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Airbus
- A330neo pylon FDT Leader
Blagnac
2014 - maintenant
Transverse Lead on A330-800/900 neo Pylon and Engine Mounts . Managing an co ordinating all the FDT work involved in development and certification phases. This involves technical support, deliverables approval and authorisation, full scale fatigue tests follow up and regular discussions with partners to ensure the F&DT work submitted is in line with Airbus standards.
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Airbus
- FDT stress engineer
Blagnac
2012 - 2014
Transverse Lead F&DT Engineer on A350 Flight Controls (Ailerons, Spoilers, Drop Panel). Managing the FDT work submitted by RSPs and suppliers on the different packages. This involves technical support, deliverables approval, fatigue tests follow up and regular discussions with partners to ensure the F&DT work submitted is in line with Airbus standards.
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Airbus
- A350 Aileron FDT Leader
Blagnac
2012 - 2014
A350 Flight Controls: Ailerons, Spoilers, Drop Panel (Airbus Fr)
(32 months)
Transverse Lead F&DT Engineer on A350-900/1000 Flight Controls (Ailerons). Managing the FDT work submitted to RSPs and suppliers (TAI and Altran) on the different packages. This involves technical support, deliverables approval and authorisation, full scale fatigue tests follow up and regular discussions with partners to ensure the F&DT work submitted is in line with Airbus standards.
Attending A350-900 Type Certification reviews with the authorities (EASA).
Writing up and compiling certification documents (ACDs, IRDs).
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Airbus
- A350 root joint FDT Integrator
Blagnac
2010 - 2011
A350 Root Joint (placement at Airbus UK on behalf of ATKINS)
(12 months) F&DT A350 Root Joint Integrator.
Co ordinating the F&DT analyses work of the different partners involved in the Root Joint design (GKN, Spirit, Airbus North America, Airbus France and Airbus UK). This was involving technical support and regular discussions with the partners to ensure that the F&DT work submitted was in line with Airbus standards (harmonised methods).
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Airbus
- A350 Root Joint FDT Integrator
Blagnac
2010 - 2011
Co ordinating the F&DT analyses work of the different partners involved in the Root Joint design (GKN, Spirit, Airbus North America, Airbus France and Airbus UK). This was involving technical support and regular discussions with the partners to ensure that the F&DT work submitted was in line with Airbus standards (harmonised methods).
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KAI and Clairis Technology
- FDT Stress Engineer
2010 - 2010
A350 Nose Landing Gear Bay (placement at Aerolia on behalf of KAI and Clairis Technology)
(8 months)
F&DT Stress Engineer.
Performing F&DT analyses on the A350-900 Nose Landing Gear Bay (NLGB) in interface with KAI/Clairis Technology and Aerolia. Sizing of the NLGB Structures: Frame Horns, Lower Angle Up lock Fitting for Maturity B. The analyses were performed by hand calculations and with Airbus fatigue software (SAFE and ISAMI Tools).
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Airbus
- FDT Stress Engineer
Blagnac
2009 - 2009
A350 Pax Door Surround (placement at Airbus Fr site on behalf of Spirit Aerosystems
(6 months)
F&DT Stress Engineer.
Performing the F&DT analyses of the door surround in interface with Spirit Aerosystems and Airbus France. Sizing of the Pax Door Surround Structures (Sill and Edge Frame) by hand and computer methods (SAFE and ISAMI Tools).
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MAGELLAN
- FDT Lead Engineer
villeurbanne
2008 - 2009
A330-200 GMF Wingtip/Winglet & Pylon Attachments (Magellan site)
(8 months)
Lead F&DT Engineer:
In charge of the technical supervision of the other team members, attending customers meetings in order to update the progress of the project, raise and resolve technical issues.
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Messier Dowty
- Stress Engineer
2008 - 2008
A330/A340 Long range Main Landing Gear (Messier Dowty
(6 months)
F&DT Stress Engineer.
In charge of the stress analyses (Static and Fatigue) of in service problems (Hard Landings and various in service problems) using hand calculation and FE analysis.
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GKN
- FDT stress engineer
Arnage
2006 - 2008
(18 months)
* Aileron & Spoiler panels.
In charge of F&DT analyses of the composite panels and developed several tools (Visual basic macros) to automate some repetitive tasks met in fatigue team (generation of the input files for AUK fatigue software DAMTOL).
* Flap track beam attachments (6 months)
Performing the F&DT analyses of the flap beam attachment. Fatigue survey was made from post processing FE results (with Patran). Analyses were performed by hand calculations and computer methods (DAMTOL package: SPECDAM, SEQDAM & SPECCRK sections).
* System brackets (6 months).
In charge of the fatigue analyses of A400M Trailing Edge electrical and hydraulic system brackets. Fatigue analysis was performed taking into account vibration high cycle fatigue loads in addition to the normal low fatigue loads. Analyses were executed by hand calculation and computer methods (DAMTOL package :SECDAM & SPECDAM sections)
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Airbus
- FDT stress engineer
Blagnac
2006 - 2006
(9 months)
In charge of the F&DT analyses on A300/A310 Pylon for Serial Repair Manual activities in the frame of A300/A310 Extended Service Goal.
Allowable damages, calculations of Repair Approval Sheets (RAS) were performed by hand and computer methods (AiF fatigue software SAFE).
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Airbus
- FDT Stress Engineer
Blagnac
2004 - 2005
A310-300 ESG Engine Mounts Fatigue Analysis (placement
(17 months)
In charge of the F&DT parametric study of engines mounts for different power plants (Pratt and Whitney / General Electric). The objective was to quantify the impact of several parameters, which were not taken into account in the previous certification (range, fuel at landing, lift off phase and lateral gusts). I developed and used a Visual Basic macro to compute the generation of input files for fatigue software SAFE.
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Airbus
- Stress Engineer
Blagnac
2001 - 2004
A340-500/600 Nose Section Floor Static Justification (placement
(23 months)
In charge of justifications of floor modifications due to different layouts. Performing static analyses of longitudinal and transverse rails, seat rails and furniture fittings. Analyses were mainly based on hand calculations and computer methods (ASSIST, CADLINK). I wrote stress reports and official Modification Sheet Justifications (MSJ) for external customers.
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Messier Dowty
- Stress Engineer
2000 - 2000
(9 months)
* A300-600ST N°5 landing gears static certification.
I performed static calculations for the nose and main landing gears and wrote certification reports for the substantiation of the weight increase of this aircraft.
* A340-500/600 central landing gear static certification.
I performed static calculations of the central landing gear with a new loads loop.
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Various
- Stress Engineer
1999 - 1999
Various projects for diverse customers (Aircelle,
(10 months)
* FEM analysis with NASTRAN / PATRAN.
Mirage 2000 shroud linear static analysis for version 5 to 9 modification studies.
A340-200/300 Pilot coatroom non-linear static analysis (large displacements).
NH90 exhaust nozzle dynamic analysis (normal modes calculation).
* Static and fatigue certification.
A340-500/600 landing gear bay fatigue certification. I performed the calculation with a new loads loop and updated the certification reports.
DO 328 static and fatigue certification. Recalculation with a new loads loop.
