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MAAXIMUS

Financiado

Cerrado

More Affordable Aircraft structure through eXtended Integrated and Mature nUme...

More Affordable Aircraft structure through eXtended Integrated and Mature nUmerical Sizing Even though composite materials are more and more used in modern airframes, many significant improvements are still achievable. Firstly, the substitution of the assembly of many small composite parts by a single one-shot large par... ver más

30/09/2016

LHT

65M€

Presupuesto del proyecto: 65M€

Líder del proyecto

LUFTHANSA TECHNIK AKTIENGESELLSCHAFT No se ha especificado una descripción o un objeto social para esta compañía.

Fecha límite participación Sin fecha límite de participación.

Ver 53 Participantes

Financiación concedida El organismo FP7 notifico la concesión del proyecto el día 2016-09-30 No tenemos la información de la convocatoria

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53 Participantes

LHT

0.00€ | Lider

LUH

N.D. | Participante

IST

N.D. | Participante

IMA

N.D. | Participante

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Líder del proyecto

LUFTHANSA TECHNIK AKTIENGESELLSCHAFT No se ha especificado una descripción o un objeto social para esta compañía.

Presupuesto del proyecto 65M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto Even though composite materials are more and more used in modern airframes, many significant improvements are still achievable. Firstly, the substitution of the assembly of many small composite parts by a single one-shot large part provides additional weight reduction. Secondly, the final assembly line process must be adapted to composite properties (lack of ductility, stiffness). Thirdly, if the appropriate level of confidence and cycle time was available, Simulation-based design would provide a faster and less expensive path to find the optimal structures than the current development process, which relies on physical tests. Lastly, more conductive composites are necessary to avoid additional weight for system protection. The aim of MAAXIMUS (More Affordable Aircraft structure through eXtended, Integrated, & Mature nUmerical Sizing) is to demonstrate the fast development and right-first-time validation of a highly-optimised composite airframe. The MAAXIMUS objectives related to the highly-optimised composite airframe are: 50% reduction of the assembly time of large composite sections; 10% reduction of manufacturing & assembly recurring costs; 10% reduction of the structural weight. The MAAXIMUS objective related to a faster development is to reduce by 20% the current development timeframe of aircraft structures and by 10% the corresponding cost. The MAAXIMUS objective related to the right-first-time structure is to additionally reduce the airframe development costs by 5% through the delivery of a predictive virtual test capability for large composite structures with a quantified level of confidence, to avoid late and costly changes This will be achieved through coordinated developments on a physical platform, to develop and validate the appropriate composite technologies for low weight aircraft and a virtual structure development platform, to identify faster and validate earlier the best solutions through major improvements in airframe Simulation-base design.

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