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152results about How to "No microcracks" patented technology

Low-damage processing method of film holes in single crystal high-pressure-turbine hollow blade of aircraft engine

The invention provides a low-damage processing method of film holes in a single crystal high-pressure-turbine hollow blade of an aircraft engine. The low-damage processing method comprises the following steps: wiping the surface of the blade through degreasing cotton with absolute alcohol; transferring into a drying box to dry; arranging a clamp on a machine table, and aligning; assembling the dried blade on the clamp and locking; presetting scanning system parameters; scanning the blade; saving axis moving coordinate value of each hole to be processed under an automatically-generated machine coordinate system as a *.xls file; importing and generating a hole position file; performing compensative correction on the deviation value of a focus position of the hole to be processed; and setting the optimized laser processing technological parameters through a main processing interface. With the adoption of the low-damage processing method, the processed hole is outstanding in quality; a remelting layer, microcacks and recrystallization can be avoided after the single crystal material is processed, so that subsequent processing can be saved, and as a result, the fatigue life and the processing cycle of the blade can be prolonged and improved; the ablation threshold of the single crystal material can be effectively reduced; the recrystallization of the single crystal material can be avoided.
Owner:SHENYANG LIMING AERO-ENGINE GROUP CORPORATION

Automatic control system and method for high-precision straightening machine

The invention relates to an automatic control system and method for a high-precision straightening machine and belongs to the field of automatic control. Through the automatic control system and method, the straightness (curvature) reaches over 0.3 mm/m according to the straightening precision of the high-precision straightening machine; a hardware structure and a software method of the automatic control system for the high-precision straightening machine are designed considering closed-loop control of oil source pressure and oil cylinder piston displacement of a hydraulic system of the high-precision straightening machine, continuous detection of straightening operation process data, stepless speed regulation control for calibrating transmission of all sets of straightening rollers and the like, the international advanced level of three-dimensional rotation straightening under high-precision automatic control is reached, consistency of roller gap precision in the straightening process, stability of evenly distributed and balanced straightening force and reliability of nonlinear variable gain automatic compensation can be guaranteed, the straightness is improved to 0.2 mm/m from 0.3 mm/m according to the straightening precision of the high-precision straightening machine, and the straightening target that straightened materials have no blind area or tiny crack or scratch or oval or bounce is achieved.
Owner:辽宁银捷装备科技股份有限公司

Surface-nanocrystallization low-temperature aluminizing treatment method for steel products

The invention relates to a surface-nanocrystallization low-temperature aluminizing treatment method for steel products. According to the method, uniform nanocrystallines are obtained on the surface of a material substrate by virtue of mechanical grinding, and then the steel products are subjected to low-temperature aluminizing by virtue of a rare-earth-catalyzed solid aluminizing method, so as to form a high-performance aluminized layer; the steel products and grinding balls different in particle size and quantity are put into a vibration mill together and are subjected to vibration grinding, and the impact energies of the grinding balls of different particle sizes to the surfaces of the steel products are different, so that the surface nanocrystallization treatment of the steel products is easily realized; the problems in a traditional aluminizing process that the aluminizing temperature is high, the temperature preservation time is long, the obtained aluminized layer is not compact, and the use effect is poor are solved to some degree, and a workpiece produced by virtue of the method has relatively high temperature oxidation resistance and corrosion resistance; the obtained aluminized layer is relatively uniform and compact, an aluminide coating with a single-layer structure is well combined with the substrate, a microscopic crack is avoided, the middle of the aluminized layer is a relatively narrow transition region, and Fe and Al elements are uniformly distributed.
Owner:SHANDONG AGRICULTURAL UNIVERSITY

SiCf/SiC composite material flame tube and automatic preparation method thereof

The invention discloses an automatic preparation method of a SiCf/SiC composite material flame tube. The preparation method comprises the following steps: preparing an interface layer from SiC fibersby adopting chemical vapor deposition, so as to obtain SiC fibers with a continuous interface layer; performing unidirectional tape laying and filament winding on the SiC fibers with the continuous interface layer according to the fiber volume and fiber orientation obtained by simulation calculation, so as to obtain net size forming preform; performing densifying treatment on the obtained preformby adopting a reactive melt infiltration process and the chemical vapor deposition process; preparing an environmental barrier coating on the surface of the obtained preform; finally, continuously preparing a thermal barrier coating on the surface, thereby fully intelligently obtaining the high-density SiCf/SiC composite material flame tube. The SiCf/SiC composite material flame tube prepared withthe method disclosed by the invention has the characteristics of high temperature resistance and long service life and also has the advantages such as low thermal expansion coefficient, high thermalconductivity, high thermal shock resistance and excellent mechanical property. Meanwhile, the preparation method is high in degree of automation, short in production cycle, low in cost and controllable in quality.
Owner:CENT SOUTH UNIV

Rapid descaling device and descaling treatment method thereof

The invention discloses a rapid descaling device and a descaling treatment method thereof, and the descaling device comprises a pallial chute and a lining chute, wherein the lining chute is arranged in the pallial chute; the bottom end inside the pallial chute is provided with an ultrasonic sound board which is in contact fit with the bottom part of the lining chute; and the lining chute is internally provided with at least one heating pipe. The using method is as follows: a, injecting a proper amount of descaling solution in the lining chute, controlling the heat temperature of the heat pipe and setting the descaling time; b, placing a workpiece shelf loaded with workpieces in the lining chute, starting the ultrasonic sound board, and rapidly descaling the workpieces under the jointed action of descaling solution chemical etching and ultrasonic vibration; and c, taking the workpiece shelf out when the set descaling time is over, and stopping the descaling operation. The invention can effectively and rapidly remove oxide layers after valve thermal treatment with the descaling efficiency 2-3 times quicker than that of shot blast, and the processed valve surface has no cracks; the intrinsic defect on the valve surface is not covered after descaling treatment, so that the valve with the intrinsic defect can be selected to discard as soon as possible to avoid waste of subsequent machining.
Owner:HUAI JI DENG YUE VALVE CO LTD

Special-shaped hole machining method and special-shaped hole

The invention discloses a special-shaped hole machining method and a special-shaped hole and relates to the technical field of laser machining. According to the method, femtosecond or picosecond or nanosecond pulse laser is adopted, and a mode completely based on scanning galvanometer filling machining is provided. The method comprises the steps that firstly, a through hole smaller than the hole diameter requirement is machined so that gasification objects and fusion objects formed in the machining process can be discharged and re-coagulation objects are prevented from depositing; then, roughmachining of a special-shaped hole diffusion section is conducted; then, the laser focusing position is adjusted, broaching is conducted on the basis of a dust discharge through hole, and a cylindrical through hole meeting the hole diameter requirement is machined; and finally, the focus position is precisely adjusted, and the diffusion section is machined layer by layer. By means of the special-shaped hole machining method and the special-shaped hole, heat-induced defects such as recasting layers, microcracks, coating collapse and the like generated in the process that in the prior art, a special-shaped hole is machined, and in particular, the special-shaped hole is machined in a workpiece with the surface coated with a thermal barrier coating are avoided; and in addition, the shape and dimension precision of the special-shaped hole are improved.
Owner:AVIC BEIJING AERONAUTICAL MFG TECH RES INST

In-situ preparation method for manufacturing high-entropy alloy by gradient powder feeding laser additive material

The invention discloses an in-situ preparation method for manufacturing high-entropy alloy by gradient powder feeding laser additive materials. The in-situ preparation method comprises the following steps of raw material preparation and gradient powder feeding laser additive material preparation. The material forming efficiency prepared by the in-situ preparation method is high, and a part model is not subjected to technological constraints, so the in-situ preparation method can be used to prepare parts with complex shapes, and the near-net forming of the materials can be realized, the production cost of the parts is greatly reduced. Samples have good forming effect, no air holes and macroscopic cracks, no micro-air holes and micro-cracks, good density, uniform organization and coexistenceof three phase structures. Composition detecting is carried out by using an energy disperse spectroscopy, and the definition of high-entropy alloy is met from the composition. The boundary between aprinting layer and two sides of base is fuzzy, the combination is better, and the crack tendency is low. It can be concluded that the gradient powder feeding mode greatly reduces the crack tendency atthe joint.
Owner:TIANJIN UNIV
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