AEROSPACE CAE ENGINEER

10/2013 – 7/2015

1. Static Analysis of Electrical Installation Brackets of A350XWB-1000
(MATB Phase – MSN59 & MSN65) (SSCVR, SSFDR, 8LU3)

SAFRAN Labinal, Hamburg Germany.

1 Year ( Oct 2013 – Till date)
• FE model creation and validation for electrical brackets
• Normal mode analysis to check the model (Free Free Analysis)
• Static analysis for flight & crash load cases
• Buckling analysis for electrical brackets under critical load conditions
• IRMAT load sheets creation at the interface points
• SDL (stress dossier light) preparation
• Preparation of standard documents for reference
• Work co-ordination between onsite and offshore

Finite-Elemente-Methode (FEM)

3/2012 – 9/2013

2. Static Analysis of System Brackets of A350XWB-900 (Certification – MSN5)
( EMP Fittings, Yellow Tank Fittings)

AKKA Technologies, Toulouse France.

6 Months ( March 2013 – SEP 2013)
• FE model creation and validation for system brackets
• Static 1G check, Zero stress check, Groundcheck validation is performed
• Normal mode analysis to check the model (Free Free Analysis)
• Static analysis for flight & crash load cases
• Buckling analysis for system brackets under critical load conditions
• JDV shear/bearing, tension, tension/shear check for fasteners.
• Unfolding analysis for metallic fittings using ISAMI v7.2
• Composite Filled hole analysis for composite junctions (Fastener shear,
bearing, Pull through, Bypass & combined checks) using ISAMI v7.2
• ACD4 & Certification dossier preparation

3. Static Analysis of primary structural components of A350XWB-900
(Certification – MSN5) (MLGD Central Fittings, MLGD AFT Fittings)

AKKA Technologies, Toulouse France

6 Months (Sep 2012 - Feb 2013)
• 3D Tetra 10 mesh creation for MLGD Central Fittings (as per AM2036)
• Model validation is done as per AM2036
• Normal mode analysis to check the model (Free Free Analysis)
• Load extraction using FastPPH tool
• Static analysis is carried out for unitary load case and linear interpolation
is done for 8000 load cases using Excel VBA
• Buckling analysis is carried out for critical loads
• Composite filled hole analysis for skin, upper panel and upper corner
(Fastener shear, bearing, Bypass & combined) using ISAMI v7.2
• Unfolding check for metallic fittings using ISAMI v7.2
• JDV shear/bearing, tension, tension/shear check for fasteners
• ACD4 & Certification dossier preparation

4. Static Analysis of ALS components of A350XWB-900 (Justification – MSN1)
(CFRP-Cargo-Shearwebs)

AKKA Technologies, Toulouse France

6 Months (March 2012 –Aug 2012)
• FE model creation and validation for Shearwebs (as per AM2036)
• Static and buckling analysis for all the Shearwebs
• Composite damage tolerance analysis for Shearwebs using ISAMI v7.2
• Composite Bolted Joint 1D analysis to extract loads for filled hole
analysis using ISAMI v7.2
• JDV shear/bearing, tension, tension/shear check for fasteners.
• Unfolding analysis is carried out for all the Shearwebs using ISAMI v7.2
• Composite Filled hole analysis for Skin and Shearwebs using ISAMI v7.2
• Post processing of results using MSC Patran
• Justification dossier preparation

Finite-Elemente-Methode (FEM)