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Sound Engineering For Aircraft (SEFA)
ID: 502865
Start date: 2004-02-01, End date: 2007-06-30
The aim of SEFA is to develop technology design criteria (Sound Engineering) based on a thorough assessment of which characteristics would make aircraft more acceptable for airport communities from a noise signature standpoint (spectral and directivity shapes, impact of separ...
Programme: FP6-AEROSPACE
Record Number: 72808
Last updated on: 2017-06-09
GLOBAL MONITORING FOR SECURITY AND STABILITY (GMOSS)
ID: 503699
Start date: 2004-03-01, End date: 2008-02-29
The aim of the GMOSS network of excellence is to integrate Europe´s civil security research so as to acquire and nourish the autonomous knowledge and expertise base Europe needs if it is to develop and maintain an effective capacity for global monitoring using satellite earth...
Programme: FP6-AEROSPACE
Record Number: 72834
Last updated on: 2016-11-15
AIRBORNE INTEGRATED SYSTEMS FOR SAFETY IMPROVEMENT, FLIGHT HAZARD PROTECTION AND ALL WEATHER OPERATIONS
ID: 516167
Start date: 2005-02-01, End date: 2009-08-31
Worldwide Air traffic is expected to increase threefold within the next 20 years, which raises an unprecedented challenge for safety. New means have to be invented and implemented, in particular on-board aircraft, to maintain the current low level of accidents.FLYSAFE will be...
Programme: FP6-AEROSPACE
Record Number: 75794
Last updated on: 2015-01-22
Novel Innovative Competitive Effective Tilt Rotor Integrated Project
ID: 30944
Start date: 2006-11-01, End date: 2014-11-30
This proposal has been prepared in the framework of a research and development roadmap defined by the European rotorcraft community that aims to develop a civil tilt-rotor aircraft. A key target of the road map is a flying demonstrator in the 2010 decade. NICE-TRIP specifical...
Programme: FP6-AEROSPACE
Record Number: 81483
Last updated on: 2014-09-29
Foldable, Adaptable, Steerable, Textile Wing Structure for Delivery of Capital Loads
ID: 30778
Start date: 2006-12-01, End date: 2010-06-30
FASTWing CL is to developing a navigated parafoil system for carrying loads of up to 6 tons. FASTWing CL is the successor of the FP5 programme. FASTWing which was completed successfully in June 2005. The latter has developed a prototype demonstrator capable to fly autonomous ...
Programme: FP6-AEROSPACE
Record Number: 81460
Last updated on: 2014-08-11
Distributed equipment Independent environment for Advanced avioNic Applications
ID: 30985
Start date: 2006-12-01, End date: 2010-05-31
The DIANA Project is the first step for the implementation of an enhanced Integrated Modular Electronics (IME) platform, providing secure distribution and execution on virtual machines to avionics applications. DIANA will define and standardize the development and certificati...
Programme: FP6-AEROSPACE
Record Number: 81487
Last updated on: 2014-08-11
Automated Diagnosis for Helicopter Engines and Rotating parts
ID: 30907
Start date: 2006-12-01, End date: 2008-11-30
Helicopters availability, in-flight reliability and low cost maintenance are major concerns for helicopters operators. HUMS (sensor based health monitoring) is an enabling technology seeking to provide a Condition-Based Maintenance (CBM) relying on automated diagnosis / progn...
Programme: FP6-AEROSPACE
Record Number: 81478
Last updated on: 2014-08-11
Towards Lean Combustion
[PROJECT] TLC - Towards Lean Combustion
ID: 12326
Start date: 2005-03-01, End date: 2010-03-31
The mitigation of aviation emissions in terms of their environmental impact is a priority for both air quality (local impact) and the greenhouse effect (global impact). For a fixed engine cycle, the margin of progress depends on the combustor technology. Lean combustion is the...
Programme: FP6-AEROSPACE
Record Number: 74772
Last updated on: 2013-03-26
Cellular Structures for Impact Performance
ID: 31038
Start date: 2006-09-01, End date: 2009-09-30
The European aircraft industry has strong interest in novel structural concepts for future aircraft fuselage and wing structures with lower fabrication costs and high performance. An important class of these next generation aerospace materials will employ advanced manufacturin...
Programme: FP6-AEROSPACE
Record Number: 79967
Last updated on: 2013-03-26
Distributed and Redundant Electro-mechanical nose wheel Steering System
ID: 30841
Start date: 2006-06-15, End date: 2009-12-14
The goal of this project is to research, develop and validate a distributed and redundant electrical steering system technology for an aircraft nose landing gear, that will provide improved competitiveness and improved aircraft safety by: - reduced system weight at the aircraf...
Programme: FP6-AEROSPACE
Record Number: 79957
Last updated on: 2013-03-26
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List retrieved on: 2017-11-19
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