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Opendata, web and dolomites

TRINIDAT SIGNED

Tilt Rotor INlet Innovative Design And Testing

Total Cost €

EC-Contrib. €

Partnership

Views

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.

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

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 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.	NL (AMSTERDAM)	coordinator	733˙822.00
2	DEHARDE GMBH DEHARDE GMBH Organization address address: AM HAFEN 14A city: VAREL postcode: 26316 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (VAREL)	participant	1˙011˙403.00
3	STICHTING DUITS-NEDERLANDSE WINDTUNNELS STICHTING DUITS-NEDERLANDSE WINDTUNNELS Organization address address: VOORSTERWEG 31 city: Marknesse postcode: 8316 PR website: www.dnw.aero contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	NL (Marknesse)	participant	802˙300.00
4	ALTRAN DEUTSCHLAND SAS & CO KG ALTRAN DEUTSCHLAND SAS & CO KG Organization address address: FRANKFURTER RING 81 city: MUNCHEN postcode: 80807 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (MUNCHEN)	participant	422˙156.00
5	UNIVERSITEIT TWENTE UNIVERSITEIT TWENTE Organization address address: DRIENERLOLAAN 5 city: ENSCHEDE postcode: 7522 NB website: www.utwente.nl contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	NL (ENSCHEDE)	participant	233˙426.00
6	AIRCRAFT DEVELOPMENT AND SYSTEMS ENGINEERING (ADSE) BV AIRCRAFT DEVELOPMENT AND SYSTEMS ENGINEERING (ADSE) BV Organization address address: SCORPIUS 90 city: HOOFDDORP postcode: 2132 LR website: www.adse.nl contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	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.