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TiltHex SIGNED

Tilt Rotor Heat Exchanger

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

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 TiltHex project word cloud

Explore the words cloud of the TiltHex project. It provides you a very rough idea of what is the project "TiltHex" about.

architecture    manufacturing    conventional    exchanger    manufacture    heat    oil    team    plate    transmission    fin    flight    designs    solution   

Project "TiltHex" data sheet

The following table provides information about the project.

Coordinator
HS MARSTON AEROSPACE LIMITED 

Organization address
address: WOBASTON ROAD FORDHOUSES
city: WOLVERHAMPTON
postcode: WV10 6QJ
website: n.a.

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country United Kingdom [UK]
 Total cost 472˙890 €
 EC max contribution 331˙023 € (70%)
 Programme 1. H2020-EU.3.4.5.3. (IADP Fast Rotorcraft)
 Code Call H2020-CS2-CFP02-2015-01
 Funding Scheme /CS2-IA
 Starting year 2018
 Duration (year-month-day) from 2018-02-01   to  2020-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    HS MARSTON AEROSPACE LIMITED UK (WOLVERHAMPTON) coordinator 331˙023.00

Mappa

 Project objective

The overall objective of the project is to design, develop; manufacture and flight qualify a novel heat exchanger for oil cooling in the transmission system of a civil Tilt Rotor aircraft. The proposed solution will outperform a conventional plate-fin heat exchanger in terms of efficiency, volume, weight, robustness, reliability and will fully integrate into the transmission systems architecture.

The concept underpinning this project is to build upon Marston Aerospace’s long history of innovation within heat transfer and fluids management systems by forming an integrated project team. The team will consist of thermal modellers, mechanical design, manufacturing, experimentalists and R&D experts in order to propose three initial air cooled oil cooler designs based on different manufacturing technologies. These will be conventional plate and fin corrugated heat exchanger; chemically etched plate and pin and an additive layer manufacturing solution utilising a novel architecture. An assumption would be that the material which would be most appropriate, in terms of technology readiness and for each proposed manufacturing process the suitability would be aluminium and that the new designs will be directly compared to each other in order to select the most viable design to take forward through to prototype manufacture towards flight demonstration testing.

 Work performed, outcomes and results:  advancements report(s) 

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The information about "TILTHEX" are provided by the European Opendata Portal: CORDIS opendata.

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