Call for Technology: Spin Pit Testing of Jet Engine Fan Disk

Spin Pit Testing of Jet Engine Fan Disk:

  • Require spin pit testing of 6 fan disks to confirm fatigue life and fracture mechanics.
  • Low Cycle Fatigue limit and Fracture Mechanics results from Finite Element Analysis and risk assessment are already complete.
  • Physical verification of fatigue initiation site and crack growth pattern is required through spin pit analysis.
  • Bladed fan disk is ~50 inches in diameter, weighs ~136 pounds, and spins at ~10,000 RPMs.
  • These are used disks that will have multiple non-destructive inspections completed to confirm starting conditions.
  • Expect USAF and Original Equipment Manufacturer engineering participation in testing and evaluation of results.

Point of Contract:
Debbie Lilu, NCMS
debral@ncms.org
(734) 995-7038