Opendata, web and dolomites

TRIcEPS SIGNED

Tilt Rotor Integrated Air Intake and Engine Protection Systems

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

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

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.

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "TRICEPS" project.

For instance: the website url (it has not provided by EU-opendata yet), the logo, a more detailed description of the project (in plain text as a rtf file or a word file), some pictures (as picture files, not embedded into any word file), twitter account, linkedin page, etc.

Send me an  email (fabio@fabiodisconzi.com) and I put them in your project's page as son as possible.

Thanks. And then put a link of this page into your project's website.

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

More projects from the same programme (H2020-EU.3.4.5.3.)

RoCS (2019)

Rotorcraft Certification by Simulation

Read More  

SMAR-TeR (2019)

Next Generation of SMARt Active Inceptor for Tilt Rotor Application

Read More  

ELECTRA (2019)

Efficient and Light Electrical Compressor for Tilt-Rotor Aircraft

Read More