Opendata, web and dolomites

TRINIDAT SIGNED

Tilt Rotor INlet Innovative Design And Testing

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

 TRINIDAT project word cloud

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

configuration    manufactured    helicopter    complementary    altran    cfd    intakes    supplied    efficient    ut    equipped    plane    off    rotatable    tilting    mode    geometry    total    purpose    put    rely    36    apart    engines    instrumented    airplane    shapes    intermediate    right    size    certification    6x6    reynolds    intake    budget    manufacturer    wind    anti    inlets    facilities    uniformity    industrials    deharde    extreme    engine    university    expertise    validation    landing    performance    346    397    steadiness    trinidat    generation    made    renowned    comply    final    left    tilt    snow    itd    tools    mach    ducts    remotely    redesigned    optimized    ngctr    months    geometries    flow    centres    designed    ice    input    air    inlet    basic    gathering    characterization    dnw    full    adse    optimization    initial    nlr    aerodynamic    model    nacelle    last    modular    installed    rotor    civil    icing    sme    rake    tests    llf    subsequently    adresses    tunnel   

Project "TRINIDAT" data sheet

The following table provides information about the project.

Coordinator
STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM 

Organization address
address: Anthony Fokkerweg 2
city: AMSTERDAM
postcode: 1059CM
website: www.nlr.nl

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 Netherlands [NL]
 Total cost 3˙346˙396 €
 EC max contribution 3˙346˙396 € (100%)
 Programme 1. H2020-EU.3.4.5.3. (IADP Fast Rotorcraft)
 Code Call H2020-CS2-CFP08-2018-01
 Funding Scheme CS2-RIA
 Starting year 2019
 Duration (year-month-day) from 2019-02-01   to  2022-01-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM NL (AMSTERDAM) coordinator 733˙822.00
2    DEHARDE GMBH DE (VAREL) participant 1˙011˙403.00
3    STICHTING DUITS-NEDERLANDSE WINDTUNNELS NL (Marknesse) participant 802˙300.00
4    ALTRAN DEUTSCHLAND SAS & CO KG DE (MUNCHEN) participant 422˙156.00
5    UNIVERSITEIT TWENTE NL (ENSCHEDE) participant 233˙426.00
6    AIRCRAFT DEVELOPMENT AND SYSTEMS ENGINEERING (ADSE) BV NL (HOOFDDORP) participant 143˙287.00

Map

 Project objective

The TRINIDAT project adresses the aerodynamic characterization of an already available intake geometry (as supplied by ITD) and optimization of the intake performance by using CFD based optimization tools leading to redesigned high performance intake shapes to be implemented on the Next Generation Civil Tilt Rotor (NGCTR) configuration. A purpose of the optimization is to improve the flow steadiness and uniformity at the Air Intake Plane of the engines such as to comply with the requirements put forward by the engine manufacturer. The initial characterization and optimization will rely on dedicated CFD studies, the final validation will be made with full size model tests in DNW-LLF 6x6 wind tunnel, allowing reliable testing at full scale Mach and Reynolds conditions. For efficient testing of basic and optimized left hand and right hand intake geometries in airplane, helicopter and intermediate Extreme Short Take-Off and Landing mode, a modular wind tunnel model equipped with a remotely controlled tilting forward nacelle part will be designed and manufactured. A remotely controlled highly instrumented rotatable rake will be installed in the model to enable detailed and efficient measurement of the flow at the engine air intake plane. Apart from the aerodynamic optimization of the intakes, the project will also identify icing and snow conditions to be considered for certification and will subsequently analyse the ice and snow effects on the nacelle inlets and ducts to provide early input for anti icing measures that might be needed for NGCTR. The partners of the consortium, gathering renowned Research Centres (NLR, DNW), 2 Industrials (Deharde, ALTRAN), 1 SME (ADSE) and 1 University (UT), will use their complementary expertise and facilities to provide an optimized inlet geometry for NGCTR, based on CFD and wind tunnel analysis, with high potential for certification in snow/icing conditions. The TRINIDAT project will last 36 months for a total budget of 3,346,397€.

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "TRINIDAT" 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 "TRINIDAT" are provided by the European Opendata Portal: CORDIS opendata.

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

SMAR-TeR (2019)

Next Generation of SMARt Active Inceptor for Tilt Rotor Application

Read More  

TRINIDAT (2019)

Tilt Rotor INlet Innovative Design And Testing

Read More  

RoCS (2019)

Rotorcraft Certification by Simulation

Read More