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CROR Engine debris Middle level Impact and Mechanical test

This project focus on the analysis of different shielding configurations to protect a rear-end structure of an open rotor aircraft from an engine failure. The analysis will be performed against simple panels in the first place. Th... ver más

28/02/2021

UC3M

528K€

Presupuesto del proyecto: 528K€

Líder del proyecto

UNIVERSIDAD CARLOS III DE MADRID No se ha especificado una descripción o un objeto social para esta compañía.

Total investigadores 1335

Fecha límite participación Sin fecha límite de participación.

Ver 2 Participantes

Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2021-02-28

JTI-CS2-2015-CFP02-AIR-01-08: CROR Engine debris Middle level Imp...

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Información adicional privada

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

2 Participantes

UC3M

99.33K€ | Lider

VAZQUEZ Y TORRES INGENIERIA

299.74K€ | Participante

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Duración del proyecto: 56 meses Fecha Inicio: 2016-05-30
Fecha Fin: 2021-02-28

Líder del proyecto

UNIVERSIDAD CARLOS III DE MADRID No se ha especificado una descripción o un objeto social para esta compañía.

Total investigadores 1335

Presupuesto del proyecto 528K€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto This project focus on the analysis of different shielding configurations to protect a rear-end structure of an open rotor aircraft from an engine failure. The analysis will be performed against simple panels in the first place. The best configurations will then be studied as aircraft representative structures. Two different types of impactor will be considered from the engine failure, a metallic fragment (which will be related to an engine core part) and a composite fragment (which represents the failure of the blade). There are two overarching objectives in this project. The first one is to validate the maturity level of different technologies and structural solutions, to protect the rear-end structure from different impacts associated to engine failure. To this end both real and virtual impact tests of debris associated with the open rotor engine failure will be performed. The second objective of this project is to advance in the development of virtual testing methodologies. The economic impact of performing real experimental tests for the aircraft companies is very high, and virtual testing could diminish the number of experimental tests (and hence their economic impact). Both numerical and experimental approaches will be taken into account. Experimental tests will be performed by means of a pneumatic launcher, in order to achieve the impact velocities representatives of such event; high speed cameras, strain gauges, and 3D digital image correlation will be used to obtain the maximum quantity of data from the tests. Once impacted, non-destructive techniques will be used to determine the type and extension of the damage. Numerical simulations of the impact process will be also performed; a complete numerical methodology will be developed in order to appropriately model the phenomenon. After validation with the experimental tests, the numerical model will be used to perform parametric studies.

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