Disclosed is a nano dispersion copper alloy with high air-tightness and low free oxygen content and a brief manufacturing process thereof, wherein alloy comprises the following components: Al.sub.2O.sub.3, Ca and La. The manufacturing process comprises the following steps of: preparing Cu—Al.sub.2O.sub.3 alloy powder by an internal oxidation method; mixing the Cu—Al.sub.2O.sub.3 alloy powder with Cu—Ca—La alloy powder; sheathing the mixed powder under protection of argon; performing hot extrusion and then rotary forging; vacuumizing the sheath after the rotary forging; and sealing and placing the sheath in a nitrogen atmosphere with a temperature of 450° C. to 550° C. and a pressure intensity of 40 Mpa to 60 Mpa for 3 hours to 5 hours. The dispersion copper prepared by the present disclosure has the advantages of low free oxygen content (≤15 ppm), high dimensional stability, good air-tightness and an air leakage rate≤1.0×10.sup.−10 Pa m.sup.3/s after hydrogen annealing.

The invention relates to an additive manufacturing method comprising the steps: additive application of a layer of material (1), and modifying a part of the applied material layer (1) in a property so that a partial layer (3) in the material layer (1) is structured, the partial layer (3) differing from the remaining material layer at least in the modified property. The invention also relates to a correspondingly manufactured component and a suitable manufacturing apparatus.

The invention relates to an additive manufacturing method comprising the steps: additive application of a layer of material (1), and modifying a part of the applied material layer (1) in a property so that a partial layer (3) in the material layer (1) is structured, the partial layer (3) differing from the remaining material layer at least in the modified property. The invention also relates to a correspondingly manufactured component and a suitable manufacturing apparatus.

The present disclosure provides a method for manufacturing a multi-main-phase structure magnet having excellent coercive force and a multi-main-phase structure magnet manufactured therefrom.

In a method for manufacturing a three-dimensional shaped object, when an amount of a shaping material discharged toward a shaping surface per unit movement amount of a discharging unit is defined as a discharged shaping amount, in a layer forming step of forming a layer on the shaping surface, in a case in which a second partial shaped object to be shaped is not adjacent to a first partial shaped object that is shaped previously and is shaped with a gap between the first partial shaped object and the second partial shaped object, the second partial shaped object is shaped by setting the discharged shaping amount to a first discharged shaping amount, and in a case in which the second partial shaped object is adjacent to the first partial shaped object, the second partial shaped object is shaped by setting the discharged shaping amount to a second discharged shaping amount that is greater than the first discharged shaping amount.

In a method for manufacturing a three-dimensional shaped object, when an amount of a shaping material discharged toward a shaping surface per unit movement amount of a discharging unit is defined as a discharged shaping amount, in a layer forming step of forming a layer on the shaping surface, in a case in which a second partial shaped object to be shaped is not adjacent to a first partial shaped object that is shaped previously and is shaped with a gap between the first partial shaped object and the second partial shaped object, the second partial shaped object is shaped by setting the discharged shaping amount to a first discharged shaping amount, and in a case in which the second partial shaped object is adjacent to the first partial shaped object, the second partial shaped object is shaped by setting the discharged shaping amount to a second discharged shaping amount that is greater than the first discharged shaping amount.

A metallic part is disclosed. The part may comprise a functionally graded monolithic structure characterized by a variation between a first material composition of a tubular preform and a second material composition of at least one of a secondary structural element wherein each of the first material composition and the second material composition comprises at least one of a titanium metal or an alloy of titanium. The first material composition may comprise an alpha-beta titanium alloy. The second material composition may comprise a beta titanium alloy.

A multi-scale and multi-phase dispersion strengthened iron-based alloy, and preparation and characterization methods thereof are provided. The alloy contains a matrix and a strengthening phase. The strengthening phase includes at least two types of the strengthening phase particles with different sizes. A volume of the two types of the strengthening phase particles with different sizes having a particle size less than or equal to 50 nm accounts for 85-95% of a total volume of all the strengthening phase particles. The matrix is a Fe—Cr—W—Ti alloy. The strengthening phases include crystalline Y.sub.2O.sub.3 phase, Y—Ti—O phase, Y—Cr—O phase, and Y—W—O phase. The characterization method comprises electrolytically separating the strengthening phases in the alloy, and then characterizing by using an electron microscope. The tensile strength of the prepared alloy is more than 1600 MPa at room temperature, and is more than 600 MPa at 700° C.

A multi-scale and multi-phase dispersion strengthened iron-based alloy, and preparation and characterization methods thereof are provided. The alloy contains a matrix and a strengthening phase. The strengthening phase includes at least two types of the strengthening phase particles with different sizes. A volume of the two types of the strengthening phase particles with different sizes having a particle size less than or equal to 50 nm accounts for 85-95% of a total volume of all the strengthening phase particles. The matrix is a Fe—Cr—W—Ti alloy. The strengthening phases include crystalline Y.sub.2O.sub.3 phase, Y—Ti—O phase, Y—Cr—O phase, and Y—W—O phase. The characterization method comprises electrolytically separating the strengthening phases in the alloy, and then characterizing by using an electron microscope. The tensile strength of the prepared alloy is more than 1600 MPa at room temperature, and is more than 600 MPa at 700° C.

A vehicle compressor component includes an aluminum alloy material made by hot-extruding. The aluminum alloy material has a chemical composition consisting of Fe: 5.0% to 9.0% by mass, Mg: 0.7% to 3.0% by mass, V: 0.1% to 3.0% by mass, Mo: 0.1% to 3.0% by mass, Zr: 0.1% to 2.0% by mass, Ti: 0.02% to 2.0% by mass, and balance Al and unavoidable impurities. The aluminum alloy material has a density of 2.96 g/cm.sup.3 or more. A method for manufacturing the vehicle compressor component includes: compacting aluminum alloy powders having the chemical composition to prepare a compact; hot-extruding the compact to make an aluminum alloy material; and forming the aluminum alloy material into a desired shape.