Metallurgical Changes in the High Temperature Fretting of Ni and Ti Alloys.
Abstract
An experimental rig has been constructed for testing the fretting fatigue behavior of two materials in use in gas turbines, viz. Ti-6Al-4V and Inconel 718. Initial tests on Ti-6Al-4V show that the fatigue life is reduced as the temperature is raised and this is associated with the development of a layer structure on the surface. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1976
- Accession Number
- ADA035056
Entities
People
- R. B. Waterhouse
Organizations
- University of Nottingham