Description / Abstract:
Purpose
This SAE Aerospace Standard (AS) establishes a uniform procedure
for calculation of electron vacancy numbers in superalloys. It is
intended for use by suppliers of raw materials and parts, typically
castings, for which control of electron vacancy number is required
by the raw material specification.
Application
This procedure has been used to estimate the potential for alloy
phase instability by calculation of the density of electrons per
atom in nickel-based superalloys.
Background
Complex, highly alloyed superalloys have been observed, for some
alloy chemistries and under certain conditions, to form
precipitated phases which can adversely affect strength and
ductility. These phases, typically of a crystalline structure known
as topologically close-packed, or TCP, appear after extended
exposure at temperatures in the range from 1300 to 1650 °F (704 to
899 °C). Such phases include sigma (σ), mu (μ), or Laves. Their
tendency to precipitate from the alloy matrix has been related by
researchers such as Boesch and Slaney (see 2.1) and Woodyatt, et
al. (see 2.2) to the density of electrons per atom as expressed by
the electron vacancy number Nv.