Accession Number:

ADA244815

Title:

Fatigue in Single Crystal Nickel Superalloys

Descriptive Note:

Technical progress rept. 16 Sep-15 Dec 1991.

Corporate Author:

PRATT AND WHITNEY WEST PALM BEACH FL

Personal Author(s):

Report Date:

1991-12-20

Pagination or Media Count:

14.0

Abstract:

This program investigates the behavior of single crystal airfoil materials. The fatigue initiation processes in single crystal SC materials are significantly more complicated and involved than fatigue initiation and subsequent behavior of a single macrocrack in conventional, isotropic, materials. To understand these differences it is helpful to review the evolution of high temperature airfoils. Modern gas turbine flight propulsion systems employ single crystal materials for turbine airfoil applications because of their superior performance in resisting creep, oxidation, and thermal mechanical fatigue TMF. These properties have been achieved by composition and alloying, and by appropriate crystal orientation and associated anisotropy.

Subject Categories:

  • Aircraft
  • Properties of Metals and Alloys

Distribution Statement:

APPROVED FOR PUBLIC RELEASE