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TRIMIS

Advanced Laminar Flow tAilplane

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€2 129 109
EU Contribution
€1 610 395
Project Acronym
ALFA
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP02-2015-01
Link to CORDIS
Objectives

Project ALFA (Advanced Laminar Flow tAilplane) is initiated by an industrial partner (Fokker) and a research centre (NLR), in response to the 2nd Call for proposal of CS2, under the topic “Laminar Horizontal Tail Plane full scale ground demonstrator”.

The objective of ALFA is to push forward laminar flow technology by developing, designing and manufacturing a full scale demonstrator of a Natural Laminar Flow (NLF) Horizontal Tail Plane (HTP). The reduction of the aerodynamic drag of the aircraft by application of NLF on the HTP will offer a potential of a 1% decrease of fuel burn.

ALFA will introduce advanced materials and manufacturing technologies to meet the stringent NLF surface quality demands. New structural concepts will be developed and discussed with the topic manager taking into account all requirements regarding operations, safety, cost and environmental impact, to ensure the implementation on future business jets. ALFA’s NLF HTP demonstrator will validate the selected structural concept. This demonstrator is also prepared for future aerodynamic testing of NLF in a wind tunnel.

The comprehensive experience of the ALFA partners working on the demonstration of laminar flow in various R&T projects (e.g. EU AFLoNext, BLADE) and joint national and European collaboration on multiple aircraft programs motivate their common application. Fokker has a strong track record in designing and manufacturing complete tail sections for US and European Business Jets. As a former OEM of aircrafts, Fokker still engineers and manufactures with know-how of the entire aircraft. The complementary capabilities and competences of NLR to provide innovative solutions for composite structures and knowledge on wind tunnel testing, are keys to the project’s success.

The ALFA total grant request to EC is 1,610,395 € for the whole consortium. The project will be conducted within 23 months in close alignment with the topic manager, and with related topics in LPA and other IADP’s and ITD’s.

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.

Partners

Lead Organisation
Organisation
Fokker Aerostructures Bv
Address
Industrieweg 4, 3351 LB Papendrecht, Netherlands
Organisation website
EU Contribution
€1 210 332
Partner Organisations
Organisation
Stichting Centrum Voor De Ontwikkeling Van Transport En Logistiek In Europa
Address
Van Nelleweg 1, 3044 BC Rotterdam, Netherlands
Organisation website
EU Contribution
€400 063

Technologies

Technology Theme
Computer-aided design and engineering
Technology
Improvement of transition-prediction tools for future laminar flow aircraft
Development phase
Research/Invention

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