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BALANCE

Business Aviation Laminar Nacelle

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

BALANCE project word cloud

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

surface attaching laminar parts aerodynamic solutions disturbances extension ing nacelle trl5 length reviewing integration impacts balance technologies business demonstrator digital jet interface 40 1 airflow drag engine aircraft locations development suitable portion reducing adversely

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 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.	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.