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BALANCE

Business Aviation Laminar Nacelle

Total Cost €

0

EC-Contrib. €

0

Partnership

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Project "BALANCE" data sheet

The following table provides information about the project.

Coordinator
SAFRAN NACELLES 

Organization address
address: ROUTE DU PONT VIII
city: GONFREVILLE L ORCHER
postcode: 76700
website: www.safrangroup.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 France [FR]
 Total cost 1˙071˙350 €
 EC max contribution 749˙945 € (70%)
 Programme 1. H2020-EU.3.4.5.4. (ITD Airframe)
 Code Call H2020-CS2-CFP01-2014-01
 Funding Scheme CS2-IA
 Starting year 2016
 Duration (year-month-day) from 2016-01-01   to  2018-07-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    SAFRAN NACELLES FR (GONFREVILLE L ORCHER) coordinator 749˙945.00

Map

 Project objective

Development of nacelle concepts to allow increased laminar airflow over a business jet nacelle. The technologies developed through this project will achieve 1% drag at aircraft level, through extension of the laminar surface to 30-40% of the nacelle length. BALANCE will investigate means of reducing the number of aerodynamic disturbances present in the forward portion of the nacelle, including reviewing interface locations, methods of attaching parts, and impacts on engine integration to ensure the resulting solutions not only provide the drag targets set, but do not adversely impact the Production and Operating costs of the nacelle. Using knowledge of nacelle and engine integration, this project will provide a digital demonstrator supported by analysis and test results to achieve TRL5 level laminar nacelle suitable for business jet applications.

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

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