132 results about "Flow stress" patented technology

The invention relates to an apparatus and process for solid-state deposition and consolidation of powder particles entrained in a subsonic or sonic gas jet onto the surface of an object. Under high velocity impact and thermal plastic deformation, the powder particles adhesively bond to the substrate and cohesively bond together to form consolidated materials with metallurgical bonds. The powder particles and optionally the surface of the object are heated to a temperature that reduces yield strength and permits plastic deformation at low flow stress levels during high velocity impact, but which is not so high as to melt the powder particles.

There is provided an α-β type titanium alloy having a normal-temperature strength equivalent to, or exceeding that of a Ti-6Al-4V alloy generally used as a high-strength titanium alloy, and excellent in hot workability including hot forgeability and subsequent secondary workability, and capable of being hot-worked into a desired shape at a low cost efficiently. There is disclosed an α-β type titanium alloy having high strength and excellent hot workability wherein 0.08-0.25% C is contained, the tensile strength at room temperature (25° C.) after annealing at 700° C. is 895 MPa or more, the flow stress upon greeble test at 850° C. is 200 MPa or less, and the tensile strength/flow stress ratio is 9 or more. A particularly preferred α-β type titanium alloy comprises 3-7% Al and 0.08-025% C as α-stabilizers, and 2.0-6.0% Cr and 0.3-1.0% Fe as β-stabilizers.

The invention relates to a TiAl-intermetallic-compound vacuum diffusing connection method, belonging to the TiAl-intermetallic-compound welding field, which overcomes the technical drawbacks of high temperature of diffusing connection and high pressure of diffusing connection in the prior TiAl-intermetallic-compound diffusing connection technology. The invention adopts hydrogenated titanium or titanium alloy chaff as the interface layer of diffusing connection. Ti3Al+TiAl dual phase (Alpha2+Gamma) organ can be formed under the temperature of diffusing connection titanium, which facilitates the formation of high-intensity connector lug of TiAl-intermetallic-compound diffusing connection. And hydrogen makes the flow stress of thermal deformation of titanium or titanium alloy decrease and the thermal plasticity increase, so that hydrogenated titanium or titanium alloy is prone to deform under high temperature. Meanwhile,, the self-diffusing capacity of hydrogen in titanium or titanium alloy and the diffusing capacity of solute are enhanced, more particularly, in Beta phase the capacities are more enhanced, so that hydrogen can accelerate the diffusing of the alloy elements, reduce the atomic combination energy and the diffusing activation energy, promote the diffusing coordinated deformation capacity, and the reliable diffusing connection of connector lug of TiAl-intermetallic-compound can be realized under comparatively low temperature.

The invention discloses a quick isothermal forging method and device for preparing a less-deformable alloy cake blank. The device comprises a heating device, an automatic feeding device, a horizontal hydraulic forging device, a blank positioning device and a flame heating device. A mould material used by the device is a nickel-based alloy with creep strength which is higher than the flow stress of a forged high-temperature alloy under corresponding forging temperature and deformation rate. In the method, a homogenized electroslag remelting continuous directional solidification technology or other processes with maneuverability can be selected for preparing a high-alloyed less-deformable alloy directional solidification billet, as well as a fine grain billet prepared by adopting the processes, such as powder metallurgy and the like. The method and the device have the advantages of short production period, convenience for control and low cost, and are suitable for mass production of large-size high-clean and uniform tissue high-alloying less-deformable alloy cake blanks.

The invention discloses a refracturing well and layer selecting method based on four-dimensional crustal stress dynamic change. The method includes the steps that S1, a three-dimensional geologic model is set up; S2, a three-dimensional oil deposit model is set up, and producton/injection dynamic parameters are used for predicting a three-dimensional pore pressure field and a temperature field of different periods; S3, a three-dimensional crustal stress model is set up; S4, an initial three-dimensional crustal stress field is formed; S5, a four-dimensional dynamic crustal stress model is set up; S6, interstifial flow-stress coupling solution is carried out, and dynamic crustal stress and pore elastic parameters are analyzed and calculated; S7, a refractured well and layer position are selected preliminarily; S8, interstifial flow-stress-fracture damage coupling model of refracturing is set up; S9, the final fracturing layer segment is determined. The refracturing well and layer selecting method has the advantages of being capable of accurately reflecting the change condition of dynamic crustal stress and pore elastic parameters in the oil and gas development process, optimizing the refractured well and layer position by combining the interstifial flow-stress-fracture damage coupling model, effectively improving oil and gas recovery degree and avoiding aquifer communicating.

The invention relates to a preparation method for a titanium alloy with a high dynamic bearing performance and a low cost. The preparation method comprises the following steps: (1) setting the ranges of the target ingredients of the alloy, wherein from composition, the alloy comprises the following elements in percentage by weight: 2.5-7.0% of aluminium, 2.0-5.5% of vanadium, not greater than 2.5% of iron, 0.1-0.3% of oxygen and the balance of titanium; (2) proportioning according to the target ingredients of the alloy; (3) smelting, and deforming and processing; (4) carrying out heat treatment and surface cleaning on the finished product. According to the preparation method disclosed by the invention, the high dynamic bearing capacity of the titanium alloy is guaranteed through reasonable processing and heat treatment regimes; the impact absorption energy is not less than 300J/cm<3>; when the average dynamic flow stress is not less than 1500MPa, the maximum uniform plastic strain is not less than 0.17; when the average dynamic flow stress is not less than 1400MPa, the maximum uniform plastic strain is not less than 0.20; when the average dynamic flow stress is not less than 1300MPa, the maximum uniform plastic strain is not less than 0.22.

Provided is an austenitic stainless steel sheet which has a product of the 10% flow stress at a strain rate of 1000/s and the uniform elongation at a strain rate of 0.1/s of 450 MPa or more and also has high strength at a high strain rate and improved ductility at a low strain rate. An austenitic stainless steel sheet containing, in % by mass, 0.02 to 0.30% of C, 10.0 to 25.0% of Cr, 3.5 to 10.0% of Ni, 0 to 3.0% of Si, 0.5% to 5.0% of Mn, 0.10 to 0.40% of N, 0 to 3.0% of Mo, 0 to 3.0% of Cu, 0 to 0.10% of Ti, 0 to 0.50% of Nb and 0 to 1.0% of V, wherein the value determined by the following formula: C + 3 * N is 0.4% or more, and the remainder is made up by Fe and impurities. In the austenitic stainless steel sheet, the Md30 value which is defined by formula (1) is 0 to 50 DEG C inclusive, the volume ratio of each of a Cr carbide and a Cr nitride is 1% or less, and the average crystal particle diameter of a parent phase is 10 [mu]m or less.

The invention discloses a method for measuring a large deformation flow stress curve of a metal plate in the field of metal plate volume forming engineering, which comprises the following steps: taking the metal plate, and performing initial stretching test to acquire a real stress-strain curve; acquiring an equivalent strain interval of a subsequent rolling process; diving the equivalent strain interval into n equal parts to acquire the thickness of the plate after each theoretical rolling; taking n blocks of the metal plate, and cold-rolling and machining each block of the metal plate according to the thickness of the plate after theoretical rolling to acquire n actual thickness and then acquire each actual rolling equivalent strain; performing re-stretching test for the cold-rolled n metal plate blocks to acquire n subsequent flow stresses and n subsequent real strains; and further acquiring n data points to acquire the large deformation flow stress curve of the metal plate. The method of the invention can provide accurate material performance parameters for the numerical simulation in a plate volume forming process, and provide basis for engineering personnel to select an extrapolation model.

A superalloy made of a forging nickel-base superalloy such as Rene™ 88DT or ME3 is forged in a forging press having forging dies made of a die nickel-base superalloy. The forging is accomplished by heating to a forging temperature of from about 1700° F. to about 1850° F., and forging at that forging temperature and at a nominal strain rate. The die nickel-base superalloy is selected to have a creep strength of not less than a flow stress of the forging nickel-base superalloy at the forging temperature and strain rate.

An assembled type movable blast wall is formed by a plurality of blast wall units in an assembled mode. Each blast wall unit comprises a base, front pull rods, rear compression bars, a supporting frame, energy absorption layers and connecting bolts. Each supporting frame is fixed on the upper surface of the corresponding base, and one or more energy absorption layers are arranged inside each supporting frame in a filling mode. The energy absorption layers are formed by a plurality of prefabricated bodies which are made of EPS flow state concrete in an arrayed mode. A plurality of slide-resistant piles are distributed on the lower surface of each base. When multiple energy absorption layers are arranged, a middle layer is arranged between every two adjacent energy absorption layers. The assembled type movable blast wall can be deformed easily when undergoing impulse loads of the outside, the deformation is large, however, the flow stress level is quite low, in the compression deformation process, a large amount of power is consumed, the power is converted into energy dissipated in all sorts of modes like deformation, collapsing, fracturing and cell wall friction of holes in the structure, and thus the outside impact energy can be effectively absorbed. The assembled type movable blast wall further has the advantages of being rapid in assembling, low in cost and strong in stability.

The invention provides clad billet for hot working plastic deformation processes for the production of clad products, including, but not limited to, clad pipe and tubing by extrusion of a hollow, bicomponent composite billet having a fully dense structural component and a partially dense component of a specialty alloy at a fraction of porosity predetermined to provide a flow stress compatible with that of the structural component. The components are diffusion bonded to the predetermined fraction of porosity in the specialty component by application of heat and pressure over time, including by hot isostatically pressing the billet components. Computer modeling techniques can be used to determine processing conditions for obtaining flow stress compatibility.

The invention discloses a high-Nb-TiAl alloy diffusion bonding method. According to the method, firstly, vacuum diffusion bonding is carried out on a forged high-Nb-TiAl alloy at a low temperature, and then vacuum annealing treatment is carried out on diffusion bonding samples. By effectively combining high-Nb-TiAl alloy diffusion bonding with vacuum annealing treatment, the joint quality of high-Nb-TiAl alloy diffusion bonding is significantly improved, and the microscopic structure of a weldment can be controlled. Meanwhile, axial pressure stress smaller than alloy flow stress is applied in the diffusion bonding process, so that materials are prevented from being deformed in the diffusion bonding process. The microscopic structure of a diffusion bonding joint obtained through the method is free of unclosed holes, weld interfaces disappear completely, structural evolution is thorough, and the diffusion bonding joint is high in quality.

The invention relates to metal forming, more specifically, to methods for producing titanium alloy articles by superplastic shaping and diffusion welding. The inventive method is particularly suitable for aviation engine building for producing a fan blade-type part. The inventive method for producing an article by superplastic shaping and diffusion welding from at least two titanium alloy blanks consists in designating connectable and not-connectable sections on the surface of at least one blank, in assembling the blanks into a packet, in heating said packet to a specified temperature (T), in exposing it to a specified pressure (p) in such a way that the blanks are connected to each other by diffusion welding and a semi-finished product is obtained, in heating and supplying a pressurised working medium into the semi-finished product internal cavity for superplastically shaping at least one blank in such a way that a desirably shaped article is produced. Said method differs from known methods in that the diffusion welding is carried out through titanium alloy plates whose flow stress is less than the blank flow stress, mainly, when the article is made from at least three blanks and a connection preventing material is applied to the non-connectable sections of at least one part of at least one blank surface.

An apparatus and method for aspirating, irrigating and/or cleansing wounds is provided. The apparatus and method include one or more of the following: simultaneous aspiration and irrigation of the wound, supplying of thermal energy to fluid circulated through the wound; supplying physiologically active agents to the wound; a biodegradable scaffold in contact with the wound bed; and application of stress or flow stress to the wound bed.

The invention relates to a method for analyzing and preventing the forging through flow and the coarse grain defect, which comprises the following steps of: firstly, acquiring the original flow stress-strain data of a metal through an isothermal constant-strain-rate compression test, and constructing a constitutive model of the material; then, importing the data into finite element numerical simulation software, establishing a numerical analysis model, and calculating the metal flow, the stress strain and the temperature field distribution conditions inside a forging piece after the completion of calculation; additionally, physically simulating the forging process of the metal through an upsetting test to obtain the critical conditions such as temperature, strain and the like of the metal coarse grain; and analyzing the causes to the through flow and the coarse grain by combining the test results of numerical simulation and physical simulation, optimizing the forging process, and simulating to verify the optimized forging process in the finite element software. In the invention, the finite element numerical simulation technology and the physical simulation technology are innovatively combined, the optimization of the forging process is realized, the optimized forging process conditions can be verified, so that the material and energy sources can be saved, and the efficiency is increased.

The invention relates to an ultrasonic-assisted fine blanking process and device. According to the process, ultrasonic wave is input to a male die during the process of fine blanking to allow the male die to resonate, the bottom of the male die vibrates under high frequency, and accordingly the features of the traditional fine blanking formation are changed and the quality of blanks is improved. Compared to the traditional fine blanking, the ultrasonic-assisted fine blanking process has the advantages that forming property of fine blanking material is improved, flow stress of the material is reduced, and the quality of fine-blanked parts is improved; forming load is reduced, and the service life of the fine blanking die is prolonged. The invention further designs an ultrasonic-assisted fine blanking die device. The ultrasonic-assisted fine blanking process and device is significant to widening the range of fine blanking materials, improving the quality of fine blanks and prolonging the service life of the fine blanking die.

A method is given for fracturing a formation, in particular far-field in a tight formation, in which at least a portion of the proppant is crushable in situ at some point during pumping, during fracture closure, or at higher Fluid flow stresses experienced later during fracture closure. The closure stress or hydrostatic stress is estimated, then a proppant is selected that is at least partially crushable at that closure stress, and then the fracturing treatment is performed with at least a portion of the total proppant being the selected crushable proppant.

The invention relates to a recognition method of metal material cutting structure model parameters. The method comprises the following steps of 1, adopting a JC constitutive model to describe a cutting constitutive model of a material; 2, conducting compression experiment and fitting on a metal material specimen to solve JC constitutive model parameters of the metal material under a low strain rate; 3, using the constitutive model parameters obtained by recognition through the compression experiment in the step 2 as an initial value to establish an optimization target function; 4, setting a standard value of an error between an experiment value of a flow stress and a predicted value, and obtaining a structure parameter optimal solution of the metal material specimen based on a genetic optimization algorithm; 5, verifying the correctness of the parameters obtained by recognizing the JC structure model of the metal material. According to the recognition method of the metal material cutting structure model parameters, the flow stress value obtained through the JC structure model is very close to an actual flow stress value of the metal material, and the efficiency in the process of recognizing the constitutive model parameters is very high; meanwhile, a special apparatus is not needed to conduct a large quantity of compression experiments, and therefore the cost is lowered.

A stress-relief layer is formed by dispensing a polymer upon a substrate lower surface under conditions to partially embed a low melting-point solder bump that is disposed upon the lower surface. The stress-relief layer flows against the low melting-point solder bump. A stress-compensation collar is formed on a board to which the substrate is mated, and the stress-compensation collar partially embeds the low melting-point solder bump. An article that exhibits a stress-relief layer and a stress-compensation collar is also included. A computing system that includes the low melting-point solder, the stress-relief layer, and the stress-compensation collar is also included.