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Title: Failure analysis of a tool-steel torque shaft

Conference ·
OSTI ID:5834723

A low design load drive shaft from an experimental diesel truck engine failed unexpectedly during highway testing. The shaft was driven by a turbine used to deliver power from an experimental exhaust heat recovery system to the engine's crankshaft. During design, fatigue was not considered a major problem because of the low operating cyclic stresses. An independent testing laboratory analyzed the failure by routine metallography. The structure of the hardened S-7 tool steel shaft was banded and the laboratory attributed the failure to fatigue induced by a banded microstructure. NASA was asked to confirm this analysis. Visual examination of the failed shaft plus the knowledge of the torsional load that it carried pointed to a 100% ductile failure with no evidence of fatigue. Scanning electron microscopy confirmed this. Torsional test specimens were produced from pieces of the failed shaft and torsional overload testing produced identical failures to that which had occurred in the truck engine. This pointed to a failure caused by a high overload and although the microstructure was defective it was not the cause of the failure.

Research Organization:
National Aeronautics and Space Administration, Cleveland, OH (USA). Lewis Research Center
DOE Contract Number:
AI01-76CS51011
OSTI ID:
5834723
Report Number(s):
DOE/NASA/1011-35; NASA-TM-82758; CONF-811149-1; ON: DE82004300
Resource Relation:
Conference: Conference on deformation, fracture, wear, and nondestructive evaluation of materials, New Orleans, LA, USA, 23 Nov 1981
Country of Publication:
United States
Language:
English