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30results about How to "Increased creep life" patented technology

Thermal treatment method capable of prolonging long-time service life of welding seams in magnesium-alloy friction stir welding process

InactiveCN110438325AIncrease the degree of lattice distortionIncrease recrystallization nucleation pointFurnace typesHeat treatment furnacesQuenchingWeld seam
The invention discloses a thermal treatment method capable of prolonging the long-time service life of welding seams in the magnesium-alloy friction stir welding process. The method comprises the steps that aging treatment and water quenching are conducted on a magnesium alloy subjected to solution treatment for 0.5 h to 72 h at 180 DEG C to 280 DEG C; friction stir welding is conducted at room temperature, wherein the rotating speed ranges from 100 rpm to 1,000 rpm, and the welding speed ranges from 20 mm/min to 120 mm/min; and annealing treatment is conducted on the welded magnesium alloy for 0.5 h to 10 h at 250 DEG C to 350 DEG C, the magnesium alloy is directly cooled to 100 DEG C to 200 DEG C after being annealed, and then aging treatment and water quenching are conducted for 0.5 h to 6 h. According to the thermal treatment method, a precipitated phase is introduced for the magnesium alloy, the lattice distortion degree is increased, and the crystallization rate is increased; andrare earth magnesium alloy or high-alloyed magnesium alloy which is difficult to recrystallize is rapidly crystallized in the friction stir welding process, so that the yield strength of the weldingseams is improved, and synchronous improvement of the long-time service lives in the directions parallel to or perpendicular to the welding seam direction is achieved.
Owner:CENT SOUTH UNIV

Fir-tree type disc tenon connecting device

The invention relates to a fir-tree type disc tenon connecting device. The fir-tree type disc tenon connecting device comprises a tenon and a tenon groove which are connected in a matched mode, wherein the tenon comprises a first tenon tooth and a second tenon tooth which are symmetrically arranged in structures; tooth widths of tooth surfaces which are arranged on the first tenon tooth and the second tenon tooth are equal; tooth widths of lower planes which are arranged on the first tenon tooth and the second tenon tooth are equal; pressure angles of the tooth surfaces are the same; a tooth end surface of the second tenon tooth is a plane; the tenon groove comprises a first tenon groove and a second tenon groove, and the first tenon groove and the second tenon groove are correspondingly arranged; the first tenon groove and the second tenon groove are each provided with a plane groove surface adhered to the corresponding tooth surface and a large circular arc connected with the corresponding groove surface in a cutting mode; and the bottom of each groove is a plane. By adopting the fir-tree type disc tenon connecting device, the problem of stress concentration at a connecting partof the blade tenon and the wheel disc tenon groove is greatly improved, so that a cooling air channel between the tenon and the tenon groove is enlarged, the temperature of the connecting part is greatly reduced, the working reliability is good, and the high-quality requirement of an aeroengine for a turbine rotor is met.
Owner:BEIJING SNECMA SAIC TURBOTECH CO LTD

A kind of rhenium-free nickel-based single crystal superalloy and preparation method thereof

The invention discloses a rhenium-free nickel-based single crystal superalloy and a preparation method thereof. The composition of the rhenium-free nickel-based single crystal superalloy of the present invention is represented by mass percentage as 7.25-7.75% of Cr, 4.8-5.2% of Co, 1.8-2.2% of Mo, 7.8-8.2% of W, and 6.3-6.7% of Ta , 6.0-6.2% Al, 0.12-0.18% Hf, 0.04-0.06% C, 0.003-0.005% B, 0.010-0.030% Y, and the rest is Ni. The preparation of the above-mentioned rhenium-free nickel-based single crystal superalloy comprises the following steps: using a vacuum induction furnace to melt the master alloy, and preparing a cast rod of the master alloy by gravity casting; using the seed crystal method to pass the Bridgeman directional solidification technology at a temperature gradient of 150-250K / cm , the single crystal test bar was prepared at a pulling rate of 5-100 μm / s; the single crystal superalloy was solid solution treated in the range of 1295-1305 °C for 2-4 hours, followed by air cooling, and then in the range of 1090-1310 °C 2-4 hours of high-temperature aging treatment within 2-4 hours, followed by air cooling; then 16-24 hours of low-temperature aging treatment in the range of 850-890 ° C, followed by air cooling.
Owner:NANJING UNIV OF SCI & TECH

A heat treatment method for improving the long service life of friction stir welding welds of magnesium alloys

The invention discloses a thermal treatment method capable of prolonging the long-time service life of welding seams in the magnesium-alloy friction stir welding process. The method comprises the steps that aging treatment and water quenching are conducted on a magnesium alloy subjected to solution treatment for 0.5 h to 72 h at 180 DEG C to 280 DEG C; friction stir welding is conducted at room temperature, wherein the rotating speed ranges from 100 rpm to 1,000 rpm, and the welding speed ranges from 20 mm / min to 120 mm / min; and annealing treatment is conducted on the welded magnesium alloy for 0.5 h to 10 h at 250 DEG C to 350 DEG C, the magnesium alloy is directly cooled to 100 DEG C to 200 DEG C after being annealed, and then aging treatment and water quenching are conducted for 0.5 h to 6 h. According to the thermal treatment method, a precipitated phase is introduced for the magnesium alloy, the lattice distortion degree is increased, and the crystallization rate is increased; andrare earth magnesium alloy or high-alloyed magnesium alloy which is difficult to recrystallize is rapidly crystallized in the friction stir welding process, so that the yield strength of the weldingseams is improved, and synchronous improvement of the long-time service lives in the directions parallel to or perpendicular to the welding seam direction is achieved.
Owner:CENT SOUTH UNIV

A heat-resistant flame-retardant magnesium alloy and its deformation heat treatment method

InactiveCN110438380BSignificant age strengtheningIncreased creep lifeSolution treatmentIngot
The invention discloses a heat-resistant flame-retardant magnesium alloy and a thermo-mechanical treatment method thereof. The magnesium alloy comprises the following elements by mass: 3-16% of Gd, 4-8% of Er, 0.2-1% of Ca, 0.02-0.2% of Zn and the balance being Mg, wherein the mass ratio of Ca to Zn is >= 3. Magnesium alloy ingot billets are prepared by semi-continuous casting, and subjected to hot rolling or hot extrusion to form a plate being 5-25 mm in thickness, the plate is subjected to solid solution treatment, aging is performed at 200-260 DEG C, and water quenching is performed; and then, true strain is performed between room temperature and 100 DEG C, then aging is performed at 150-220 DEG C, and water quenching is performed. The alloy prepared in the invention contains a honeycomb microstructure consisting of a prismatic-plane precipitated phase, a prismatic-plane dislocation, a basal-plane precipitated phase and a basal-plane dislocation; the effect of the synchronous improvement on the heat-resistant and flame-retardant properties of the magnesium alloy is significant; simple equipment, low production cost and high efficiency are achieved; and the magnesium alloy is suitable for use in the industries of aeronautics and astronautics, railway trains and automobile lightweight.
Owner:CENT SOUTH UNIV
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