Opendata, web and dolomites

ORBIT SIGNED

Aerodynamic rigs for VHBR IP turbine

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

Project "ORBIT" data sheet

The following table provides information about the project.

Coordinator
FUNDACION CENTRO DE TECNOLOGIAS AERONAUTICAS 

Organization address
address: Parque Tecnologico de Alava (Minano), C/ Juan de la Cierva 1
city: MINANO (ALAVA)
postcode: 1510
website: www.ctaero.com

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 Spain [ES]
 Total cost 2˙498˙216 €
 EC max contribution 2˙498˙216 € (100%)
 Programme 1. H2020-EU.3.4.5.5. (ITD Engines)
 Code Call H2020-CS2-CFP03-2016-01
 Funding Scheme CS2-IA
 Starting year 2017
 Duration (year-month-day) from 2017-01-01   to  2018-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    FUNDACION CENTRO DE TECNOLOGIAS AERONAUTICAS ES (MINANO (ALAVA)) coordinator 2˙498˙216.00

Map

 Project objective

The ORBIT project targets the environmental and competitiveness challenge of the European aeronautics sector, by addressing the topic of experimental validation rig testing to develop aerodynamic technologies for the multi-stage IP turbine of the Very High Bypass Ratio engine (VHBR).

The advancement of multi-stage IP Turbine technologies, as an important contributor to the VHBR engine concept, will participate significantly to the global objectives from Clean Sky2, which aim towards achievement of ACARE flight-path 2050 ambitious goals about CO2, NOx and Noise emissions.

The global objectives of this proposal are therefore aligned with the targets marked by Rolls-Royce for the Middle of Market Technology configuration. This proposal will deliver individual improvements in sub-system technology developments, to support the overall development of system level technologies capable of delivering substantial reductions in emissions.

The specific objectives of CTA as applicant partner, include all the tasks to permit the experimental validation of relevant aerodynamic technologies (i.e. design, manufacture, assembly and finally testing and post-processing). First four work packages propose the test of innovative geometries to assess the improved losses and reduction in the generated noise. The fifth work package is committed for the comparison of the former results with relevant reference rig tests, as an opportunity to integrate the new knowledge and enable the application of the innovations.

To guarrantee the success of this proposal, it is required to develop European world-class test capability that includes the acquisition of testing and measurement. Experience from the participation in previous R&T European programmes is key to minimize program risks and deliver successfully aerodynamic rig test programmes in the required time scales.

Finally, the ORBIT project considers activities for the dissemination and exploitation of the results to maximize the expected impact on competitiveness.

 Deliverables

List of deliverables.
Communication, dissemination and exploitation plan Documents, reports 2019-04-18 14:35:49
Report on the signature of the Implementation Agreement Documents, reports 2019-05-30 15:32:24

Take a look to the deliverables list in detail:  detailed list of ORBIT deliverables.

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "ORBIT" 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 "ORBIT" are provided by the European Opendata Portal: CORDIS opendata.

More projects from the same programme (H2020-EU.3.4.5.5.)

AIRSEAL (2019)

Airflow characterization through rotating labyrinth seal

Read More  

ESTiMatE (2018)

Emissions SooT ModEl

Read More  

MOnACO (2019)

Manufacturing of a large-scale AM component

Read More