CASE FILE ENTRY // MATERIAL FAILURE LOG

Overview: Each case highlights metallurgical failuresβ€”voids, porosity, crackingβ€”observed in aerospace-grade forging environments.

Approach: I applied NDT, thermal history tracing, and process diagnostics to determine root causes. Visuals are based on simulated micrographs for clarity.

Note: All examples are fictionalized for instructional use and comply with NDA requirements. No proprietary data is shown.

⚠️ Note: All entries are educational and NDA-safe. No client identifiers used.

Metallographic Simulations β€” Aluminum Alloy

Subsurface Void β€” Edge Defect

This simulation presents a void located near the edge of an aluminum billet. The defect was identified during a failure investigation following machining deviations.

  • Material: Simulated aluminum alloy
  • Inspection: Cross-sectioned, polished, examined under 20Γ— magnification
  • Void dimension: Approx. 0.0004 in wide
  • Formation mechanism: Casting or rolling-induced porosity

Interpretation: Edge-located voids can disrupt tool engagement and dimensional control. Their early detection supports upstream process optimization.

⚠️ All visuals are fictionalized simulations for educational use only. No proprietary or client-specific data is included.

πŸ’» Corrosion Comparison Dashboard

Compare common corrosion and failure types in aluminum and steel alloys. Learn visual cues, estimated depths, and forge-related causes to better diagnose material integrity issues.

⚫ Pitting Corrosion β€” 6261-T6 Aluminum

Localized corrosion initiating at grain boundaries or reheated zones in aluminum billets.

πŸ“ Pit dimensions: 41.2β€―Β΅m Γ— 16.6β€―Β΅m
πŸ” Visual cue: Isolated elliptical void with dark rim, often adjacent to microstructural transitions.

πŸ“Ž Cause: Poor passivation + chloride exposure + thermal cycling (especially in wet forge environments).

🟠 Surface Corrosion β€” 304 Stainless Steel

Uniform corrosion with even material loss. Passive chromium oxide layer deteriorates in high-moisture or chloride environments.

πŸ“ Depth: ~54.9β€―Β΅m
🌊 Visual cue: Smooth matte finish, etched grain texture, no isolated pits.

πŸ“Ž Cause: Long-term exposure + humidity + uncoated storage β€” commonly observed in parts left outside prior to machining or welding.

πŸ”΅ Advanced Surface Attack β€” Steel Alloy

Trench-like corrosion with jagged, structural loss. Accelerated by press misalignment, coating failure, and environmental contamination.

πŸ“ Depth: ~129.5β€―Β΅m
⚠️ Visual cue: Rough-edged void, often spanning multiple grains or wall surfaces.

πŸ“Ž Cause: Coating breakdown + mechanical stress + electrolyte pooling during storage or forming.

🧲 Galvanic Corrosion β€” Bimetallic Joint

Dissimilar metals in electrical contact corrode at different rates. Common in bolted assemblies with aluminum and stainless steel.

πŸ”© Visual cue: Corrosion halo at fastener or joint contact.
⚑ Cause: Electrochemical potential difference + electrolyte presence.

πŸ”§ Material Pair: Aluminum bolt (anode) + Stainless steel washer (cathode)

πŸ”¬ Damage Morphology: Circular pitting and halo effect surrounding the fastener head, focused on the aluminum interface

🌧️ Environment: Humid air with periodic condensation, creating an electrolyte bridge between dissimilar metals

πŸ’₯ Why It Failed: The aluminum, being less noble, corroded preferentially in the galvanic couple. Moisture enabled ion flow, initiating and sustaining anodic attack while the stainless steel remained protected.

πŸ” Magnification: 10x | Observation: Moisture ingress along threads facilitated localized corrosion underneath the washer.

βšͺ Hydrogen Embrittlement β€” High-Strength Steel

Atomic hydrogen diffuses into the metal lattice, causing delayed cracking under stress. Often occurs during acid cleaning or plating of hardened components.

⚑ Visual cue: Subsurface cracks or brittle fracture in high-strength parts.
πŸ“‹ Cause: Hydrogen absorption combined with tensile stress.

πŸ”§ Material: Hardened steel rod (high-strength alloy, post-plating)

πŸ”¬ Damage Morphology: Intergranular cracking near the surface, with jagged crack fronts extending along stress paths

πŸ§ͺ Environment: Acid cleaning and electroplating processes introduced atomic hydrogen into the microstructure

πŸ’₯ Why It Failed: Absorbed hydrogen atoms diffused into the steel lattice, concentrating at areas of high tensile stress and leading to brittle, delayed failure under load. Crack propagation occurred without significant plastic deformation.

πŸ” Magnification: 50x | Observation: Fracture originated beneath the surface and propagated outward in a brittle pattern.

πŸ“Š Quick Comparison Table

Material Corrosion Type Depth / Risk Visual Cue Cause
6261-T6 Al Pitting 41.2 Γ— 16.6β€―Β΅m Isolated elliptical void Cl– ingress + thermal cycling
304 S.S. Surface Attack ~54.9β€―Β΅m Matte grain etch Humidity + oxide breakdown
Steel Alloy Trench Corrosion ~129.5β€―Β΅m Jagged trench void Mechanical + coating failure
Al/Stl Joint Galvanic Variable Halo at fastener zone Electrochemical mismatch
High-Strength Steel Embrittlement Crack propagation Subsurface fracture Hydrogen + stress

Simulated reference cases β€” NDA-safe visuals.

πŸ”¬ Alpha Case in Titanium β€” Root Cause & Visuals

Alpha case is a brittle, oxygen-enriched surface layer found in titanium alloys after high-temperature exposure. It must be minimized in aerospace and critical applications.

It forms when oxygen diffuses into titanium at forging or heat treat temperatures above 1000Β°F. While it can reduce ductility and fatigue life, not all alpha case is catastrophic. If within allowable limits (typically ≀0.002"), it may be tolerable or removable through surface finishing processes. Judgment depends on location, depth, and application criticality.

πŸ§ͺ Simulated Microstructural Snapshots

  • Material: Ti-6Al-4V alloy (forged, NDA-safe simulation)
  • Prep: Polished, etched, illuminated under LED ring
  • Magnification: 20x objective lens
  • Focus: Identify oxidized surface depth and grain boundary patterns

Β© 2025 Audrey Enriquez. All content is shared for educational and documentation purposes only.
No proprietary or confidential information is disclosed. All rights reserved.