243results about How to "Improve stress corrosion resistance" patented technology

The invention relates to a production method of a copper-steel composite plate. The production method comprises the following steps of: performing surface cleaning, performing texturing treatment, spraying a binding layer, rolling and annealing, wherein before rolling, alloy plating layers are respectively plated on the surfaces of a steel plate and a copper plate, which need to be compounded through an immersion plating or spray coating way, the thickness of each plating layer is 4-8 mu m, and each alloy plating layer contains the following components: 6-8 parts by weight of Zr, 25-50 parts by weight of Zn, 5-30 parts by weight of Al, 10-40 parts by weight of Fe, 0.5-1 part by weight of Si and 0.4-0.6 part by weight of Mo. The production method disclosed by the invention has the beneficial effects that as the bonding layers with the mixture ratio are adopted, the direct bonding property between the steel plate and the copper plate is good; in addition, the compounding temperature is lower, the rolling reduction is smaller and the working cost is saved; and the composite copper-steel material prepared by the method disclosed by the invention has the advantages of high strength, high plasticity and toughness and excellent stress and corrosion resistance.

A welding Al-Cu alloy wire for MIG welding and AC TIG welding contains Cu (5.5-6.5 Wt%), Mn (0.2-0.6), Ti (0.15-0.30), Zr (0.15-0.35), V (0.05-0.20), Ag (0.2-0.5), Si (0-0.1), Fe (0-0.15) and Al (rest). Its preparing process includes such steps as smelting in graphite crucible, refining, removing slag, dehydrogenating, casting, soaking, removing scale, extruding, drawing and scraping. Its advantages are high strength, high plasticity and high cracking resistance.

The invention relates to 7XXX aluminum alloy. The 7XXX aluminum alloy comprises the following components by weight percent: 6.6 to 7.6 percent of zinc, 1.25 to 1.80 percent of magnesium, 0.18 to 0.44 percent of copper, less than or equal to 0.06 percent of silicon, less than or equal to 0.16 percent of iron, , less than or equal to 0.03 percent of manganese, less than or equal to 0.03 percent of chromium, less than or equal to 0.02 percent of germanium, less than or equal to 0.02 percent of vanadium, less than or equal to 0.03 percent of titanium, less than or equal to 0.02 percent of zirconium, and less than or equal to 0.03 percent of total weight of manganese and chromium, less than or equal to 0.03 percent of each rest impurity element, less than or equal to 0.10 percent of total weight of rest impurity elements, and the balance of aluminum. On the basis of experiment, the material strength is improved by re-designing the mass fraction and a ratio of Zn to Mg; by re-designing the mass fraction of Cu, the alloy has excellent corrosion resistance, and the oxidation different color problem of silver white can be solved. By strictly controlling the weight percent of the impurity elements such as Mn and Cr, the crystal grains of the alloy material are uniform. Compared with the existing disclosed Al-Zn alloy system, the alloy has better comprehensive performance, and an oxidized membrane formed by oxidizing the material by virtue of anode is more delicate and beautiful.

The invention relates to a heat treatment process for improving the stress corrosion resistance of a high-strength aluminum alloy, which comprises the following treatments on a heat-treatable high-strength aluminum alloy sequentially: solution treatment, primary quenching treatment, pre-stretching treatment, high-temperature and short-time aging treatment, secondary quenching treatment, and low-temperature aging treatment. The alloy treated by the process can achieve adequate strength and good stress corrosion resistance.

The invention relates to an anti-explosion material, which is made of a cut and extended aluminum alloy foil mesh and has mesh-like or beehive-like porous structure, and is characterized in that: an aluminum alloy foil comprises the following chemical components in percentage by weight: 0.05 to 0.15 percent of silicon, 1.0 to 1.6 percent of copper, 0.2 to 0.5 percent of manganese, 1.0 to 3.0 percent of magnesium, 3.0 to 6.0 percent of zinc, 0.02 to 0.06 percent of titanium, 0.05 to 0.15 percent of zirconium, 0.1 to 0.3 percent of scandium and the balance of aluminum. Meanwhile, the invention also discloses a manufacturing method of the anti-explosion material. The material obtained by the method has the advantages of high electric and heat conductivities and large specific area and has the characteristics of corrosion resistance and high strength. When used as an anti-explosion material, the material is free from scraps and deformation. The material is particularly suitable for safe protection of containers for flammable and combustible liquid containers with high corrosivity as well as skid-mounted gasoline and gas filling station containers.

The invention belongs to the technical field of aluminum alloy production, and relates to a machining method for 7-series aluminum alloy thick plates. Aluminum alloy ingots comprise the following components in percentage by mass: Si not more than 0.20%, Fe not more than 0.25%, 1.2-2.1% of Cu, 1.2-2.2% of Mg, 5.0-7.0% of Zn, 0.02-0.15% of Ti, 0.02-0.15% of Zr, Ti+Zr not more than 0.15%, single impurity not more than 0.05%, total impurity not more than 0.15%, and the balance of Al. The machining method for the aluminum alloy thick plates adopts a mode of multi-pass hot rolling, and adopts double-stage solid solution and double-stage aging to enable the finally prepared 7-series aluminum alloy thick plates to achieve excellent strength and rupture toughness.

The invention relates to a quenching-partitioning thermal treatment method for the high strength and toughness of medium carbon silicon-manganese low alloy steel and aims at solving the problems that the traditional medium carbon silicon-manganese low alloy steel has poor plasticity, toughness, and stress and corrosiveness resistance although having high strength. The quenching-partitioning thermal treatment method comprises the following steps of: carrying out austenization treatment on the medium carbon silicon-manganese low alloy steel, and then carrying out isothermal quenching in the martensite transition temperature range of the medium carbon silicon-manganese low alloy steel; and two. carrying out isothermal partitioning thermal treatment on the medium carbon silicon-manganese low alloy steel treated in the step one in a partitioning temperature from amartensite start (Ms) to 500 DEG C, and then quenching the medium carbon silicon-manganese low alloy steel to reach the room temperature, i.e. finishing the quenching-partitioning thermal treatment on the medium carbon silicon-manganese low alloy steel. After the medium carbon silicon-manganese low alloy steel is treated by the method, for the medium carbon silicon-manganese low alloy steel, the tensile strength reaches 1650MPa-2115MPa, the yield strength reaches 1490MPa-1950MPa, the coefficient of elongation is 5%-10%, and the reduction of area is 20%-50%.

The invention discloses a low-hydrogen type super duplex stainless steel welding rod. The prior duplex stainless steel wire is adopted as a welding core. The coating of the welding rod comprises the compositions in percentage by weight: 35 to 45 percent of marble, 20 to 33 percent of fluorite, 0 to 5 percent of titanium pigment, 2 to 5 percent of potassium feldspar, 0 to 2 percent of sodium carbonate, 5 to 15 percent of iron alloy, 10 to 20 percent of metal powder, and 0 to 2 percent of CrN iron, wherein the iron alloy consists of ferrosilicon and ferromolybdenum under the condition of constant total content, and the metal powder consists of manganese metal, chromium metal, and nickel powder under the condition of the constant total content. After raw materials of the compositions of the coating are mixed evenly, pure sodium water glass with certain Baume concentration is added, and the pressing of the welding rod is performed on welding rod production equipment. The use of the welding rod can satisfy the welding need of super duplex stainless steel in the national engineering construction, the welded welding seam has excellent mechanical property and good corrosion resistance, the tensile strength can reach 800MPa, and the welding rod has good low-temperature toughness.

The invention discloses a high-strength aluminum alloy subjected to carbonitride complex treatment and a preparation method thereof. The alloy comprises the following components in percentage by weight: 2.0-3.2 percent of Cu, less than or equal to 0.2 percent of Mn, 0.2-0.5 percent of Mg, less than or equal to 0.01 percent of Cr, less than or equal to 0.01 percent of Ni, less than or equal to 0.1 percent of Zn, less than or equal to 0.15 percent of Ti, less than or equal to 0.5 percent of Si, less than or equal to 0.5 percent of Fe, and the balance of Al and inevitable trace impurities, wherein the carbonitride MX(C,N)Y is 0.05-2.5 percent of total mass of the furnace burden. The aluminum alloy has the characteristics of high strength and good casting performance.

The present invention relates to one kind of free machining high manganese Cu-Zn alloy, which consists of Cu 45- 70 wt%, Mn 7-30 wt%, Pb 0.2-4 wt%, X 0.0001-2 wt%, and Zn and inevitable impurity for the rest; where, X is at least one of elements Fe, As, P, B, Cr, Li, Ni, Sn, Al. The free machining high manganese Cu-Zn alloy has free machining performance similar to that of lead brass, lowered material cost and excellent plastic working performance, and may be used in producing plastic worked product and cast product.

The invention discloses Ta-contained stress corrosion-resistant Al-Zn-Mg-(Cu) alloy and a preparation method thereof. The alloy contains main alloying elements of Al-Zn-Mg or Al-Zn-Mg-Cu and microalloying elements of Zr, Ta, Fe and Si; moreover, a mass ratio of the microalloying elements satisfies the conditions that Ta is larger than or equal to 0.1Zr and less than or equal to 0.5Zr, Si is larger than or equal to 0.1Zr and less than or equal to 0.3Zr, and Fe/Si is larger than or equal to 0.7 and less than or equal to 1.5; according to the preparation method of the Ta-contained stress corrosion-resistant Al-Zn-Mg-(Cu) alloy, after an ingot metallurgy method is adopted for preparing the alloy, the alloy is subjected to homogenizing treatment, deformation treatment and solid solution waterquenching, and then artificial ageing is conducted. According to the Ta-contained stress corrosion-resistant Al-Zn-Mg-(Cu) alloy and the preparation method thereof, a multielement microalloying methodis adopted, cooperation of the multielement microalloying elements is strictly controlled to form a multielement coherent dispersed phase, recrystallization is completely inhibited, the microalloyingelements are used for improving the corrosion resistance effect of aluminium alloy passive film, high strength and good corrosion resistance performance are combined, and the problem that the strength and the corrosion resistance of existing Al-Zn-Mg-Cu ultrahigh-strength aluminium alloy cannot be achieved at the same time is solved; the preparation method of the Ta-contained stress corrosion-resistant Al-Zn-Mg-(Cu) alloy is simple in technology, and the Ta-contained stress corrosion-resistant Al-Zn-Mg-(Cu) alloy is suitable for industrialized production.

The invention relates to 7000 series aluminum alloys, in particular to a heat treatment method capable of reducing stress of spray-formed 7000 series aluminum alloy products. The heat treatment method comprises a two-stage solid solution treatment step and an artificial ageing treatment step sequentially and is characterized in that after the artificial ageing treatment step and before rough machining or after the rough machining and before finish machining, high-temperature stress-relieving aging is performed, that is, heat preservation is performed at the temperature of 125-155 DEG C for 8-32 h. The heat treatment method can maintain the higher strength level of the spray-formed 7000 series aluminum alloy products, reduce residual stress efficiently and improve the comprehensive performance of the products, the problem of cracking of the products in follow-up machining process is solved, machining deformation of the products is reduced, the machining efficiency is improved, and the dimensional precision is improved.

The invention discloses duplex stainless steel which comprises the following components by weight percent (wt%): not more than 0.03 wt% of C (carbon), 0.4-0.7 wt% of Si (silicon), 1.4-1.7 wt% of Mn (manganese), not more than 0.03 wt% of P (phosphorus), not more than 0.001 wt% of S (sulfur), 22.3-22.7 wt% of Cr (chromium), 5.6-5.9 wt% of Ni (nickel), 3.0-3.2 wt% of Mo (molybdenum), not more than 0.5 wt% of Cu (copper), not more than 0.15 wt% of Al (aluminum), 0.0028-0.0043 wt% of B (boron), 0.145-0.175 wt% of N (nitrogen), not more than 0.005 wt% of Ti (titanium), not more than 0.99 wt% of Pb (plumbum) and the balance of Fe (ferrum). The invention further provides a production process of the duplex stainless steel with strong corrosion resistance, and the duplex stainless steel has the advantages of higher strength, more excellent chloridion pitting corrosion resistance and stress corrosion resistance; simultaneously, the production process is conductive to better product quality.

The present invention relates to ferrite stainless steel and its application in rolling heat resistant steel pipe. The ferrite stainless steel contains: C not more than 0.06 wt%, Cu not more than 0.30 wt%, Si 0.5-2.0 wt%, S not more than 0.030 wt%, Mn not more than 0.6 wt%, P not more than 0.030 wt%, Cr 16.0-25.0 wt%, Ti not more than 0.3wt%, Al 0.5-2.0 wt%, Ni not more than 0.60 wt%, N not more than 0.030 wt%, except Fe. During making heat resistant steel pipe with the ferrite stainless steel, temperature control mode in 100-1050 deg.c is adopted.

The invention relates to a complex processing method for prolonging the service lift of chain grate key parts, belonging to mechanical manufacturing and material processing and application technical field, which comprises: firstly, surface nondestructive testing is carried out on the key parts of the chain grate of process; molten salt complex processing are carried out in parts of the surface according to the surface drawbacks tested by surface nondestructive testing; before the laser shocks, the workpiece surface is coated with black coating layer and use water as protective layer, and the laser shock processes the area which is easy to fatigue and fracture and has concentrated stress. The molten iron pretreatment spray-feeding device before iron-making blast furnace has the advantages of simple shortcut, high efficiency, low maintenance cost, short processing time (30 minutes to 5 hours), and the continuous operation can be realized, thus, high efficiency of production is ensured.

The invention discloses a domestic 08Ni3DR steel thin multi-pass welding process, which is characterized by comprising the following steps of: machining a welding part into a single V-shaped or symmetrical double V-shaped groove, employing thin layer multi-pass welding, wherein on each layer, the weld pass thickness is less than 3mm, the diameter of a welding wire is 3.2mm, the welding current is 350 to 380A, the welding voltage is 34 to 38V and the welding speed is 36 to 45cm per minute, and controlling the interlayer and inter-pass temperature to be less than or equal to 150 DEG C; and performing dehydrogenation treatment and overall stress relief heat treatment after welding, and manufacturing a pressure container with the temperature level of 100 DEG C below zero such as main low temperature methanol wash equipment H2S and a CO2 absorption tower by employing the process, wherein the impact work kv2 of the welding joint of the equipment at the temperature of 101 DEG C below zero is more than or equal to 47J, and the mean value of the technical index and physical level is higher than American society of mechanical engineers (ASME) standard technical index.

The invention discloses high-toughness mining chain steel and a manufacturing method thereof. The high-toughness mining chain steel comprises the following components in percentage by weight: 0.20-0.28% of C, 0.01-0.40% of Si, 0.50-1.50% of Mn, less than or equal to 0.015% of P, less than or equal to 0.005% of S, 0.30-2.00% of Cr, 0.50-2.00% of Ni, 0.10-0.80% of Mo, 0.01-0.30% of Cu, 0.01-0.05% of Al, 0.001-0.10% of Nb, 0.001-0.10% of V, less than or equal to 0.00018% of H, less than or equal to 0.0150% of N, less than or equal to 0.0020% of O and the balance of Fe and inevitable impurities. The manufacturing process comprises the working procedures of smelting, refining, vacuum treatment, casting, heating, forging or rolling, quenching and tempering heat treatment and the like. The chain steel has high strength and good impact toughness, ductility and percentage reduction of area, can resist stress corrosion cracking, has good weather resistance, wear resistance and fatigue resistance, and can be used for engineering machinery, ocean engineering and other occasions needing high-strength and high-toughness steel.

The invention discloses an aluminum alloy variable section extruded profile for spaceflight and a preparation method of the aluminum alloy variable section extruded profile. The profile consists of the following elements of, in percentage by weight, 5.0%-6.0% of Zn, 1.0%-2.0% of Cu, 0.04%-0.1% of Mn, 2.0%-3.0% of Mg, 0.15%-0.25% of Cr, 0.35%-0.42% of Fe, less than or equal to 0.25% of Si, and thebalance Al. During preparation, a finished product is obtained after being subjected to smelting, purifying, standing, casting, homogenizing treatment, ingot heating, extrusion, pre-finishing, solution treatment, straightening finishing, deep machining, aging treatment and fine adjustment treatment. According to the method, by setting specific alloy composition and the preparation process, the aluminum alloy variable section extruded profile formed by once is obtained, the strength, fatigue resistance, corrosion resistance and stress corrosion resistance of the aluminum alloy profile are greatly improved, comprehensive performance requirements of a carrier rocket launcher on the variable section aluminum alloy profile can be met, the bottleneck of extrusion forming of the variable sectionprofile at present is broken, various indexes of the aluminum alloy profile are ensured to meet standards and use requirements, and material guarantee is provided for research of new carrier rockets in China.

A glass grit blasting technology for increasing the stress corrosion resistance of the welded seam between stainless steels includes such steps as cleaning the surface of the welded seam, blasting the glass grits onto the welded seam by a blasting gun driven by compressed air and with an inclination by 70-100 deg.C, cleaning the surface of welded workpiece, and detecting the residual stress by X-ray diffractometer.

The invention relates to a forging and heat treating technology of 7085 aluminum alloy. The forging and heat treating technology comprises the following operation steps of blank material purchasing, blank material cutting and discharging, forging and heating, blank making, inner bore machining, heating, mandrel supporter bore broadening, remelting and heating, ring rolling, cooling, solid solution, cold deformation, aging and machining to the required size. According to the forging and heat treating technology, operation is convenient, transgranular precipitates and grain boundary precipitates are regulated and controlled through a multi-step aging technique under the condition of ensuring the strength, and the stress resistance and the corrosion resistance are promoted.