Patent classifications
C22C2200/00
High-performance corrosion-resistant high-entropy alloys
This disclosure provides alloy compositions comprising the main constituent elements iron, nickel, cobalt, molybdenum, and chromium. In one embodiment, the alloy comprises 10.0 to 30.0 wt % iron; 30.0 to 60.0 wt % nickel; 10.0 to 25.0 wt % cobalt; 1.0 to 15.0 wt % molybdenum; 15.0 to 25.0 wt % chromium by weight; where the sum of iron and nickel is at least 50 wt %; and, where the balance comprises minor elements, the total amount of minor elements being about 5% or less by weight. The alloy compositions have use as coatings to protect metals and alloys from corrosion in extreme environments where corrosion is a major concern such as with exposure to sea water or sea water with CO.sub.2.
SINTERED MEMBER AND ELECTROMAGNETIC COUPLING
A sintered member having an annular shape, includes: a first face facing one side in an axial direction; a second face facing the other side in the axial direction; an inner peripheral face connected to an inner peripheral edge of the first face; and a plurality of tooth groups and a plurality of tooth-missing parts which are alternately disposed along a circumferential direction of the inner peripheral face. The second face includes a plurality of ball grooves arranged in parallel in the circumferential direction. Each tooth group includes a plurality of spline teeth that are continuous in the circumferential direction of the peripheral face. The number of plurality of tooth-missing parts is the same as the plurality of ball grooves. Positions in a radial direction in which the plurality of tooth-missing parts are formed are within ranges in the radial direction in which the ball grooves are formed.
SINTERED MEMBER AND ELECTROMAGNETIC COUPLING
A sintered member having an annular shape, includes: a first face facing one side in an axial direction; a second face facing the other side in the axial direction; an inner peripheral face connected to an inner peripheral edge of the first face; and a plurality of tooth groups and a plurality of tooth-missing parts which are alternately disposed along a circumferential direction of the inner peripheral face. The second face includes a plurality of ball grooves arranged in parallel in the circumferential direction. Each tooth group includes a plurality of spline teeth that are continuous in the circumferential direction of the peripheral face. The number of plurality of tooth-missing parts is the same as the plurality of ball grooves. Positions in a radial direction in which the plurality of tooth-missing parts are formed are within ranges in the radial direction in which the ball grooves are formed.
Sintered oil-impregnated bearing
Provided is a novel sintered oil-impregnated bearing superior in wear resistance and cost performance under a severe use condition where the bearing collides with a shaft due to a high load and vibration, such as a condition associated with an output shaft of an electric motor installed in a vehicle and a wiper motor installed therein. The sintered oil-impregnated bearing contains: 15 to 30% by mass of Cu; 1 to 4% by mass of C; and a remainder consisting of Fe and inevitable impurities, in which a metal structure with copper being melted therein is provided at least on a bearing surface; pearlite or a pearlite with ferrite being partially scattered therein is provided in a matrix; a copper-rich phase arranged in a mesh-like manner is also provided in the matrix; and a free graphite is dispersed and distributed in the matrix as well.
Sintered oil-impregnated bearing
Provided is a novel sintered oil-impregnated bearing superior in wear resistance and cost performance under a severe use condition where the bearing collides with a shaft due to a high load and vibration, such as a condition associated with an output shaft of an electric motor installed in a vehicle and a wiper motor installed therein. The sintered oil-impregnated bearing contains: 15 to 30% by mass of Cu; 1 to 4% by mass of C; and a remainder consisting of Fe and inevitable impurities, in which a metal structure with copper being melted therein is provided at least on a bearing surface; pearlite or a pearlite with ferrite being partially scattered therein is provided in a matrix; a copper-rich phase arranged in a mesh-like manner is also provided in the matrix; and a free graphite is dispersed and distributed in the matrix as well.
METHOD OF OPERATING AN APPARATUS FOR PRODUCING A THREE-DIMENSIONAL WORK PIECE AND APPARATUS FOR PRODUCING A THREE-DIMENSIONAL WORK PIECE
A method of operating an apparatus (10) for producing a three-dimensional work piece (18) by irradiating layers of a raw material powder with electromagnetic or particle radiation comprises the steps of a) applying a layer of raw material powder onto a carrier (12); b) selectively irradiating the layer of raw material powder with electromagnetic or particle radiation in accordance with a geometry of a corresponding layer of the work piece (18) to be produced; and c) repeating steps a) and b) until the work piece (18) has reached the desired shape and size. For at least a portion of at least some of the layers, a scanning time (t.sub.s) from the beginning of the exposure of a respective raw material powder layer portion to electromagnetic or particle radiation until the beginning of the exposure of a new raw material powder layer applied on top of said layer portion to electromagnetic or particle radiation is controlled so as to not fall below a specific minimum value which is individually set for said layer portion in dependence on a layer portion specific quality parameter. layer portion specific quality parameter
METHOD OF OPERATING AN APPARATUS FOR PRODUCING A THREE-DIMENSIONAL WORK PIECE AND APPARATUS FOR PRODUCING A THREE-DIMENSIONAL WORK PIECE
A method of operating an apparatus (10) for producing a three-dimensional work piece (18) by irradiating layers of a raw material powder with electromagnetic or particle radiation comprises the steps of a) applying a layer of raw material powder onto a carrier (12); b) selectively irradiating the layer of raw material powder with electromagnetic or particle radiation in accordance with a geometry of a corresponding layer of the work piece (18) to be produced; and c) repeating steps a) and b) until the work piece (18) has reached the desired shape and size. For at least a portion of at least some of the layers, a scanning time (t.sub.s) from the beginning of the exposure of a respective raw material powder layer portion to electromagnetic or particle radiation until the beginning of the exposure of a new raw material powder layer applied on top of said layer portion to electromagnetic or particle radiation is controlled so as to not fall below a specific minimum value which is individually set for said layer portion in dependence on a layer portion specific quality parameter. layer portion specific quality parameter
HARDFACING WITH LOW CARBON STEEL ELECTRODE
A method of hardfacing a metal component includes welding a surface area of the metal component using a Cold Metal Transfer (CMT) process. The method of hardfacing the metal component includes performing the CMT welding process in a weaving pattern over the surface area of the component. A consumable, low carbon steel wire electrode is used in the CMT process.
ALUMINUM ALLOY FORGING
An aluminum alloy forging includes 0.30 mass % or more and 1.0 mass % or less of Cu; 0.63 mass % or more and 1.30 mass % or less of Mg; 0.45 mass % or more and 1.45 mass % or less of Si; the balance being Al and inevitable impurities, wherein the following relations are satisfied,
[Mg content]×1.587≥−4.1×[Cu content].sup.2+7.8×[Cu content]−1.9 (1)
[Si content]×2.730≥−4.1×[Cu content].sup.2+7.8×[Cu content]−1.9 (2)
and the ratio of the integrated intensity Q1 of the X-ray diffraction peak of the CuAl.sub.2 phase to the integrated intensity Q2 of the X-ray diffraction peak of the (200) plane of the Al phase obtained by the X-ray diffraction method, Q1/Q2, is 2×10.sup.−1 or less.
ADDITIVE MANUFACTURING METHODS AND APPARATUS FOR FORMING OBJECTS FROM A NICKEL-BASED SUPERALLOY IN A LAYER-BY-LAYER MANNER
An additive manufacturing method wherein an object is formed by selectively solidifying layers of powder with at least one energy beam. The method includes forming the object from a nickel-based superalloy, wherein exposure parameters and an exposure pattern for the at least one energy beam result in the object having a directionally solidified microstructure with columnar grains aligned with a build direction, perpendicular to the layers. A composition of the nickel-based alloy by weight % may include: 9.3-9.7W, 9.0-9.5Co, 7.5-8.5Cr, 5.4-5.7Al, 3.1-3.3Ta, 1.4-1.6Hf, 0.6-0.9Ti, Mo 0.4-0.6, 007-0.015Zr, 0.01-0.02B with a carbon concentration of around 0.07-0.09 wt % and a balance of Ni.