C22C19/007

NICKEL ALLOYS FOR BIOSENSORS

The present disclosure relates to metal alloys for biosensors. An electrode is made from the metal alloy, which more specifically can be a nickel-based alloy. The alloy provides physical and electrical property advantages when compared with existing pure metal electrodes.

Method for designing alloys

A computer assisted method of designing a designed alloy composition comprising a plurality of elements, the method comprising the steps of: populating a multi-dimensional alloy space with a plurality of candidate alloy compositions, the plurality of candidate alloy compositions including for each of the plurality of elements at least three candidate alloy compositions with different amounts of the respective element to each other; performing at least one test on each individual one of the plurality of candidate alloy compositions until each of the individual ones of the plurality of candidate alloy compositions fails a test or has passed all tests; outputting the designed alloy composition based on one or more of the individual ones of the plurality of candidate alloy compositions which have passed all tests, wherein the at least one test includes at least: a phase equilibrium test in which predicted phase equilibrium is determined as a function of elemental composition of the individual one of the plurality of candidate alloy compositions; and at least one merit index test in which a predicted property of the individual one of the plurality of candidate alloy compositions is predicted as a function of the elemental composition of the individual one of the plurality of candidate alloy compositions and failing the individual one of the plurality candidate alloy compositions if the predicted property does not meet a desired predicted property.

System and method for pyrolysis using a liquid metal catalyst

A process for decomposing a hydrocarbon-containing composition includes feeding the hydrocarbon-containing composition to a reactor containing a catalytically active molten metal or a catalytically active molten metal alloy, wherein the metal or alloy catalyzes a decomposition reaction of the hydrocarbon-containing composition into a hydrogen-rich gas phase and a solid carbon phase. The solid carbon phase is insoluble in the metal or alloy. The process may be a continuous process.

Nanocrystalline high temperature machine parts

Novel metallic systems and methods for their fabrication provide high temperature machine parts formed of a consolidated nano-crystalline metallic material. The material comprises a matrix formed of a solvent metal having a melting point greater than 1,250 C. with crystalline grains having diameters of no more than about 500 nm, and a plurality of dispersed metallic particles formed on the basis of a solute metal in the solvent metal matrix and having diameters of no more than about 200 nm. The particle density along the grain boundary of the matrix is as high as about 2 nm.sup.2 of grain boundary area per particle so as to substantially block grain boundary motion and rotation and limit creep at temperatures above 35% of the melting point of the consolidated nano-crystalline metallic material. The machine parts formed may include turbine blades, gears, hypersonics, radiation shielding, and other high temperature parts.

Aluminized metallic scaffold for high temperature applications and method of making an aluminized metallic scaffold

An aluminized metallic scaffold for high temperature applications comprises a porous non-refractory alloy structure including a network of interconnected pores extending therethrough. The porous non-refractory alloy structure comprises a transition metal phase and an aluminide phase, and portions of the porous non-refractory alloy structure between interconnected pores have a thickness no greater than about 500 nm. A method of making an aluminized metallic scaffold for high-temperature applications comprises introducing aluminum into a surface of a porous metallic structure at an elevated temperature. The porous metallic structure comprises a transition metal and has a network of interconnected pores extending therethrough, where portions of the porous metallic structure between interconnected pores have a thickness no greater than about 500 nm. As the aluminum is introduced into the surface and diffusion occurs, an aluminide phase is formed, resulting in a porous non-refractory alloy structure comprising the aluminide phase and a transition metal phase.

SHAPE MEMORY ALLOY MICROFILAMENT YARNS
20240011199 · 2024-01-11 ·

Shape memory yarns described herein include twisted microfilaments made from a shape memory alloy that may provide superelastic or shape memory properties. The shape memory yarns are formed into coils that provide a high degree of actuation or elasticity along an axis of the coiled shape memory yarn, and may have relatively low porosity, low rigidity, and/or low change of volume compared to shape memory coils formed from solid structures. Coiled shape memory yarns may provide further tailorability of a superelastic or shape memory response of a system or device incorporating the coiled shape memory yarns through various coil parameters, such as coil pitch or density, or torque balancing, such as heat treating or plying the coiled shape memory yarns.

Nickel material and method for manufacturing nickel material

Provided is a nickel material having excellent corrosion resistance and high strength, and a method for manufacturing the nickel material. A nickel material has a chemical composition consisting of, in mass %, C: 0.001 to 0.20%, Si: 0.15% or less, Mn: 0.50% or less, P: 0.030% or less, S: 0.010% or less, Cu: 0.10% or less, Mg: 0.15% or less, Ti: 0.005 to 1.0%, Nb: 0.040 to 1.0%, Fe: 0.40% or less, sol. Al: 0.01 to 0.10%, an N: 0.0010 to 0.080%, with the balance being Ni and impurities, and satisfying Formula (1) and Formula (2).
0.030( 45/48)Ti+( 5/93)Nb( 1/14)N<0.25(1)
0.030<( 3/48)Ti+( 88/93)Nb( 1/12)C(2) A content (mass %) of a corresponding element is substituted for each element symbol in Formula (1) and Formula (2).

Wear resistant piston seal

Aspects are directed to a tribological and creep resistant system configured to operate at temperature in excess of 750 C., comprising: a piston seal that includes a nickel base alloy, where the nickel base alloy includes a Ni.sub.3(Al,X) type precipitated phase in an amount greater than 40% by volume. Aspects are directed to a system comprising: a piston seal that includes a cobalt-based alloy. Aspects are directed to a method comprising: heat treating an ingot of a nickel base alloy that includes coarsening a precipitated phase to facilitate forging or wrought forming the ingot, machining the ingot to include a substantially flat surface, and processing the ingot to generate a piston seal.

METHOD FOR PRODUCING A SHAPED CATALYST BODY

Provided herein is a novel process for producing shaped catalyst bodies in which a mixture having aluminum contents of Al.sup.=.sup.0 in the range from 80 to 99.8% by weight, based on the mixture used, is used to form a specific intermetallic phase, shaped catalyst bodies obtainable by the process of the invention, a process for producing an active catalyst fixed bed including the shaped catalyst bodies provided herein, the active catalyst fixed beds and also the use of these active catalyst fixed beds for the hydrogenation of organic hydrogenatable compounds or for formate degradation.

TURBINE PART MADE OF SUPERALLOY COMPRISING RHENIUM AND/OR RUTHENIUM AND ASSOCIATED MANUFACTURING METHOD
20200248562 · 2020-08-06 · ·

A turbine part, such as a turbine blade or a distributor fin, for example, including a substrate made of superalloy based on monocrystalline nickel, including rhenium and/or ruthenium, and having a -NisAI phase that is predominant by volume and a -Ni phase, the part also including a sublayer made of metal superalloy based on nickel covering the substrate, wherein the sublayer has a -NisAI phase that is predominant by volume and wherein the sublayer has an average atomic fraction of aluminium of between 0.15 and 0.25, of chromium of between 0.03 and 0.08, of platinum of between 0.01 and 0.05, of hafnium of less than 0.01 and of silicon of less than 0.01. A process for manufacturing a turbine part including a step of vacuum deposition of a sublayer made of a superalloy based on nickel having predominantly by volume a -NisAI phase, on a substrate made of superalloy based on nickel including rhenium and/or ruthenium.