Pasquale CERULLO

En résumé

Entreprises

• Aerosoft - Stress Analyst Engineer

  2015 - maintenant Project: "A350/900 Batch 3"

• Airbus - Stress Analyst Engineer

  Blagnac 2013 - 2014 Project: ``A330/340''
  Description: Fatigue and Damage Tolerance Widespread Issue 4.0, maintenance
  documents redaction.
  * Lateral frame/lower frame splicing - Rod floor attachment -
  Fatigue analysis in consideration of fastener hole modification (Interference) using
  SAFE models (Joint).
  Damage Tolerance Analysis in accordance with Widespread Issue 4. DT analysis
  using SAFE models ( CC02, AR01, TC03, Plate-n-holes).
  * Junction between CWB and passenger floor - Damage Tolerance Analysis in
  accordance with Widespread Issue 4. DT analysis using SAFE models ( CC03+TC04
  (LUG), CC02, AR01, TC03, Plate-n-holes). Severe Turning Cases consideration.
  * Upper cross junction - stress extraction, F&DT calculation in accordance with
  Widespread Fatigue Damage.
  * Equivalent stress extraction: ACSA, PSN-Tool, Macro_Moulinette. ;
  * IRD redaction: redaction of new Inspection Requirement Dossier as result of
  Widespread.
  * Grace Period: justification to shift the value of Threshold Fatigue Inspection for the
  airlines companies and technical note redaction.
  Software: SAFE, Excel, ACSA, PSN tools, VBA

• Sogeclair - Stress Analyst Engineer

  BLAGNAC 2012 - 2013 Project: ``A350-900 CWB''
  Description:
  * External Foot Frames for FFR - Equivalent Stress Calculation: STF run on GISEH,
  Macro GENE, Macro Spectre. F&DT Analysis using ISAMI models (Plate Hole, L-
  Section, Corner Crack).
  * Typical Ribs - Loads extraction by PSN13 tool and customer tool for SMM10.
  Equivalent Stress Calculation: STF run, Macro GENE, Macro Spectre.
  Software: ACSA, PSN13, ISAMI, Excel, VBA.

• Aerolia S.p.A. - Stress Analyst Engineer

  2012 - 2012 Project: ``Nose Fuselage A400M''
  Description: My task is checking report and analyzing the critical cases. I use software
  like SAFE and Product View. Furthermore I check also the certification document by
  ACD4. The main components that I checked are the elements of the Nose Fuselage, for
  example Crew Entrance Door and Frame Splicing.
  Software: SAFE, Product View, Office (Excel, Word).

• Aerosoft S.p.A. - Stress Analyst Engineer

  2011 - 2012 Project: ``A350XWB MLGB''
  Description: I worked on fatigue and damage tolerance analysis of components of the
  Main Landing Gear Bay. My principal task was Triangular Panel F&DT analysis and
  relative document redaction.
  Software: MSC Patran, MSC Nastran, Excel, ISAMI.

• Aerosoft S.p.A. - Stress Analyst Engineer

  2011 - 2011 of job Activity: ``Stress Analyst Training''
  Description: Training on job on SW Patran/Nastran and application of concepts learned
  about Aeronautics projects for the Alenia Aeronautica Customer. I learned to use the
  Isami, SAFE and CATIA V5.
  Software: Windows, MSC Patran, MSC Nastran, Office (Excel, Word), CATIA V5.

Formations

• Università Federico II Di Napoli

  Naples 2003 - 2010 Master's Degree

Réseau

• Adeline PERRINELLE

• Delphine ACHARD

• Marion THIBEAUT GUILLOU

• Sandrine EYMERY