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Faculté des Sciences appliquées
Faculté des Sciences appliquées
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Final work : Modeling and analysis of composite pressure vessels

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Moreno Jiménez, Francesc Roger ULiège
Promoteur(s) : Bruyneel, Michaël ULiège
Date de soutenance : 26-jui-2023/27-jui-2023 • URL permanente : http://hdl.handle.net/2268.2/17745
Détails
Titre : Final work : Modeling and analysis of composite pressure vessels
Titre traduit : [en] Modeling and analysis of composite pressure vessels.
Auteur : Moreno Jiménez, Francesc Roger ULiège
Date de soutenance  : 26-jui-2023/27-jui-2023
Promoteur(s) : Bruyneel, Michaël ULiège
Membre(s) du jury : Ponthot, Jean-Philippe ULiège
Strepenne, François 
Langue : Anglais
Nombre de pages : 105
Mots-clés : [en] Pressure vessel
[en] Axisymmetric
[en] Carbon fiber
[en] Damage
[en] Delaminations
[en] FEM
[en] Hydrogen
[en] Burst pressure
[en] Burst mode
Discipline(s) : Ingénierie, informatique & technologie > Ingénierie aérospatiale
Organisme(s) subsidiant(s) : GDTech
Public cible : Chercheurs
Professionnels du domaine
Etudiants
Institution(s) : Université de Liège, Liège, Belgique
Diplôme : Master en ingénieur civil en aérospatiale, à finalité spécialisée en "turbomachinery aeromechanics (THRUST)"
Faculté : Mémoires de la Faculté des Sciences appliquées

Résumé

[en] In recent years, the use of green fuels such as compressed natural gas or hydrogen has increased enormously, so it has become necessary to improve their storage technology: pressure vessels, which must be as cheap as possible without compromising their structural integrity.
From this situation arises the need to develop models capable of faithfully predicting the behavior of the structure. Having a reliable damage and stress calculation model means being able to operate with lower safety factors, which reduces weight and costs.
During this project, the main objective will be to validate different approaches to address the problem. For this purpose, the finite element software Samcef will be used to predict damage propagation, especially in the dome region where the laminate becomes extremely complex.
The first iterations consist of a series of 2D axisymmetric models, 3D models where a single portion of the structure is modeled by implementing periodic boundary conditions, and a full 3D model that will serve as validation. Once a reliable model with low computational cost is available, different techniques will be implemented to predict the appearance and evolution of damage in the structure, so that it will be possible to predict both the burst pressure and the failure mode of the structure. Among these techniques are the classical failure criteria (Max. Stress, Tsai-Wu and Hashin), the advanced failure material models, which make use of an iterative calculation process in order to solve the problem in discrete times and thus, evaluate the degradation of the material and the appearance of plastic strains over time. Finally, the possible onset of delaminations will also be evaluated thanks to the use of cohesive elements.
Once it has been determined in which situation it is more convenient to use one or another of the previously generated models, a real case will be studied and an attempt will be made to predict the burst pressure and the failure mode. Subsequently, the limitations of the model generated during this project will be evaluated and improvements will be proposed in order to enhance its accuracy.


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Auteur

  • Moreno Jiménez, Francesc Roger ULiège Université de Liège > Master ingé. civ. aérospat., à fin. (THRUST)

Promoteur(s)

Membre(s) du jury

  • Ponthot, Jean-Philippe ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > LTAS-Mécanique numérique non linéaire
    ORBi Voir ses publications sur ORBi
  • Strepenne, François
  • Nombre total de vues 94
  • Nombre total de téléchargements 35










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