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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.

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

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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