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TRINIDAT SIGNED

Tilt Rotor INlet Innovative Design And Testing

Total Cost €

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EC-Contrib. €

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Partnership

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 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.

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

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

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