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Metastable Beta Titanium Spring Performance at Elevated Temperature Honeywell Engine Systems and Services

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Rateick, Richard G., author.
Conference Name:
World Aviation Congress & Exposition (2002-11-05 : Phoenix, Arizona, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2002
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
2002-01-3004
Access Restriction:
Restricted for use by site license

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