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.

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

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  

STEADIEST (2019)

Design, development and flight qualification of a supercritical composite shaft drive line for tiltrotor main drive system

Read More  

TRINIDAT (2019)

Tilt Rotor INlet Innovative Design And Testing

Read More