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Giusi TERRIZZI

TOULOUSE

En résumé

Hi,
During my first important professional experience I work to ALENIA SPACE (to Torino), for the advanced studies team. This first contact with the aerospace world allowed me to improve to work on a team and to complex projects.
My professional iter shows my curiosity and my ability to adapt: I start as thermal-analyst to become stress engineer by several dynamic experiences.
My most important aeronautical experience is at A400M nose fuselage systems integration. It has permitted to me to use my experience on vibration environment. More I add at my curriculum, a new methodology necessary for the systems integration and to have a global view on the steps necessaries to certification phase. During this mission I demonstrated initiative, effectiveness and capability to give some solutions when necessary.

I thank you for your kind attention and look forward to hearing from you.
Giusi TERRIZZI



Mes compétences :
NASTRAN
Airbus A380/A400M/A320NEO/A350 Aircrafts
Patran
Systems integration
Dynamic and static analysis
UNIX
SAP
Aircraft Structures

Entreprises

  • GECI - Engenieur calcul

    maintenant

  • GECI France Group - Stress engineer

    2014 - maintenant Pylon A320 NEO: systems and structure

  • GECI to behalf AIRBUS - Stress analyst

    2012 - 2013 AIRBUS - A350 Program - APF structure stress analysis- GECI [
    APF is a secondary structure of pylon, submitted to a severe thermo-dynamic environment:
    very high temperature and very specify pressure blow out from engine.

    Main tasks:

    - Analysis: thermo-mechanical and sonic fatigue of several configurations, in order to
    choose the best one in term of shape deformation and mechanical performance.

  • GECI to behalf AIRBUS - Dynamic and stress analyst

    2009 - 2013 A400M Program - Systems installation (nose section) - On site [
    Responsible for the follow up of the sub-contracting activity with LATELEC (Latécoère) and
    SNCentrair companies. In charge of the mechanical study of the following cockpit systems:
    Arinc electrical racks, panel floor and lining system (AEROSUD).

    Main tasks:

    - Delivery of Airbus input data (ground and flight loads, abuse loads, decompression,
    methods of calculation, Airbus requirements)
    - Checking of sub-contractor `s output work in accordance with specifications, methods and
    delays - checking of justification/certification stress reports
    - Validation of calculated components (numerical modelling and hand calculations) ;
    - Interface with the drawing and stress departments at Airbus for the definition of conflicting
    components
    - Interface with Airbus primary structure departments (cockpit) ;
    - Study of systems integration with the aircraft structure: dynamic behaviour of the systems
    connected with the aircraft primary structure (windmilling requirement) and static
    calculations of the interfaces

  • GECI to behalf AIRBUS - Dynamic and stress analyst

    2004 - 2008 A350 Program & IPAS - Engine Loads Department - on site [
    - Integration of typical design AIRBUS pylon into new resized engine: A30X A/C ;
    - Sensitivity study about several pylon configuration for A350 A/C Dynamic analyses of
    IFEM
    - Optimization of procedure to analyse the tip clearance for engine performance study ;
    - Feasibility study of several pylon design for new aircraft: IAPA and A330HGW ;
    - Numerous French or English results' presentations

  • GECI to behalf AIRBUS - Dynamic analyst

    2002 - 2004 A380 Program - Engine Loads Department - on site [
    - Dynamic sizing and optimization of thrust links system of EA GP7200 and RR TRENT900
    engines
    - Dynamic test on interface engine - pylon of A380 (Thrust Link) ;
    - Correlation of analysis and test results ;
    - Analyses of Out of Balance test on TRENT900 engine thrust link by MATLAB S/W ;
    - Numerous French or English results' presentations

  • GECI to behalf ASTRIUM - Dynamic engineer

    2001 - 2002 FEM modelling of parts of satellite platform ;
    - Dynamic sizing (modal, sinus, notching, random analyses) ;
    - Thermo-elastic analysis during orbit phase. ;
    - Redaction of English technical reports

  • GECI - Thermo-mechanical engineer

    2000 - 2001 Pre-analysis and detailed thermal analysis for qualification and acceptance processes of
    electronic boxes for Eurostar 3000.
    - Resetting mechanical model to tests for SNECMA project (STENTOR)

  • ALENIA SPAZIO - Thermo-Mechanical analyst

    1998 - 2000 LISA: (Laser Interferometer Space Antenna) Mechanical analyst for optical bench madden
    with not-conventional materials: dynamic and static analysis with ANSYS S/W
    - MERCURY: Mechanical analyst for instrument plate in the satellite: thermo-elastic
    analysis with NASTRAN S/W
    - AEVI: Mechanical analyst in not linear field with ANSYS S/W and dynamic analysis for the
    Columbus case with PATRAN pre and Post-Processor and NASTRAN S/Ws
    - GOCE: Scientific satellite as thermo analyst (steady state analysis with THERMICA and
    ESATAN S/W


    OTHER EXPERIENCES, TRAINING PERIODS

  • ALENIA SPAZIO - Stage

    1996 - 1996 Training at ALENIA Spazio in Turin (Advanced Studies Group): space capsule thermal control
    design during renter, in order to carry out a thesis in aerothermodynamics

Formations

  • Università Degli Studi Di PALERMO DIPARTIMENTO D'AERONAUTICA (Palermo)

    Palermo 1990 - maintenant BAC+5

  • Università Degli Studi Di PALERMO (Palermo)

    Palermo 1990 - 1996 Laurea Ingegneria Aeronautica

    BAC+5

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