NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Stress-rupture strength and microstructural stability of W-HF-C wire reinforced superalloy compositesW-Hf-C/superalloy composites were found to be potentially useful for turbine blade applications on the basis of stress-rupture strength. The 100-and 1000-hour rupture strengths obtained for 70 volume percent fiber composites tested at 1090 C were 420 and 280 MN/sq m (61,000 and 41,000 psi). The investigation indicated that with better quality fibers, composites having 100- and 1000-hour rupture strengths of 570 and 370 MN/sq m (82,000 and 54,000 psi) may be obtained. Metallographic studies indicated sufficient fiber-matrix compatibility for long time applications at 1090 C for 1000 hours or more.
Document ID
19740012042
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Petrasek, D. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Signorelli, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Materials, Nonmetallic
Report/Patent Number
E-7931
NASA-TM-X-71529
Report Number: E-7931
Report Number: NASA-TM-X-71529
Meeting Information
Meeting: Composite Reliability Conf.
Location: Las Vegas
Start Date: April 15, 1974
End Date: April 16, 1974
Sponsors: Am. Soc. for Testing and Mater.
Accession Number
74N20155
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available