Hola,
¿eres nuevo aquí?

Regístrate gratis y conecta tu empresa con financiación pública, partners y proyectos.

Tengo cuenta

Regístrate

Ver video

ITURB

Financiado

Cerrado

Optimal High Lift Turbine Blade Aero Mechanical Design

"The need for high speed low pressure turbine modules to be used with innovative aircraft engine concept establishes critical mechanical constraints with very high hub stresses for the rotor blades, thus representing a real challe... ver más

30/06/2015

UNIGE

839K€

Presupuesto del proyecto: 839K€

Líder del proyecto

UNIVERSITA DEGLI STUDI DI GENOVA No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Fecha límite participación Sin fecha límite de participación.

Ver 3 Participantes

Financiación concedida El organismo FP7 notifico la concesión del proyecto el día 2015-06-30 No tenemos la información de la convocatoria

0% 75% 100%

Información adicional privada

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

3 Participantes

UNIGE

0.00€ | Lider

UNIFI

N.D. | Participante

UNIPD

N.D. | Participante

Conecta tu I+D

¿Tienes un proyecto y buscas un partner? Gracias a nuestro motor inteligente podemos recomendarte los mejores socios y ponerte en contacto con ellos. Te lo explicamos en este video

Proyectos interesantes

FURADO Full Fairing Rotor Head Aerodynamic Design Optimization 399K€ Cerrado

ADHERO Aerodynamic Design Optimisation of a Helicopter Fuselage inc... 825K€ Cerrado

ANACO Advance Nacelle Aerodynamic Optimisation 2M€ Cerrado

EUIN2015-62882 OPTIMIZACION AERODINAMICA DE LA CABEZA DEL ROTOR 9K€ Cerrado

HElAIrcOPT Helicopter Engine Air Intake OPtimization Tool 530K€ Cerrado

CODE-TILT Contribution to design optimization of tiltrotor components... 894K€ Cerrado

Líder del proyecto

UNIVERSITA DEGLI STUDI DI GENOVA No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 839K€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto "The need for high speed low pressure turbine modules to be used with innovative aircraft engine concept establishes critical mechanical constraints with very high hub stresses for the rotor blades, thus representing a real challenge for the design. In order to assist the designer with reliable tools it is mandatory to assess the performance of turbine rotor blades of innovative concept with both numerical and experimental investigations. Starting from a baseline configuration, representative of the state-of-the-art of LPT high-lift rotor blades, an aerodynamic optimization will be performed exploiting modern optimization techniques. These techniques are based on the coupling between fast and flexible parametric handling of the geometries, CFD computations and meta-models like Artificial Neural Networks (ANN) or Radial Basis Functions (RBF). Such an approach will accomplish a multi-objective design aimed at enhancing the aerodynamic performance while meeting mechanical and geometrical constraints. Tests will be performed on both baseline and optimized rotors within a cold-flow, large-scale laboratory turbine. Tests on turbine configuration will ensure the reproduction of the correct radial equilibrium effects as well as of the rotor-stator aerodynamic interaction. The Reynolds number will be investigated in the range between 50000 and 300000, which represents the operative range of the LP rotor blades of the engine. The large scale of the facility will allow detailed aerodynamic investigations, and an accurate performance analysis. The numerical and experimental frameworks will allow one to validate and verify the optimized solution and to highlight the key features of the new design with respect to the baseline. The validation of the design and optimization procedures will be accomplished with the availability of detailed experimental data obtained for the innovative rotor blade row in a realistic environment."

Conecta tu I+D

Entra hoy

¿Olvidé mi contraseña?

Financiación

Empresas

CTIs/Universidades

Proyectos

Investigadores