Hola,
¿eres nuevo aquí?

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

Tengo cuenta

Regístrate

Ver video

TAILTEST

Financiado

Cerrado

Development of a multipurpose test rig and validation of an innovative rotorcraf...

Development of a multipurpose test rig and validation of an innovative rotorcraft vertical tail The overall objectives of TAILTEST project are to perform structural tests to support the certification process of a rotorcraft tail and to develop and validate advanced numerical models for the simulation of debonding propagation... ver más

31/12/2023

VZLU

697K€

Presupuesto del proyecto: 697K€

Líder del proyecto

VYZKUMNY A ZKUSEBNI LETECKY USTAV AS 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 2 Participantes

Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2023-12-31

JTI-CS2-2018-CFP09-AIR-02-74: Development of a multipurpose test...

I+D

Cerrada hace 5 años

0% 100% 100%

Información adicional privada

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

2 Participantes

VZLU

440.50K€ | Lider

ATHENA - RESEARCH AND INNOVA...

256.25K€ | 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

AMTRAS Adaptive Multifunctional Test Rigs for Aeronautical Structur... 349K€ Cerrado

OUTCOME The outstanding challenge in solid mechanics engineering st... 2M€ Cerrado

ELEMENT CROR Engine debris Middle level Impact and Mechanical test 528K€ Cerrado

DPI2017-89197-C2-2-R TALADRADO DE COMPONENTES HIBRIDOS CFRPS/TI Y TOLERANCIA AL D... 88K€ Cerrado

WISDOM WING STRUCTURAL TEST DEVELOPMENT METHOD 3M€ Cerrado

DAHLIAS Development and application of hybrid joining in lightweight... 1M€ Cerrado

Duración del proyecto: 51 meses Fecha Inicio: 2019-09-19
Fecha Fin: 2023-12-31

Líder del proyecto

VYZKUMNY A ZKUSEBNI LETECKY USTAV AS No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 697K€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto The overall objectives of TAILTEST project are to perform structural tests to support the certification process of a rotorcraft tail and to develop and validate advanced numerical models for the simulation of debonding propagation in structural joints. A multipurpose test rig is required to serve the purposes of performing rotorcraft vertical tail structural tests, as well as, testing of representative structural joints (e.g. fin spar to skin). The starting point of the technical developments of TAILTEST will be the design and manufacturing of this multipurpose test rig. The results of the tests performed using the multipurpose test rig will have triple use: • they will support the certification process of the innovative fin, (testing of the innovative fin) • they will be used for the validation of the fin global FE model and • they will contribute to the investigation of stiffness and strength of novel joining technologies (testing of novel hybrid joint concepts). One key characteristic required by the test rig design is that the test rig will have variable stiffness, such that the actual behaviour of the fuselage at which the fin will be attached will be properly emulated. Having the test rig available, structural tests at sub-scale level will be performed, by incorporating the minimum amount of modifications at the test rig design. In this way, the multipurpose test rig will be exploited to the sub-scale level testing, too. Results of the tests at sub-component level, e.g. fin spar to skin hybrid joints, will facilitate the validation of advanced numerical models, which will be developed for predicting the debonding at the hybrid joint. These numerical models will be applied in the simulation of static and fatigue crack growth (debonding) of bonded composite joints. The model’s input parameters will be obtained from experimental tests on coupon level.

Conecta tu I+D

Entra hoy

¿Olvidé mi contraseña?

Financiación

Empresas

CTIs/Universidades

Proyectos

Investigadores