUBLIME" data sheet

The following table provides information about the project.

Coordinator
UNIVERSITA DEGLI STUDI DI PADOVA 

Organization address
address: VIA 8 FEBBRAIO 2
city: PADOVA
postcode: 35122
website: www.unipd.it

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Italy [IT]
 Total cost 3˙612˙549 €
 EC max contribution 3˙612˙549 € (100%)
 Programme 1. H2020-EU.3.4.5.1. (IADP Large Passenger Aircraft)
 Code Call H2020-CS2-CFP09-2018-02
 Funding Scheme CS2-RIA
 Starting year 2019
 Duration (year-month-day) from 2019-12-01   to  2022-11-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    UNIVERSITA DEGLI STUDI DI PADOVA IT (PADOVA) coordinator 25˙000.00
2    AIRCRAFT RESEARCH ASSOCIATION LIMITED UK (BEDFORD) participant 2˙559˙623.00
3    HIT09 SRL IT (PADOVA PD) participant 422˙562.00
4    CRANFIELD UNIVERSITY UK (CRANFIELD - BEDFORDSHIRE) participant 394˙738.00
5    CHALMERS TEKNISKA HOEGSKOLA AB SE (GOETEBORG) participant 210˙625.00

Map

 Project objective

SUBLIME (Supporting Understanding of Boundary Layer Ingestion Model Experiment)

The introduction of engines integrated with the rear fuselage (BLI engines) in large passenger aircrafts poses new challenges regarding accurate experimental assessment of their performance, especially in terms of power savings, over conventional propulsive architectures (e.g. podded engines) as the engine is fed with a distorted flow. The SUBLIME project will address this challenge, resulting in a flexible and robust experimental set-up to establish dependencies among the propulsor shape/position, the fan inlet distortion pattern and the corresponding power savings. A consortium of an R&D institute, an SME, and 2 Universities with complementary skills will produce this result in close coordination with the topic manager in 36 months, asking for a grant of € 3.612.500. Coordinator ARA will provide a number of aircraft configurations equipped with BLI propulsors integrated in the rear fuselage, designed and optimized in cooperation with HIT09 (mainly responsible for CFD studies and fan design), Cranfield University (mainly responsible for theoretical and experimental force bookkeeping) and Chalmers University of Technology (mainly involved in engine cycle studies), to be subsequently manufactured and tested by ARA in their transonic wind tunnel. The project will advance the state of the art in BLI studies by means of wind tunnel activities supported by high-fidelity CFD simulations to consistently predict full-scale behaviour of the aircraft architectures suitable for appropriate propulsor installation which minimizes inlet flow distortions and maximizes power saving. The results of installed wind-tunnel tested aircraftpropulsors will be delivered in full compliance with the call. SUBLIME will provide methodologies, tools and facilities to the European aviation industry, therefore contributing to releasing the full potential of power saving of BLI engines.

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "SUBLIME" project.

For instance: the website url (it has not provided by EU-opendata yet), the logo, a more detailed description of the project (in plain text as a rtf file or a word file), some pictures (as picture files, not embedded into any word file), twitter account, linkedin page, etc.

Send me an  email (fabio@fabiodisconzi.com) and I put them in your project's page as son as possible.

Thanks. And then put a link of this page into your project's website.

The information about "SUBLIME" are provided by the European Opendata Portal: CORDIS opendata.

More projects from the same programme (H2020-EU.3.4.5.1.)

C-ALM AOHE (2019)

Compact - Additive Layer Manufactured Air Oil Heat Exchanger

Read More  

PROTEUSS (2019)

Pressurised Rotational Oil Transfer – Experimental Unit & System

Read More  

LIFT (2018)

Lightweight Innovative Generator for Future Air Transportation

Read More