A fan blade includes a blade body and a shape memory alloy actuator. The blade body has a pressure side disposed opposite a suction side. Each of the pressure side and the suction side extends radially from a root towards a tip and extends axially from a leading edge towards a trailing edge. The blade body defines a passageway that is disposed between the pressure side and the suction side. The shape memory alloy actuator is received within the passageway and is operatively connected to the blade body.

The present disclosure relates to the field of endodontic instrumentation, and more particularly to apparatus and methods for manufacturing that include applying a variable heat-treat to an endodontic file blank based on geometric parameters that will be formed in the blank.

A production method for a medical linear member is provided which is not abraded upon production and which includes a flat shape in a cross section.

The method includes the steps of: forming a first spiral body (1) of an oval shape in a horizontal section by spirally winding a base body (3), in which a plurality of wires (2) formed of a shape-memory alloy is arrayed, around a winding core (4); subjecting the first spiral body (1) to first shape-memory treatment; cutting the first spiral body (1) into a first predetermined length; forming a second spiral body (5) of a flat shape in a horizontal section by compressing the first spiral body (1) in a direction along a short diameter; subjecting the second spiral body (5) to second shape-memory treatment; and removing the winding core (4) from the second spiral body (5).

Disclosed herein is a shape memory alloy comprising 48 to 50 atomic percent nickel, 15 to 30 atomic percent hafnium, 1 to 5 atomic percent aluminum; with the remainder being titanium. Disclosed herein too is a method of manufacturing a shape memory alloy comprising mixing together to form an alloy nickel, hafnium, aluminum and titanium in amounts of 48 to 50 atomic percent nickel, 15 to 30 atomic percent hafnium, 1 to 5 atomic percent aluminum; with the remainder being titanium; solution treating the alloy at a temperature of 700 to 1300 C. for 50 to 200 hours; and aging the alloy at a temperature of 400 to 800 C. for a time period of 50 to 200 hours to form a shape memory alloy.

A fastening apparatus includes a retaining member comprising a shape memory material configured to transform, responsive to application of a stimulus, from a first solid phase to a second solid phase. The retaining member is disposed within a hole in a body and secured within the hole by phase change which creates an interference fit to secure the retaining member against rotational and axial movement. The hole has a second axial cross-sectional shape. The retaining member has a first axial cross-sectional shape that is preferably either circular or rectangular.

A haptic actuator device includes a surface with a mechanical property responsive to localized temperature changes. The surface can include a layer or sheet comprising a shape-memory material. The haptic actuator device can further include an actuator configured to selectively deform a plurality of regions in the sheet; and a temperature controller adapted to control the temperatures of the plurality of regions. A method of localized actuation includes selectively controlling the temperatures of the plurality of regions to be above a shape-memory transition temperature of the shape-memory material; selectively deforming at least one of the regions; while maintaining the deformation of the at least one region, lowering the temperature of the at least one region to below the shape-memory transition temperature; subsequently withdrawing the applied stress; and thereafter heating the at least one region to above the shape-memory transition temperature, causing the region to return to its pre-deformation shape.

A display device includes a first shape-memory wire that memorizes an extended state and a second shape-memory wire that memorizes a bending state. The laminated layers include a first flexible layer, a second flexible layer, and a display element layer on which light emitting elements are disposed. The first flexible layer includes a first interface between the first flexible layer and a layer in contact with an upper side or a lower side of the first flexible layer. The second flexible layer includes a second interface between the second flexible layer and a layer in contact with an upper side or a lower side of the second flexible layer. The first shape-memory wire is disposed within the first flexible layer or on the first interface. The second shape-memory wire is disposed within the second flexible layer or on the second interface.

Guide wire devices fabricated from a linear pseudo-elastic NiTi alloy and methods for their manufacture. The NiTi alloy that includes nickel, titanium, and about 3 atomic % (at %) to about 30 at % niobium (Nb). Cold working the NiTi alloy stabilizes the alloy's martensitic phase and yields a linear pseudo-elastic microstructure where reversion to the austenite phase is retarded or altogether blocked. The martensitic phase of cold worked, linear pseudo-elastic NiTiNb alloy has an elastic modulus that is considerably higher than the comparable cold worked, linear pseudoelastic binary NiTi alloy. This yields a guide wire device that has better torque response and steerability as compared to cold worked, linear pseudoelastic binary NiTi alloy or superelastic binary NiTi alloy.

Composite alloys comprising a first alloy portion comprising nickel and titanium and a second alloy portion comprising nickel and titanium in a different stoichiometry than the first alloy portion are disclosed, along with related methods of manufacture and use. Particularly, the composite alloys may be used in customized medical devices where a shape memory effect would be beneficial.

A fatigue-resistant Nitinol instrument has a working portion in the deformed monoclinic martensitic state and an austenite finish temperature in the range of 40 to 60 C. Because the operating environment of the instrument is about 37 C., the working portion remains in the monoclinic martensitic state during its use. The relatively high austenite finish temperature and fatigue resistance is achieved by subjecting the nickel-titanium alloy to a final thermal heat treat in a temperature range of about 410 to 440 C. while the nickel-titanium alloy is under constant strain of about 3 to 15 kg. Further, the high austenite finish temperature is achieved without subjecting the alloy to thermal cycling to produce shape memory. Additionally, there are no intermediate processing steps occurring between obtaining a finished diameter of the wire or blank through cold working and the final thermal heat treat under constant strain.