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9 European Projects Found

Searched on 125080 European Projects

 FINISHED 

Jigs and Fixtures for Assembly of the Laminar Wing at the BLADE flight test demonstrator Final Assembly Line (JIF2LAND)

Start date: Sep 1, 2014, End date: Dec 31, 2016,

The objective of JIF2LAND proposal it to conduct the evelopment, design, manufacture and installation of jig platforms, staging and operational tooling for removing the BLADE wing (Natural Laminar Flow) sections of an A340-300, after the flight test and to assembly the original wings tips of the aircraft. The SFWA flight test demonstrator aims to validate that a specific wing profile can sustain l ...
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 3

 FINISHED 

ROTATING COWLS (LIGHT-COWLS)

Start date: Mar 25, 2013, End date: Nov 24, 2016,

The Project LIGHT-COWLS is aimed to find out a way to produce rotating nacelle components for aircraft engines by using composites materials with high Tg, production method can be RTM or ATL. In particular the design and manufacturing of rotating nacelle of the CROR is targeted. The materials to be used for this development will be high Tg resins and fibers as reinforcement. Thus the project will ...
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 4

 FINISHED 

Rotating nozzle (R-NOZZLE)

Start date: Feb 15, 2013, End date: Nov 14, 2016,

The Project R-NOZZLE is aimed to find out a way to produce 360º components for aircraft engines by combination of near-net-shape rolled ring process, plus machining. In particular the design and manufacturing of rotating exhaust nozzle of the CROR is targeted. The materials to be used for this development will be Inconel718 and Titanium Alloy. Thus the project will look for a cost effective way of ...
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 2

 FINISHED 

Contra-Rotating Open Rotor (CROR) Propeller barrels (GREENBARRELS)

Start date: Mar 1, 2012, End date: Sep 30, 2016,

The Project GREENBARRELS is aimed to find out a way to produce 360º components for aircraft engines by spinning methods, such as: spinning lathe, flowforming, shearforming. In particular the manufacturing of barrels for CROR propellers of SAGE2 ITD will be assessed. The materials to be used for this development will be Inconel718 and Titanium Alloy. Thus the project will look for a cost effective ...
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 4

 FINISHED 

Implementation carbon fibres for rotor of high speed rotating electric machine (HIGHPSLEEVE)

Start date: Jun 1, 2014, End date: Sep 30, 2016,

The Project HIGHPSLEEVE is aimed to find out a way to produce a fixation component for electrical motor, which turns at 50.000 RPM and works in -50 to 250ºC, of an aircraft by using composites materials with high Tg, such as BMI or Cyanate ester, reinforced with carbon fibers. Production method needs to be researched but Filament Winding seems to be the right candidate process. In particular the d ...
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 4

 FINISHED 

Final Assembly Line Assembly Jigs and Fixtures for flight test demonstrator (JIF4FLIGHT)

Start date: Jan 3, 2012, End date: Aug 2, 2016,

The objective of JIF4FLIGHT proposal it to conduct the development, design, manufacture and installation of jig platforms, stagingand operational tooling, plus project tooling for remowing the outer wing sections of an A340-300 and to assembly the SFWA laminar flow flight test demonstrator wings.The SFWA flight test demonstrator aims to validate that a specific wing profile can sustain laminar flo ...
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 3

 FINISHED 

Development of a composite sleeve for spatial separation of rotor and stator in an electric motor (COMPOSLEEVE)

Start date: Oct 1, 2014, End date: May 31, 2016,

The Project COMPOSLEEVE is aimed to find out a way to produce a stator sleeve for stator/rotor separation in electrical motor, which need to be cooled with aggressive fluids such as Skydrol, with high internal pressure and a temperature range that goes above 200ºC. For this application possible materials are composites with high Tg resins, such as BMI or Cyanate ester, reinforced with non conducti ...
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 4

 FINISHED 

Feasibility study and prototypes manufacturing of oil tank in thermoplastic for Helicopter Engine (LIGHT-TANK)

Start date: Apr 1, 2012, End date: Nov 30, 2014,

"The Project LIGHT-TANK is aimed to find out a way to produce oil tank and connection pipes in Thermoplastic Composites to be used in helicopter engine for the Gearbox system. Different thermoplastics materials, need of reinforcement and processes will be analysed to find out the cost effective way of producing such a components. When material and process are selected. Part desing will be carried ...
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 4

 FINISHED 

Automated Riblets Application on Aircraft Parts (INARAS)

Start date: Apr 1, 2012, End date: Mar 31, 2014,

"The Project INARAS (Intregal Automated Riblets Application System) is aimed to find out an automatic and cost effective way to paint riblets on an aircraft surface.The research and development to carry out in this Project will develop, integrate and test an Integral System to be used on real aircraft parts or mock-up to paint riblets. Riblets are a drag reduction technique that consists of small ...
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 2