Published 1991 | Version v1
Book

The structure and properties of a Ti-25Al-10Nb-3V-1Mo alloy

  • 1. Army Materials Research Agency, Watertown, MA (United States). Materials Technology Lab.
  • 2. Johns Hopkins Univ., Baltimore, MD (United States). Dept. of Materials Science and Engineering

Description

This paper reports on six super α2 titanium aluminide pancakes produced by rapid omnidirectional compaction of prealloyed Ti-25Al-10Nb-3V-1Mo (at%) (Ti-14.1Al-19.5Nb-3.2V-2Mo (wt%)) powder. Various solution and aging heat treatments were investigated to yield the best combination of tensile and stress rupture properties. The β transus temperature was found to be about 1,090 degrees C (1,990 degrees F). The alloy was heat treated with four different schedules to develop various structure combinations of α2 and β and followed by a series of microstructural analyses and mechanical property determinations. The highest ultimate tensile strength and yield strength attained at room temperature were 1,174.9 and 977.7 MPa (170.4 and 141.8 ksi), respectively, for a specimen heat treated at 1,140 degrees C (2,084 degrees F) for 1 hr and aged at 816 degrees C (1,500 degrees F) for 4 hr + air cooling

Additional details

Publishing Information

Publisher
Materials Research Society.
Imprint Place
Pittsburgh, PA (United States)
ISBN
1-55899-105-0
Imprint Title
High-temperature ordered intermetallic alloys 4
Imprint Pagination
1082 p.
Journal Page Range
p. 931-936.

Conference

Title
Fall meeting of the Materials Research Society (MRS).
Dates
24 Nov - 1 Dec 1990.
Place
Boston, MA (United States).

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
23041747
Subject category
S36: MATERIALS SCIENCE; S36: MATERIALS SCIENCE;
Resource subtype / Literary indicator
Conference
Descriptors DEI
ALUMINIUM ALLOYS; COMPACTING; HEAT TREATMENTS; MECHANICAL PROPERTIES; MICROSTRUCTURE; MOLYBDENUM ALLOYS; NIOBIUM ALLOYS; TENSILE PROPERTIES; TITANIUM ALLOYS; VANADIUM ALLOYS; YIELD STRENGTH
Descriptors DEC
ALLOYS; CRYSTAL STRUCTURE; FABRICATION

Optional Information

Secondary number(s)
CONF-901105--.