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49results about How to "Uniform strain" patented technology

Method for simultaneously rolling and expanding two trapezoid-cross-section flange ring forge pieces

The invention relates to a method for simultaneously rolling and expanding two trapezoid-cross-section flange ring forge pieces. The method comprises cutting a cylindrical billet into material sections; heating the material sections from room temperature to austenitizing temperature evenly and keeping warm; then heading, punching and chambering the material sections to be manufactured into ring piece blanks to be rolled and expanded; baking again and heating the obtained blanks to reach target temperature and keep warm; placing the obtained blanks into a hole mould of a ring rolling machine formed by an irregular-shaped driving roller and an irregular-shaped core roller to be rolled, expanded and formed; achieving the ring forge pieces which is narrow at two ends and wide in middle and with the axial height as twice as the height of a target trapezoid flange; cutting the ring forge pieces from the middle of the axial height, symmetrically dividing a work piece into two parts to obtain two trapezoid-cross-section flange ring forge pieces; and finally turning the forge pieces into end product flanges. The method for simultaneously rolling and expanding two trapezoid-cross-section flange ring forge pieces is high in production efficiency, energy-saving, environmental-friendly and capable of improving utilization rate of raw materials and quality of products.
Owner:SHANDONG JIANZHU UNIV

Extrusion forming mould for annular ribs of magnesium alloy shell parts

The invention discloses an extrusion forming mould for annular ribs of magnesium alloy shell parts. The extrusion forming mould mainly comprises an upper mould plate, a mandrel, a split male mould pull rod, split male moulds, tension springs, a male mould sliding guide rail, a split male mould sliding bottom plate, a supporting plate and a cylindrical female mould, wherein the head part of the mandrel is conical, a center hole is formed in the axial direction of the mandrel, one end of the split male mould pull rod is inserted in the center hole, the other end of the split male mould pull rod is fixed on the split male mould sliding bottom plate, the at least two split male moulds are symmetrically arranged around the split male mould pull rod, are fixedly connected with the split male mould pull rod through the tension springs and are arranged in a radial sliding groove of the split male mould sliding bottom plate through the male mould sliding guide rail, a wedge-shaped inclined plane adapting to the conical head part of the mandrel is arranged at the inner side of each split male mould, an arc-shaped extruding bulge is arranged at the arc-shaped wall surface of the outer side of each split male mould, and the arc length of each extruding bulge is more than the distance between each two adjacent extruding bulges. According to the extrusion forming mould, all the split male moulds do radial movement by virtue of the axial movement of the mandrel, metal flows in the radial direction, and thus the annular ribs are generated.
Owner:ZHONGBEI UNIV

Thermal medium bulging test machine

The invention discloses a thermal medium bulging test machine, which mainly consists of a base, a vertical column, a middle beam, an upper beam, a blank cylinder, a heating furnace, a high pressure medium generation device, a bulging device, a bulging height measuring device, a pressure measuring device, an anti-oxidation device and a cooling device, wherein the vertical column is arranged on the base; the middle beam is arranged on the vertical column; the upper beam is arranged on the vertical column; the blank cylinder is arranged on the upper beam; the heating furnace is arranged between the middle beam and the upper beam; the high pressure medium generation device is arranged between the base and the middle beam; the bulging device is arranged in the heating furnace; the bulging height measuring device is arranged on the upper beam; the pressure measuring device is arranged at the outlet end of the high pressure medium device; the anti-oxidation device is connected with the side wall of the heating furnace through a pipeline; and the cooling device is connected with the outlet end of the high pressure medium device and an ejector rod through the pipeline. The base, the middle beam and the upper beam are integrally connected through bolts; the heating furnace is welded and fixed on the middle beam; a cooling separator is fixed on the blank cylinder through the bolts; the ejector rod is fixed on the cooling separator through the bolts; and a cooling water jacket is fixed on the middle beam through the bolts.
Owner:BEIHANG UNIV

Manufacturing method of composite material pressure container

InactiveCN103016950AReduce self-tightening pressureSelf-tightening pressure is metPressure vesselsInternal pressureFree cooling
The invention relates to a manufacturing method of a composite material pressure container, which comprises the following steps: 1, connecting an inflating and pressure-maintaining tooling with a lining, inflating the lining with air having a certain pressure to enable the lining to be subjected to swelling deformation, and calculating to determine the internal pressure of the inflated metal lining according to a formula; 2, keeping the lining in a pressure-maintaining state, and performing twisting processing of fibrous composite materials; 3, after the twisting operation is finished, transferring into a curing oven, and performing rotary hot curing; and 4, after the curing operation is finished, naturally cooling, and slowly releasing the internal air to relieve the pressure, thereby ensuring that the elastic contraction of the lining counteracts the compression stress in the twisting process and the curing contraction of the composite material and the lining can be peeled and separated from the composite material layer. According to the invention, the internal stress required in the self tightening process can be reduced, and the swelling deformation rate of the composite material layer can be reduced, thereby lowering the fiber breakage rate of the composite material layer and ensuring high overall performance of the composite material.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Mask plate, evaporated mask plate assembly and mask plate manufacturing method

InactiveCN108611594AImprove wrinkle stateWrinkled state reducedVacuum evaporation coatingSolid-state devicesEngineeringUtilization rate
The invention relates to a mask plate, an evaporated mask plate assembly and a mask plate manufacturing method, and relates to the technical field of displaying. The mask plate comprises at least twoauxiliary mask plates, and all the auxiliary mask plates extend in the first direction and comprise a plurality of mask units arranged in the first direction in sequence; the side surfaces, facing towards the auxiliary mask plates adjacent to the corresponding auxiliary mask plates, of the corresponding auxiliary mask plates are provided with protruding parts corresponding to the mask units; all the protruding parts protrude outwards in the second direction which is perpendicular to the first direction; and the protruding parts between the adjacent auxiliary mask plates can be in overlap jointso that all the auxiliary mask plates can be spliced to form the mask plate with a flat surface. According to the mask plate, the evaporated mask plate assembly and the mask plate manufacturing method, the edges of the mask units are provided with the protruding parts, all the protruding parts are in overlap joint, thus, on the one hand, stress of an opening zone is balanced, and the corrugated state of the mask plate after stretching is improved; on the other hand, the distance between the mask plates is decreased so that the space utilization rate can be increased; and on another hand, theoverall weight of the mask plates is decreased so that the gravity ptotic amount of the mask plates can be reduced.
Owner:BOE TECH GRP CO LTD

MEMS capacitor film vacuum gauge

The invention provides an MEMS (Micro Electro Mechanical System) capacitor film vacuum gauge, which can realize the measurement of the vacuum degree in a range of 1-1000Pa, and the measurement resolution is 0.5 Pa. A pressure sensing film is a circular film with an island-shaped structure film. The circular film is very uniform in radial stress and strain, and under the same pressure, the deflection of the circular film is larger than that of a square film, so that the sensitivity of the pressure sensing film is higher. The island-shaped structure film can increase the rigidity of the film, sothat the deflection of the pressure sensing film is reduced, the basic capacitance is increased, the resolution ratio is improved, and meanwhile, the linearity of the pressure-capacitance relationship is better. Meanwhile, the circular film with the island-shaped structure film is of a double-side electrode differential type sensitive capacitor structure. When the pressure sensing film deforms due to pressure, the sensitive capacitor outputs two capacitances which are equal in variation and opposite in direction, and a double-differential structure is formed through a subsequent differentialmeasurement circuit, so that the common-mode rejection ratio is improved, the influence of parasitic capacitance, temperature and other factors on a measurement result is eliminated, and the measurement resolution is improved.
Owner:LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH

Forward and backward extrusion forming die and method for curved generatrix type shell

The invention discloses a forward and backward extrusion forming die and method for a curved generatrix type shell. Forward extrusion forming space is formed in the bottom of an extrusion female die forming cavity, when an extrusion male die moves downwards, a blank at the lower end of the extrusion male die mainly flows in the forward direction, the forward extrusion forming space is preferentially filled, forward flowing of materials is promoted, and the dependent variable of the materials in a dead area is increased; and when the extrusion male die continues to move downwards, after the forward extrusion forming space is filled, the blank at the lower end of the extrusion male die mainly flows reversely and fills the forming cavity. An overflow groove is formed in the upper portion of abackward extrusion forming cavity, the extrusion male die is pressed downwards into the overflow groove, the blank is extruded in the forming cavity in a closed mode, the blank flows forwards and backwards at the same time, forward flowing of the materials at an opening is promoted, the dependent variable of the materials in a rigid translation area is increased, and therefore uniform material strain of different parts of the shell is achieved, the problems that after an existing curved generatrix type shell is formed, deformation is uneven, and the difference of mechanical properties of different parts and in different directions is large are solved.
Owner:SHANGHAI JIAO TONG UNIV

Torsion fiber optic acceleration transducer

The invention belongs to metering and testing technologies, and relates to a torsion fiber optic acceleration transducer. The transducer comprises an elastomer, a mass block, and a fiber bragg grating; two end parts of an elastic torsion shaft of the transducer are fixed on a shell of the transducer; the middle part of the elastic torsion shaft is provided with a rotary disc; the rotary disc is provided with an eccentric mass block; the fiber bragg grating with a prestressing force is wound on the periphery of the rotary disc; a leading-out terminal of the fiber bragg grating is fixed on an installation ring; the installation ring is fixed on the shell of the transducer; and an optical signal accesses a demodulation instrument via the leading-out terminal. The torsion fiber optic acceleration transducer has great difference from various design schemes of the conventional fiber optical acceleration transducers; factors of influencing sensitivity and a natural frequency are designed separately, so the sensitivity can be improved by winding a radius under the condition of not changing relevant parameters of the torsion shaft and the mass block, and the contradiction between the sensitivity and the natural frequency is solved; furthermore, by two sections of gratings with equal length and equal prestressing force, which are wound reversely, the temperature compensation problem of the sensor is solved.
Owner:BEIJING CHANGCHENG INST OF METROLOGY & MEASUREMENT AVIATION IND CORP OF CHINA

Preparation method and preparation device of flexible electronic device

The invention provides a preparation method and a preparation device of a flexible electronic device. The preparation method comprises the following steps: uniformly stretching a flexible substrate along the outer contour direction of the flexible substrate; after the flexible substrate is stretched in place, under the stretching state of the flexible substrate, coating the sensitive unit materials on the surface of the flexible substrate in an array mode; and after the sensitive unit material on the flexible substrate is cured, releasing the flexible substrate to enable the flexible substrate to retract to the initial size. According to the preparation method, the flexible substrate is uniformly stretched along the outer contour direction of the flexible substrate, so that the flexible substrate is uniformly deformed outwards along the outer contour direction, the periphery of the flexible substrate is uniformly retracted after the flexible substrate is retracted, the sensitive unit coated on the surface of the flexible substrate is uniformly retracted along with the flexible substrate, the sensitive unit is uniformly retracted, and the strain of the sensitive unit in each direction is uniform; and after retraction, the sensitive unit does not generate cracks or wrinkles.
Owner:SUZHOU INST OF BIOMEDICAL ENG & TECH CHINESE ACADEMY OF SCI

Multidirectional extrusion molding process and die for aluminum alloy shell parts with branches

The invention mainly discloses a multidirectional extrusion molding process and a multidirectional extrusion molding die for an aluminum alloy shell parts with branches. The die mainly comprises driving radial outer sleeves, two split female dies, and a vertical male die. The split female dies are vertically symmetrical to each other and are fixed on a stroke mechanism and can move horizontally; and a model cavity which has a part shape is formed in each split female die. The driving radial outer sleeves are sleeved outside the split female dies; and the inner die surfaces of the driving radial outer sleeves are in fit with the outer die surfaces of the split female dies. The invention also discloses the molding process implemented by using the die. The process comprises the following steps of: performing multidirectional extrusion on the aluminum alloy shell part blank with branches by using the multidirectional extrusion die, placing the blank in a die cavity of the die, and forming the aluminum alloy shell part with branches at one time under the continuous action. The invention effectively overcomes the problems of the conventional manufacturing processes, such as the extrusion molding process, a casting process, a welding process and the like, and the die has a simple structure and a high forming property.
Owner:ZHONGBEI UNIV

Stamping backplane of a micro-arc reflector

The invention discloses a punched back plate of a micro-arc surface reflector, which belongs to the field of back support of solar concentrator reflectors, and comprises a ring-shaped forming part along the edge of the reflector, which is distributed on the left and right sides of the ring-shaped forming part. Two arc-shaped molding parts that are left-right symmetrical and protrude inward, two sets of upper and lower symmetrical arc-shaped connecting arms connecting the central areas of the two arc-shaped molding parts, and at least four evenly distributed circumferentially connecting ring-shaped molding parts. point and intersect with the arc-shaped forming part to form or intersect to form a rhombus or regular polygonal reinforcing arm; the ring-shaped forming part forms a plane structure, and the arc-shaped forming part, connecting arm and reinforcing arm form a plane structure opposite to the plane. Slightly curved surface concave towards its central region. The invention improves the surface shape accuracy and reflection light spot quality of the reflective surface of the heliostat, improves the manufacturing efficiency and the consistency of component sizes of the supporting structural parts of the reflective mirror, and reduces the manufacturing cost of the structural parts of the heliostat.
Owner:DONGFANG BOILER GROUP OF DONGFANG ELECTRIC CORP

Manufacturing method of composite material pressure container

InactiveCN103016950BReduce self-tightening pressureSelf-tightening pressure is metPressure vesselsInternal pressureFree cooling
The invention relates to a manufacturing method of a composite material pressure container, which comprises the following steps: 1, connecting an inflating and pressure-maintaining tooling with a lining, inflating the lining with air having a certain pressure to enable the lining to be subjected to swelling deformation, and calculating to determine the internal pressure of the inflated metal lining according to a formula; 2, keeping the lining in a pressure-maintaining state, and performing twisting processing of fibrous composite materials; 3, after the twisting operation is finished, transferring into a curing oven, and performing rotary hot curing; and 4, after the curing operation is finished, naturally cooling, and slowly releasing the internal air to relieve the pressure, thereby ensuring that the elastic contraction of the lining counteracts the compression stress in the twisting process and the curing contraction of the composite material and the lining can be peeled and separated from the composite material layer. According to the invention, the internal stress required in the self tightening process can be reduced, and the swelling deformation rate of the composite material layer can be reduced, thereby lowering the fiber breakage rate of the composite material layer and ensuring high overall performance of the composite material.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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