90results about How to "Eliminate processing stress" patented technology

The invention discloses a method for welding a thick aluminum alloy plate. The method comprises the following steps of: blanking from a large aluminum plate according to a specified size: butting two opposite edges to be welded and forming two U-shaped welding grooves on the upper surface and the lower surface of the thick aluminum alloy plate; washing an aluminum alloy and a welding wire with acetone, removing oxidation films on the surfaces of the U-shaped welding grooves, and wiping; and welding the U-shaped welding grooves by using an inverted consumable electrode argon arc welding machine of which the maximum output current is 500 A, welding, annealing, and performing relief annealing in a subsequent further machining process. In the method, preheating is not required before welding, so that the labor intensity is effectively lowered, the mechanical property of a welding joint is improved, the internal quality of a weld seam of a thick aluminum plate is improved, and the welding strength is required to be over 90 percent of parent substrate strength.

The invention discloses high-strength steel. The high-strength steel comprises the following chemical elements in percentage by mass: 0.07% to 0.15% of C, 0.1% to 1.0% of Si, 2.0% to 2.6% of Mn, 0.05% to 0.6% of Ni, 0.2% to 1.0% of Cr, 0.1% to 0.6% of Mo, 0.001% to 0.006% of B, 0.05% to 0.50% of Cu, 0.015% to 0.060% of Al, 0.02% to 0.1% of Nb, 0.02% to 0.15% of V, and the balance Fe and unavoidable impurities. Correspondingly, the invention further discloses a high-strength plastic seamless steel pipe for automotive driver shafts. The high-strength plastic seamless steel pipe for the automotive driver shafts is manufactured by the high-strength steel. In addition, the invention further discloses a manufacturing method of the high-strength plastic seamless steel pipe for the automotive driver shafts. The high-strength plastic seamless steel pipe for the automotive driver shafts is high in strength, high in strength and ductility product and good in anti-torsion fatigue performance.

The invention belongs to the technical field of powder metallurgy machining, and particularly relates to a preparing method for a molybdenum and molybdenum alloy pipe. The technology steps of molybdenum and molybdenum alloy pipe blank preparing, molybdenum pipe hot rolling, molybdenum pipe warm rolling and surface treatment and control over the technology conditions are adopted, and the super-long and thin-wall seamless molybdenum and molybdenum alloy pipe is prepared. Due to the comprehensive effects of hot rolling and warm rolling, the molybdenum and molybdenum alloy pipe prepared through the method achieves the beneficial effects that the molybdenum pipe is super long, thin in wall and seamless, the yield is high, and the comprehensive utilization rate of materials is high. The large deformation rate is achieved when molybdenum and a molybdenum alloy are used for preparing the pipe, an inner structure of the molybdenum pipe is refined and homogenized, and the mechanical performance is excellent; and an existing molybdenum pipe preparing technology is simplified, the materials are saved, and implementation is easy.

The invention discloses a forming process of a nickel-based bimetal composite tube, comprising the steps of pretreating, forming by cold pushing, performing solution treatment, and tempering; the stepof forming by cold pushing includes placing a nickel-based bimetal composite tube in a die of a cold-extrusion former, and allowing a punch of the cold-extrusion former to act on the nickel-based bimetal composite tube through a forming hole arranged in the die so as to finish forming by cold pushing; the forming by cold pushing, solution treatment and tempering are performed sequentially repeatedly until the nickel-based bimetal composite tube reaches finish specifications; ends of the nickel-based bimetal composite tube are cut off by flame cutting, sawing, toothless saw cutting or plasma cutting, and the finished composite tube is obtained; iron oxide skin on the inner and outer surfaces of the finished composite tube is removed by chemical or mechanical means. The forming process of the nickel-based bimetal composite tube can provide reduced production cost and improved production efficiency.

The invention discloses a method for machining sealing rings. The method comprises the following steps of (1) carrying wiredrawing on metal bar materials, (2) carrying out heat treatment, (3) winding the wiredrawn metal bar materials into a spring shape, (4) cutting the metal bar materials into multiple twisted ring-shaped components with openings, (5) leveling the ring-shaped components, (6) carrying out quench tempering, (7) grinding the inner circumferential surfaces and the outer circumferential surfaces of the ring-shaped components so that the inner circumferential surfaces and the outer circumferential surfaces of the ring-shaped components can be regular arcs, (8) opening the openings of the ring-shaped components to a preset size and then carrying out heat shaping, (9) obtaining the formed sealing rings. According to the method for machining the sealing rings, material waste is quite low, the machined sealing rings are high in strength, toughness and elasticity and uniform in wall thickness, the thermal elastic loss and the residual deformation of the machined sealing rings are both small, latent defects of the sealing rings can be exposed in the early stage of machining, and the sealing rings with the latent defects can be picked out.

The invention belongs to the technical field of heat treatment, in particular to a composite stepped carburizing and quenching technology of a gear shaft. The composite stepped carburizing and quenching technology of the gear shaft includes the steps of entering furnace and heating, preserving heat, reheating, preserving heat of the stepped carburizing and quenching, reducing temperature and preserving heat, outing furnace and quenching, and the like. By adoption the composite stepped carburizing and quenching technology of the gear shaft, a constant temperature is firstly applied at a temperature below the critical point of the transformation before the workpiece is carburized, the temperature of the workpiece tends to be uniform inside and outside the temperature, thus, the internal and external temperature difference, the heating speed, and the thermal stress are reduced; and in carburizing stage, the stepped carburizing is adopted, that is, increase of cyclation and decrease of carbon concentration gradient, thus, the diffusion rate of carbon atoms is increased, the holding time of workpieces at high temperature is reduced, the deformation of heat treatment is reduced, and the requirements of metallurgical structure and mechanical properties are met.

The invention relates to a post-forging dehydrogenation annealing technology of a chromium-containing high-nickel alloy steel forged piece. The technology comprises the specific steps of after forging, slowly cooling the forged piece to 500 to 700 DEG C, keeping the temperature, increasing the temperature with full power to a temperature 100 to 150 DEG C above a complete austenitizing temperature, keeping the temperature, cooling to a temperature 50 to 100 DEG C below a martensite transformation starting temperature, and keeping the temperature for a short time; increasing the temperature to a high-temperature tempering zone at the speed of 30 to 60 DEG C/h, keeping the temperature, after temperature keeping, carrying out furnace cooling to 400 DEG C at the speed of 30 to 60 DEG C/h, and carrying out furnace cooling to a temperature 10 to 50 DEG C below a martensite transformation ending temperature at the speed of 10 to 30 DEG C/h; and increasing the temperature to the high-temperature tempering zone at the speed of 30 to 60 DEG C/h, keeping the temperature, after temperature keeping, carrying out furnace cooling to 100 to 150 DEG C at the speed of 10 to 30 DEG C/h, taking the forged piece out of a furnace, and carrying out air cooling. According to the post-forging dehydrogenation annealing technology of the chromium-containing high-nickel alloy steel forged piece, the problems that annealing and dehydrogenation are difficult to carry out on the chromium-containing high-nickel alloy steel forged piece through a conventional method, and ultrasonic flaw detection defects are caused by white dots of forged pieces with relatively large specifications are solved better.

The invention discloses an annealing method of a ceramic rear cover, and belongs to the field of ceramic rear cover machining. The method comprises the following steps: putting the ceramic rear coverinto an annealing furnace, rising the temperature to a 600 to 800 DEG C medium temperature zone, and performing heat preservation for 1 to 2 hours; rising the temperature to a 1000 to 1200 high temperature zone after heat preservation is performed in the medium temperature zone, and performing heat preservation for 3 to 4 hours in the high temperature zone; reducing the temperature to 800 to 900 DEG C after high temperature preservation is performed, and ensuring that the time is controlled to be 1 to 2 hours; naturally cooling the ceramic rear cover to the room temperature, and then discharging the ceramic rear cover, so as to accomplish annealing. The method has the benefits that a gradient temperature rising and reducing technology is adopted; through twice time rise and twice temperature reduction, the ceramic rear cover is kept in the two temperature zones for a certain period of time, then crystal particles inside the ceramic rear cover are grown by stages, interaction force among the crystal particles is fully released, the crystal particles are more uniformly distributed, and an arrangement structure among the crystal particles is more stable, so that stress produced duringfine carving of the ceramic rear cover is effectively reduced, the fact that the deformation of the ceramic rear cover is below 0.08mm after annealing treatment is ensured, and the assembly requirement of mobile phones is met.

The invention relates to a machining technology of U-shaped pieces, in particular to a binaural U-shaped piece welding-free integrated finish machining method for a thermonuclear fusion reactor. The binaural U-shaped piece welding-free integrated finish machining method comprises the steps of manufacturing U-shaped blank pieces by using a forming die; carrying out first ultrasonic flaw detection on the U-shaped blank pieces after rough machining is carried out on the U-shaped blank pieces; carrying out rough machining again after heat treatment is carried out, then carrying out second ultrasonic flaw detection, picking out qualified U-shaped pieces, and carrying out a performance test by extracting samples from bodies; machining the U-shaped pieces which are qualified in the performance test into U-shaped pieces with allowance, and then manufacturing the U-shaped pieces into primary semi-finish machining U-shaped pieces by carrying out first artificial aging treatment on the U-shaped pieces; machining the primary semi-finish machining U-shaped pieces into U-shaped pieces with allowance, and then manufacturing the U-shaped pieces into secondary semi-finish machining U-shaped pieces by carrying out second artificial aging treatment on the U-shaped pieces; machining the secondary semi-finish machining U-shaped pieces into finish machining U-shaped pieces, drilling through holes in the end surfaces of side plates of the finish machining U-shaped pieces, and obtaining finished U-shaped pieces through WEDM (Wire Electrical Discharge Machining) after a metal wire is enabled to penetrate through the through holes. The binaural U-shaped piece welding-free integrated finish machining method disclosed by the invention has the advantages that the machining efficiency is high, and the product quality is good.

The invention discloses a necking process method for a titanium alloy self-locking nut. The method comprises the following steps: S1: performing solid solution heat treatment on a titanium alloy self-locking nut sample prepared by machining to manufacture a sample to be necked; S2: performing necking processing on the sample to be necked at room temperature; and S3 after the necking processing isfinished, performing aging treatment on the titanium alloy self-locking nut, thereby finishing the necking processing of the whole titanium alloy self-locking nut. The possibility that the titanium alloy self-locking nut generates cracks in the process of necking processing process is reduced, the difficult problem that the titanium alloy nut is necked and deformed at room temperature and threadsare cracked is solved, and the necking is realized at the room temperature; and meanwhile, a necking tool is matched, and the tool is more compact in structure, more convenient to operate, more accurate in position and size control, and higher in safety and reliability.

The invention discloses a production method of high-silicon electrical steel. Molten steel with the contents of two kinds of silicon being 2.0%-3.5% and 4.5%-7.0% correspondingly is smelted, and the superheat degree of the molten steel is 10-30 DEG C; a drainage device is arranged in a continuous casting crystallizer, opened downwards and suspended in the molten steel, the gap between the drainagedevice and the crystallizer is 10-40 mm, the high-silicon molten steel is added into the drainage device, low-silicon molten steel flows between the drainage device and the crystallizer, the pullingspeed is 0.4-0.9 m/min, the thickness ratio of a low-silicon blank shell to a high-silicon blank core of a cast blank is 1:2-1:5, inert gas is charged into the drainage device, and thus the internal liquid level of the drainage device is 10-20 mm lower than the external liquid level of the drainage device; the thickness of a hot-rolled roll is 0.8-1.8 mm; and before cold rolling, preheating is carried out to 200-450 DEG C, the annealing temperature is 600-1000 DEG C, and heat-preserving time is 10-200 min. Finished products have good electromagnetic performance and iron loss performance.

The invention relates to the technical field of cutters, in particular to a preparation method of a high-strength and high-toughness titanium alloy material cutter. The preparation method comprises the following steps that S1, raw materials are prepared; S2, punching is carried out, wherein the prepared titanium alloy materials are fed into a punching workshop for cutting, and a cutter blank is cut according to the size of the cutter, and the size and the thickness of a cutter sample; S3, heat treatment is carried out, and specifically heat treatment is carried out on the cut cutter blank; S4,surface hydrogen permeation is carried out; and S5, film coating is carried out, wherein a Ti-DLC film is plated on the surface of the cutter blank by using a magnetron sputtering method, microporesin the DLC film layer are plugged through fluorine-containing acrylate monomers, so that the wear resistance of the cutter is improved, the toughness of a substrate is not reduced, the coating has a fine structure, so that the compressive stress is produced inside the coating, the anti-crack propagation capability is high, and the service performance of the cutter is improved.

The invention discloses a thermal processing method for a spiral bevel gear. The method comprises the steps of basket loading operation, cleaning treatment before furnace charging, carburizing treatment, isothermal quenching treatment, cleaning treatment after quenching, tempering treatment, air cooling treatment, and the like. According to the thermal processing method for a spiral bevel gear, the carburizing treatment adopts a heating manner of step temperature rising and temperature preserving, therefore, temperature differences of respective parts of the spiral bevel gear can be reduced, generation of a machining stress is eliminated, and deformation of the spiral bevel gear caused by too fast heating is reduced; since the isothermal quenching treatment is adopted after the carburizing treatment, a constant oil pool temperature ensures uniform cooling of the spiral bevel gear, deformation of the spiral bevel gear is reduced, the thermal processing deformation of the spiral bevel gear is reduced, and a higher thermal processing finished product rate of the spiral bevel gear is ensured.

The invention discloses a machining method for a PH13-8Mo part used for aviation. The machining method includes the following steps that firstly, a PH13-8Mo bar is subjected to blanking and blank manufacturing and subjected to at least one time of die forging and edge cutting, a forge piece in a certain shape is formed, annealing is conducted at the temperature being 600 DEG C to 760 DEG C, and residual stress in the forging process is eliminated; secondly, the forge piece is subjected to solution treatment; thirdly, the forge piece is subjected to cold treatment; fourthly, after cold treatment is completed, the forge piece is subjected to rough machining, and a blank part is formed initially; fifthly, the manufactured blank part is subjected to manual aging treatment; and sixthly, finishmachining is conducted on the blank part, and a finished product is manufactured. By means of the machining method, a cold and heat combined technology scheme is adopted, the part is subjected to rough machining in a solid solution state, removing work of most of materials is completed under the low hardness, the cutting speed is increased, and the tool loss amount is reduced; and the equivalent thickness of the forge piece obtained after rough machining is reduced, the heating time and energy consumption of subsequent manual aging are reduced, furthermore, heat correction can be conducted onpart deformation, part of machining stress is eliminated, and part deformation is reduced.

The invention discloses a preparing method for a spliced combined structure composite metal sheet and the composite metal sheet of the preparing method. At least two kinds of heterogeneous metal materials are subjected to solid-phase composition, and a non-side-face composite structural layered composite initial blank is obtained; the layered composite metal initial blank is subjected to plastic forming machining, straightening and cutting treatment, and a non-side-face composite structural layered composite metal long strip is manufactured; a slicing type cutting technology is adopted on the obtained non-side-face composite structural layered composite metal long strip, and multiple composite metal sheet blanks are manufactured; and the composite metal sheet blanks are subjected to machining and surface treatment, and the composite metal sheet is formed. The manufactured spliced metal sheet is formed in the manner that at least two kinds of metal sheets are tightly combined through mutual contact side faces in a firm physical metallurgy bonding manner. The spliced composite metal sheet has more reliable welding characteristics, and the production cost is obviously reduced while the performance requirements for good electric conduction, heat dissipation, weight reduction, transition connection and the like of overall parts are met.

The process of making environment friendly silver metal oxide rivet contact includes the following steps: pre-upsetting the silver metal oxide wire in a cold upsetting machine to form upset ball, annealing in an air annealing furnace, washing and stoving, punching the upset ball in a rotary rivet forming punch to form the metal oxide rivet contact, and high temperature annealing to obtain soft environment friendly silver metal oxide rivet contact without cracking.

The invention relates to a manufacturing method of a thin-walled large-diameter pipe with high-pressure copper-nickel alloy for marine engineering. The manufacturing method comprises the following steps: (1), performing semi-continuous casting on copper and nickle as raw materials to obtain a copper-nickel alloy solid round billet; (2), performing boring: boring in the center of the copper-nickelalloy solid round billet to obtain an inner hole which can penetrate through the center of the copper-nickel alloy solid round billet in the axial direction; (3), performing reaming: heating a billetmaterial, controlling the outside diameter to be invariable, and reaming the inner hole by 3.5 times to 7 times; (4), performing hot extrusion: carrying out water sealing and extrusion on the billet material into hot extrusion pipe in a way of matching with an extrusion module and extruding a steel pipe in the radial direction and in the axial direction, enabling a discharging end of the extrusionmodule to be directly in abutting joint with a water sealing tank, and directly immersing a pipe billet subjected to hot extrusion molding into water to ensure that the pipe billet is isolated from the air so as to prevent oxidation, removing a surface layer of the pipe billet subjected to hot extrusion, and eliminating surface defects; (5), performing straightening: straightening the pipe billetsubjected to hot extrusion; (6), stretching or cold-rolling the pipe billet in several times until a final specification of the pipe billet is obtained, and carrying out annealing after stretching orcold rolling is performed every time; (7) shaping; and (8) performing formation and thermal treatment.