Fatigue and Damage Tolerance Engineer

4 days ago

Bengaluru, Karnataka, India Expleo Group Full time ₹ 1,04,000 - ₹ 1,30,878 per year

Overview:

This Job is for Fatigue and Damage tolerance Engineer

Responsibilities:

  • The translation of customer specifications into engineering solutions including the identification and mitigation of technical risk.
  • The production of engineering calculations that are necessary to support any conceptual or detail engineering solution for which they are responsible.
  • The detailing of engineering solutions in accordance with Industry Standards or client standards, sufficient for manufacture or purchase of such items.
  • Contributing to technical reports and feasibility studies. Also for ensuring that any contractual, safety or legislative requirements have been taken into account.
  • Guidance of technicians, sub-contractors or suppliers in support of projects ensuring that this is carried out in a safe manner.
  • Engineering contribution in support of sales proposals.
  • The production of clear written technical reports and presentations.
  • Right first time and on time delivery of their work. The ability to estimate the time to carry out tasks and to plan their own work.
  • The Company's Quality Assurance Policies in any work undertaken. In particular to be fully conversant with the requirements of the Company's Processes Manual.
  • Continuous improvement contribution to their personal development and company development in all appropriate areas.

Qualifications:

BTech/MTech

Essential skills:

  • Knowledge of aircraft Fuselage and wing structure and aircraft loads
  • Experienced in spectrum generation and Kt Calculation
  • Autonomous in Fatigue and Damage Tolerance (F&DT) calculations of Airbus aircrafts (fuselage section)
  • Well versed in ISAMI modules (including crack models, joint models) and ISAMI template preparation
  • Should have Fatigue and Damage Tolerance experience related to Single Aisle, Long Range and A350 programs
  • F&DT Analysis of Junctions, notches, unfolding radius, lugs & pins
  • Sizing and stress analysis of the Fuselage and Wing Structure and interfaces by means of hand calculations, numerical simulations (FEM)
  • Experience in numerical modeling, post-processing and reporting of the results
  • Very well-versed in stress dossier writing
  • Good in excel macros

Below tools knowledge is requitred.

  • ISAMI
  • Hyperview (post processing knowledge)
  • Catia V5, PASS SSI (Basic Knowledge)
  • Nastran/Patran
  • Microsoft Office
  • Airbus Supply

Desired skills:

  • Knowledge of Airbus processes and procedures
  • Visual basic and or python programming knowledge.
  • Automation of repeatable tasks / processes.
  • Experience in initial Design Stress (Static, FDT and FEM) tasks of Aircraft Structures.

Experience:

4-8 Years

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