Skip to main content
U.S. Department of Energy
Office of Scientific and Technical Information

High-strength iron aluminide alloys

Technical Report ·
DOI:https://doi.org/10.2172/115406· OSTI ID:115406

Past studies have shown that binary Fe{sub 3}Al possesses low creep-rupture strength compared to many other alloys, with creep-rupture lives of less than 5 h being reported for tests conducted at 593{degrees}C and 207 MPa. The combination of poor creep resistance and low room-temperature tensile density due to a susceptibility to environmentally-induced dynamic hydrogen embrittlement has limited use of these alloys for structural applications, despite their excellent corrosion properties. Improvements in room temperature tensile ductility have been realized mainly through alloying effects, changes in thermomechanical processing to control microstructure, and by control of the specimen`s surface condition. Ductilities of 10-20% and tensile yield strengths as high as 500 MPa have been reported. In terms of creep-rupture strength, small additions of Mo, Nb, and Zr have produced significant improvements, but at the expense of weldability and room-temperature tensile ductility. Recently an alloy containing these additions, designated FA-180, was shown to exhibit a creep-rupture life of over 2000 h after a heat treatment of 1 h at 1150{degrees}C. This study presents the results of creep-rupture tests at various test temperatures and stresses and discusses the results as part of our effort to understand the strengthening mechanisms involved with heat treatment at 1150{degrees}C.

Research Organization:
Oak Ridge National Lab., TN (United States)
OSTI ID:
115406
Report Number(s):
ORNL--6874; ON: DE95015441
Country of Publication:
United States
Language:
English

Similar Records

Development of weldable high-strength iron aluminides
Conference · Wed Jul 01 00:00:00 EDT 1992 · OSTI ID:10154731

Development of weldable high-strength iron aluminides
Conference · Tue Dec 31 23:00:00 EST 1991 · OSTI ID:5133728

High-strength iron aluminide alloys
Technical Report · Sat Jun 01 00:00:00 EDT 1996 · OSTI ID:450762