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180results about How to "Reduce processing deformation" patented technology

Method and clamp for moulding surface positioning clamping of finish forge blade

The invention relates to a method and a clamp for moulding surface positioning clamping of a finish forge blade. According to the method, a vane is subjected to positioning clamping through a basin mounding surface of the blade, an inner side moulding surface of a blade root marginal plate, and a V point on the inner side mounting surface of the blade root marginal plate, by the positioning of an air inlet edge, and the clamping of a back mounding surface of the blade, as well as by using a high-accuracy positioning adhesive, and an adhesive coating method, and through a positioning block of the basin moulding surface of the blade and a clamping block of the back moulding surface of the blade. According to the method and the clamp, a satisfying contact area can be obtained by adoption of the high-accuracy adhesive, and the positioning rigidity of the blade is enhanced by adoption of the basin moulding surface of the blade, the inner side moulding surface of the blade root marginal plate and the V point on the inner side moulding surface of the blade root marginal plate for the positioning. According to the method and the device, the problems that the accurate positioning is difficult to realize and the moulding surface of the blade deforms or is damaged because the blade is thin, the blade body is small and the moulding surface is complex are solved. By the method and the device, the positioning accuracy of the mechanical processing of the blade is improved, and the technological process is optimized, so that the processing quality and the production efficiency of the blade are improved, the process is simple, the number of fixtures is reduced, the processing cycle is shortened, and the production cost is reduced.
Owner:AECC AVIATION POWER CO LTD

Processing method of large-scale thin-wall cabin shell body and clamp

The invention relates to a processing method of a large-scale thin-wall cabin shell body. The processing method comprises the steps of 1, reserving a criterion boss on the shape of the shell body when casting the shell body, conducting rough machining on the lineation criterion, leveling a front and back end surfaces of the shell body, and conducting rough machining on the front and back end surfaces of the shell body; 2, conducting rough machining on shape and an inner cavity of the shell body according to the processing criterion in the step 1, conducting aging treatment after the rough machining, and detecting form and location tolerance deformation quantities of the shell body before and after the aging treatment; 3, analyzing remaining quantities of various parts of specially shaped end of the shell body according to a deformation rule of the shell body, judging whether there is a need to borrow quantity, finishing semi-finishing on the shape and the inner cavity of the shell body, and conducting aging treatment after the semi-finishing; 4, detecting the form and location tolerance deformation quantities before and after the aging treatment of the shell body in the step 4, further figuring out the deformation rule of the shell body, and finishing finish machining of the shell body; 5, finally detecting all the sizes of the shell body and storing the shell body into a storage after the shell body is qualified. The invention also relates to a clamp used according to the method. The processing method can improve sharply processing efficiency, guarantee the quality of a product, causes a small processing deformation, and can guarantee the homogeneity of shell wall thickness.
Owner:航天科工哈尔滨风华有限公司

Integrated active-passive compliant one-dimensional variable force grinding and polishing device and control method

The invention belongs to the technical field of intelligent processing and manufacturing, and particularly discloses an integrated active-passive compliant one-dimensional variable force grinding andpolishing device and a control method. The integrated active-passive compliant one-dimensional variable force grinding and polishing device comprises a linear module servo motion platform, a mountingflange, a limiting plate, a position and orientation sensor, a speed-adjustable compliant grinding and polishing mechanism and a controller, and the linear module servo motion platform is used for driving the grinding and polishing mechanism to perform linear motion; the mounting flange and the limiting plate are mounted on a base of the linear module servo motion platform, and the position and orientation sensor and the speed-adjustable compliant grinding and polishing mechanism are installed on the limiting plate; and the position and orientation sensor is used for measuring position and orientation of the one-dimensional variable force grinding and polishing device and sending the position and orientation to the controller, a force sensor is arranged between the compliant grinding and polishing mechanism and sliding blocks, the force sensor is used for collecting a contact force signal and send to the controller which can calculate speed control quantity, and the speed-adjustable compliant grinding and polishing mechanism is driven to move by rotation of a servo motor according to the speed control quantity. According to the integrated active-passive compliant one-dimensional variable force grinding and polishing device and the control method, the contact status of a abrasive belt and a workpiece can be adjusted in real time, and a stable and compliant grinding and polishingprocess is realized.
Owner:HUAZHONG UNIV OF SCI & TECH

Thin-walled bearing ring lathing process

The invention discloses a thin-walled bearing ring lathing process. The thin-walled bearing ring lathing process includes the following steps of firstly, conducting rough lathing, wherein the outer circle, the inner hole, the ditch and the two end faces of a thin-walled bearing ring part are lathed in a numerical control mode, a balance of 0.3 mm to 0.5 mm is controlled to be reserved for the outer circle, a balance of 0.6 mm to 0.8 mm is reserved for the inner hole, a balance of 0.2 mm to 0.3 mm is reserved for the ditch, and a balance of 0.2 mm to 0.5 mm is reserved for the two end faces; secondly, conducting annealing, wherein the roughly-lathed thin-walled bearing ring part is annealed at a temperature of 650 DEG C to 680 DEG C for 3 hours to 4 hours and then cooled in a furnace till the temperature reaches 180 DEG C to 200 DEG C and cooled outside the furnace through air; thirdly, conducting fine lathing, wherein the outer circle, the inner hole, the ditch and the two end faces of the annealed thin-walled bearing ring part are latched in a numerical control module, and the sizes of the outer circle, the inner hole, the ditch and the two end faces are lathed into the sizes required by grinding. In this way, the machining deformation of a thin-walled bearing ring can be reduced, and the machining accuracy of a product can be ensured.
Owner:CHANGSHU CHANGZHOU BEARING

Processing method for stop plate-free split casing

ActiveCN103769816AUniform finishing allowanceReduce processing difficultyOne passMachining deformation
The invention provides a processing method for a stop plate-free split casing. The processing method for the stop plate-free split casing comprises the following steps: milling the external profile section of a part into two semicircles with offset at a roughing stage; turning an internal profile section into a circle; performing finish milling on the back face of the junction surface of the casing to meet the set tolerance requirements; performing linear cutting along the junction surface of the casing to cut off the casing and performing the finish milling on the junction surface to meet the set tolerance requirements, and connecting the two half casings by using bolts at the junction surface of the casing to finish reassembly of the casing; performing finishing on the internal profile and the external profile of the casing. After roughing, the non-uniform wall thickness of the casing is formed; after the casing is cut off by the linear cutting, the finish milling is performed on the junction surface and the casing is reassembled, uniform finishing allowance can be obtained by the external profile of the casing, and the uniformization of the allowance of the external profile of the casing is realized, and therefore, the processing difficulty is lowered; the finishing of the external profile can be finished by one-pass, so that machining deformation is reduced, and the machining efficiency is improved.
Owner:AECC AVIATION POWER CO LTD

Forging method for ultra-large titanium alloy whole frame forged piece

ActiveCN105215245AImprove organizational performance levelsImprove safety and reliabilityMetal-working apparatusTitanium alloyMachining
The invention belongs to the technical field of forging, and relates to a forging method for an ultra-large titanium alloy whole frame forged piece. The forging method includes the following steps that firstly, blank manufacturing is performed, wherein an initial blank is prepared through a local upsetting method or a machining method; the prepared initial blank is longitudinally drawn long on a free forging and pressing machine; the free forging and pressing machine presses down a material opening plate which reciprocates so that the blank can be transversely drawn long; the blank is placed on a die forging and pressing machine to be subjected to loose tooling forging, and the outer contour of the blank reaches the outer contour size of the forged piece; and wad piercing burr, corresponding to an inner hole of the forged piece, of the blank is cut and removed; and secondly, die forging is performed, wherein positioning forging is performed; pre-forging is performed; and final forging is performed. According to the forging method for the ultra-large titanium alloy whole frame forged piece, production of the ultra-large whole frame forged piece is achieved through the method, and the forging method has the beneficial effects of being simple in technology, good in economical efficiency, good in mechanical performance of the forged piece and the like.
Owner:XIAN TRIANGLE AVIATION TECH +1

Split knotter

The invention relates to a split knotter which belongs to the field of agricultural mechanical equipment. A drive shaft is installed in a shaft hole I of a main installation frame; a rope clamping drive mechanism and a split drive disk mechanism are coaxially installed at both ends of the drive shaft; a cam swinging rod is installed on a shaft hole III of the main installation frame, and the cam swinging rod and the split drive disk mechanism form a cam mechanism; the rope clamping mechanism and a rope clamping right helical gear are coaxial and are installed on a shaft hole V of the main installation frame; a rope clamping left helical gear is installed on a shaft hole VI of the main installation frame; an olecranon intermittent gear and an olecranon tongue are axially connected with an olecranon shaft respectively and installed on a shaft hole II of the main installation frame; and the olecranon tongue and the main installation frame form a small cam mechanism. Key mechanisms of the invention are formed by combining split parts, thereby reducing the processing deformation of integrated parts and the manufacture and maintenance cost of a press baler, being beneficial to the adjustment of relative positions during assembly, overcoming the defect of replacing the whole part due to the damage of a structure, prolonging the service life of the knotter and enhancing the processing strength of the parts.
Owner:CHINA AGRI UNIV

Method for eliminating residual stress of aluminum alloy die forging piece

The invention discloses a method for eliminating residual stress of an aluminum alloy die forging piece. The method comprises the following steps: step 1: carrying out cold pressing on the aluminum alloy die forging piece subjected to solution hardening treatment; step 2: carrying out deep cooling treatment on the forging piece subjected to the cold pressing; step 3: carrying out rapid temperature-rising double-grade ageing treatment on the forging piece subjected to the deep cooling treatment; step 4: carrying out air cooling on the forging piece subjected to the rapid temperature-rising double-grade ageing treatment. Aiming at reducing the residual stress, a cold pressing finishing die is used for carrying out cold-pressing deformation on the die forging piece firstly; then the die forging piece is put into liquid nitrogen and is subjected to the deep cooling treatment; then the temperature of the forging piece subjected to the deep cooling treatment is rapidly raised and the double-grade ageing treatment is carried out. The residual stress of the aluminum alloy die forging piece can be reduced by 90 percent or more through treatment of a solution hardening, cold pressing, deep cooling and ageing combined technology; the method is especially suitable for the large-size and high-strength aluminum alloy die forging pieces with complicated shapes.
Owner:HUNAN UNIV

Aero-engine compressor blade and machining method thereof

The invention belongs to the technical field of aero-engines, and discloses a compressor blade machining method. The compressor blade machining method includes the steps that step 1, three-dimensionalmeasurement is carried out, specifically, a crest curve and a trough curve are built by extracting actual curve crest points and trough points of cross sections according to a three-dimensional diagram of a compressor blade; virtual curves of a blade body and a jog are built; step 2, point cloud is extracted, specifically, curvatures of the actual curve, the crest curve and the trough curve of the step 1 are analyzed, and the curves of the crest curve and the trough curve are regulated according to actual curve curvatures; a center line is built according to the crest curve and the trough curve; step 3, a hook face is rebuilt, specifically, a mesh hook face is built with center lines of the cross sections to generate a three-dimensional digital model; step 4, procedures are regulated, specifically, the blade three-dimensional digital model is imported to a three-dimensional software and corrected compared with blade master body data scanned by the three-dimensional software; and step5, numerical control machining is carried out, specifically, numerical control programming is carried out according to the blade three-dimensional digital model of the step 4, and a blade is subjectedto numerical control milling with a ball end milling. According to the compressor blade machining method, the blade precision and the surface roughness of a compressor can be effectively ensured.
Owner:株洲丰发精工实业有限公司

Special fixture for milling long and thin axle parts

The invention discloses a special fixture for milling long and thin axle parts. A three-jaw chuck is fixedly connected with the upper surface of a base of the fixture and is fixedly connected with an inner ring of a bearing, the outer ring of the bearing is fixedly connected with a support arm, the bottom of the support arm can rotate around the bearing and support in a round sliding chute by taking the three-jaw chuck as the center of a circle on the upper surface of the base of the fixture in a sliding manner, a support arm is provided with a handle, a handle box, a hand wheel handle and a tailstock, the handle box is connected with the hand wheel handle and the tailstock, the hand wheel handle controls the tailstock to longitudinally move along the support arm, the tailstock is connected with a tip block, the tip block is connected with a tip locking handle, a tip is fixed on the tip block and realizes clamping by combining a tapered hole on the end face of a part, and the tip locking handle finely adjusts the tip to longitudinally shift along the support arm and lock a tip device. The special fixture disclosed by the invention can effectively slow down processing deformation, and the support arm is prevented from rotating and interfering with a milling cutter, thus the machining accuracy of milling on the long and thin axle parts can be obviously improved, the cost can be reduced and the productivity can be improved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Dried type clamp for quilting and grinding air cylinder sleeve

The invention discloses a dried type clamp for quilting and grinding an air cylinder sleeve. The clamp comprises a fixed outer sleeve, a spring sleeve and a positioning base, wherein the fixed outer sleeve is nested in the positioning base; a spring is mounted in a spring mounting hole which is sleeved outside a lug boss below the inner wall of the fixed outer sleeve; at least one internal conical face is arranged on the inner wall of the fixed outer sleeve; the spring sleeve is mounted in the fixed outer sleeve; the lower end of the spring sleeve is arranged on the spring; the outer circumference face of the spring sleeve is provided with an external conical face matched with the internal conical face on the inner wall of the fixed outer sleeve; and a vertical opening is arranged on the spring sleeve. The inner circumference face of the fixed outer sleeve and the conical face on the outer circumference face of the spring sleeve are in compact contact so that the inner hole of the spring sleeve and the outer circumference of the air cylinder sleeve can be ensured to be in gapless contact; the machining deformation of the air cylinder sleeve is small; and the machining precision is high. Furthermore, a gap is reserved between the inner circumference face of the spring sleeve and the outer circumference of the air cylinder sleeve, so that the scrapping rate of the outer circumference face of the air cylinder sleeve is reduced and the yield is improved.
Owner:长子县丹朱缸套有限公司

Stress uniformizing method for high-temperature alloy casing ring forging

The invention relates to a stress uniformizing method for a high-temperature alloy casing ring forging. The circumference lengths L1 and L2 at the maximum ring diameter position and the minimum ring diameter position of the high-temperature alloy casing ring forging are measured, the yield stress sigma and required strain epsilon of high-temperature alloy are obtained through a material tensile test, and a bulging mold is manufactured according to the cross section shape and size of the high-temperature alloy casing ring forging; the high-temperature alloy casing ring forging is heated to be lower than the forging temperature and is placed in the bulging mold after soaking, a bulging cone head operates downwards by H1 and then returns after being kept for a period of time, the high-temperature alloy casing ring forging is rotated by a certain angle around the axis of the ring forging, and the bulging cone head operates downwards by H2 on the basis of H1 and is kept for a period of time, so that it is guaranteed that all positions of the high-temperature alloy casing ring forging are in the state of micro plastic deformation; and finally, the bulging cone head returns, and the high-temperature alloy casing ring forging is taken out and air-cooled to the room temperature. Uniform circumferential plastic strain is applied to the high-temperature alloy casing ring forging through the minimum deformation so as to adjust uniform distribution of residual stress.
Owner:WUHAN UNIV OF TECH
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