22 results about "Stress cycle" patented technology

The application provides a ship structure fatigue strength analysis method and system, which calculates the main engine vibration load and the wave load received by the ship structure based on the ship data, the characteristic data of the ship structure and the global sea state data, then calculates the stress response process under the combined action of the wave load and the main engine vibration load, the spectral density function of the stress response process, each order spectral moment of the stress response process and the zero-crossing rate of the stress response process, then calculates the stress response and the stress response peak of the ship structure under the action of the sinusoidal vibration load, calculates the stress cycle number of the ship structure based on the stress response and in combination with the fatigue life S-N curve, further calculates the fatigue damage under the action of the main engine vibration load, and finally calculates the total coupling fatigue damage under the long-term sea state, and further calculates the fatigue damage of the ship structure under the combined action of the high and low frequency loads, which effectively improves the accuracy and reliability of the ship structure fatigue strength calculation.

The invention relates to a life prediction method for an automobile differential system, which comprises the following steps of: 1) dividing working conditions according to a motion relation between a planetary gear and a half axle gear of the automobile differential system, and constructing a differential system finite element model; 2) performing stress analysis on the plurality of working conditions to obtain a stress matrix table of each torque and stress parameter under different working conditions; 3) acquiring a durability load spectrum in a whole vehicle durability test and stress cycle times under different torques; and 4) combining the S-N curve of each part of the differential system to obtain the safety coefficient of each part, and predicting the service life. According to the method, a differential system finite element model is established by distinguishing two types of working conditions, a stress matrix table is generated through targeted stress analysis, the number of stress cycles is obtained in combination with a load spectrum, the safety coefficient is calculated by means of a part S-N curve and a Miner rule, the stress rule of the real working condition can be accurately captured, and the service life prediction precision is improved. The high reliability requirement of a new energy automobile differential system is met, and key technical support is provided for research and development and reliability guarantee of the new energy automobile differential system.

This application discloses a fatigue design method for high-strength bolts used in aircraft wheels, specifically relating to the field of aircraft components. The method includes: determining the bolt preload and preload torque based on the bolt's nominal diameter, the bolt material's yield strength, and a first preset relationship, combined with the bolt's application environment; determining the minimum and maximum stresses on a single bolt; determining the stress cycle ratio of a single bolt; when the stress cycle ratio reaches a preset value, determining the equivalent stress based on the minimum and maximum stresses on a single bolt; determining the bolt's cycle life based on the equivalent stress, and combining the product of the tire's rolling circumference and the aircraft's takeoff and landing distance to determine the bolt's takeoff and landing life. Based on the above method, the service life of high-strength bolts under fatigue cyclic loading can be improved.

The technology is generally directed to determining fatigue damages to an electronic component or a hardware system caused by the transport or movement of the electronic component or hardware system. The electronic components may be, for example, data center hardware components. The electronic components are susceptible to fatigue damage resulting from thermal, shock and vibration events. The thermal, shock, and vibration events may occur, for example, during transport or movement of the electronic components. To fully characterize fatigue, the acceleration and stress cycles may be tracked, which correlate with natural phenomena in the global supply chain and data center environment.

The invention discloses a filter backwashing system, relates to the technical field of filter backwashing, and aims to solve the technical problems that metal fatigue is accelerated by thermal stress circulation and crystals are difficult to wash and clean. The anti-thermal-stress pipe is of a composite structure, thermal stress generated by temperature shock is effectively relieved through cooperation of the low-expansion inner layer, the shape memory middle layer and the high-expansion outer layer, the service life of equipment is prolonged, the air suction outer sleeve forms air-liquid mixed flow according to the Venturi principle, impact force generated by bubble breakage can strengthen crystal removal, and the service life of the equipment is prolonged. The deformation flow channel mechanism achieves two-section type washing, impurities easy to wash are removed in a large-flow mode in the initial stage, gas-liquid mixing needles are used for stubborn crystals in the later stage, pulse flow is generated through cooperation of a pulse pressing sleeve and a pressing piece, and the cleaning effect is enhanced through instantaneous high-pressure shock waves. In addition, a corrugated pipe head adapts to thermal expansion and cold contraction, and the washing distance can be shortened through the multi-section sleeve design of a back-flushing spraying cover; and the recoil performance is optimized, and stable operation of the system under complex working conditions is ensured.

This invention discloses a method, system, equipment, and medium for dynamic operation and maintenance of distribution networks based on point cloud technology, belonging to the field of distribution network operation and maintenance technology. It includes: inferring the connection stiffness of obstructed insulators from deformation correlation data to construct a stress topology map; identifying modally abnormal devices and calculating stress redistribution results, which are then transmitted to the distribution network equipment; constructing a fault evolution map and detecting stress cycle structures; iteratively executing stress correction values ​​until convergence; calculating bifurcation risk values ​​based on the stress distribution dispersion and maximum propagation depth of bifurcation state nodes; simulating the impact of stiffness enhancement on the number of faulty nodes in insulators; and outputting priority reinforcement equipment. This invention enables all insulators to obtain connection stiffness, eliminates accumulated deviations on the cycle path using stress correction values, comprehensively quantifies the unevenness of stress distribution and propagation depth using bifurcation risk values, and prioritizes reinforcement equipment located at critical bifurcation nodes.

This invention relates to the field of building material structural testing technology, specifically a system and method for testing the impact resistance performance of railings and handrails. The system includes: launching a standard test impactor at a preset impact point using a controllable electromagnetic launcher; acquiring a sequence of transient deformation images from multiple perspectives using a high-speed camera; extracting the spatial coordinates of structural feature points through image enhancement and feature point calibration; and calculating the dynamic displacement field and dynamic strain field. An elastoplastic dynamics inversion algorithm is used to calculate the stress distribution time history and local plastic deformation within the impact contact area, identifying stress concentration areas and determining the stress peak and stress cycle number. Combined with the degree of residual deformation, the impact resistance performance level of the railing and handrail is quantitatively assessed, achieving standardization of the testing process and quantification of the results. This method enables controllable impact process and multi-dimensional deformation acquisition, accurately obtaining the internal mechanical response parameters of the component.

The application provides a kind of fan power scheduling optimization method and system, based on the operating characteristics of fan key components and external environmental factors, the stress characteristic model of key components is constructed;Based on the stress characteristic model of the key components, combined with four-point rain flow counting method and residual wave series method, the stress cycle in the operation of fan is identified and corrected, based on fatigue damage theory, the cumulative fatigue damage of fan key components is calculated;A power scheduling model is constructed to minimize the fatigue damage of the fan, the objective function is defined as the weighted minimum value of the main shaft and tower fatigue damage, and all aspects of constraints are considered comprehensively;The power scheduling model is solved by nonlinear programming method, and the optimal power scheduling strategy of each wind turbine generator is generated.The application can effectively reduce the cumulative speed of fan fatigue damage, prolong the service life of fan key components, and realize the comprehensive improvement of wind farm operation economy and equipment reliability through optimizing power scheduling strategy.

The invention provides a shield hobbing cutter replacement prediction method and system under complex geological conditions, and relates to the technical field of shield hobbing cutters, and the method comprises the steps: collecting the installation position, the stress parameter, the cutterhead rotation speed and the propulsion speed of a cutterhead hobbing cutter of a shield tunneling machine; dividing the stress parameters into a plurality of stress cycles according to the rotation period of the cutterhead to obtain the peak-valley ratio and the time ratio of each cycle; generating a stress characteristic trajectory curve according to the peak-valley ratio and the time ratio, and determining soil property mutation points according to the change rate of the envelope area of the stress characteristic trajectory curve; the hob soil body cutting volume is determined through the time interval of two continuous stress cycles, a characteristic coefficient curve is constructed according to the projection area of the volume on a cutterhead rotation plane, and the characteristic coefficient curve and the stress characteristic track curve are mapped to obtain stress characteristic coefficients; and taking a section between adjacent soil mass property mutation points as a stable interval, and determining the hobbing cutter changing time according to an internal stress characteristic coefficient accumulated value and a change rate in the stable interval. The technical problem that the prediction accuracy of shield hob abrasion under complex geological conditions is low is solved.

The invention discloses a diaphragm compressor diaphragm head fatigue life prediction simulation method, which comprises the following steps: S1, establishing a fluid-solid-thermal coupling model of a to-be-predicted diaphragm head according to structural parameters of a diaphragm compressor; s2, based on the fluid-solid-thermal coupling model, performing simulation analysis on air pressure distribution, diaphragm dynamic and stress-strain characteristics in the diaphragm compressor under different working conditions to obtain simulation data including pressure load, diaphragm displacement amplitude, a stress cycle curve and temperature distribution; and S3, based on the simulation data, calculating the fatigue life of the to-be-predicted film head. Through a pure simulation means, a fluid-solid-thermal coupling model is established, the flow characteristic and the structure stress state are dynamically corrected by using real-time simulation data, and aiming at the problem that the opening and closing state of the hydrogen compressor valve is difficult to directly monitor, the opening time point and the duration of the valve are accurately determined by monitoring the state parameters of the gas cavity in real time, so that the hydrogen compressor valve opening and closing state is accurately monitored. Indirect and accurate judgment of the working state of the valve is achieved, and the simulation accuracy and reliability are improved.

The application discloses a tunnel time-lag type rock burst dynamic stress and geology comprehensive discrimination method and system, and relates to the technical field of tunnel engineering. The application discriminates the risk of current disturbance-induced time-lag type rock burst after the excavation of a working face by analyzing the disturbance stress size, the spatial relationship between the disturbance stress source and the tunnel, the disturbance stress cycle frequency, the disturbance stress superposition condition, the working face condition, the spatial relationship between the structural plane and joint and the tunnel, and the self characteristics of the structural plane and joint. The judgment of disturbance-induced time-lag type rock burst is combined with the actual working condition, the time-lag type rock burst can be comprehensively evaluated, and the time-lag type rock burst can be better and more accurately judged. Targeted support and prevention and control measures are taken according to different disturbance stresses and geological defect conditions, the engineering construction risk can be reduced to a certain extent, the economic damage can be reduced, the safety of construction personnel can be ensured, and the application has good application value for underground engineering with frequent rock burst disasters, frequent excavation disturbance, frequent earthquakes and complex geological structure.

The invention relates to the technical field of digital twinning, in particular to a digital twinning-based wind turbine generator full life cycle management system, which comprises a deformation parameter resolving module, a skeleton driving reconstruction module, a load damage calculation module, a health difference evaluation module and a balance control decision module. According to the method, the instantaneous curvature and the torsion rate are calculated by collecting cross section wavelength drift data, the dynamic bending posture of the flexible part in the space is reconstructed in real time, continuous tracking of stress circulation and a closed lag loop is achieved by combining pneumatic simulation and the residual peak-valley sequence stack technology, the accumulated damage degree of the part in the whole service cycle is accurately quantified, and the reliability of the part is improved. By analyzing the discrete deviation of individual damage relative to a group mean value, an asymmetric load distribution mechanism based on health state difference is established, the fatigue extension trend of high-damage parts is effectively relieved, premature failure caused by uneven load distribution is avoided, and life balance and collaborative life extension of key parts of a unit in the whole life cycle are achieved.

The application discloses an improved step counting method based on hip gait stress data, and is characterized in that stress step range and stress step number of the improved step counting method are preset based on hip gait stress data characteristics; stress steps crossed by gait stress data are sequentially judged according to a counting principle of the improved step counting method, and the number of the crossed stress steps is counted; and the crossed stress steps are combined into a stress cycle according to a stress cycle determination method of the improved step counting method, so that the amplitude and the average of the stress cycle are obtained. The method overcomes the problems of poor real-time performance and loss of time sequence information in the data counting process of the traditional fatigue counting method, effectively saves the time sequence information of femoral structure gait stress, and improves the accuracy of the artificial hip joint structure fatigue life analysis result.

The invention relates to the technical field of aviation turbine shaft engines, and discloses a power turbine disc stress cycle calculation and engine life management method and system.The method comprises the steps that the rotating speed of a power turbine rotor and the temperature of a gas turbine outlet are obtained and converted into regular cycle data, and pulsation stress cycle data are extracted; calculating the stress of the key part of the power turbine rotor at the rated rotating speed according to the pulsating stress cycle data of the rotating speed of the power turbine rotor; calculating the stress caused by the temperature field of the key part of the power turbine rotor at different rotating speeds except the rated rotating speed by combining the rotating speed of the power turbine rotor and the pulsating stress cycle data of the outlet temperature of the gas turbine; and calculating centrifugal stress and temperature stress of the power turbine rotor at the maximum rotating speed to obtain resultant stress, calculating maximum equivalent stress according to the resultant stress, and performing service life management. According to the method, the calculation efficiency can be improved while the calculation precision of the stress of the power turbine disc is ensured, and the service life of an aviation turbine shaft engine is prolonged.

The invention provides a mold clamping force and tapping synchronization performance analysis method which comprises the following steps: acquiring tool path data, and simulating a torque transmission process by combining a boundary condition of a narrow area in a mold to obtain torque distribution; tool root position coordinates are determined according to the torque distribution data, material attribute parameters are overlaid on the tool root position coordinates, and torque is optimized through a genetic algorithm; the optimized torque is input into the finite element grid model, stress concentration factor distribution is calculated from the finite element grid model, and the grid density is adjusted to obtain a refined stress diagram; acquiring peak stress data from the refining stress diagram, counting the number of stress cycles to determine a fatigue damage value, generating an adaptive control signal, and inputting the adaptive control signal into the simulated tapping cycle to obtain a tool running state; according to the tool operation state, three-dimensional space displacement data generated by the root of the lead screw under the torque effect are extracted and reflected by monitoring the axial and radial displacement data of the lead screw, and a stable torque path is confirmed.

The invention discloses a spherical tank supporting structure, a storage and transportation system and a manufacturing method thereof.The spherical tank supporting structure comprises a transition piece, a skirt shell section and a basic annular plate, the transition piece is welded to a lower pole spherical shell of a spherical tank through a butt joint, smooth transition is achieved between the transition piece and the spherical tank, and the upper end of the skirt shell section is welded to the lower end of the transition piece; the lower end of the skirt shell ring is welded with the foundation ring plate; according to the supporting structure, the transition piece and the spherical tank are in smooth transition, a stress concentration system at the transition position is reduced, the fatigue life of equipment under pressure circulation is prolonged, the transition piece and the spherical tank are welded through the butt joint, a welding seam for connecting the transition piece and the spherical shell is eliminated, welding defects and heat affected zones at the connecting position are fundamentally eradicated, and the service life of the equipment is prolonged. The reliability of the supporting structure is improved.

The application relates to the technical field of aviation turbine shaft engines, and discloses a power turbine disc stress cycle calculation and engine life management method and system, which comprises the following steps: acquiring the power turbine rotor rotating speed and the gas turbine outlet temperature and converting the acquired data into regular cycle data to extract the pulsating stress cycle data; calculating the stress of key positions of the power turbine rotor at the rated rotating speed according to the pulsating stress cycle data of the power turbine rotor rotating speed, and calculating the stress caused by the temperature field of the key positions of the power turbine rotor at different rotating speeds except the rated rotating speed in combination with the pulsating stress cycle data of the power turbine rotor rotating speed and the gas turbine outlet temperature; calculating the centrifugal stress and the temperature stress of the power turbine rotor at the maximum rotating speed and obtaining the resultant stress from the centrifugal stress and the temperature stress; and calculating the maximum equivalent stress according to the resultant stress and performing life management. The application can ensure the stress calculation precision of the power turbine disc, improve the calculation efficiency, and prolong the service life of the aviation turbine shaft engine.

The application discloses a kind of safety evaluation method, equipment, medium and product of high-temperature thick-walled component of peak-shaving power station boiler, relate to the field of safety evaluation of power station boiler component, the method includes according to the historical operation condition data of high-temperature thick-walled component of peak-shaving power station boiler, determine multiple stress cycle conditions and examination points;According to the condition data corresponding to each stress cycle condition and examination point determines low-cycle fatigue life loss rate and creep life loss rate;The low-cycle fatigue life loss rate corresponding to all stress cycle conditions is accumulated, and total low-cycle fatigue life loss rate is obtained;The creep life loss rate corresponding to all stress cycle conditions is accumulated, and total creep life loss rate is obtained;The safety of high-temperature thick-walled component is evaluated based on total low-cycle fatigue life loss rate and total creep life loss rate.The application can improve the efficiency and precision of safety evaluation of high-temperature thick-walled component of peak-shaving power station boiler.

The invention discloses a string vibration multi-modal fatigue life prediction method and system, and belongs to the technical field of structure fatigue life prediction, and the method comprises the steps: obtaining the feature data of a string structure, the curvature during multi-modal vibration, and the environment data of the environment where the string structure is located; according to the characteristic data of the chord structure and the curvature during multi-modal vibration, generating dynamic stress of structural points of the chord structure; the dynamic stress is processed through a rain flow counting method, a complete stress cycle is analyzed, and the stress cycle comprises the stress amplitude and the average stress; generating an equivalent zero average stress amplitude according to the stress amplitude and the average stress; according to the equivalent zero average stress amplitude, generating an initial fatigue damage value of the structural point of the chord structure; generating an environmental influence factor according to the environmental parameters of the environment where the chord structure is located; generating a fatigue life prediction value of the chord structure according to the initial fatigue damage value of the structural point of the chord structure and the environmental influence factor; the method has the advantage of improving the accuracy of fatigue life prediction under multi-modal vibration and complex environment conditions.

This invention belongs to the cutting-edge interdisciplinary field of structural safety assessment and intelligent operation and maintenance management of engineering machinery. It provides a method for intelligent life assessment and management of tower crane tower structures, including: establishing unique identifiers for each standard section of the tower; identifying operating parameters for each work cycle; establishing a finite element model of the tower crane tower; training a proxy model; inputting actual operating parameters into the trained proxy model to obtain the stress cycle spectrum of each standard section; calculating the fatigue damage value and remaining life of the main structure of each standard section; establishing weld sub-models for dangerous weld areas in the standard sections; establishing a standard section life cycle database; and performing reassembly judgment and installation management based on the standard section life cycle database and the stress conditions of the sections. Through the collaborative assessment of the main structure and dangerous weld areas, the life consumption characteristics of the overall load-bearing structure and local weld weakness areas can be reflected across scales, improving the completeness of fatigue life assessment results.

The invention discloses a method for calculating the fatigue damage life of a photovoltaic support and a related product. The method comprises the steps of obtaining stress power spectral density according to wind speed data, a wind speed time history prediction model and a finite element model about a photovoltaic support; wherein the stress power spectral density comprises a dangerous section of each component in the photovoltaic support, n stress cycle grades corresponding to the dangerous section and stress cycle times corresponding to each stress cycle grade; for one stress cycle grade in the n stress cycle grades, determining stress cycle times and material fatigue damage life corresponding to the stress cycle grade; according to the number of stress cycles and the fatigue damage life of the material, fatigue damage of the stress cycle grade is obtained; and obtaining the fatigue damage life of the photovoltaic support according to the fatigue damage of each stress cycle grade. According to the embodiment of the invention, the service life of the photovoltaic support is calculated from the angle of structural fatigue damage accumulation, so that the accuracy of calculating the service life of the photovoltaic support is improved.

The utility model discloses an aluminum alloy profile stress circulation strengthening device, and belongs to the technical field of aluminum alloy profile machining. The aluminum alloy section is placed between the upper tooth plate and the lower tooth plate, the control motor controls the sliding block to slide on the sliding rail, the jacking frame is arranged at the bottommost part of the sliding rail when stress of the aluminum alloy section is not eliminated, and the jacking frame ascends to abut against the bottom face of the aluminum alloy section when stress needs to be eliminated. The stress of an aluminum alloy profile is eliminated through occlusion between an upper tooth plate and a lower tooth plate, in order to guarantee occlusion stability and avoid the problem of deflection in the occlusion process, a reinforcing block is installed at the tail of a fixing frame, the fixing frame is connected with the reinforcing block through a traction rod, the stability of the fixing frame is kept, a pulley slides on a guide rail and can do reciprocating motion, and therefore the stress of the aluminum alloy profile is eliminated. And the stress of the aluminum alloy profile is eliminated by pressing the aluminum alloy profile for many times.