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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.

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

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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