A thermal spray powder according to the present disclosure is a thermal spray powder which is used to form a thermal spray film having a characteristic of abradability, the thermal spray powder includes Ni alloy particles, solid lubricant particles, and aluminum flakes, the content of oxygen in the aluminum flakes is within a range of 0.29 mass % to 4.1 mass %, and the coverage of aluminum flakes on the surfaces of the Ni alloy particles is within a range of 60% to 100%.

A method of manufacturing a multi material device for heat transfer, and a multi material device is disclosed comprising: depositing, by an additive manufacturing technique, a first material onto a scaffold; depositing, by an additive manufacturing technique, a second material onto at least part of the first material, wherein, one of the first or second material is a heat transfer material having first thermal conductivity, a first chemical resistance and a first erosion resistance and the other is a rugged material of a second thermal conductivity, a second chemical resistance and a second erosion resistance, such that the second thermal conductivity is lower than the first thermal conductivity and at least one of the second chemical resistance or second erosion resistance is higher that the respective first chemical resistance or first erosion resistance.

Disclosed are single atom dispersions and multi-atom dispersions, and systems and methods for synthesizing the atomic dispersions. An exemplary method of synthesizing atomic dispersions includes: positioning a loaded substrate which includes a substrate in which is loaded with at least one of: a precursor of an element or a cluster of an element, applying one or more temperature pulses to the loaded substrate where a pulse of the temperature pulse(s) applies a target temperature for a duration, maintaining a cooling period after the pulse, and providing single atoms of the element dispersed on the substrate after the one or more temperature pulses. The target temperature applied by the pulse is between 500 K and 4000 K, inclusive, and the duration is between 1 millisecond and 1 minute, inclusive.

A method for making an improved nuclear fuel cladding tube includes reinforcing a Zr alloy tube by first winding or braiding ceramic yarn directly around the tube to form a ceramic covering, then physically bonding the ceramic covering to the tube by applying a first coating selected from the group consisting of Nb, Nb alloy, Nb oxide, Cr, Cr oxide, Cr alloy, or combinations thereof, by one of a thermal deposition process or a physical deposition process to provide structural support member for the Zr tube, and optionally applying a second coating and optionally applying a third coating by one of a thermal deposition process or a physical deposition process. If the tube softens at 800° C.-1000° C., the structural support tube will reinforce the Zr alloy tube against ballooning and bursting, thereby preventing the release of fission products to the reactor coolant.

The present disclosure relates to catalytic static mixers comprising catalytic material. The static mixers can be configured for use with continuous flow chemical reactors, for example tubular continuous flow chemical reactors for heterogeneous catalysis reactions. This disclosure also relates to processes for preparing static mixers. This disclosure also relates to continuous flow chemical reactors comprising the static mixers, systems comprising the continuous flow chemical reactors, processes for synthesising products using the continuous flow reactors, and methods for screening catalytic materials using the static mixers.

A thixomolding material includes: a metal body that contains Mg as a main component; and a coating portion that is adhered to a surface of the metal body via a binder and contains Si particles containing Si as a main component. An average particle diameter of the Si particles is 1 μm or more and 100 μm or less, and a mass fraction of the Si particles in a total mass of the metal body and the Si particles is 1.0 mass % or more and 30.0 mass % or less. The binder may contain waxes. A content of the binder may be 0.001 mass % or more and 0.200 mass % or less.

Methods of forming a desired geometry at a location on a superalloy part are disclosed. The method may include directing particles of a powder mixture including a low melt temperature superalloy powder and a high melt temperature superalloy powder to the location on the superalloy part at a velocity sufficient to cause the superalloy powders to deform and to form a mechanical bond but not metallurgical bond to the superalloy part. The directing of particles continues until the desired geometry is formed. Heat is applied to the powder mixture on the repair location. The heat causes the low melt temperature superalloy powder to melt, creating the metallurgical bonding at the location. Another method uses the same directing to form a preform for repairing the location on the part. The low melt temperature superalloy powder melts at <1287° C., and the high melt temperature superalloy powder melts at >1287° C.

Systems and methods for application of stress corrosion cracking resistant cold spray coatings include a method of forming a partial coating on a canister having a perimeter wall with a surface. The method may include identifying a compromised region on the surface of the wall of the canister, and impacting a substantially linear flow of particles of a powder against an area in the compromised region of the surface in a manner effective to cause the particles of the powder to bond to the surface of the wall to produce a coating on the area of the compromised region. The method may also include moving the substantially linear flow in a direction substantially parallel to the surface of the wall to cause the particles to impact an additional area of the compromised region to cause the particles to bond to the surface of the additional area.

A system for spraying a coating material to a substrate includes an optical sensor that monitors a thickness, a controller that generates a first signal corresponding to an amount of gas propellant to be heated, a second signal corresponding to a temperature to which the gas propellant is to be heated, a third signal corresponding to an amount of a solid powder composition to be mixed with the heated gas, and a fourth signal corresponding to a distance between the nozzle and the substrate, a first regulator that supplies an amount of gas propellant corresponding to the first signal, a heater that heats the gas propellant to the temperature corresponding to the second signal, a second regulator that supplies an amount of solid powder composition corresponding to the third signal, and an actuator that moves the nozzle corresponding to the fourth signal.

There is provided a manufacturing method of a Ni-based alloy repaired member having a repair piece formed at a damaged portion of a base material. The base material and the repair piece are made of a high precipitation-strengthened Ni-based alloy material. The manufacturing method includes the steps of: preprocessing a surface of the damaged portion; preparing a Ni-based alloy powder having a predetermined chemical composition; depositing a sprayed piece on the damaged portion by a high-speed collision spraying process using the Ni-based alloy powder; subjecting the sprayed piece to a predetermined heat treatment so that the sprayed piece is thermally refined to a softened sprayed piece; processing the softened sprayed piece into a shaped sprayed piece with a desired shape; and subjecting whole of the shaped sprayed piece and the base material to a predetermined heat treatment so that the shaped sprayed piece is thermally refined to the repair piece.