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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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Developement of CNT doped reinforced aircraft composite parts and a 
ssociated tooling, using the Liquid Resin Infusion method
ID: 325967
Start date: 2013-08-01, End date: 2016-03-31
BULCANATU project wants to develop feasible techniques for advanced and cost effective composite manufacturing of aviation parts. The development of new epoxy resin Carbon Nanotube doping techniques compatible with Liquid Resin Infusion will open a new era on fabrication of a...
Programme: FP7-JTI
Record Number: 110472
Last updated on: 2017-04-10
WING STRUCTURAL TEST DEVELOPMENT METHOD
ID: 325978
Start date: 2013-01-14, End date: 2016-10-13
The proposal approach innovative solutions for the design and manufacturing of the test rig and the definition of the method and prformance for the structural testing of two different kinds of configuration for the outer wings within a Smart Fixed Wing Aircraft. The WISDOM pr...
Programme: FP7-JTI
Record Number: 108866
Last updated on: 2017-01-23
Experimental Subsonic Investigation of a Complete Aircraft Propulsion system Installation and Architecture power plant optimization
ID: 325954
Start date: 2013-06-01, End date: 2017-02-28
The proposed project tackles a CfP from the JTI-GRA ITD. Is focuses on the experimental optimization of a regional aircraft configuration and a subsequent optimization of take-off/ landing configuration. The regional aircraft has a wing designed for natural laminar flow, fuse...
Programme: FP7-JTI
Record Number: 110471
Last updated on: 2016-12-26
LORD Engine Mounting System for the SAGE2 Open-Rotor demonstrator
ID: 338539
Start date: 2013-09-01, End date: 2016-12-31
This response to the SAGE-02 call details the proposed approach to an engine mounting system for the open-rotor demonstrator. The goal of the program is to define the requirements of the mounting system, design and develop the system so that it meets the requirements and can ...
Programme: FP7-JTI
Record Number: 185393
Last updated on: 2016-12-19
Microstructure Based Material Mechanical Models for Superalloys
ID: 620078
Start date: 2013-10-01, End date: 2016-03-31
A microstructure-based model will be developed to simulate the mechanical behaviour of polycrystalline Ni-based superalloys containing gamma’ and gamma’’ precipitates and processed by casting and forging. The model will be based in a multiscale approach in which deformation a...
Programme: FP7-JTI
Record Number: 111118
Last updated on: 2016-11-07
Rolled-Only IN718 Ring-shaped Components
ID: 325974
Start date: 2013-03-01, End date: 2016-02-29
The objective of this proposal is to develop and validate a robust and reliable ring-rolling-only route for manufacturing IN718 alloy near-net-shaped rotating aero-engine disk components, RORC (e.g., low-pressure turbine disks). The material and mechanical response of the ROR...
Programme: FP7-JTI
Record Number: 108809
Last updated on: 2016-11-07
OPTImised Model for Accurately measured in-flight Loads
ID: 338538
Start date: 2013-09-02, End date: 2016-03-01
In recent years, Counter Rotating Open Rotors (CROR) have received considerable attention as the CROR concept promises a considerable reduction of fuel consumption over conventional ducted turbofan engines. Specifically for Smart Fixed Wing Aircraft CROR is expected to contri...
Programme: FP7-JTI
Record Number: 110833
Last updated on: 2016-10-31
Innovative fabrication routes and materials for METal and anode supported PROton conducting fuel CELLs
ID: 277916
Start date: 2011-12-01, End date: 2015-05-31
PCFC is one of the most promising technologies to reach the requirements related to cogeneration application, especially for small power systems (1-5 kWel). The investigation in the concept of advanced thin-film ceramic fuel cell technology at operating intermediate temperatu...
Programme: FP7-JTI
Record Number: 101146
Last updated on: 2016-10-17
Validation of high load capacity gear material
ID: 338510
Start date: 2013-05-01, End date: 2016-12-31
The VHLGM project goal is to integrate the currently available knowledge of the strength properties of the high load innovative aeronautical gear’s material used into the Power Reduction Gearbox of Geared Open Rotor demonstrator (SAGE 2) through an optimized characterization ...
Programme: FP7-JTI
Record Number: 108868
Last updated on: 2016-10-03
High performance composites for demanding high Temperature applications
ID: 325939
Start date: 2013-03-01, End date: 2015-09-30
One of the major limitations of polymeric composites for structural applications is the ability of the matrix to withstand and maintain load transfer capability at high temperatures. The current project, HicTac, address this drawback and aims at development of composites capa...
Programme: FP7-JTI
Record Number: 109261
Last updated on: 2016-09-12
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List retrieved on: 2017-04-28
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