The invention relates to a precipitation-strengthened shape memory alloy (SMA) comprising a composition designed and processed such that the precipitation-strengthened SMA meets property objectives comprising a yield strength being more than about 1500 MPa at room temperature, a transformation temperature in a range of about −15 to 20° C., a misfit in a range of about 0.9-1.1%, wherein the property objectives are design specifications of the precipitation-strengthened SMA.

The invention relates to a precipitation-strengthened shape memory alloy (SMA) comprising a composition designed and processed such that the precipitation-strengthened SMA meets property objectives comprising a yield strength being more than about 1500 MPa at room temperature, a transformation temperature in a range of about −15 to 20° C., a misfit in a range of about 0.9-1.1%, wherein the property objectives are design specifications of the precipitation-strengthened SMA.

A thermal treatment method for conditioning or restoring bismuth containing lead-free solder in a solder joint assembly. The method comprising heating the solder in the assembly to a temperature near the solvus.

A thermal treatment method for conditioning or restoring bismuth containing lead-free solder in a solder joint assembly. The method comprising heating the solder in the assembly to a temperature near the solvus.

Present invention is about a transformation-induced plasticity high-entropy alloy which can provide improved mechanical properties compared to those obtained by conventional methods, due to the phase transformation occurring at the time of deformation at a cryogenic temperature. According to the present invention, the high-entropy alloy (HEA) includes 10-35 at % of Co, 3-15 at % of Cr, 3-15 at % of V, 35-48 at % of Fe, and 0-25 at % of Ni (exclusive of 25), and mainly consists of an FCC phase at room temperature, wherein transformation-induced plasticity, in which at least part of the FCC phase changes to a BCC phase, occurs at a cryogenic temperature (−196° C.)

Present invention is about a transformation-induced plasticity high-entropy alloy which can provide improved mechanical properties compared to those obtained by conventional methods, due to the phase transformation occurring at the time of deformation at a cryogenic temperature. According to the present invention, the high-entropy alloy (HEA) includes 10-35 at % of Co, 3-15 at % of Cr, 3-15 at % of V, 35-48 at % of Fe, and 0-25 at % of Ni (exclusive of 25), and mainly consists of an FCC phase at room temperature, wherein transformation-induced plasticity, in which at least part of the FCC phase changes to a BCC phase, occurs at a cryogenic temperature (−196° C.)

A method for producing a porous member, whereby a member having smaller microgaps can be produced, and additionally, the outermost surface alone can be made porous and a porous layer can be formed on the surface while maintaining the characteristics of portions in which no porous layer is formed, is provided.

A method for producing a porous member, whereby a member having smaller microgaps can be produced, and additionally, the outermost surface alone can be made porous and a porous layer can be formed on the surface while maintaining the characteristics of portions in which no porous layer is formed, is provided.

Commercially-available lithium metal foils have been found to have a high density of crystalline defects. When such foils are used as the anode in a secondary lithium metal battery cell, repeated cycling may lead to the formation of lithium shunts near the crystalline defects, which can cause shorting. Methods described herein may be used to reduce the density of crystalline defects in lithium metal foils. Such lithium metal can be used as the anode in lithium battery cells.

[Object] To provide a cobalt-chromium alloy member suitable for use in a medical or aerospace device.

[Solving Means] There is provided a cobalt-chromium alloy member, which is obtained by performing heat treatment for 1 minute or more and 60 minutes or less at a temperature exceeding a recrystallization temperature of a cobalt-chromium alloy material and not more than 1100° C. on a cobalt-chromium alloy as-processed material obtained by causing a cobalt-chromium alloy material to be subjected to cold plastic working into a predetermined shape, the cobalt-chromium alloy material having a composition of, in terms of mass %, 23 to 32% of Ni, 37 to 48% of Co, and 8 to 12% of Mo, a remainder thereof containing Cr and an unavoidable impurity, the composition satisfying a relationship of 20≤[Cr %]+[Mo %]+[unavoidable impurity %]≤40, the cobalt-chromium alloy member having a tensile strength of 800 to 1200 MPa, a uniform elongation of 25 to 60%, and a breaking elongation of 30 to 80%.