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Horizon 2020 project information and now also report summaries are available on CORDIS. All H2020 projects can be downloaded from the EU Open Data Portal .

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Multi-physics mOdelling of high Temperature engIne ValvEs
ID: 785530
Start date: 2018-03-01, End date: 2022-02-28
"Aim: Predictive assessment of the functionality, performance and controllability of pneumatic aircraft engine valves through modelling of elementary physical phenomena encountered in the engine environment.Achievement of this project aim will be accomplished via two major...
Programme: H2020-EU.3.4.5.1.
Record Number: 213820
Last updated on: 2018-02-22
Vision-based Inspection Systems for automated Testing of Aircraft interiors
ID: 785410
Start date: 2018-02-01, End date: 2020-07-31
The VISTA project aims to post-assembly testing of aircraft interior installations in both cabin and cargo units in order to ensure quality and reliability of located components. This goal will be pursued by the development and implementation of a multi-sensor platform and...
Programme: H2020-EU.3.4.5.1.
Record Number: 213589
Last updated on: 2018-02-22
Airline Maintenance Operations implementation of an E2E Maintenance Service Architecture and its enablers
ID: 681858
Start date: 2015-12-01, End date: 2019-11-30
The AIRMES project focusses on optimising end-to-end maintenance activities within an operator’s environment. It will develop and validate an innovative, state-of-the-art, integrated maintenance service architecture that will be a key step in achieving the goal of no...
Programme: H2020-EU.3.4.5.1.
Record Number: 200486
Last updated on: 2017-06-23
Environmentally Friendly Fire Suppression System for Cargo using Innovative Green Technology
ID: 685482
Start date: 2016-02-01, End date: 2020-07-31
Fire suppression and explosion protection have used halons in many applications because they are electrically nonconductive, dissipate rapidly without residue, are safe for limited human exposure, and are extremely efficient in extinguishing most types of fires. However they...
Programme: H2020-EU.3.4.5.1.
Record Number: 199348
Last updated on: 2017-05-30
FLOW Control Actuators at Aircraft scale manufacturing by SLM with high aerodynamic performance for using in Harsh environment
ID: 785408
Start date: 2018-04-01, End date: 2020-03-31
The main goal of FLOWCAASH project is to design and manufacture reliable and safe flow control actuators at aircraft scale by Selective Laser Melting (SLM) able to withstand the high temperatures (up to 260 °C) and pressures (5 bar) during flight test with aerodynamic...
Programme: H2020-EU.3.4.5.1.
Record Number: 213592
Last updated on: 2018-02-22
Turbo electRic Aircraft Design Environment (TRADE)
ID: 755458
Start date: 2017-09-01, End date: 2020-02-29
The improvement potential in conventional aero engines will be realized over the next decades. While a number of evolutionary improvements remain, the limits to thermal efficiency are becoming visible in terms of material constraints, NOx emissions and engine operability. The...
Programme: H2020-EU.3.4.5.1.
Record Number: 210614
Last updated on: 2017-05-23
SURFACE INTEGRITY CONSCIOUS HIGH-PERFORMANCE HYBRID MACHINING FOR SAFETY-CRITICAL SUPERALLOY AEROENGINE PARTS
ID: 754807
Start date: 2017-10-01, End date: 2020-09-30
STIMULANT aims to develop and demonstrate “surface integrity conscious” hybridisation of machining processes for safety-critical aeroengine parts that is able to deliver a step-change in Material Removal Rates (MRR) and reduction in production costs. STIMULANT will take...
Programme: H2020-EU.3.4.5.1.
Record Number: 210360
Last updated on: 2017-05-05
MULTI-PHYSICS METHODOLOGY FOR PHASE CHANGE DUE TO RAPIDLY DEPRESSURISED TWO-PHASE FLOWS
ID: 785549
Start date: 2018-03-01, End date: 2020-02-29
A multi-physics methodology is proposed to couple CFD calculations with models for phase change of rapidly depressurised mist of a fire suppression system. The methodology combines existing models with newly developed ideas with considers the coupling between large and small...
Programme: H2020-EU.3.4.5.1.
Record Number: 213823
Last updated on: 2018-02-22
Multiscale Analysis of AiRframe Structures and Quantification of UncErtaintieS System
ID: 754581
Start date: 2017-06-01, End date: 2020-05-31
MARQUESS has been specifically designed to address the challenges outlined in the Topic Description reference JTI-CS2-2016-CFP04-LPA-02-15 to fit into the activities of WP2.4.3 in the LPA IADP in Clean Sky 2. MARQUESS will serve as a valuable precursor to the above as it will...
Programme: H2020-EU.3.4.5.1.
Record Number: 210608
Last updated on: 2017-05-18
High Cycle Fatigue Prediction Methodology for Fibre Reinforced Laminates for Aircraft Structures in CROR Environment – Development and Validation
ID: 738130
Start date: 2017-02-01, End date: 2020-01-31
The aim is to develop high cycle fatigue (HCF) testing capabilities for composite materials to study the long-term fatigue life of composite laminates used in new structural architectures subjected to high sound pressure loading in CROR environment.The achievement of the...
Programme: H2020-EU.3.4.5.1.
Record Number: 208065
Last updated on: 2017-08-17
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List retrieved on: 2018-02-25
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