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40 results about "Particle erosion" patented technology

Thermal barrier coating working condition simulation and real-time monitoring device

The invention provides a thermal barrier coating working condition simulation and real-time monitoring device. The device comprises a box, a working condition simulation assembly, a sample clamping assembly, a monitoring assembly and a system control assembly, wherein the working condition simulation assembly is used for simulating the working condition of a sample to be tested; the sample clamping assembly is arranged inside the box; the sampling clamping assembly is used for clamping the sample to be tested; the monitoring assembly is used for collecting and processing test data in the simulation process; a detection assembly is electrically connected with the system control assembly, and the system control assembly is used for controlling the simulation process. Through the arrangementof the working condition simulation assembly, the working condition of an aircraft engine can be simulated, and real-time monitoring is performed on the simulation process by using the monitoring assembly, so that an extreme multi-field coupling environment can be realized, and the complex multi-field coupling service environments, such as high temperature thermal shock, hard particle erosion andhigh temperature corrosion, of the thermal barrier coating material in the real service process can be simulated.
Owner:XIANGTAN UNIV

Thermal barrier coating, as well as preparation method and application thereof, and aero-engine turbine blade

The invention relates to a thermal barrier coating, as well as a preparation method and application thereof, and an aero-engine turbine blade, and belongs to the field of aero-engine hot end part protection coatings. The thermal barrier coating comprises a 7YSZ ceramic layer and an aluminum oxide layer arranged on the surface of one side of the 7YSZ ceramic layer, wherein the 7YSZ ceramic layer isin a feather column shape; and aluminum oxide in the aluminum oxide layer is nanocrystals. The thermal barrier coating not only has high thermal insulation and high stress tolerance, but also has favorable fused salt corrosion resistance and resistance to high temperature oxidation and particle erosion. The preparation method comprises the steps of adopting a plasma spraying-physical vapor deposition method for preparing the 7YSZ ceramic layer; adopting a magnetron sputtering technology for preparing the aluminum oxide layer; and then carrying out vacuum treatment. The method is simple, and the uniform thermal barrier coating can be prepared. The thermal barrier coating is applied to be arranged on an aero-engine hot end part such as the surface of a turbine blade, so that the turbine blade has favorable resistance to high temperature oxidation, CMAS corrosion and particle erosion.
Owner:GUANGDONG INST OF NEW MATERIALS

Prediction method for erosion life of sand control screen pipe in perforation completion gas well

ActiveCN106596312AErosion Life PredictionAccurate prediction of erosion lifeInvestigating abrasion/wear resistanceSand sampleParticle erosion
The invention provides a prediction method for erosion life of a sand control screen pipe in a perforation completion gas well. The method includes the steps of: S1. preparing a screen pipe erosion resistance testing device; S2. adding abrasive particles into the screen pipe erosion resistance testing device to perform jet erosion test on the sand control screen pipe so as to obtain the abrasive particle content C0, the abrasive particle erosion velocity v0 and the screen pipe test erosion destruction time t; S3. extracting a formation sand sample in the perforation completion gas well to obtain formation sand shape coefficient k1 and the formation sand density rho1; S4. performing pilot production on the perforation completion gas well to obtain the formation sand production content C1 and blasthole gas flow rate v1; and S5. predicting the erosion life of the sand control screen pipe in the perforation completion gas well according to the following formula as shown in the specification. The method provided by the invention can truly and accurately predict the erosion life of the sand control screen pipe in the perforation completion gas well, and provides basis for selection of an appropriate sand control screen pipe in gas well sand control operation.
Owner:PETROCHINA CO LTD

Self-crosslinking silicon-boron-containing high polymer matrix ablation-resistant heat insulation material and preparation method

ActiveCN109486201AImprove ablation resistance and heat insulation performanceGood compatibilityRubber materialFiber
The invention discloses a self-crosslinking silicon-boron-containing high polymer matrix ablation-resistant heat insulation material and a preparation method, and belongs to the field of high polymercomposite materials. The material comprises, by weight, 100 parts of heat-vulcanized silicone rubber, 10-30 parts of polyborosiloxane prepolymers, 10-30 parts of white carbon black, 5-10 parts of fibers, 10-20 parts of light ablation-resistant fillers, 3-5 parts of vulcanizing agents and 1-3 parts of hydroxyl silicone oil. The method includes the steps: mixing the polyborosiloxane prepolymers andthe light ablation-resistant fillers; sequentially adding all materials to a mixer and performing plasticating; vulcanizing mixed rubber materials for three times to obtain the self-crosslinking silicon-boron-containing high polymer matrix ablation-resistant heat insulation material. The material serves under the condition of oxygen enrichment and high temperature, is subjected to carbonizing andceramic reaction in a high-temperature environment, serves as a high-temperature ablation-resistant protective layer and directly bears combined action of thermochemical ablation, gas denudation and particle erosion, and the ablation-resistant heat insulation performance of the material is effectively improved.
Owner:SHENYANG LIGONG UNIV

Bismaleimide resin/silicone rubber ablation-resistant thermal insulation composite material and preparation method thereof

InactiveCN106589962AHigh vulcanization molding qualityImproves ablation resistanceFiberCarbon layer
The invention discloses a bismaleimide resin/silicone rubber ablation-resistant thermal insulation composite material and a preparation method thereof. The composite material is prepared from the following components in parts by mass: 20-80 parts of methylvinylsilicone rubber, 20-80 parts of methyl vinyl phenyl polysiloxane rubber, 1-5 parts of dicumyl peroxide, 15-40 parts of white carbon black, 5-15 parts of chopped fibers, 5-40 parts of bismaleimide, 1-5 parts of hydroxyl silicone oil and 1-20 parts of zirconium boride. The bismaleimide resin/silicone rubber ablation-resistant thermal insulation composite material has high vulcanization molding quality, and a dense hard carbon layer can be formed on the surface of an ablation layer of the thermal insulation composite material in the ablation process to play a role of preventing the thermal insulation composite material from further ablation, thereby improving the ablation resistance and antioxygenic property of the thermal insulation composite material, enabling the thermal insulation composite material to meet the requirements of operating environments with oxygen enrichment, high temperature, high-speed gas flow and particle erosion, and solving the problem that the thermal insulation material is easy to flaw and be burnt out under the working environments with high temperature, high pressure, oxygen enrichment and particle erosion.
Owner:湖北三江航天江北机械工程有限公司

A method and system for acquiring a material removal model in ultra-high pressure water jet machine

ActiveCN109508472AEffectively guide the optimization of efficient precision machining processAccurate predictionGeometric CADDesign optimisation/simulationUltra high pressureMaterial removal
According to the emdoiment, A method for acquiring a material removal model in ultra-high pressure water jet machine includes solving a kinetic equation of a single abrasive particle erosion motion toobtain a motion trajectory equation of that single abrasive particle; Integrating the motion trajectory equation to obtain a first expression of the material removal amount of a single abrasive particle in the cutting time; Obtaining a cutting stop condition of a single abrasive particle, and solving a first expression according to the cutting stop condition to obtain a second expression of a material removal amount of the single abrasive particle; According to the flow rate of abrasive particles and the second expression, the third expression of material removal rate in ultra-high pressure water jet machining is obtained. The third expression is the material removal model in ultra-high pressure water jet machining. Considering the mechanism of material removal, the model can predict themachining process more accurately, and can guide the optimization of high efficiency and precision machining process in practical machining, which has theoretical guidance and engineering applicationsignificance.
Owner:BEIHANG UNIV

Oil-submerged pump damage degree evaluation method and system based on particle analysis

The invention relates to an oil-submerged pump damage degree evaluation system and method based on particle analysis. The method comprises the steps: measuring the temperature, pressure and flow of transformer oil through a measuring system; detecting the components and granularity of solid particles in oil at an inlet and an outlet of an oil-submerged pump by using an oil granularity detector; determining boundary conditions according to the temperature, the pressure, the flow, and the components, the density and particle size distribution of the oil at the inlet and the outlet of the oil-submerged pump; selecting a proper erosion model for numerical simulation of a main eroded area and the overall erosion rate of the oil-submerged pump; calculating the accumulation of the volume of the oil-submerged pump generated by particle erosion along with time; detecting the particle concentration and particle size distribution of the inlet and the outlet of the oil-submerged pump after a specific period of time, and comparing with a simulation result of the erosion model; and predicting the damaged part and damage degree of the oil-submerged pump through the simulation model after comparison and calibration, and giving a warning when the oil-submerged pump reaches a threshold value.
Owner:ELECTRIC POWER RES INST OF STATE GRID ANHUI ELECTRIC POWER +2

A deep peaking steam turbine blade erosion test system and its test method

The invention discloses a blade erosion test system and a test method of a deep peak-shaving steam turbine. The present invention includes steam turbine test equipment, a particle erosion system and a droplet erosion system; the particle erosion system includes a particle tank, a vibrating device installed under the particle tank, a screening device, a weighing machine, a propulsion device, a high-frequency Electric heating furnace, mixer and particle injector. The particles in the particle tank enter the screening device after passing through the vibrating device. The screened particles enter the propulsion device through the weighing machine. The propulsion device is used to push the particles into the high-frequency electric heating furnace. The frequency electric heating furnace heats the particles, and after heating, the particles enter the mixer, and then enter the particle injector, and the particle injector sprays the particles into the test chamber for the particle erosion test. The invention can be used to study the influence of different experimental conditions on the erosion of steam turbine blades, has the advantages of multiple functions and strong applicability, and is therefore especially suitable for the research on the vibration of deep peak-shaving steam turbines.
Owner:ELECTRIC POWER RES INST OF STATE GRID ZHEJIANG ELECTRIC POWER COMAPNY +1

A Simulation Method of Soil Internal Erosion Deformation Response

ActiveCN113237722BImprove accuracyIn line with the actual erosion situationPreparing sample for investigationEarth material testingSoil scienceInternal erosion
The invention discloses a soil internal erosion deformation response simulation method, comprising the following steps: S1: collecting a soil sample, constructing a numerical simulation sample model, and pressurizing the numerical simulation sample model according to the actual stress state of the soil Consolidation; S2: Calculate the stress reduction coefficient of each fine particle in the numerical simulation sample model; S3: Generate the statistical distribution map of the stress reduction coefficient of fine particles in the numerical simulation sample model; S4: Calculate the fine particle in the soil sample The critical value of the stress reduction coefficient of particle erosion is to determine the total amount of fine particle erosion; S5: determine the erosion deformation sample model; S6: determine the strength characteristics and deformation characteristics of the erosion deformation sample model; S7: determine the total amount of fine particle erosion , strength characteristics and deformation characteristics as the simulation results of soil internal erosion deformation response. The invention judges the erodible particles based on the stress state of the particles and the hydraulic gradient to be applied, which conforms to the actual erosion conditions.
Owner:CHINA INST OF WATER RESOURCES & HYDROPOWER RES

Soil body internal erosion deformation response simulation method

ActiveCN113237722AImprove accuracyIn line with the actual erosion situationPreparing sample for investigationEarth material testingInternal erosionParticle erosion
The invention discloses a soil body internal erosion deformation response simulation method which comprises the following steps of: S1, collecting a soil body sample, constructing a numerical simulation sample model, and pressurizing and solidifying the numerical simulation sample model according to the actual stress state of a soil body; S2, calculating a stress reduction coefficient of each fine particle in the numerical simulation sample model; S3, generating a stress reduction coefficient statistical distribution diagram of the fine particles in the numerical simulation sample model; S4, calculating a stress reduction coefficient critical value of erosion of the fine particles in the soil body sample, and determining the total erosion amount of the fine particles; S5, determining an erosion deformation sample model; S6, determining strength characteristics and deformation characteristics of the erosion deformation sample model; and S7, taking the erosion total amount of the fine particles, the strength characteristics and the deformation characteristics as results of soil internal erosion deformation response simulation. According to the method, the erodible particles are judged based on the stress state of the particles and a hydraulic gradient to be applied, and the actual erosion condition is met.
Owner:CHINA INST OF WATER RESOURCES & HYDROPOWER RES

A kind of thermal barrier coating and its preparation method and application, aeroengine turbine blade

The invention relates to a thermal barrier coating, as well as a preparation method and application thereof, and an aero-engine turbine blade, and belongs to the field of aero-engine hot end part protection coatings. The thermal barrier coating comprises a 7YSZ ceramic layer and an aluminum oxide layer arranged on the surface of one side of the 7YSZ ceramic layer, wherein the 7YSZ ceramic layer isin a feather column shape; and aluminum oxide in the aluminum oxide layer is nanocrystals. The thermal barrier coating not only has high thermal insulation and high stress tolerance, but also has favorable fused salt corrosion resistance and resistance to high temperature oxidation and particle erosion. The preparation method comprises the steps of adopting a plasma spraying-physical vapor deposition method for preparing the 7YSZ ceramic layer; adopting a magnetron sputtering technology for preparing the aluminum oxide layer; and then carrying out vacuum treatment. The method is simple, and the uniform thermal barrier coating can be prepared. The thermal barrier coating is applied to be arranged on an aero-engine hot end part such as the surface of a turbine blade, so that the turbine blade has favorable resistance to high temperature oxidation, CMAS corrosion and particle erosion.
Owner:GUANGDONG INST OF NEW MATERIALS

Experimental system for testing association rule of particle concentration and surface damage

The invention discloses an experimental system for testing a particle concentration and surface damage association rule. The experimental system comprises a particle flow mixing section, an erosion testing section and a particle collecting section, the particle flow mixing section is used for ensuring uniform distribution of particles in the loop, the erosion testing section is used for carrying out a particle erosion test, and the particle collecting section is used for temporarily collecting particles in the loop of the whole experimental device. The test elbow in the experiment system can be detached, so that the weight loss measurement of the eroded sample is realized. Besides, the particle collecting device can temporarily store the particles, so that after the test elbow is weighed, the test elbow can be arranged back to the erosion loop, and the next round of erosion experiment can be carried out on the basis of the existing particle accumulation. According to the experimental system provided by the invention, the correlation rule of the particle concentration and the surface damage under the time dimension can be obtained, and an important reference basis is provided for predicting the erosion of the particles in the pipe.
Owner:ELECTRIC POWER RES INST OF STATE GRID ANHUI ELECTRIC POWER +1

Single particle-target plate erosion morphology prediction method based on energy conversion mechanism

PendingCN114218843AEfficient description of elastoplastic contact propertiesAccurate simulation measurementGeometric CADDesign optimisation/simulationFatigue damageDiscrete element method
The invention discloses a single particle-target plate erosion morphology prediction method based on an energy conversion mechanism, and belongs to the field of numerical simulation prediction. The simulation prediction method comprises the following steps: establishing normal, tangential and rolling contact stiffness expressions between a single particle and a target plate in a contact force calculation link in an erosion process; simulating and measuring normal and tangential collision energy between a single particle and a target plate in an erosion process by using a discrete element method; according to the normal collision energy and the tangential collision energy absorbed by the target plate, the normal erosive wear volume lost due to normal low-cycle fatigue damage of the target plate and the tangential erosive wear volume lost due to the ploughing-fracture effect in the single-particle erosion process are calculated respectively; and based on the normal and tangential wear volumes of the target plate in the single particle erosion process, predicting the single particle-target plate surface erosion wear geometric morphology by adopting a geometric superposition method. According to the method, the erosive wear morphology of the surface of the single particle-plastic metal target plate at different incident angles can be effectively predicted.
Owner:JIANGHAN UNIVERSITY
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