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Romain COËMET

Blagnac

En résumé

During 5 years, I studied mechanical engineering at school and I developped my skills in international companies through internships. The last year,I spent 6 months in Sherbrooke University (Canada) where I had the opportunity to extend my competences in project management and development.

After these multiple experiences, I integrated Airbus Operations in order to take part to the development of the A350, first composite fuselage aircraft. Based on my 4 years mission for this program, I have built solid background in composite structure analysis.
That's why I moved recently to the new Beluga XL program in order to open my knowledge to different flying structures compared to what I knew before. On top, this mobility is fully in line with the company strategy and the global market regarding the development of multi-skills and networking.

Mes compétences :
Aéronautique
Mécanique
Ingéniérie
Matériaux composites
Maintenance
Résistance des matériaux
Modélisation
Calcul mécanique
Design industriel
Test

Entreprises

  • Airbus Group - Metallic Structure Stress Engineer

    Blagnac 2015 - maintenant Within the new Beluga XL program, I am working for structure assembly work package. Main objective of the team is to design and stress all structure parts between A330 baseline and the bubble on top of the fuselage.
    In order to ensure robust design and stress in front of airworthiness autorities, test pyramid including tests of structure sub-components and full scale tests (ground tests, flight tests) has been agreed.
    I am involved on all tests items relevant to the structure parts under responsability of the work package I am working for. My mission is to follow on stress side all these activities in order to be compliant with airworthiness requirements and to secure program global planning.

  • Airbus Group - Repair Stress Engineer - Composite Structure

    Blagnac 2011 - 2015 Repairs and robustness activities related to A350 Development
    - method and tools development via stress analysis and test correlation
    - definition of Allowable Damage Limit (scratch, lightning strike) / Leader of ADL activities for method and tools development
    - sizing process and method development/improvement as regards bolted repair
    - test follow-up for robustness demonstration of bonded reworks

  • STELIA Aerospace - Composite MAP Engineer

    Colomiers 2010 - 2010 Internship in new MAP team dedicated to preparation of A350 Nose Fuselage entry into production.

    Main activity:
    - Identify all recurrent production non conformity topics on composite structure
    - Provide quick stress assessment and way forward for repair
    - Create the first composite repair hand-book for blue collar on production line gathering all required information to solve recurrent non conformity in order to improve lead time, cost and quality.

  • LMS International - Structure Analysis Engineer

    Paris 2009 - 2009 Internship in international environment. ­

    Static and modal analysis of a composite aircraft (A350) on FE model
    Working on MAAXIMUS project led by AIRBUS

  • FINIMETAL - Intern / Computing department

    2008 - 2008 Summer Job

    Mission:
    - Data management
    - Industrial drawing (SolidWorks)

  • Air France Industry - Intern / Maintenance department for Ground Vehicle

    Roissy CDG 2007 - 2007 Assist mechanical blue collar on Ground Vehicle maintenance

    Missions:
    - engine check
    - engine maintenance
    - engine repair
    - engine installation

Formations

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