Aircraft (Airframe) Fatigue and Damage Tolerance (F&DT) Analysis Engin

3 weeks ago


Mysore Road Tolgate, Karnataka, India Infosys Limited Full time
Job Description

- 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

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