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TRIMIS

innovative ICE Protection And Shielding System for HLFC Demonstrator

PROJECTS
Funding
European
European Union
Duration
-
Status
Ongoing
Geo-spatial type
Other
Total project cost
€998 620
EU Contribution
€699 034
Project Acronym
ICEPASS
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Environmental/Emissions aspects,
Safety/Security,
Other specified
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP10-2019-01
Link to CORDIS
Objectives

Aircraft manufacturers are continuously seeking for decreasing their CO2 emissions and trying to make flights more efficient and eco-friendlier. As part of this searching one major warhorse is the drag reduction during flight; One of this systems is the Laminar Flow Control LFC, where Hybrid Laminar Flow Control (HLFC) is included. Classic systems as IPS and shielding systems have to coexist with the new HLFC system in a much-reduced allocation space.

Towards the new generation of more efficient aircraft the use of More Electric Aircraft (MEA) is increasing during the recent years and modern aircrafts such as Airbus A350 and especially Boeing 787 are mounting more electrical systems.

This project faces two challenges. Firstly, to develop an electrical harness for power feed and monitoring systems of the HLFC, and secondly to develop an innovative way of carrying electricity in an aircraft to solve the big problem of lack of space in the leading edge where these HLFC systems operate. Regarding the first challenge IcePass proposal includes a detailed study of the new routings, with selection of components, and application of additive manufacturing technologies for brackets, in order to fulfil the complex space requirements of HLFC. For the second challenge IcePass proposes an innovative flat harness concept with application of 3d printing technology which will solve the space problem in the L/E and make possible an HLFC system. What is more, IcePass proposes as well an innovative way of routing harnesses through mechanisms, and particularly for the actuation system, by application of slip rings.

Solving both challenges, IcePass will manage to design and manufacture the electrical system of the HLFC thanks to the application of innovative wiring system concept which will change the state of the art in aerospace industry and manage to achieve the bigger MEA challenge.

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
Adatica Engineering SL
Address
AVENUE LEONARDO DA VINCI 8, 28906 GETAFE, Spain
EU Contribution
€699 034
Partner Organisations
EU Contribution
€0

Technologies

Technology Theme
Computer-aided design and engineering
Technology
Improvement of transition-prediction tools for future laminar flow aircraft
Development phase
Research/Invention
Technology Theme
Aircraft design and manufacturing
Technology
Hybrid Electro-Expulsive De-Icing System
Development phase
Research/Invention
Technology Theme
Aircraft design and manufacturing
Technology
Electric aircraft
Development phase
Research/Invention

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