Design of Solution Heat Treatments for Aerospace Alloys

Many high strength aerospace alloys undergo solution heat treatment (SHT) and aging to develop precipitate strengthening. Most simply, SHT involves an isothermal hold in a single phase region followed by relatively rapid cooling to develop a super-saturated solid solution from which precipitates form during aging. However, subsequent properties are sensitively dependent on the details of the SHT, which frequently also serves a homogenization function. Altering the details of the thermal cycle during SHT significantly improves the properties attained during aging, as presented by examples of SHT design for titanium aluminide intermetallics, polycrystalline and single crystal superalloys, and 7075 aluminum.