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45results about How to "Deterioration of mechanical properties" patented technology

Alloying-element-strengthened high-silicon aluminum composite and preparation method thereof

The invention provides a preparation method of an alloying-element-strengthened high-silicon aluminum composite and belongs to the technical field of material preparation. The preparation method is particularly suitable for preparation of electronic packaging material. The designed alloying-element-strengthened high-silicon aluminum composite comprises, by mass percent, 48.0%-52.0% of silicon, 0.5%-4.0% of X and the balance aluminum. The X is copper and/or magnesium. The preparation method of the alloying-element-strengthened high-silicon aluminum composite comprises the steps that a silicon source, an aluminum source and an X source are prepared according to the designed components, the prepared silicon source, the prepared aluminum source and the prepared X source are smelted, and then a melt is obtained; and atomized spray deposition is conducted on the obtained melt, so that a deposition preform is obtained, hot isostatic pressing treatment is conducted on the deposition preform, and then a finished product is obtained, wherein during hot pressing pressure treatment, the temperature is controlled to be 520-600 DEG C, and the pressure is controlled to be 150-200 MPa. The designed composite has the advantages of being excellent in comprehensive performance, outstanding in mechanical property, low in preparation cost and the like and is suitable for large-scale industrial production.
Owner:CENT SOUTH UNIV

Magnesium-aluminum alloy with continuous eutectic structure and preparation method thereof

The invention discloses a magnesium-aluminum alloy with continuous eutectic structure and a preparation method thereof, and the alloy is composed of a magnesium-aluminum alloy matrix and a continuouseutectic phase distributed at the grain edge of the matrix. The preparation method comprises the following steps that (1) nano-sized titanium powder and the magnesium-aluminum alloy powder are placedin a ball mill, and ball milling is conducted under protective atmosphere to obtain the mixed powder; and (2) the mixed powder is used as a raw material, and the magnesium-aluminum alloy with the continuous eutectic structure is prepared through selective laser melting under the protective atmosphere. According to the preparation method, the titanium is introduced in the magnesium-aluminum alloy preparation process, aluminum atoms in a molten pool are attracted to migrate, and eutectic reaction is generated on the edge of the crystal grain to generate the continuous eutectic phase; meanwhile,the characteristic that the selective laser melting solidification speed is high is utilized, the formation of the continuous eutectic phase is promoted while the content of a second phase Mg17Al12 isreduced, so that galvanic corrosion effect of the magnesium aluminum alloy is effectively weakened, and the corrosion resistance of the magnesium-aluminum alloy is improved; and meanwhile, better interface combination is achieved, so that the mechanical property of the magnesium-aluminum alloy is improved.
Owner:CENT SOUTH UNIV

Aviation aluminium alloy U-shaped frame section bar and preparation method thereof

The invention discloses an aviation aluminium alloy U-shaped frame section bar and a preparation method thereof. The aviation aluminium alloy U-shaped frame section bar is prepared from the followingelements in percentage by weight: 5.6-6.5% of Zn, 1.4-2.4% of Cu, less than 0.1% of Mn, 1.8-2.6% of Mg, 0.2-0.25% of Cr, 0.25-0.35% of Fe, equal to or less than 0.1% of Si, less than 0.08% of Ti and the balance of Al. According to the preparation method, through the set alloy composition and the specific preparation technology including extruding, rolling and bending, the aviation aluminium alloyU-shaped frame section bar formed at one time is obtained, on one hand, the tensile strength and yield strength of U-shaped frame section bar are greatly improved, finally, the tensile strength can reach 550-609 MPa, the yield strength can reach 490-546 MPa, the elongation is 7-11%, the planar clearance is equal to or less than 1 mm, the perpendicularity is equal to or less than 1 degree, which are much better than the using standard, and on the other hand, the precision of the U-shaped frame section bar is greatly improved, the prepared U-shaped frame section bar has excellent planar flatnessto ensure stability consistency of quality, can completely meet the using requirement of aviation aluminium alloy section bar, and provides material guarantee for research of a novel spaceflight carrier rocket in China.
Owner:西北铝业有限责任公司

Magnesium-zinc-germanium alloy with cathode inhibition effect and preparation method thereof

The invention discloses a magnesium-zinc-germanium alloy with a cathode inhibition effect and a preparation method thereof. The magnesium-zinc-germanium alloy comprises a magnesium matrix and a magnesium-zinc-germanium second phase, the preparation method comprises the following steps that (1), the magnesium-zinc alloy and a nano-germanium powder are placed in a ball mill, and the magnesium-zinc alloy and the nano-germanium powder are subjected to ball milling under a protective atmosphere to obtain a magnesium-zinc-germanium mixed power; (2), the mixed powder is taken as a raw material, and the magnesium-zinc-germanium alloy is prepared by performing selective laser melting under a protective atmosphere. According to the magnesium-zinc-germanium alloy with a cathode inhibition effect andthe preparation method, the germanium is introduced into the magnesium-zinc alloy, and the second phase containing germanium is generated in the alloy, so that the aggregation of medium hydrogen atomsin the solution on the cathode can be inhibited, the generation rate of hydrogen is reduced by weakening the recombination of the hydrogen atoms, so that the corrosion resistance of the magnesium-zinc alloy is improved; and on the other hand, the mechanical property of the magnesium-zinc alloy is improved through solid solution strengthening, fine grain strengthening and second phase strengthening.
Owner:JIANGXI UNIV OF SCI & TECH +1

Five-element high-entropy alloy Cu0.5FeNiVAlx and strength and hardness improvement method thereof

The invention discloses five-element high-entropy alloy Cu0.5FeNiVAlx and a strength and hardness improvement method thereof. The five-element high-entropy alloy Cu0.5FeNiVAlx mainly comprises Cu, Fe,Ni, V and Al with purities greater than or equal to 99.9%. The five-element high-entropy alloy Cu0.5FeNiVAlx comprises, by atomic percent, 10 to 15 at% of the Cu, 20 to 30 at% of the Fe, 20 to 30 at%of the Ni, 20 to 30 at% of the V, and 0 to 26 at% of the Al. A preparation method of the five-element high-entropy alloy Cu0.5FeNiVAlx is as follows: performing arc-strike smelting in a vacuum environment protected by argon gas on the alloy raw materials Cu, Fe, Ni, V and Al for repeated several times. The strength and hardness improvement method of the five-element high-entropy alloy Cu0.5FeNiVAlx is as follows: using a quartz tube for vacuum sealing of a prepared Cu0.5FeNiVAlx ingot, then using a muffle furnace at 500 DEG C, 750 DEG C and 1000 DEG C respectively for annealing treatment, andfinally thermally-insulating and cooling to room temperature. The five-element high-entropy alloy Cu0.5FeNiVAlx obtained by the method has an effective improvement in strength and hardness, and contributes to broadening the application range of a high-entropy alloy and improving the economic value.
Owner:GUANGXI UNIV

Thermal shock device and method for shield tunneling machine

The invention relates to a thermal shock device and method for a shield tunneling machine, and belongs to the technical field of shield construction. The thermal shock device comprises a temperature measuring device arranged on a cutter head, heating pipelines and cooling pipelines, wherein the heating pipelines and the cooling pipelines are parallelly arranged on the end surface of the cutter head of the shield tunneling machine and uniformly distributed in the circumferential direction of the cutter head; the position, away from the end surface of the cutter head, of each heating pipeline isprovided a plurality of ignition devices which are sequentially distributed in the length direction of the heating pipeline, and heating switches used for controlling the ignition devices; the position away from the end surface of the cutter head, of each cooling pipeline is provided a plurality of cooling spray heads sequentially distributed in the length direction of the cooling pipeline, and cooling switches used for controlling the cooling spray heads; and the ignition devices and the cooling spray heads are lower than cutters on the cutter head. By utilizing a thermal shock principle, aspecial competent formation is rapidly heated and cooled, a lot of heat exchange is quickly generated, shock thermal stress is generated inside, and shock fracturing is caused, the mechanical propertyof the special competent formation is reduced, the rock breaking speed is increased, and cutter head abrasion is reduced.
Owner:CHINA COAL TECH & ENG GRP CHONGQING RES INST CO LTD

A kind of alloying element reinforced high-silicon-aluminum composite material and preparation method thereof

The invention provides a preparation method of an alloying-element-strengthened high-silicon aluminum composite and belongs to the technical field of material preparation. The preparation method is particularly suitable for preparation of electronic packaging material. The designed alloying-element-strengthened high-silicon aluminum composite comprises, by mass percent, 48.0%-52.0% of silicon, 0.5%-4.0% of X and the balance aluminum. The X is copper and / or magnesium. The preparation method of the alloying-element-strengthened high-silicon aluminum composite comprises the steps that a silicon source, an aluminum source and an X source are prepared according to the designed components, the prepared silicon source, the prepared aluminum source and the prepared X source are smelted, and then a melt is obtained; and atomized spray deposition is conducted on the obtained melt, so that a deposition preform is obtained, hot isostatic pressing treatment is conducted on the deposition preform, and then a finished product is obtained, wherein during hot pressing pressure treatment, the temperature is controlled to be 520-600 DEG C, and the pressure is controlled to be 150-200 MPa. The designed composite has the advantages of being excellent in comprehensive performance, outstanding in mechanical property, low in preparation cost and the like and is suitable for large-scale industrial production.
Owner:CENT SOUTH UNIV

Multi-principal-element alloy containing BCC/B2 double-phase structure and preparation method of multi-principal-element alloy

The invention relates to a multi-principal-element alloy containing a BCC / B2 double-phase structure and a preparation method of the multi-principal-element alloy and belongs to the technical field of metal materials. The multi-principal-element alloy is of a woven BCC / B2 double-phase structure, the chemical formula of the multi-principal-element alloy is recorded as TiaTabNbcZrdAleMf according to the atomic percentage content of all elements, M is at least one of V, Cr, Ni, Cu, Fe, Si, Mg, Y, B, C and O, a is greater than 30 and less than or equal to 60, b is greater than 0 and less than or equal to 15, c is greater than or equal to 5 and less than or equal to 50, d is greater than or equal to 5 and less than or equal to 40, e is greater than or equal to 5 and less than 15, f is greater than or equal to 0 and less than or equal to 10, b+c+d is greater than or equal to 40 and less than or equal to 75, b / d is greater than or equal to 0.3 and less than or equal to 0.6, and the multi-principal-element alloy has good plasticity and high strength by optimizing the composition elements of the multi-principal-element alloy, the content of all the elements and the microstructure. In addition, the multi-principal-element alloy can be obtained through alloy smelting and annealing treatment, the preparation method is simple, safe and reliable, and good application prospects are achieved.
Owner:浙江省科创新材料研究院
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