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Guévenoux Camille


Office : 3:20-02&C
Department/Laboratory/Direction : CA/DER/LAB/LMS

Biography and Current Works


PhD Student at the Laboratoire de Mécanique des Solides (LMS) and Safran Tech (CIFRE thesis) since February 2018 working on the fatigue of components repaired using laser cladding.


Advisors : Andrei Constantinescu (LMS), Eric Charkaluk (LMS) and Alexandre Charles (Safran Tech).




2018 : Start of PhD thesis with LMS and Safran Tech

2017 : Internship at Safran Aircraft Engines (Villaroche, France) working on a HCF criterion including scale effect for single-cristal blades

2016-2017 : Master of Science in Aerospace Engineering at KTH (Stockholm, Sweden)

2016 : Internship at PSA group on the fatigue of thermoplastics reinforced with short glass fibers

2013-2016 : Engineering degree at Ecole polytechnique




TD de mécanique des milieux continus (L3 et M1) à l'Université Pierre et Marie Curie (Sorbonne Universités), enseignants : Hélène Dumontet, Amâncio Fernandes.

TD du cours Fatigue des Matériaux et des Structures (2ème année de cycle ingénieur) à l'ENSTA, enseignant : Habibou Maitournam.



PhD thesis: High-Cycle Fatigue of components repaired using laser cladding.



Abstract :


Due to the rising price of energy and the scarcity of metal resources, the repair of metal parts is of paramount importance for many industries. An additive manufacturing process, the Laser Cladding or Laser Metal Deposition (LMD), allows to locally repair worn parts for repair. As for any manufacturing or repair process, the microstructures induced by the LMD are very dependent on the parameters chosen and these microstructures have a direct impact on the mechanical properties obtained. This thesis will focus on the link between microstructure and fatigue performance of repaired parts. This aspect still little mentioned in the literature is however a prerequisite for the deployment of repair by Laser Cladding on a large scale. An experimental part on repaired specimens will be used to characterize the microstructure in the repaired zone and to identify the damage phenomena responsible for HCF failure. In order to describe the microstructure at the interface between the initial part and the repaired area, a gradient fatigue criterion will be calibrated via a dialogue between experimental results and simulations.

Main Publications and Links

HAL Publications: 


Publications HAL: 

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