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The hot workability and superplasticity of Ti-48Al-2Nb-2Cr alloys

Technical Report ·
DOI:https://doi.org/10.2172/329558· OSTI ID:329558
 [1]
  1. Lockheed Martin Corp., Schenectady, NY (United States)

The hot compression behavior and microstructure evolution of ingot metallurgy (I/M) and powder metallurgy (P/M) processed samples of the near-{gamma} Ti-aluminide alloy, Ti-48Al-2Nb-2Cr (at%), were determined. Three I/M conditions and two P/M conditions were examined in this study. Hot compression tests were performed in the temperature range 1,100--1,300 C at strain rates ranging from 1.67 {times} 10{sup {minus}1}/sec to 1.67 {times} 10{sup {minus}4}/sec. P/M materials consolidated by either hot isostatic pressing (HIP`ing) or extrusion exhibited the best hot workability in most cases. The P/M materials possessed finer, more homogeneous microstructures than the I/M materials. It was also noted that improved workability, and in some cases superplastic behavior, was observed in the materials with equiaxed microstructures without any lamellar constituents.

Research Organization:
Knolls Atomic Power Lab., Schenectady, NY (United States)
Sponsoring Organization:
USDOE Assistant Secretary for Nuclear Energy, Washington, DC (United States)
DOE Contract Number:
AC12-76SN00052
OSTI ID:
329558
Report Number(s):
KAPL-P--000208; K--97162; CONF-980202--; ON: DE99002103
Country of Publication:
United States
Language:
English

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