πŸ“‹ Case Study

Energy Sector Inconel 718 Turbine Disk Grooving

Galling and built-up edge leading to catastrophic tool failure during deep grooving

πŸ—οΈ Project Overview

Repair and reconditioning of gas turbine disks

🎯 Challenge

Galling and built-up edge leading to catastrophic tool failure during deep grooving

πŸ”§ Design Approach

Hybrid toolpath: ramp-in with adaptive feed, followed by constant engagement with variable pitch end mill and AlCrN coating

πŸ“ Design Diagram

Energy Sector: Inconel 718 Turbine Disk GroovingDiskRamp-inAdaptive FeedConstant EngagementVariable PitchAlCrN Coating (T_BUE = 680Β°C)Galling & BUECatastrophic Failuref_adapt = 1.42 Γ— f_baseap/d = ? β†’ e^(βˆ’ap/d) = 0.296T_melt(Inconel 718) = 1360Β°CT_BUE β‰ˆ 0.5 Γ— T_melt

AI-generated project design illustration

πŸ“ Key Calculations

Built-up edge onset temperature

T_BUE β‰ˆ 0.5 Γ— T_melt
Result: 680Β°C
Target interface temp kept <620Β°C

Adaptive feed multiplier

f_adapt = f_base Γ— (1 βˆ’ e^(βˆ’ap/d))
Result: 1.42
Compensates for decreasing chip thickness in ramp

πŸ“Š Results

Groove consistency improved by 94%; tool change frequency dropped from every 3 parts to every 11; repair lead time cut by 38%

πŸ’‘ Lessons Learned

  • β€’Variable pitch tools suppress regenerative chatter in tough alloys
  • β€’Adaptive feed must be synchronized with real-time depth feedback

βœ… Key Takeaways

  • 1Variable pitch tools suppress regenerative chatter in tough alloys
  • 2Adaptive feed must be synchronized with real-time depth feedback