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TRIcEPS SIGNED

Tilt Rotor Integrated Air Intake and Engine Protection Systems

Total Cost €

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EC-Contrib. €

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Partnership

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 TRIcEPS project word cloud

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

bypass    compressor    considering    bell    certification    protection    technologies    flight    operation    triceps    competitiveness    flow    cs2ju    fulfilling    right    air    qualifying    separation    demonstrator    particle    market    thermoelectric    protecting    layer    sub    barrier    stable    cfp08    fit    meet    aircraft    lower    cleaning    equipped    ice    removable    vortex    significantly    respect    mission    heater    iprs    designing    nextgenctr    supplying    frc    washing    2018    rotorcraft    emergency    left    cs2    trl    01    easier    patenting    filter    faa       infringe    helicopters    drop    securing    forget    actuation    maintenance    leonardo    blade    wp1    ing    profile    position    tilt    21    tubes    instead    geared    regional    industry    intake    reference    expose    intakes    icing    pressure    clean    efficiency    wing    jti    solution    compromise    self    ingestion    harsh    brownout    rotor    engine    environment    particles    goals    manufacturing    requiring    despite    full   

Project "TRIcEPS" data sheet

The following table provides information about the project.

Coordinator
AIT AUSTRIAN INSTITUTE OF TECHNOLOGY GMBH 

Organization address
address: GIEFINGGASSE 4
city: WIEN
postcode: 1210
website: http://www.ait.ac.at/

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 Austria [AT]
 Total cost 3˙281˙251 €
 EC max contribution 2˙614˙290 € (80%)
 Programme 1. H2020-EU.3.4.5.3. (IADP Fast Rotorcraft)
 Code Call H2020-CS2-CFP08-2018-01
 Funding Scheme CS2-IA
 Starting year 2019
 Duration (year-month-day) from 2019-05-01   to  2023-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    AIT AUSTRIAN INSTITUTE OF TECHNOLOGY GMBH AT (WIEN) coordinator 605˙065.00
2    PALL EUROPE LIMITED UK (PORTSMOUTH) participant 590˙803.00
3    CI COMPOSITE IMPULSE GMBH & CO DE (GEVELSBERG) participant 475˙266.00
4    RTA RAIL TEC ARSENAL FAHRZEUGVERSUCHSANLAGE GMBH AT (WIEN) participant 311˙838.00
5    VILLINGER GMBH AT (MIEDERS) participant 241˙062.00
6    PRIME AEROSTRUCTURES GMBH AT (KLOSTERNEUBURG) participant 216˙256.00
7    VYZKUMNY A ZKUSEBNI LETECKY USTAV AS CZ (PRAHA 18) participant 174˙000.00

Map

 Project objective

TRIcEPS aims at fulfilling all the requirements of the JTI-CS2-2018-CfP08-FRC-01-21, “Development of integrated engine air intake and protection systems for Tilt Rotor” by designing, manufacturing, testing and qualifying the left-hand and the right-hand side air intakes and their integrated engine protection system for the NextGenCTR technology demonstrator, contributing to meet the goals of the CS2JU FRC WP1. The proposed engine protection system is geared on two key enabling technologies: • a removable thermoelectric ice protection system based on the heater layer technology. This is already under development on the blade of the NextGenCTR and on the wing of the regional aircraft; • a vortex tubes filter for protecting the engine from ingestion of particles in harsh environment. The air intake will be equipped with a bypass for operation in clean flow and a compressor washing system. The choice of a vortex tubes instead of a barrier filter is key in TRIcEPS. This solution, despite providing 1-to-2% lower particle separation efficiency, allows for: • full self-cleaning capabilities, thus not requiring maintenance (i.e. fit and forget approach); • stable pressure drop in brownout operation, resulting in no need of emergency bypass actuation which would expose the engine to the harsh environment; • significantly reduced icing issues; • easier flight certification path, according to FAA; resulting in the best technical compromise for the NextGenCTR considering its mission profile. Moreover, this choice does not to infringe IPRs on tilt rotor air intake (as per patenting activities by Bell Helicopters on barrier filter), thus securing the position of Leonardo with respect to the future market. TRIcEPS will deliver the air intake, its engine protection system and all the relevant sub-systems at TRL 7, supplying Leonardo with the reference technical solution for engine protection of the NextGenCTR, strengthening the competitiveness of the European rotorcraft industry.

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

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