Abstract
Single crystals with 〈001〉 orientation of Cu-14.1Al-xNi (x=0, 1.0, 2.1, 3.2 and 4.3 mass%) alloys have been tensile-tested at various temperatures above and below Ms, except for the binary Cu–Al alloy tested only at 243 K below Ms. Critical stresses on loading, σL, and on unloading, σU, for the γ1′\
ightleftarrowsβ1″(β1′), β1″(β1′)\
ightleftarrowsα1′ and β1\
ightleftarrowsβ1′ transformations have been measured as a function of temperature. Then, the equilibrium stress, σE (=(σL+σU)/2), vs. temperature, T, phase diagram, which involves four phases of β1 parent and γ1′, β1′ (β1″) and α1′ martensites, has been constructed for the four kinds of alloys with different Ni contents, and the critical and equilibrium stresses have been plotted as a function of Ni content. As a result, σL extrapolated to 0% Ni for the γ1′→β1″ transformation at 243 K was found to be higher than that for the β1″→α1′ transformation, and the β1′ (β1″) phase region in the σE vs. T diagram was found to become narrower with decreasing Ni content. The stress region of the β1′(β1″) phase at 243 K, which was extrapolated to 0% Ni, was between ∼320 MPa and ∼410 MPa. Hence, the γ1′→α1′ direct transformation so far reported for binary Cu–Al alloys was revealed to be due to the consecutive γ1′→β1″→α1′ transformations in which the β1″ martensite stress-induced from the γ1′ martensite immediately transforms into the α1′ martensite. Meanwhile, the temperature where slip deformation took place in the α1′ martensite was found to decrease from far above Af to below Mf with decreasing Ni content. Hence, the reason for no appearance of pseudoelasticity in the binary Cu–Al alloys was ascribed to the effect that the slip deformation in α1′ martensite lowered the critical stress for reverse transformation below zero stress.