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HEGEL SIGNED

High Cycle Fatigue Prediction Methodology for Fibre Reinforced Laminates for Aircraft Structures in CROR Environment – Development and Validation

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

HEGEL project word cloud

Explore the words cloud of the HEGEL project. It provides you a very rough idea of what is the project "HEGEL" about.

architectures numerical tools heating influence methodology laminates demonstrated configurations achievement materials performance virtual loading composite structure environment source final validated accomplishment extensive curves cfrp amplification integration ibp environmental frequency sound cycle life meet shift structures hcf tackled experimental enhanced pressure framework integrity consist physical aerospace designed outcome successively master phenomena aero representative specifications fatigue self predictive dependent accelerated structural manufactured safety community iadp certification delivered models expanded fraunhofer subjected cror fe validating prediction

Project "HEGEL" data sheet

The following table provides information about the project.

Coordinator	TWI LIMITED Organization address address: GRANTA PARK GREAT ABINGTON city: CAMBRIDGE postcode: CB21 6AL website: www.twi.co.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	United Kingdom [UK]
Total cost	399˙842 €
EC max contribution	399˙842 € (100%)
Programme	1. H2020-EU.3.4.5.1. (IADP Large Passenger Aircraft)
Code Call	H2020-CS2-CFP03-2016-01
Funding Scheme	CS2-IA
Starting year	2017
Duration (year-month-day)	from 2017-02-01 to 2020-01-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	TWI LIMITED TWI LIMITED Organization address address: GRANTA PARK GREAT ABINGTON city: CAMBRIDGE postcode: CB21 6AL website: www.twi.co.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (CAMBRIDGE)	coordinator	108˙130.00
2	STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM Organization address address: Anthony Fokkerweg 2 city: AMSTERDAM postcode: 1059CM website: www.nlr.nl contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	NL (AMSTERDAM)	participant	189˙996.00
3	UNIVERSITEIT TWENTE UNIVERSITEIT TWENTE Organization address address: DRIENERLOLAAN 5 city: ENSCHEDE postcode: 7522 NB website: www.utwente.nl contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	NL (ENSCHEDE)	participant	98˙262.00
4	UNIVERSITY OF BRISTOL UNIVERSITY OF BRISTOL Organization address address: BEACON HOUSE QUEENS ROAD city: BRISTOL postcode: BS8 1QU website: www.bristol.ac.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (BRISTOL)	participant	3˙454.00

Map

Project objective

The aim is to develop high cycle fatigue (HCF) testing capabilities for composite materials to study the long-term fatigue life of composite laminates used in new structural architectures subjected to high sound pressure loading in CROR environment.

The achievement of the overall project aim will be tackled through the accomplishment of two technical objectives: developing a sound source and amplification system representative of the high sound pressure generated by the CROR; developing and validating an enhanced accelerated fatigue prediction methodology framework to HCF life prediction of CFRP laminates used in the new aero-structures configurations in CROR environment.

Concepts for the sound source and amplification system will be designed according to the specifications. The best concept will be demonstrated and validated and successively the system will be manufactured and delivered to Fraunhofer IBP. The development of the methodology framework for HCF prediction of CFRP materials will be achieved through extensive experimental testing, physical analysis and numerical FE modelling activities. Following on from existing approaches, the final outcome of the project will be an expanded methodology framework for HCF prediction of CFRP laminates able to take into account the influence of environmental conditions as well as the presence of frequency dependent phenomena (e.g self heating). The framework will consist of fatigue models based on fatigue master curves and shift as well as FE predictive models that can be used as virtual assessment tools for HCF performance of CFRP materials.

The immediate impact of the project will be providing the IADP’s Partners and the aerospace community with advanced testing capabilities to facilitate the design process and the structural integrity assessment of the new aero-structure configurations as result of the CROR integration in order to meet safety and certification requirements.

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The information about "HEGEL" are provided by the European Opendata Portal: CORDIS opendata.