223 results about "Bending stiffness" patented technology

The invention provides a reinforcing beam reinforced by adopting an out-of-service wind power blade and a method for determining the bending rigidity. According to the reinforcing beam, a plurality of grooves are formed in at least one surface of a reinforced concrete beam; the reinforcing layer comprises reinforcing ribs and a cement-based composite matrix, a plurality of protrusions are arranged on the surface of the cement-based composite matrix, the protrusions are arranged at intervals in the length direction of the cement-based composite matrix, and the protrusions are correspondingly embedded into the grooves, so that the reinforcing layer is connected with the reinforced concrete beam to obtain a reinforced concrete reinforced beam; wherein the reinforcing ribs are obtained by disassembling and cutting a main beam of the retired wind power blade. According to the reinforcing beam, the combining capacity of the reinforced concrete beam and the reinforcing layer is high, mutual slippage is avoided, the retired wind power blade composite material resources are utilized, the environment is protected, and the cost is saved while high-performance reinforcing treatment can be conducted on the damaged reinforced concrete beam structure or the reinforced concrete beam structure with insufficient bearing capacity.

A shaft for a golf club includes a tip end configured to couple to a golf club head; a butt end opposite to the tip end; and a butt end portion that extends in a butt-to-tip direction from the butt end by at least 50 mm and has an average rate of change of bending stiffness in a tip-to-butt direction, wherein a greatest rate of change of bending stiffness of the shaft in the tip-to-butt direction is at least 2.7 times the average rate of change of bending stiffness of the butt end portion.

The invention discloses an acoustic black hole structure and a vibration damping device.The acoustic black hole structure comprises an acoustic black hole body and a damping layer, the acoustic black hole body is provided with a uniform thickness area and an acoustic black hole area, the acoustic black hole area is provided with a plurality of grooves, the grooves are distributed from the first end to the second end of the acoustic black hole area, and the damping layer is arranged between the first end and the second end of the acoustic black hole area. The depths of the grooves are gradually increased in the direction from the first end to the second end, and the damping layer is arranged in the acoustic black hole area. By machining the groove in the acoustic black hole area, the local bending rigidity of the acoustic black hole body is changed, the bending wave speed of the acoustic black hole body is reduced, the acoustic black hole effect is achieved, due to the arrangement of the groove, the local resonance effect can be utilized, and then structural vibration suppression in the low-frequency range is achieved; the problem that a traditional acoustic black hole structure is poor in low-frequency-band vibration reduction effect is solved, in addition, thickness cutting of an acoustic black hole area of an original structure is avoided, and the manufacturing difficulty and the requirement for the precision of machining equipment are lowered.

The invention provides a parameter determination method and device for an elastic flywheel, a storage medium and electronic equipment, and the method comprises the steps: constructing an optimization model, and carrying out the solving calculation of the optimization model according to an optimization variable, a constraint condition and an optimization target, and obtaining a calculation result; wherein the optimization variables are the number of the middle diaphragms, the thickness of a single middle diaphragm and the position relation between any two middle diaphragms, the constraint conditions are the total thickness of the diaphragms and the minimum strength range of the diaphragms, and the optimization target is to minimize the bending rigidity of the middle diaphragms; the target solution of the calculation result comprises the target diaphragm number of the middle diaphragms, the target thickness of each middle diaphragm and the target position relation between any two middle diaphragms. According to the method, under the condition that the torsional rigidity is not changed, the bending rigidity and strength are flexibly controlled by flexibly combining the number of diaphragms, the thickness of the diaphragms, the arrangement sequence of the diaphragms and the like, so that the effects of high reliability and shafting centering compensation capability are considered.

The invention discloses a frame structure design method based on rigidity reduction. The method comprises the following steps that 1, rod end bending moments Mb and Mc and axial force Nc of frame beams and columns are obtained through calculation; step 2, obtaining actual reinforcement areas Asb0 and Asc0, section sizes and concrete strength of frame beams and columns; 3, the equivalent stiffness Kb1 of the frame beam is obtained through calculation according to the formula Kb1 = Mb0.75y / phi b0.75y; 4, the equivalent stiffness Kc1 of the frame column is obtained through calculation according to the formula Kc1 = Mc0.75y / phi c0.75y; 5, comparing the equivalent stiffness of the frame beam and the frame column with the initial flexural stiffness, and ending after the deviation is less than or equal to 15%; 6, calculating a shear force design value of the frame beam, calculating stirrups needing to be configured for the frame beam, and rechecking a shear-resistant section; and 7, calculating a shear force design value of the frame column, calculating stirrups needing to be configured for the frame column, and rechecking a shear-resistant section. Compared with the prior art, an overall calculation model of the frame structure is established, the real rigidity of a structural member is obtained through multiple iterations, section reinforcement is optimized, and the reinforcement amount is reduced; and the overall anti-seismic performance is improved.

The invention discloses a damage quantitative evaluation method based on an intelligent agent model and knocking scanning, and aims to realize accurate recognition and quantitative evaluation of beam structure damage through the agent model. The evaluation method comprises the following steps: firstly, according to a theoretical relational expression of a beam structure, selecting a cross-sectional inertia moment, a structure length, a damage position and a detection vehicle equivalent acceleration as input random variables, and taking a bending stiffness ratio of a damage position as a damage quantitative index, constructing and optimizing an agent model; establishing a nonlinear mapping relation between input and output; secondly, applying excitation by utilizing an intelligent knocking scanning detection vehicle, acquiring an acceleration signal, processing the signal by adopting a time-frequency analysis technology, and extracting feature information related to structural damage; and finally, predicting a damage quantitative index according to the agent model in combination with the identified damage position and feature data, and verifying and outputting a result.

The invention provides a calculation method and system for a herringbone micro anti-slide pile structure, the herringbone micro anti-slide pile structure is dispersed, and the interaction between a micro pile and a stratum is simplified into transverse and axial non-linear springs acting on nodes; determining nonlinear spring parameters; calculating the soil displacement and direction of each micro pile structure according to the landslide mass motion characteristics; establishing a structural overall stiffness matrix; establishing an overall increment balance equation set including the spring stiffness; the landslide mass displacement is divided into a plurality of displacement increments to be solved respectively, the spring stiffness and the pile bending stiffness are updated after each increment step, and the internal force and deformation of the herringbone micro pile structure under the corresponding landslide mass displacement effect are obtained through accumulation. According to the calculation method and system for the herringbone miniature anti-slide pile structure, material and geometric nonlinearity of the pile and interaction nonlinearity of the pile and the stratum can be considered at the same time, and calculation precision and efficiency are high.

The utility model belongs to the technical field of steel structures, and particularly relates to I-shaped steel for a bridge, which comprises an I-shaped steel body, a plurality of holes are uniformly distributed on a web of the I-shaped steel body, and foamed aluminum is filled in each hole. A plurality of reinforcing ribs are further arranged on a web of the I-shaped steel body, the reinforcing ribs and the holes are distributed in a staggered mode, every two adjacent I-shaped steel bodies are connected through a connecting mechanism, the holes are of a hexagonal structure and evenly divided into a plurality of groups, and the multiple groups of holes are evenly distributed in the length direction of the I-shaped steel body. The plurality of groups of holes and the plurality of reinforcing ribs are alternately distributed; according to the utility model, the plurality of holes are formed in the I-shaped steel body, and the foamed aluminum is filled in each hole to form a'metal framework + core material 'composite structure, so that compared with a solid web, the weight is reduced by 25%-30%, and the flexural rigidity is improved at the same time; the adjacent I-shaped steel is connected through the connecting mechanism, and detachable connection is achieved.

The present invention relates to an evaluation method for steel structure splicing nodes, comprising the following steps: (a) obtaining defect information of the steel structure splicing nodes after the steel structure splicing nodes are disassembled; (b) obtaining a correction factor of the rotational stiffness of the steel structure splicing nodes based on the defect information; (c) obtaining the theoretical shear stiffness and theoretical bending stiffness of the steel structure splicing nodes; (d) obtaining the actual rotational stiffness of the steel structure splicing nodes based on the correction factor, the theoretical shear stiffness and the theoretical bending stiffness; (e) obtaining the actual geometric shape of the steel structure splicing nodes after all steel structure splicing nodes are installed; (f) obtaining the actual bearing capacity of the steel structure splicing nodes based on the actual geometric shape and the actual rotational stiffness; (g) obtaining the design bearing capacity of the steel structure splicing nodes; and (h) evaluating the reusability of the steel structure splicing nodes based on the actual bearing capacity and the design bearing capacity of the steel structure splicing nodes.

The utility model provides a kind of electronic thoracoscope with universal bending insertion part, including operating part and insertion part extending along length direction, the insertion part includes front end portion, active bending section, passive bending section and rigid pipe section from distal end to proximal end in order, the front end portion is equipped with optical imaging module and illumination light source;Active bending section is set in the proximal end of the front end portion, by multiple jointed snake bone unit, actively bends in response to operating part control;Passive bending section is connected to the proximal end of active bending section, the passive bending section has universal bending characteristic and the bending stiffness of the passive bending section is less than active bending section;Rigid pipe section is connected to the proximal end of passive bending section.The utility model expands the observation range of thoracoscope by passive bending section, reduces observation blind area, avoids the direct confrontation of active bending section and the rigid structure of guide sleeve inlet, prolongs the service life of equipment, reduces the loss risk of equipment.

The present application relates to a kind of pre-tensioned steel wire rope lateral impact response calculation method considering geometric and friction nonlinear coupling.First, the linear tensile constitutive model of pre-tensioned steel wire rope is constructed, Von Kármán large deflection theory is introduced, and the geometric hardening relationship of the nonlinear growth of axial tension with lateral deflection is established;Subsequently, a bilinear bending stiffness model is constructed to calculate the critical anti-sliding torque that evolves dynamically with tension;Based on the principle of energy conservation and Rayleigh-Ritz method, the system total potential energy functional of axial tensile potential energy and nonlinear bending potential energy is constructed, and the maximum impact deflection and tension response of the steel wire rope are obtained by solving the energy residual equation, the maximum response is substituted back into the constitutive equation, and the maximum nominal stress of the midspan cross section, the maximum axial tension and the extension length of the internal slip zone are calculated.The present application has very high calculation efficiency compared with full-size finite element simulation, and is suitable for the rapid design and safety evaluation of steel wire rope protection system.

A tail assembly for a rotorcraft having a fuselage. The tail assembly includes a stabilizer having an aft spar and a forward spar. An aft joint couples the aft spar to the fuselage and defines a pitch axis such that the aft joint allows the stabilizer to pivot about the pitch axis. A forward joint couples the forward spar to the fuselage. The forward joint has an axial stiffness configured to tailor a chordwise pivot mode of the stabilizer and a bending stiffness configured to tailor a beamwise bending mode of the stabilizer. The chordwise pivot mode of the stabilizer is decoupled from the beamwise bending mode of the stabilizer.

This invention discloses a method, system, equipment, and storage medium for calculating the deformation of a pipe-jacking structure considering the soil resistance between the pipe and culvert. The method includes the following steps: S1. Simplifying the pipe-jacking structure as an elastic thin plate, and further simplifying the problem to the deformation of an elastic thin plate with fixed opposite sides and simply supported opposite sides under a uniformly distributed load on a Winkler elastic foundation, obtaining the differential equation of the bending surface of the thin plate on the Winkler elastic foundation and the expression for the boundary conditions of the thin plate; S2. Determining the elastic modulus when the pipe-jacking structure is simplified to an elastic thin plate, and calculating the bending stiffness D of the pipe-jacking structure; S3. Solving the differential equation of the bending surface of the thin plate on the Winkler elastic foundation using a hybrid solution method combining trigonometric series and the force method, obtaining the deflection formula of the elastic thin plate placed on the elastic foundation under a uniformly distributed load. This invention can accurately predict the deformation of pipe-jacking structures.

The invention relates to the field of buildings, in particular to a reinforced concrete member manufacturing method and a post-cracking bending rigidity calculation method.The reinforced concrete member manufacturing method comprises the following steps that S1, a steel reinforcement framework is fixed to the set position of a concrete pouring mold, and a reinforced area of a concrete body is determined; s2, determining structural parameters of the reinforcing grooves and the reinforcing ribs; s3, the foam board is cut to enable the shape of the foam board to correspond to the shape of the reinforcing groove, and the foam board is fixed to the position, corresponding to the reinforcing area, in the concrete pouring mold; s4, concrete is poured into the concrete pouring mold, a concrete main body is formed after the concrete is cured and solidified, and after the concrete main body is demolded, the internal foam plate is emptied to form a reinforcing groove; and S5, reinforcing ribs are inserted into the reinforcing grooves, the reinforcing grooves are filled with UHPC, and machining of the concrete member is completed after maintenance. The bearing capacity and durability of the reinforcing system are improved, meanwhile, the glass fiber reinforced resin composite material in the retired wind power blade is applied to the reinforcing system, and the reinforcing cost is reduced.

The present disclosure provides a Timoshenko beam model equivalent method and system of a corrugated steel plate support structure, and relates to the technical field of stress analysis of a corrugated steel plate support structure, comprising: solving the stiffness coefficients of the corrugated steel plate in a local coordinate system, including tensile stiffness, bending stiffness and shear stiffness; solving the equivalent stiffness coefficients of the orthotropic corrugated steel plate in a global coordinate system, including equivalent tensile stiffness, equivalent bending stiffness and equivalent shear stiffness; solving the equivalent section bending stiffness of the corrugated steel support structure; solving the equivalent section shear stiffness of the corrugated steel support structure; and equivalent the corrugated steel support structure to a Timoshenko beam model. The present disclosure can realize the rapid equivalent of the corrugated steel plate support structure to a Timoshenko beam model.

The application provides a short cable force and stiffness meta-heuristic intelligent identification method considering bending stiffness, and belongs to the field of bridge structure health monitoring and parameter identification. First, based on the measured vibration frequency of the cable structure, the initial value range of the cable force and the bending stiffness is determined by using a simplified analytical model; then a parameter space is constructed within the range, and candidate parameter combinations are generated by random sampling or distribution sampling; the corresponding theoretical frequency is calculated based on the W-W algorithm; the data items of the loss function between the measured frequency and the theoretical frequency are constructed, and the physical loss items of the loss function are constructed by using the vibration differential equation; the parameter inversion is carried out by combining global search and local optimization, and the adaptive interval contraction strategy is introduced to improve the calculation efficiency and the identification accuracy; finally, the optimal cable force and bending stiffness parameters are obtained. The method does not need to rely on the initial accurate parameters, has high robustness and engineering applicability, and can significantly improve the identification accuracy of the cable force and the stiffness.

Method for determining a static bending stiffness (C B,stat ) of an object (1) which is vibrationally decoupled from an environment and arranged on at least two support means (2, 3), from dynamic acceleration measurements after vibration excitation of the object (1), comprising the steps a) Establishing a plurality of force application points (4) on the object (1), b) Arranging a number of accelerometer means (5) on the object (1), c) Exciting the object (1) at the force application points (4) determined in step a) using vibration generating means and determining a number of frequency response functions from the accelerations measured using the acceleration sensor means (5), d) Calculating an acceleration vector of the object (1) from the frequency response functions obtained in step c), e) Calculating a displacement vector from the acceleration vector determined in step d), f) Calculating a number of dynamic bending stiffness curves from the forces acting at the force application points (4) and the deflections of the object (1) induced by the displacements with the displacement vector, g) Extrapolating at least one of the dynamic bending stiffness curves obtained in step f) to a frequency f=0 Hz to obtain the static bending stiffness (C B,stat ) of the object (1).

This invention discloses an XIE beam, comprising a box girder body, which is formed by an upper panel (1), a left web (2), a lower panel (3), and a right web (4). Inside the box girder body are scissor bracing plates (6) and horizontal steel plates (5). The two ends of the horizontal steel plates (5) are connected to the longitudinal midpoints of the left web (2) and the right web (4), respectively. The midpoint of the scissor bracing plates (6) is located at the transverse midpoint of the horizontal steel plates (5). The upper ends of the scissor bracing plates (6) are connected to the longitudinal 1 / 4 points of the left web (2) and the right web (4), respectively, and the lower ends of the scissor bracing plates (6) are connected to the longitudinal 3 / 4 points of the left web (2) and the right web (4), respectively. Compared to traditional box-section beams of the same area, the XIE beam significantly increases the bending stiffness EI without causing web instability.

The invention discloses a similar design method for an underwater vibration table test model of a reinforced concrete rectangular pier. The method comprises the steps of determining geometric similarity constants; determining an elastic modulus similarity constant, a longitudinal bar strength similarity constant, a stirrup strength similarity constant and a water density similarity constant of the reduced-scale pier; determining an acceleration similarity constant of the reduced-scale pier; determining a structural density similarity constant; determining a flexural rigidity similarity constant of the rectangular section of the reinforced concrete pier; determining the wall thickness of the reduced-scale pier with the hollow structure; determining the weight of the bridge pier in unit height and converting the weight into a mass block of an iron block or a lead block with the same weight; determining a longitudinal bar area similarity constant and a stirrup area similarity constant of the reduced-scale pier; and correcting the stirrup area similarity constant and the like. The method provided by the invention can provide a feasible method for similar design of the reinforced concrete rectangular pier model in an underwater vibration table test.

The invention relates to a chopped fiber reinforcement-based modularized paddle main beam structure and a manufacturing method, and relates to the technical field of aircraft parts, the chopped fiber reinforcement-based modularized paddle main beam structure comprises a main beam body used for supporting a paddle, the main beam body is composed of a plurality of module units, the module units are made of chopped fiber reinforced composite materials, and the interior of each module unit is of a hollow structure; the gradient supporting pieces are arranged in the module units, each gradient supporting piece comprises a vertical strip and a transverse supporting strip, the vertical strips and the transverse supporting strips are arranged in a density stepped change mode, and the density of the ends, close to the connecting ends, of the vertical strips and the transverse supporting strips is large; according to the gradient supporting piece, the density stepped change design is adopted, high-fiber-content metal powder or metal powder mixed with the high-fiber-content metal powder is adopted close to the connecting end, and the rigidity, the abrasion resistance and the bolt pre-tightening force resisting capacity are improved; and the middle part adopts a low-density core material for weight reduction, so that the bending rigidity is kept while the overall weight is reduced, and the balance of light weight and high strength is realized.

The invention relates to the technical field of switch rails, in particular to a production method of an elastic bendable switch rail for a compound dividing turnout, which comprises the following steps: determining the steel rail model of the switch rail according to the model of a stock rail; determining the machining range of the switch rail according to the steel rail model; precise cutting is conducted on the determined machining range through slicing machining, the horizontal inertia moment and the flexural rigidity of the switch rail are weakened, and an elastic bendable section is formed; the cut switch rail is subjected to precision verification; forging and pressing the point rail subjected to precision verification, and processing the section of the point rail into a common steel rail section consistent with that of the stock rail; the forged and pressed switch rail is cooled, straightened and detected, the switch rail produced through the method is stable and simple in structure, the problems that bolts are broken off, rail seams are eroded and the like are reduced, the reliability of the switch rail is improved, the service life of the switch rail is prolonged, and maintenance convenience of the switch rail is improved.

The embodiment of the invention provides an ANSYS-based spherical wood reticulated shell shape finding analysis method, which comprises the following steps that: an association table of a reticulated shell structure model and parameter elements is constructed, the association table comprises a reticulated shell structure model identifier and a parameter element identifier corresponding to the reticulated shell structure identifier, the reticulated shell structure model comprises a crossed truss system model, and the parameter element identifier corresponds to the crossed truss system model; the parameter elements comprise structural physical parameters, a material constitutive model, node flexural rigidity, initial defects, structural nonlinearity and node semi-rigidity; obtaining parameter elements, and determining a reticulated shell structure model through the association table according to the parameter elements; and constraint conditions and loads are determined, iterative stress analysis is conducted on the latticed shell model, an optimized structure model is obtained, the constraint conditions include that the node rigidity of the latticed shell support should be larger than the node rigidity between components, the variable parameters include vertical loads, and the vertical loads include the self weight, the snow load and the wind load. And the shape finding efficiency and accuracy are improved.

This application discloses a BIM-based automatic optimization method and system for substation cable laying paths. The method includes: acquiring a building information model; extracting equipment spatial information, equipment operation information, building structural spatial information, and target cable information; constructing the equipment thermal radiation potential energy field and power frequency magnetic leakage potential energy field; determining the cable type and, based on the cable type, determining the magnetic field repulsion response coefficient, thermal radiation repulsion response coefficient, and bending stiffness coefficient; constructing a virtual cable model; constructing an energy coupling function based on the equipment thermal radiation potential energy field, power frequency magnetic leakage potential energy field, magnetic field repulsion response coefficient, thermal radiation repulsion response coefficient, and bending stiffness coefficient; determining the optimal laying path using the energy coupling function; generating a cable spatial constraint potential energy distribution based on the optimal laying path; and determining all optimal laying paths based on the cable spatial constraint potential energy distribution. This application can effectively improve the accuracy of substation cable laying path optimization.

Closure arrangement (10) for covering and closing openings in buildings, roofs, walls, in particular for weather protection, for pergolas, for canopies, for doors, gates and the like, comprising at least one profile arrangement (5, 5'), wherein the profile arrangement (5, 5') has at least one hollow chamber (50, 51) and at least one connecting element (3) and / or at least one connecting device (4), wherein the profile arrangement (5, 5') has at least one structural layer (6), wherein the at least one structural layer (6) has at least a portion of a polymeric material, wherein the profile arrangement (5, 5') has at least one reinforcing insert (7), preferably fully embedded in the structural layer (6), characterized in that the profile arrangement (5, 5') has a bending stiffness about the x-axis of approximately 17 to 29 × 10 9 N / mm 2 , preferably about 18 to 22 × 10 9 N / mm 2according to DIN EN ISO 178-2019-08, the profile arrangement (5,5') has a linear coefficient of thermal expansion α of approximately 12 to 64 × 10 -6 / K, preferably 16 to 30 × according to DIN EN ISO 11359-2:2021-11, having the material of the at least one structural layer (6) comprising microhollow spheres consisting of a plastic shell filled with a gas.

The present application belongs to the technical field of industrial detection, and particularly relates to a forging round steel straightness online detection method based on point cloud data, which comprises the following steps: firstly, obtaining original point cloud and multi-dimensional physical characteristic data of the round steel in a transmission state; then, slicing the point cloud, and combining local geometric missing features and thermal deformation driving features to calculate a compensation step, and correcting a primary centroid to obtain a real three-dimensional physical axis; subsequently, projecting the axis to an orthogonal plane, and using a restriction relationship between local curvature and material bending stiffness to obtain a pseudo-boundary penalty factor, and then correcting an envelope angle and calculating a comprehensive straightness error. The present application eliminates the interference of point cloud missing, thermal eccentricity and surface microscopic defects, and improves the accuracy of the forging round steel straightness detection.

The application provides a new type of structure of a main tower in a multi-tower suspension bridge and a construction method thereof, which comprises a main tower, a plurality of oblique suspension cables, a first stiffening beam and a plurality of main cable saddles; the plurality of main cable saddles are vertically fixed on the top of the main tower in parallel and at intervals along the transverse direction of the main tower; the plurality of oblique suspension cables are respectively arranged on the two sides of the main tower in an inclined manner, the upper end of each oblique suspension cable is anchored in the lower bearing plate of the top of the main tower, and the lower end is connected to the corresponding first stiffening beam; and the first stiffening beam is arranged on the two sides of the main tower. The structure and the method utilize the components of the structure to improve the longitudinal bending stiffness of the main tower, do not affect the overall appearance of the whole bridge, are convenient for construction and do not increase the process.

The invention relates to a bending test method for an asphalt mixture composite board. The bending test method comprises the following steps: preparing an asphalt mixture composite board test piece; carrying out heat preservation on the asphalt mixture composite board test piece; placing the asphalt mixture composite board test piece subjected to heat preservation on a clamp, vertically and downwards loading the asphalt mixture composite board test piece at a constant speed, and collecting pressure load and midspan displacement when the test piece is damaged; and calculating the flexural tensile strength, the maximum flexural tensile strain and the bending stiffness modulus. The invention provides a special low-temperature crack resistance test method for a multi-layer asphalt mixture structure.

The application belongs to the field of high-stability anti-deformation folding pallets, and particularly relates to a high-stability anti-deformation folding pallet, which comprises a middle plate, the outer side of the middle plate is hingedly connected with two symmetrically distributed pallet plates, the inner side top of each pallet plate is fixedly installed with a fixing cover, and the inside of the fixing cover is slidably connected with a moving strip. Through the sliding insertion cooperation of the supporting pipe and the locking rod, a multi-point continuous supporting structure is established between the pallet plate and the middle plate, the traditional hinge force transmission mode is changed, the load is directly transmitted, the bending stiffness is significantly improved, the bearing deflection deformation is effectively inhibited, the radial constraint of the supporting pipe by the multiple linearly distributed locking rods and the reinforcing guide plate is cooperated to make the connection part have excellent bending moment capacity, and no cumulative deformation is generated under long-term heavy load or frequent folding, the problems of easy hinge loosening and permanent deformation are fundamentally solved, and the service life of the pallet is greatly prolonged.

This application provides a method, apparatus, storage medium, and electronic device for determining the parameters of an elastic flywheel. The method includes: constructing an optimization model and solving the optimization model based on optimization variables, constraints, and an optimization objective to obtain calculation results. The optimization variables are the number of intermediate diaphragms, the thickness of a single intermediate diaphragm, and the positional relationship between any two intermediate diaphragms. The constraints are the total diaphragm thickness and the minimum strength range of the diaphragms. The optimization objective is to minimize the bending stiffness of the intermediate diaphragms. The target solution of the calculation results includes the target number of intermediate diaphragms, the target thickness of each intermediate diaphragm, and the target positional relationship between any two intermediate diaphragms. This method, while ensuring constant torsional stiffness, flexibly controls bending stiffness and strength by combining the number of diaphragms, diaphragm thickness, and diaphragm arrangement order, thus achieving both high reliability and shaft alignment compensation capability.

The invention discloses a longitudinal loading device and method for a shield tunnel longitudinal deformation test, and the method comprises the steps: driving a first support and a second support to drive a first axial loading part and a second axial loading part to move relatively through an axial load loading mechanism, so as to apply an axial load to a segment sample group at two axial ends; and meanwhile, the bending moment loading mechanism drives the first axial loading piece and the second axial loading piece to rotate so as to apply bending moment to the segment sample group at the two axial ends, so that the segment sample group can be subjected to an equivalent bending rigidity test under the action of the applied axial load and bending moment. In addition, a vertical load loading mechanism capable of applying a vertical load to the segment sample is also arranged, so that the segment sample group can be subjected to an equivalent shear stiffness test under the action of the applied axial load and vertical load. Therefore, the method has good universality, so that the test efficiency can be improved, and the cost can be remarkably reduced.