CASE FILE ENTRY // MATERIAL FAILURE LOG
Overview: Each case highlights metallurgical failuresβvoids, porosity, crackingβobserved 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.
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.
β οΈ All visuals are fictionalized simulations for educational use only. No proprietary or client-specific data is included.
π» 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.
β« Pitting Corrosion β 6261-T6 Aluminum
Localized corrosion initiating at grain boundaries or reheated zones in aluminum billets.
π Pit dimensions: 41.2β―Β΅m Γ 16.6β―Β΅m
π Visual cue: Isolated elliptical void with dark rim, often adjacent to microstructural transitions.
π Cause: Poor passivation + chloride exposure + thermal cycling (especially in wet forge environments).
π Surface Corrosion β 304 Stainless Steel
Uniform corrosion with even material loss. Passive chromium oxide layer deteriorates in high-moisture or chloride environments.
π Depth: ~54.9β―Β΅m
π Visual cue: Smooth matte finish, etched grain texture, no isolated pits.
π Cause: Long-term exposure + humidity + uncoated storage β commonly observed in parts left outside prior to machining or welding.
π΅ Advanced Surface Attack β Steel Alloy
Trench-like corrosion with jagged, structural loss. Accelerated by press misalignment, coating failure, and environmental contamination.
π Depth: ~129.5β―Β΅m
β οΈ Visual cue: Rough-edged void, often spanning multiple grains or wall surfaces.
π Cause: Coating breakdown + mechanical stress + electrolyte pooling during storage or forming.
π§² Galvanic Corrosion β Bimetallic Joint
Dissimilar metals in electrical contact corrode at different rates. Common in bolted assemblies with aluminum and stainless steel.
π© Visual cue: Corrosion halo at fastener or joint contact.
β‘ Cause: Electrochemical potential difference + electrolyte presence.
π§ Material Pair: Aluminum bolt (anode) + Stainless steel washer (cathode)
π¬ Damage Morphology: Circular pitting and halo effect surrounding the fastener head, focused on the aluminum interface
π§οΈ Environment: Humid air with periodic condensation, creating an electrolyte bridge between dissimilar metals
π₯ 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.
π Magnification: 10x | Observation: Moisture ingress along threads facilitated localized corrosion underneath the washer.
βͺ 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.
β‘ Visual cue: Subsurface cracks or brittle fracture in high-strength parts.
π Cause: Hydrogen absorption combined with tensile stress.
π§ Material: Hardened steel rod (high-strength alloy, post-plating)
π¬ Damage Morphology: Intergranular cracking near the surface, with jagged crack fronts extending along stress paths
π§ͺ Environment: Acid cleaning and electroplating processes introduced atomic hydrogen into the microstructure
π₯ 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.
π Magnification: 50x | Observation: Fracture originated beneath the surface and propagated outward in a brittle pattern.
π 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 | Clβ 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.
π¬ 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 β€0.002"), it may be tolerable or removable through surface finishing processes. Judgment depends on location, depth, and application criticality.
π§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
Connect with Meβ
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Email: audreyenriquez98@gmail.com
Β© 2025 Audrey Enriquez.
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