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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.

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

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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