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Title: Navy product-improvement program for Turbomach T-62t APU's corrosion-resistant turbine wheel/improved bearing and lubrication system. Final report, 19 January 1983-12 April 1986

Technical Report ·
OSTI ID:6423691

Titan T-27 and T-40-1 gas turbine engines have used IN-713 LC turbine wheels for many years without serious hot-corrosion problems. For extended operation in marine environments, however, the well-known susceptibility of Alloy 713 to hot corrosion (sulfidation) could lead to deterioration of airfoil surfaces resulting eventually in loss of engine performance, or even engine failure. Corrosion protection could be enhanced by protective coatings; however, with base material so poor in hot-corrosion resistance as Alloy 713, the reliability of a 713 turbine wheel would be suspect. Also, degradation of mechanical properties accompanying the coating process would reduce the safety margin below acceptable, and appears to justifya material change to an alloy with better hot-corrosion resistance. The alloy selected was MAR-M247, a nickel-based alloy with 10% cobalt, 10% tungsten, 8,25% chromium, 5.5% aluminum, 3% tantalum, 1.5% hafnium, 1% titanium, and other elements. The expected improvements over IN-713 LC include improved oxidation/hot corrosion resistance, blade creep resistance, and tensile strength.

Research Organization:
Sundstrand Turbomach, San Diego, CA (USA)
OSTI ID:
6423691
Report Number(s):
AD-A-178084/0/XAB; ERR-0632
Country of Publication:
United States
Language:
English