A shape memory alloy (SMA) with a composition of
Ni60Ti40
(wt%) was chosen for the fabrication of active beam elements intended for use as
cyclic actuators and incorporated into a morphing aerospace structure. The active
structure is a variable-geometry chevron (VGC) designed to reduce jet engine noise
in the take-off flight regime while maintaining efficiency in the cruise regime.
This two-part work addresses the training, characterization and derived material
properties of the new nickel-rich composition, the assessment of the actuation
properties of the active beam actuator and the accurate analysis of the VGC and
its subcomponents using a model calibrated from the material characterization.
The characterization performed in part I of this work was intended to provide
quantitative information used to predict the response of SMA beam actuators
of the same composition and with the same heat treatment history. Material
in the form of plates was received and ASTM standard tensile testing coupons
were fabricated and tested. To fully characterize the material response as an
actuator, various thermomechanical experiments were performed. Properties such
as actuation strain and transformation temperatures as a function of applied
stress were of primary interest. Results from differential scanning calorimetry,
monotonic tensile loading and constant stress thermal loading for the as-received,
untrained material are first presented. These show lower transformation temperatures,
higher elastic stiffnesses (60–90 GPa) and lower recoverable transformation strains (≈1.5%) when compared to equiatomic NiTi (Nitinol). Stabilization (training) cycles were applied
to the tensile specimens and characterization tests were repeated for the stable (trained)
material. The effects of specimen training included the saturation of cyclically generated
irrecoverable plastic strains and a broadening of the thermal transformation hysteresis. A
set of final derived material properties for this stable material is provided. Finally, the
actuation response of a structural beam component composed of the same material given
the same thermomechanical processing conditions was assessed by applying a constant
bias load and a variable bias load as thermal actuation cycles were imposed.