Your browser does not support javascript! Please enable it, otherwise web will not work for you.

Aircraft (airframe) Fatigue And Damage Tolerance (f&dt) Analysis Engin @ Infosys

Home > Other

 Aircraft (airframe) Fatigue And Damage Tolerance (f&dt) Analysis Engin

Job Description

Role & responsibilities:


  • Identification of PSE ( Principal Structural Elements )
  • Calculate Stress Concentration Factor. Wide Spread Fatigue Damage Factor, effect in fatigue due to Size, Material, joints, Machining quality, technology process, etc.
  • Fatigue Index Calculation
  • Fatigue Equivalent Stress Calculation and extraction of Reference Stresses
  • Fatigue Spectrum Analysis for various mission and Damage Stimulation Analysis
  • Fatigue Life Estimation and Damage Tolerance Analysis
  • Damage Tolerance Analysis for SLP (Single Load Path), MLP (Multiple Load Path), and DCF (Damage Contaminant Feature) structures
  • Initial Crack definition and determination of Critical Crack Length for Airworthiness Limitation Item, Threshold and Inspection Interval
  • Low Life Mitigation, various low life mitigation techniques based on OEM based process
  • Preparation of Fatigue and Damage Tolerance Analysis Documentation like ACD/ACS, SCNs and Stress Dossiers
  • Candidate Should have good hand-on work experience in Fatigue and Damage Tolerance Analysis of Airframe Structural Analysis
  • Candidate should have in depth knowledge of Fatigue Design Philosophies
  • Knowledge and experience in Structural Failure and Fatigue Failure Characteristics
  • Aware of various types of fatigue, Fatigue assessment Principles and Methods
  • Calculate Fatigue Life (High Cycle Fatigue, Low Cycle Fatigue and Very High Cycle Fatigue)
  • Fatigue Analysis of Metallic and Fastener parts.
  • Composite Fatigue Analysis experience
  • Candidate should have experience in Damage Tolerance Analysis and Crack Propagation Analysis of Airframe Structures

Preferred candidate profile:


Must have

  • Knowledge of Fatigue Design Guidelines, Principles and Methods
  • Fatigue Life Calculation
  • Crack Propagation Analysis / Damage Tolerance Analysis
  • Aware of DT calculation in several different stages like corner crack , through crack, etc.
  • Fatigue Criteria for Crack Propagation Analysis to determine the critical crack length
  • Awareness and knowledge about the Inspection Techniques for Crack Propagation Analysis
  • Detectable Crack Length Determination

Tools:


NASGRO, MSC NASTRAN, PATRAN, HyperMESH. OEM Specific Fatigue Tools

Basic Knowledge on CATIA V5

Job Classification

Industry: IT Services & Consulting
Functional Area / Department: Other
Role Category: Other
Role: Other
Employement Type: Full time

Contact Details:

Company: Infosys
Location(s): Mysuru

+ View Contactajax loader


Keyskills:   Damage Tolerance Fatigue crack propagation life residual fatigue life calculation fracture mechanics life integration Linear Elastic Fracture Mechanism airframe fatigue and damage tolerance

 Fraud Alert to job seekers!

₹ Not Disclosed

Similar positions

Urgent Hiring // Evaluation Engineer // Mumbai

  • Cars24
  • 3 - 8 years
  • Mumbai
  • 3 days ago
₹ 1.25-4.25 Lacs P.A.

Proposal Engineer

  • Clar Aqua
  • 1 - 6 years
  • Chennai
  • 3 days ago
₹ 2.4-6 Lacs P.A.

Lead Consultant - GCP Platform Engineer

  • Genpact
  • 6 - 8 years
  • Kolkata
  • 4 days ago
₹ 13-20 Lacs P.A.

7. Civil Design Manager/ Structural Engineer

  • Aquatech Systems
  • 9 - 14 years
  • Pune
  • 4 days ago
₹ Not Disclosed

Infosys

Infosys Limited