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TRIMIS

Multi-Material Thermoplastic high pressure Nitrogen Tanks for Aircraft

PROJECTS
Funding
European
European Union
Duration
-
Status
Ongoing
Geo-spatial type
Other
Total project cost
€819 071
EU Contribution
€650 000
Project Acronym
TRINITI
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Other specified
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP09-2018-02
Link to CORDIS
Objectives

TRINITI aims at developing and demonstrating concepts and methodologies enabling the realization of an integrated multi-material airborne pressure vessel for long-term storage of nitrogen, in particular, a halon-free fire extinguishing system employing water-mist and nitrogen.

TRINITI’s tank has been conceived to fulfil technical requirements foreseen by the CfP e.g. very low permeation of gases, mechanical loads according to RTCA Do160 Rec. G, good fire-smoke-toxicity (FST) properties, survival of high temperatures, large temperature gradients, as well as resistance against various chemical media.

Demonstration multi-material thermoplastic tanks will be fabricated through a combination of processes such as co-extrusion of thermoplastic materials to form a multi-layer and multifunctional thermoplastic material, followed by In-situ consolidation Laser-Assisted Automated Fiber Placement process.

The application of highly performing thermoplastic materials combined with advanced automated and out-of autoclave technologies on the one hand will answer to the need for less consuming and faster manufacturing processes (1 stage process), while on the other hand it will ensure reduced weight of the tank, reduced operational costs as well as reduced fuel consumptions and emissions of an aircraft.

TRINITI's linerless tank, thanks to the versatility of the Laser assisted AFP antropomorphic robot and possibility to use a dedicate simulation tool to optimise the design of the vessel, is expected to range not less than 10% lighter than their nearest Type IV tanks.

A better weight-to-tank capacity ratio, however, is not the only advantage of the high-pressure vessel, in fact a significant manufacturing cost flow reduction is expected mainly because the chain of manufacturing processes will be optimized and number of fabrication stages will be reduced.

Consortium will aim to reach at the end of the project TRL 6.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.6. - ITD Systems
Other Programme
JTI-CS2-2018-CfP09-SYS-01-14 - Multi-Material Thermoplastic high pressure Nitrogen Tanks for Aircrafts

Partners

Lead Organisation
Organisation
Novotech Aerospace Advanced Technology Srl
Address
VIA COSTANZI 3, 74024 MANDURIA (TA), Italy
EU Contribution
€228 075
Partner Organisations
Organisation
Ctl Tastail Teoranta Limited
Address
UDARAS INDUSTRIAL ESTATE, GALWAY, Ireland
Organisation website
EU Contribution
€166 425
Organisation
Centro Di Ricerche Europeo Di Tecnologie Design E Materiali
Address
Strada Statale 7 Per Mesagne Km 7.3, 72100 Brindisi, Italy
Organisation website
EU Contribution
€255 500

Technologies

Technology Theme
Unclassified
Technology
Non-technology
TRL
TRL 6
Development phase
Demonstration/prototyping/Pilot Production

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