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58results about How to "Reduce test volume" patented technology

Asphalt mixture mixing proportion design method based on inert solid fractal distribution characteristic

The invention relates to a method of designing a mixed ratio for a bitumen mixture based on fractal and distributional features of ore materials. The method comprises the following steps: (1) mathematical models for particle diameter distribution and mass distribution of the ore materials are set up respectively; (2) the type and the grading limit of the bitumen mixture are determined; (3) raw materials are selected and checked; (4) graduations of two arbitrary groups of the ore materials are determined and corresponding fractal dimension values(D) are worked out; (5) the use level of the bitumen is worked out; (6) the bitumen mixture is prepared by stirring; (7) a Marshall test sample is made, the relative density of the bulk volume of the test sample is determined, the theoretical maximum relative density is determined, and the volume index is worked out; (8) relationship curves between the fractal dimension values(D) and the volume indexes are drawn; (9) the graduation of the ore materials and the optimum use level of the bitumen are determined; (10) the road performance of the bitumen mixture is tested; and (11) the construction mixed ratio of the bitumen mixture is determined. The invention utilizes the fractal theory to set up the mathematical models, and in the process of designing the mixed ratio of the bitumen mixture, the optimum bitumen use level and the optimum graduation of the ore materials meeting and regulating all design rules of the bitumen mixture can be quickly determined.
Owner:LANZHOU JIAOTONG UNIV

Method and device for testing axial rigidity and radial rigidity of rotary hydrostatic guide rail

The invention provides a method and device for testing axial rigidity and radial rigidity of a rotary hydrostatic guide rail. A rotary guide rail seat is fixed on a platform, a pressing plate and a rotary assembly are fixedly connected to form a rotary part, and the rotary part is used for guiding in a rotary motion way by depending on a hydrostatic guide rail pair; an axial load assembly comprises a flange sleeve, a screw rod, a thrust bearing, a radial bearing, a sleeve, a connecting piece, force sensors and a terminal pad which are vertically arranged; a radial load assembly comprises a flange sleeve, a screw rod, a thrust bearing, a radial bearing, a sleeve, a connecting piece, a force sensor, a loading piece and a connection bending plate which are horizontally arranged; and a mounting support of a displacement sensor assembly is fixed on the rotary guide rail seat, and a measuring head aligns to the rotary assembly. The method and device provided by the invention can be used for acquiring the axial and the radial rigidity data of the hydrostatic guide rail in a rotary motion and can also be used for an confirmatory experiment on a method for analyzing the rigidity of the hydrostatic guide rail in the rotary motion and the influence of oil film tangential adhesive force.
Owner:XIAN UNIV OF TECH

Air gap breakdown voltage prediction method

The invention relates to an air gap breakdown voltage prediction method. The method is characterized by selecting several typical electrode structure air gaps and determining a factor and a level range which influence a breakdown voltage; selecting an orthogonal table which can be used to inspect each level of the above factor and successively carrying out breakdown voltage tests according to a test condition corresponding to each test number; loading a breakdown voltage test value so as to carry out electrostatic field calculation on the typical electrode structure air gaps and extracting an electric field distribution parameter from a calculation result; using a support vector machine to establish a breakdown voltage prediction model, taking the electric field distribution parameter as an input of a model, taking whether the gap is in a breakdown state under a loading voltage as an output of the model, using typical electrode structure air gap breakdown voltage test data to train a support vector machine model so that an air gap breakdown voltage of another electrode structure is predicted and obtained. By using the method in the invention, a prediction process is simple; accuracy is high; a test quantity needed by air gap discharge characteristic research can be decreased and test cost is reduced.
Owner:WUHAN UNIV +1

Permanent magnet temperature on-line detection method and device

The invention provides a permanent magnet temperature on-line detection method and device which are applied to a permanent magnet motor. The permanent magnet temperature on-line detection method comprises the steps that the rotating speed and the counter electromotive force of the permanent magnet motor are acquired; the temperature value of a permanent magnet is obtained through calculation according to a preset temperature calculating rule, the rotating speed and the counter electromotive force, and the preset temperature calculating rule represents the corresponding relation of the rotating speed, the counter electromotive force and the temperature value of the permanent magnet. In the detection process, only the rotating speed and the counter electromotive force of the permanent magnet motor need to be acquired and calculated, the temperature of the permanent magnet can be directly obtained, the measuring method is simple, the testing amount is small, and the testing time is short. Moreover, due to the fact that high-cost devices such as a thermal infrared imager do not need to be used, and the testing cost is lowered. In the measuring process, constant temperature maintaining of cooling liquid of the motor is not involved, and operation is easy. In addition, the permanent magnet temperature on-line detection device is achieved in practical, and the measuring structure is simple.
Owner:CSR ZHUZHOU ELECTRIC LOCOMOTIVE RES INST

Solid propellant formulation optimization design method based on genetic algorithm

The invention discloses a solid propellant formulation energy optimization design method based on a genetic algorithm. The method comprises a first step of modeling, and building an energy characteristic calculation model of solid propellant according to a minimum free energy principle; a second step of setting and storing initial parameters, inputting component species used by the solid propellant, and a chemical formula and a quality proportion range of each component, and inputting species of combustion products produced by the solid propellant after being combusted, and chemical formulas and relative molecular mass of all the combustion products or selecting all the combustion products in a combustion product data base; and a third step of calling a genetic algorithm module by a data processor, and conducting optimization design to quality proportion of the designed solid propellant. The solid propellant formulation energy optimization design method based on the genetic algorithm is simple in steps, reasonable in design, convenient to achieve, good in using effect, capable of fast obtaining an optimum proportion of highest specific impulse of the solid propellant and effectively overcoming the defects, existing in an existing solid propellant compound design process, of being high in energy characteristic test cost, long in period, large in test dose, and the like.
Owner:XIAN MODERN CHEM RES INST

Electric arc additive forming prediction modeling method based on molten drop transition

The invention provides an electric arc additive forming prediction modeling method based on molten drop transition, and relates to an electric arc additive forming process numerical calculation modeling method. According to the modeling method, the molten pool flow field calculation and a molten drop transition process are coupled, a computational domain is updated by adopting a dynamic grid technology and considering the movement of a welding gun, and transportation equations are uniformly solved in a molten pool computational domain and a molten drop transition computational domain, so thatthe simulation prediction of electric arc additive manufacturing forming morphology, temperature field and flow field is achieved, and the problems that the size of an existing arc additive cladding layer cannot be predicted and the physical field evolution is not clear are solved. The method is implemented through the following steps of 1, establishing a material and geometric model, and definingthe computational domain and boundary conditions; 2, establishing a molten drop mechanical model, and determining a molten drop transition computational domain transportation equation source item; 3,establishing a molten pool thermodynamic model, and determining a molten pool computational domain transportation equation source item; and 4, loading a thermodynamic source item, and uniformly solving molten drop and molten pool computational domain transportation equations.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Multi-nozzle solid attitude control engine blocking cover structure

ActiveCN109026445AAccurate indication of opening pressureSolve the problem of difficult processing and large dispersion of opening pressureRocket engine plantsAttitude controlEngineering
The invention provides a multi-nozzle solid attitude control engine blocking cover structure. The blocking cover is mainly composed of a spraying pipe clamping ring, a piston and sealing rings, the control device for opening the opening pressure design value of a spray pipe plug cover is mainly used for changing machining materials of the piston, geometrical parameters and structural forms; and according to the selected machining materials, the geometrical parameters and the structural form of the piston, the opening pressure of the novel spray pipe plug cover can be predicted through structural calculation. Meanwhile, the spray pipe plug cover can solve the problems that a small-size conventional spray pipe plug cover used for a special spray pipe is difficult to machine and the discretedegree of the opening pressure is large. The connection mode of the spray pipe plug cover and a spray pipe assembly can be selected but not limited to threaded connection, pin connection and clampingkey connection mode. According to the multi-nozzle solid attitude control engine blocking cover structure, the accurate control of the opening pressure of the nozzle cover of the spray pipe is realized by means of the mature structure calculation, the test amount is reduced, the product performance reliability is improved, and the design cost is saved.
Owner:SHANGHAI XINLI POWER EQUIP RES INST

Oil-paper insulation system breakdown voltage prediction method based on support vector machine

The invention discloses an oil-paper insulation system breakdown voltage prediction method based on a support vector machine. The oil-paper insulation system breakdown voltage prediction method comprises the steps of: (1) selecting a typical oil-paper insulation structure in a transformer, and forming an influence factor execution table; (2) conducting a breakdown voltage experiment according to the influence factor execution table, and recording breakdown voltage experimental data; (3) establishing an SVM regression prediction model; (4) separating a to-be-predicted oil-paper insulation system to establish an equivalent circuit model of each insulation structure; (5) calculating a breakdown voltage of each insulation structure by utilizing the SVM regression prediction model; (6) and comparing the breakdown voltage with a withstand voltage of the equivalent circuit model of each insulation structure to obtain a predicted breakdown voltage of the oil-paper insulation system. The oil-paper insulation system breakdown voltage prediction method utilizes the support vector machine to perform prediction analysis on the oil-paper insulation breakdown voltage, is simple and efficient, is conductive to solving the uncertainty in transformer oil-paper insulation analysis, reduces the amount of oil clearance breakdown tests in transformer oil and electrical feature study, and reduces test cost.
Owner:SOUTH CHINA UNIV OF TECH +1

Inspection and state confirmation method for simulation result in simulation system

The invention discloses a method for inspecting a simulation result and determining the state thereof in a simulation system. The method comprises the following steps: the simulation result is inspected first, if a formula that F is equal to that (SA/m)/(SE/(n-m)) is equal to or more than F alpha (m, n-m) is established, the simulation result is not correct; otherwise, the simulation result is correct; when the simulation result is not correct, the simulation result requires further state determination. If a formula that Fi is equal to that (ni Y<i.><2>/1)/(SE/(n-m)) is equal to or more than F alpha (1, n-m) is established under a certain state, a simulation result under the state is not correct; otherwise, the simulation result under the state is correct. Therefore, after the state of simulation error is found, the state of simulation can be modified without modifying the whole simulation system. The method requires small tested number with high inspection accuracy, and can directly establish and modify the simulation system under small sample conditions. Furthermore, in order to lead the method of the invention to be more convenient for engineering application, the invention also establishes a simulation result inspection table and a simulation result state determination table, therefore, small sample inspection and state determination of the simulation result in the simulation system can be completed by filling out the tables.
Owner:BEIHANG UNIV

Solid propellant formula optimization method based on genetic algorithm and energy feature graph

The invention discloses a solid propellant formula optimization method based on a genetic algorithm and an energy feature graph. The solid propellant formula optimization method based on the genetic algorithm and the energy feature graph includes a first step of modeling, namely, establishing four energy feature calculation models according to a minimum free energy principle; a second step of setting and storing initial parameters; a third step of utilizing the genetic algorithm to implement formula optimization design; a fourth step of setting a value range used for graphic plotting and calculating mass contents of various kinds of raw material; and a fifth step of drawing the energy feature graph. The drawing process includes the steps of energy feature parameter inputting, energy feature curvilinear equation fitting, energy feature graph drawing, and synchronous energy feature graph displaying. The method is simple in step, reasonable in design, convenient to achieve and good in use effect, combines the genetic algorithm and the energy feature graph to carry out the solid propellant formula optimization design, and overcomes the defects that the energy feature experimental cost is high, the period is long and the experimental quantity is large and the like in an existing solid propellant formula optimization design process.
Owner:XIAN MODERN CHEM RES INST

Lithium battery long-term degradation trend prediction method

ActiveCN112257348AEnables degradation trend/remaining life predictionImprove training effectDesign optimisation/simulationAlgorithmOriginal data
The invention discloses a lithium battery long-term degradation trend prediction method, which comprises the steps of performing normalization and smoothing processing by taking a partial degradationtrend curve for a lithium battery as original data to obtain a lithium battery to-be-predicted sample used for being input to a trained prediction model; when the prediction model receives the to-be-predicted sample of the lithium battery, generating a prediction action corresponding to the initial state of the to-be-predicted sample of the lithium battery, and splicing the prediction action corresponding to the initial state to the end of the initial state of the to-be-predicted sample of the lithium battery to serve as a first prediction trend curve by the interaction environment used by theprediction model; intercepting a sequence with the length equal to the single state length from the first prediction trend curve result, inputting the sequence into the prediction model as a next moment state, enabling the prediction model to give a prediction action corresponding to the next moment state, and splicing the prediction action corresponding to the next moment state to the end of thenext moment state by the interactive environment, and taking the prediction trend curve as a second prediction trend curve until a final prediction trend curve is obtained.
Owner:BEIHANG UNIV

Intelligent sliding bearing capable of adjusting viscosity of lubricating fluid automatically and control method thereof

The invention discloses a method for controlling an intelligent sliding bearing capable of adjusting the viscosity of lubricating fluid automatically, which belongs to the technical field of mechanical design and automatic control. The bearing makes magnetic fluid (5) held between a rotating shaft (6) and a bearing inner bush (7) through a sealing structure. The method firstly determines a coil control current of the rotating shaft when the bearing friction torque is minimum under different rotating speeds and the condition of the born load through a series of tests, and at this time the size of the control current is the optimal control current under the condition. And then according the test result the method establishes a database of the optimal control current aiming at the rotating speed and the born load condition. Finally in the actual application, a force sensor and a rotating speed sensor are used to measure the rotating shaft speed and the born load under an actual work condition, and according to the result the database is inquired, thus an adjusting coil (4) is used to control the current, so that the viscosity of the magnetic fluid (5) is automatically adapted to the work condition, and the friction power consumption and waste are reduced.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Design method for supercharging system of aviation piston two-stroke engine

The invention discloses an aviation piston two-stroke engine supercharging system design method, and belongs to the technical field of aviation piston two-stroke engine supercharging system design. The method comprises the steps that basic parameters and performance strengthening target parameters of the aviation piston two-stroke engine are determined; selecting and matching a supercharger and preliminarily designing structural parameters of a resonant tube; determining common working condition parameters of the aviation piston two-stroke engine and a use weighted value of each working condition; optimizing structure parameters of the resonant tube through a genetic algorithm, and determining control target parameters; and according to a supercharger and the optimized resonance tube, a supercharging system is machined and assembled for the aviation piston two-stroke engine, and test verification is carried out. The design method of the aviation piston two-stroke engine supercharging system is suitable for an aircraft with high lift limit, high maximum level flight speed and long endurance, high comprehensive performance under all working conditions is considered, the design period is short, and the trial-manufacturing cost is low.
Owner:AEROSPACE TIMES FEIHONG TECH CO LTD

Asphalt mixture pressure type permeameter and method for measuring permeability

An asphalt mixture pressure type permeameter comprises a controller air storage sac, wherein the air inlet end of the air storage sac is communicated with an air-filling device through an electromagnetic air inlet valve which is installed on a guide pipe, the air outlet end of the air storage sac is communicated with a sealing cover through an electromagnetic air outlet valve which is installed on the guide pipe, the electromagnetic air inlet valve and the electromagnetic air outlet valve are connected with a controller through leads, and a pressure sensor which is connected with the controller through the lead is arranged on the side wall of the air storage sac. The asphalt mixture pressure type permeameter further comprises a timing device and a counter weight which is arranged on the edge of the sealing cover. Air is taken as medium, the controller controls the air inlet valve and the air outlet valve of the air storage sac, so the compressed air passes by an asphalt mixture test piece which is linked with the sealing cover, the pressure sensor sends the pressure signal to the controller, the controller converts the pressure signal into time signal, the timing device displays the time for reducing the air storage sac from one fixing air pressure to another fixing air pressure, so the permeability of the test piece is measured, the test time is greatly shortened, the efficiency is high, and water resources are saved.
Owner:CHANGAN UNIV
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