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TRIMIS

Development of ECO-friendly protection procedures for LANDing gear aluminium alloys

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€366 951
EU Contribution
€346 921
Project Acronym
ECOLAND
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues,
Environmental/Emissions aspects
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP06-2017-01
Link to CORDIS
Background & Policy context

The need of using high performance lightweight materials is pushing the aerospace industry to incorporate aluminium alloys in many parts of the aircraft. But all aircraft components, and especially those of landing gears, need to be able to withstand friction and corrosive environments while continuing to operate at optimum levels.

Nowadays most landing gear parts made of aluminium alloys are protected against corrosion by surface anodising and multilayer painting. The treatment is usually carried out on Cr(VI) based compounds. To date, there is not any Cr-free accepted protecting treatment for Al 7000 series alloys that fulfils the aeronautics requirements, so, it is necessary to develop an environmentally and Cr-free acceptable alternative process.

Objectives

The main objective of ECOLAND project is to face the research of a suitable REACH compliant anaphoretic electrocoating treatment (including both the optimal pre-treatment method and anaphoretic electrocoating application conditions) that can replace the currently used anodising + painting treatment for protection of Al 7000 series alloys in aeronautic applications. This anaphoretic electrocoating will allow a reduction of emissions, saving of coat and improvement of corrosion protection.

The following improvements will be aimed for from the ECOLAND Cr-free project:

  • The lifetime of the anaphoretic electrocoating system shall be 25% longer than the lifetime of traditional.
  • It is expected a minimum of around 30% cost and 45% energy consumption reduction in manufacturing compared to currently available systems.
  • Thanks to the new coating systems more complex geometry parts could be coated and so landing gears might be designed lighter than current ones.
  • The production time to be shortened by 55%.
  • A decrease of the risk of mechanical failure due to the reduction of the alloy exposure time to acids.
  • VOCs emissions will be reduced by 50%.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.6.

Partners

Lead Organisation
Organisation
Fundacion Cidetec
Address
PASEO MIRAMON 196 PARQUE TECNOLOGICO DE MIRAMON, 20014 SAN SEBASTIAN, Spain
Organisation website
EU Contribution
€237 305
Partner Organisations
Organisation
Fundacion Centro Tecnologico De Miranda De Ebro
Address
CALLE MONTANANA PARCELAS R60 Y R61, 09200 MIRANDA DE EBRO BURGOS, Spain
Organisation website
EU Contribution
€62 878
Organisation
L.v.h. Coatings Ltd
Address
WALLACE HOUSE 20 BIRMINGHAM ROAD, WALSALL, WS1 2LT, United Kingdom
EU Contribution
€46 738

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Laminar flow aircraft coatings
Development phase
Research/Invention

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