Metastable Beta Titanium Spring Performance at Elevated Temperature

2002-01-3004

11/05/2002

Event
World Aviation Congress & Exposition
Authors Abstract
Content
The application of metastable beta titanium alloy Beta-C™ (Ti-3Al-8V-6Cr-4Mo-4Zr) in spring applications is increasing. A Ti-3Al-8V-6Cr-4Mo-4Zr, or more simply Ti-38-6-44, coil spring can be comparatively smaller than the steel mechanical equivalent on account of its high strength and lower shear modulus. This paper reviews the testing methods and results of load-life fatigue tests performed on helical compression springs at 177 °C with a stress ratio of R=0.456. All springs were compliance tested prior to fatigue testing as a means of measuring the shear modulus. To support spring behavior modeling, the shear modulus was also determined using a torsionally loaded strain gauged specimen tested at room temperature and 177 °C. The thermal expansion behavior was studied from room temperature to above 177 °C.
Meta TagsDetails
DOI
https://doi.org/10.4271/2002-01-3004
Pages
11
Citation
Rateick, R., McCool, K., Leonard, E., and Hoeffer, J., "Metastable Beta Titanium Spring Performance at Elevated Temperature," SAE Technical Paper 2002-01-3004, 2002, https://doi.org/10.4271/2002-01-3004.
Additional Details
Publisher
Published
Nov 5, 2002
Product Code
2002-01-3004
Content Type
Technical Paper
Language
English