Patents
Literature
Patsnap Copilot is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Patsnap Copilot

38 results about "Limit state function" patented technology

Active reliability analyzing and evaluating method for highly-reliable mechanical products

The invention provides an active reliability analyzing and evaluating method for highly-reliable mechanical products. The active reliability analyzing and evaluating method for the highly-reliable mechanical products includes: firstly, establishing ultimate state functions of mechanical products, utilizing a Monte Carlo simulation method to produce sample points conforming to parameter distribution, utilizing a Kriging meta-model to simulate the ultimate state functions, improving simulation precision and confirming an optimal sampling radius by automatically updating DOE (design of experiment), constructing important sampling density functions, producing random sample points through the important sampling density functions, updating the DOE continually, then extracting radius random sample points obeying chi-square distribution, confirming failure probability and failure coefficient of variation of the mechanical products, and limiting whether updating finishes or not by the failure coefficient of variation so as to obtain reliability of the mechanical products finally. The active reliability analyzing and evaluating method for the highly-reliable mechanical products has the advantages of high efficiency, good robustness and high simulation precision, comprehensive design and analysis of rail wear life and reliability to spatial mechanisms are achieved, and the active reliability analyzing and evaluating method for the highly-reliable mechanical products is significant to reliability design technology engineering of complex mechanisms of aerospace equipment.
Owner:BEIHANG UNIV

Turning machining parameter optimization method considering uncertain parameters,

The invention provides a turning machining parameter optimization method considering uncertain parameters. The method comprises the steps of obtaining a stability limit-state function according to preset initial vibration conditions and stability critical-state information of a turning machining system; adopting an AFOSM to obtain reliability indexes for evaluating the stability of the system; with MRR as preset constraint conditions of an optimization target, ,establishing an optimization model of the reliability of turning process parameters in the system, wherein the constraint conditions comprise reliability constraint conditions and stochastic design variable boundary constraint conditions; optimizing and processing the optimization model, and obtaining a target function value which is optimized and converged and meets the reliability constraint conditions, wherein certainty parameters, stochastic design variables and stochastic parameters which correspond to the target function value serve as output turning machining parameters. According to the method, the reliability can serve as an evaluation index and optimization condition, and the influences of uncertain factors on the turning process are analyzed in order to obtain the best turning machining parameters.
Owner:NORTHEASTERN UNIV

Dynamic coupling time varying failure rate analysis method of on-orbit space flexible gear mechanism

ActiveCN104008240AAvoid the problem of low reliability calculation accuracySuitable for highly nonlinear situationsSpecial data processing applicationsFailure rateEngineering
A dynamic coupling time varying failure rate analysis method of a on-orbit space flexible gear mechanism comprises the seven steps that firstly, according to the fact that a shaft in the on-orbit space flexible gear mechanism is an elastic body, a kinetic equation of the flexible shaft is built, and the finite element method is adopted for analysis; secondly, a gear kinetic equation is built; thirdly, a nonlinear kinetics equation of coupling of the flexible shaft and a gear in the on-orbit space flexible gear mechanism is built; fourthly, transmission stimulation analysis is performed on the space flexible gear mechanism; fifthly, the Newmark algorithm is adopted to calculate a dynamic load coefficient; sixthly, a gear bending stress reliability limit state function is built in the on-orbit space flexible gear mechanism; seventhly, dynamic reliability and failure rate analysis are performed on the space flexible gear mechanism. The method solves the problem that reliability calculating accuracy is low because of nonlinear factors of a traditional transfer matrix method and mode superposition method, and has engineering practical value for improving reliability of the on-orbit space flexible gear mechanism and other spacecrafts. The method is also suitable for other flexible gear mechanisms.
Owner:BEIHANG UNIV

Structural reliability method based on dynamic weight response surface under mixed uncertainty

The invention discloses a structural reliability method based on dynamic weight response surface under mixed uncertainty. The invention is applied to the field of reliability technical field, and aimsat structural reliability problems under mixed variables. The method comprises the following steps of determining a fitted sample of a current iterative response surface; fitting and getting the response surface of the current iteration by weighted least squares; getting the reliability design point of the current response surface according to the hybrid variable decoupling method; stopping the iteration, when the value of the random variable part of the reliability design point obtained by two adjacent iterations satisfies the convergence criterion; calculating the failure probability of thestructure by Monte Carlo simulation according to the response surface obtained from the last iteration. The invention constructs the response surface, so that the limit state function in the standardnormal space is explicitly approximated in the form of a quadratic response surface, which facilitates subsequent reliability analysis. And a double weighting mechanism is introduced to effectively improve the accuracy and computational efficiency of the response surface method.
Owner:UNIV OF ELECTRONICS SCI & TECH OF CHINA

Bridge-ballastless track structure extreme temperature prediction method and system

The present invention relates to the technical field of probability statistical analysis and prediction of concrete temperature fields, and discloses a bridge-ballastless track structure extreme temperature prediction method and system, so as to avoid subjectivity of the conventional experience distribution method and the cumbersome derivation process of the first-order second-moment method and to obtain a relatively preciser temperature extremum in the case of a certain amount of data. The method disclosed by the present invention comprises: forming a statistical sample by means of measured bridge-ballastless track structure temperature data; calculating firt to fourth moments of the stastical sample to obtain a statistical feature of the sample; constructing virtual distribution by means of standard regular distribution to indirectly describe a distribution condition of the sample; solving a key parameter and feature estimation of the virtual distribution; constructing an extreme state function considering an extreme temperature, and giving an exceedance probability; and calculating first to fourth moments of the extreme state function by means of a reliability indicator formula, and reversing an extreme temperature value corresponding to the exceedance probability and giving a corresponding reoccurrence period.
Owner:CENT SOUTH UNIV

Method for synthesizing for non-probability time-varying reliability of link mechanism containing hinge gap

ActiveCN105760578AIncreased time-varying reliabilityEffectively account for and quantify cumulative effects over timeGeometric CADSpecial data processing applicationsMechanism synthesisDiscretization
The invention provides a method for synthesizing for non-probability time-varying reliability of a link mechanism containing a hinge gap. Firstly, according to the rod length and initial position of the link mechanism and specific characteristics of the hinge gap, a mathematic expression of a mechanism motion error function is obtained in combination with a vector method; secondly, rod length and hinge uncertainty information is introduced into an interval process model for establishing mechanism motion errors, and the time-varying uncertainty characteristic quantity of a mechanism motion precision limit state function is quickly calculated; thirdly, based on the first crossing theory and the dispersed strategy, index definition and solution of crossing failure possibility in any micro cyclic loading increment segment are completed, and then a time-varying reliability model is constructed; finally, the non-probability time-varying reliability index of motion precision serves as a target, non-probability reliability of mechanism existence conditions serves as a constraint condition, and synthesis of the non-probability time-varying reliability of the link mechanism containing the hinge gap is completed. In the process of mechanism synthesis, synthetic effects of uncertainty on the mechanism in a motion period are reasonably represented, and the time-varying reliability of the mechanism can be effectively improved.
Owner:BEIHANG UNIV

Reliability analysis method for heat transfer system containing fuzzy parameters

The invention discloses a reliability analysis method for a heat transfer system containing fuzzy parameters. The method comprises the following steps that: carrying out the finite element modeling of a heat transfer system; utilizing a fuzzy variable to represent uncertain input parameters, and establishing the fuzzy finite element equation of the heat transfer system; selecting a cut set level, and converting the fuzzy variable into an interval variable so as to obtain one group of interval finite element equations; utilizing a perturbation theory to solve the interval finite element equations to obtain the upper and lower bounds of interval temperature response; according to the temperature response, establishing an ultimate state function which represents system reliability, and calculating the upper and lower bounds of the ultimate state function; utilizing an interval sorting method to process the ultimate state function to obtain an interval reliability index under each cut set level; and carrying out integral computation on the interval reliability index under the cut set level, and finally, obtaining the fuzzy reliability index of the heat transfer system. On a premise that calculation efficiency is guaranteed, by use of the method, the fuzzy reliability calculation accuracy of the heat transfer system can be effectively improved, which can not be realized by general commercial software.
Owner:BEIHANG UNIV

Method for determining design coefficient of reinforced thermoplastic pipe (RTP)

The invention discloses a method for determining a design coefficient of a reinforced thermoplastic pipe (RTP). The method comprises the following steps: analyzing an internal pressure load, bending load, external pressure load, axial tension load, temperature difference load and combined load of the RTP, and analyzing the load resistance of the RTP; establishing a limit state function, load probability model and resistance probability model under different load conditions; determining an average value, standard difference and variation coefficient of the loads and the resistance; giving a target reliability index, and determining a partial load coefficient and partial resistance coefficient by virtue of a FORM method; determining the design coefficient by virtue of an LRFD method. The method has the beneficial effects that the loads of the RTP are classified into the internal pressure load, the bending load, the external pressure load, the axial tension load, the temperature difference load and the combined load; the target reliability index is combined to form a calculation method for the design coefficient by establishing a limit state equation and establishing the probability models, so that a foundation is laid for the future engineering application of the RTP to an oil and gas transmission pipeline.
Owner:BC P INC CHINA NAT PETROLEUM CORP +2

Interval model time varying reliability based on active service structure optimized maintenance design method taking into account dynamic uncertainty

The invention discloses an interval model time varying reliability based on active service structure optimized maintenance design method taking into account dynamic uncertainty. According to the invention, influence on mechanical behaviors of an on active service structure by time varying uncertainty is taken into account comprehensively. First, through defining the uncertainty characteristics ofquantified basic variables of a non-probability interval model and through uncertainty propagation analysis, a limit state function of the structure taking into account a static-dynamic hybrid uncertainty condition is deduced; reliability indexes of the on active service structure based on the non-probability interval model are established based on a first-time passage theory; establishment of a maintenance cost model under a non-probability frame is tried by taking a maintenance cost formula proposed by Frangopol as the basis and an optimized maintenance design method for the on active service structure is constructed; the optimal scheme for maintenance in the service cycle of the on active structure is finally determined through repeated iteration of particle swarm optimization by takingthe structure maintenance total cost as the optimization target, taking the maintenance frequency, the type and the corresponding time points as design variables and taking the structure reliabilityas optimization constraints.
Owner:BEIHANG UNIV

Method for calculating reliability of long-span bridge members under action of windmill load

The invention discloses a method for calculating the reliability of long-span bridge members under the action of a windmill load. The method comprises the steps of firstly, determining parameter typesof a target bridge structure limit state function, collecting parameter data, randomly grouping the collected data, and performing normalization processing on the data; secondly, establishing an optimized limit state function fitting program based on a thought evolution algorithm and a neural network, performing calculation by adopting the thought evolution algorithm in the program to obtain an optimal individual as an initial weight value and a threshold value of the next-step calculation, substituting input data of a test set into a trained neural network for performing simulation prediction, comparing load effect data obtained by prediction with expected data, calculating an error, and evaluating a fitting effect of the obtained neural network; and finally, combining the trained network with a Monte Carlo method optimized by a particle swarm algorithm, thereby establishing an optimized reliability calculation method for finishing the calculation of the reliability of the long-spanbridge members under the action of the windmill load.
Owner:CHANGAN UNIV

Non-backfill arch open-cut tunnel structure probability reliability degree design method under fallen rock impact

ActiveCN107239645AAccurate Optimization StrategyGeometric CADSpecial data processing applicationsLoad modelRockfall
The invention discloses a non-backfill arch open-cut tunnel structure probability reliability degree design method under fallen rock impact. The method comprises the steps that a limit state function of an arch open-cut tunnel structure ultimate bearing capacity model, an impact load model of an arch open-cut tunnel by fallen rocks and a non-backfill arch open-cut tunnel structure under the fallen rock impact is built; according to the limit state function, a JC method of a first-order quadric moment method is adopted to calculate a structure reliability index of the arch open-cut tunnel; when the structure reliability index is equal to a target reliability index, and the structure reliability index is larger than the target reliability index and the value which exceeds the target reliability index is smaller than or equal to a set threshold valve, the arch open-cut tunnel structure probability reliability degree which is designed by a selected structure design parameter meets design requirements; when the structure reliability index is smaller than the target reliability index, and the structure reliability index is larger than the target reliability index and the value which exceeds the target reliability index is larger than a set threshold value, the structure design parameter is adjusted until the arch open-cut tunnel structure probability reliability degree which is designed by the selected structure design parameter meets the design requirements.
Owner:SOUTHWEST JIAOTONG UNIV

A bridge crane reliability optimization design method

The invention discloses a bridge crane reliability optimization design method which comprises the following steps: S1, defining uncertain structure parameters in a crane, and describing the uncertainparameters as interval variables; S2, establishing a limit state function according to the structural failure form, and solving a reliability index in the optimization model by adopting a Vparalove function in MATLAB based on an interval analysis method; S3, introducing a non-probabilistic reliability index, and establishing a non-probabilistic reliability optimization design model by taking a given required reliability index as a constraint condition; S4, solving an optimization problem;. According to the method, the reliability index can be effectively, quickly and accurately solved; Secondly, the common defects of low iteration rate, low optimization precision, large storage space and the like of an optimization algorithm in the actual solving process are considered; On the basis of researching a traditional moth flame algorithm, the method is effectively improved, and the convergence rate and the convergence precision of the outer layer optimizer are remarkably improved. And the method has an important value in structural reliability optimization design in engineering practice.
Owner:ZHUZHOU TIANQIAO CRANE

Non-probability interval interference time-varying reliability analysis method

PendingCN110472264AImprove analysis of overly conservative issuesSpecial data processing applicationsStress strengthAnalysis method
According to a non-probabilistic interval interference time-varying reliability analysis method provided by the invention, the time-varying reliability of a structure can be evaluated without specificdistribution of parameters, and a reference is provided for structural time-varying reliability analysis. Firstly, based on a non-probability interval theory, structural stress and strength at any moment are converted into an interval variable form; secondly, in combination with a stress-strength interference theory, structural stress and strength interval are converted into a standardized interval, and a relationship between a structural limit state function and the standardized interval is changed at different moments; and an interval interference time-varying reliability index eta belonging to [0, + infinity] is defined according to the relationship between the structure limit state function and the standardized interval. Wherein eta = 0 indicates that the storage tank is in a failurestate, 0 < eta < 1 indicates the reliability of the storage tank, and eta > = 1 indicates the safety margin of the storage tank. Finally, comparative analysis is made with an interval reliability andstress-intensity interference reliability method to verify the effectiveness of the non-probabilistic interval interference time-varying reliability evaluation method provided by the invention.
Owner:PLA PEOPLES LIBERATION ARMY OF CHINA STRATEGIC SUPPORT FORCE AEROSPACE ENG UNIV

A Time-varying Failure Rate Analysis Method for Dynamic Coupling of On-orbit Space Flexible Gear Mechanism

ActiveCN104008240BAvoid the problem of low reliability calculation accuracySuitable for highly nonlinear situationsSpecial data processing applicationsFailure rateEngineering
A dynamic coupling time varying failure rate analysis method of a on-orbit space flexible gear mechanism comprises the seven steps that firstly, according to the fact that a shaft in the on-orbit space flexible gear mechanism is an elastic body, a kinetic equation of the flexible shaft is built, and the finite element method is adopted for analysis; secondly, a gear kinetic equation is built; thirdly, a nonlinear kinetics equation of coupling of the flexible shaft and a gear in the on-orbit space flexible gear mechanism is built; fourthly, transmission stimulation analysis is performed on the space flexible gear mechanism; fifthly, the Newmark algorithm is adopted to calculate a dynamic load coefficient; sixthly, a gear bending stress reliability limit state function is built in the on-orbit space flexible gear mechanism; seventhly, dynamic reliability and failure rate analysis are performed on the space flexible gear mechanism. The method solves the problem that reliability calculating accuracy is low because of nonlinear factors of a traditional transfer matrix method and mode superposition method, and has engineering practical value for improving reliability of the on-orbit space flexible gear mechanism and other spacecrafts. The method is also suitable for other flexible gear mechanisms.
Owner:BEIHANG UNIV

Reliability Assignment Design Method of Function Mechanism of Mechanical Products

ActiveCN106383948BReduce computational workloadThe distribution results are meaningfulGeometric CADConfiguration CADScheme valuePerformance index
The invention discloses a reliability allocation design method of the function mechanism of a mechanical product, and belongs to the technical field of the reliability design of mechanical products. The reliability allocation design method aims to solve the problem that a tolerance allocation method adopted by the function mechanism design of an existing mechanism product only can guarantee the performance index of the mechanical product but can not meet the reliability requirement of the mechanical product. The method comprises the following steps of: determining a functional characteristic quantity and a design variable; combining with a failure criterion to establishing a limiting condition function; obtaining the mean value and the standard deviation expression of the limiting condition function; obtaining the target value of a reliability degree index of the function mechanism; obtaining the target value of the standard deviation of the limiting condition function; obtaining the standard deviation upper limit value of each design variable; obtaining the reliability sensitivity of the design variable, and calculating a relative sensitivity factor; according to the ratio of the relative sensitivity factor, regulating the standard deviation of the design variable, and determining the regulated standard deviation of the design variable; and the taking the regulated standard deviation of the design variable as a design scheme value of the function mechanism. The reliability allocation design method is used for the allocation design of the function mechanism.
Owner:NORTHWESTERN POLYTECHNICAL UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products