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TRINIDAT

Financiado

Cerrado

Tilt Rotor INlet Innovative Design And Testing

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 hig... ver más

30/04/2022

Royal Netherlands...

3M€

Presupuesto del proyecto: 3M€

Líder del proyecto

STICHTING KONINKLIJK NEDERLANDS LUCHT EN RUI... No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Fecha límite participación Sin fecha límite de participación.

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Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2022-04-30

JTI-CS2-2018-CfP08-FRC-01-23: Experimental characterization and o...

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No hay información privada compartida para este proyecto. Habla con el coordinador.

6 Participantes

Royal Netherlands Aerospace...

945.39K€ | Lider

UNIVERSITEIT TWENTE

182.30K€ | Participante

DEHARDE GMBH

1.01M€ | Participante

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Duración del proyecto: 38 meses Fecha Inicio: 2019-02-26
Fecha Fin: 2022-04-30

Líder del proyecto

STICHTING KONINKLIJK NEDERLANDS LUCHT EN RUI... No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 3M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto 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 39 months for a total budget of 3,346,397€.

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