73 results about "Tensile fatigue" patented technology

The invention relates to the technical field of fatigue life testing, and particularly discloses a method for testing the fatigue life of a diaphragm of a diaphragm compressor, which comprises the following steps of: measuring the material tensile strength value of each diaphragm tensile sample piece through a tensile fatigue test, and simultaneously determining the fatigue life of the diaphragm of the diaphragm compressor by combining geometric parameters of each diaphragm tensile sample piece; the method comprises the following steps of: constructing association expressions between geometric parameters of a diaphragm tensile sample piece and tensile test results, and further performing global polymerization analysis on each group of constructed association expressions, so as to intelligently estimate the sigma b value of the diaphragm material of the diaphragm compressor. Therefore, the tensile property of the diaphragm material can be evaluated more accurately, so that a more reliable basis is provided for testing the fatigue life of the diaphragm.

A fatigue performance test device and method. When being used for testing the tensile fatigue performance of a rubber material, the test device comprises loading frames (1), a pressing mechanism, and gaskets (3), and when being used for testing the shear fatigue performance of the rubber material, the test device comprises loading frames (1) and a pressing mechanism. During testing, the loading frames (1) are fixed by means of positioning panels (6), and after samples (5) are mounted in place, the positioning panels (6) are removed, and a fatigue testing machine is used to load the two loading frames (1), so as to test the tensile fatigue performance or the shear fatigue performance. A plurality of samples (5) can be mounted at the same time for testing the fatigue performance, and mutual influence is avoided, so that the test efficiency is effectively improved, the test cost is reduced, and the test cycle is shortened.

The invention relates to an aviation titanium alloy laser shock peening and mechanical shot peening composite process strengthening method. The method comprises the following steps: cutting an aviation titanium alloy material into a plurality of square blocks and tensile fatigue parts by using a wire cutting machine; grinding with abrasive paper, and then polishing with a polishing agent, so that the surface of the aviation titanium alloy test material is smooth; carrying out laser shock peening treatment on one part of the aviation titanium alloy test material subjected to surface treatment; performing various detections on the aviation titanium alloy test material subjected to the same parameter and different impact strengthening times; the method comprises the following steps: carrying out mechanical shot blasting on an aviation titanium alloy sample with the best detection effect, carrying out mechanical shot blasting on part of original samples, then carrying out laser shock peening, and comparing the mechanical properties of the materials subjected to shock peening in different modes to obtain an optimal result. According to the method, two processes of mechanical shot peening and laser shock peening are combined, so that the fatigue resistance, the damage resistance and the stress corrosion resistance of the material are improved.

The invention provides a self-adaptive double-entropy-multi-scale Transform unsupervised cross-domain composite material damage prediction method, which comprises the following steps: preprocessing an acoustic emission signal and extracting a double-entropy feature matrix based on the acoustic emission signal acquired by a composite material test piece under a tensile-tensile fatigue load; constructing a data set based on the double-entropy feature matrix and training a damage evolution model; and inputting the double-entropy feature matrix corresponding to an acoustic emission signal into the trained damage evolution model based on the acoustic emission signal acquired by the composite material test piece under the shear fatigue load, so as to realize real-time prediction of the shear fatigue damage. According to the method, the cross-load high-reliability prediction is realized, the feature dimension redundancy is improved, the physical interpretability is improved, the supervision marking cost is reduced, and a brand new solution is provided for engineering application.

The invention discloses an air pressure-temperature-damage coupled flexible material air tightness test system and method.The test system comprises a tensile fatigue device, sample holders, a high-pressure permeation device, a fixing and supporting device and a lifting device, and the two ends of a sample are fixed through the sample holders; the method comprises the following steps: firstly, fixing a sample holder on a tensile fatigue device to carry out a cyclic tension test so as to obtain samples with different fatigue damage degrees; the circularly tensioned sample is transferred and fixed on the fixed supporting device through the lifting device, so that a central test area of the sample is positioned in a high-pressure sealing box permeation area formed by an upper box assembly and a lower box assembly in the high-pressure permeation device, and air tightness detection is performed at different temperatures and different air pressures; therefore, the gas permeability and the gas permeability coefficient of the sample are obtained, and comprehensive evaluation of the gas tightness and the fatigue resistance of the flexible material is realized.

The invention relates to the technical field of pavement material mechanical property testing, and discloses a pavement material deformation adaptability fatigue testing machine, which comprises a servo drive and control system, a mechanical transmission system and a structure support and reference system, the servo drive and control system comprises a servo motor, a PLC, a servo driver and an analog quantity output module, the PLC is electrically connected with the analog quantity output module, the analog quantity output module is electrically connected with the servo driver, and the servo driver is electrically connected with the servo motor. The load coverage range is wide, the test requirements of pavement material test pieces with different strengths are met, the requirements of various mechanical property tests on loads are met, the loading modes are flexible and diversified, single loading such as horizontal stretching, stretching containing vertical deformation and fatigue stretching circulation can be achieved, and the test efficiency is improved. The device can be combined with MMLS3 small acceleration loading equipment to realize composite loading of tire cyclic load and test piece deformation, and composite working conditions of the seamless expansion joint in actual service are accurately simulated.

The invention provides an all-electric measurement and control instrumented tensile impact fatigue experiment system, and mainly solves the problems that stress wave pulses are transmitted back and forth in a rod, and a cyclic loading test and an automatic test cannot be repeated. According to the invention, the Hopkinson pull rod system, the stress wave riveting gun module, the lead screw dragging device and the comprehensive detection and control device are utilized to realize single-time repeated impact loading of a test piece, control the launching and recovery of a projectile body, realize closed-loop control of loading force, and improve the reliability of the test piece. According to the invention, a single loading impact fatigue function of continuous tensile impact on a sample is realized through the energy absorption and limiting device and the screw rod dragging device, and instrumentation and full automation of an impact tensile fatigue experiment are realized.

The invention relates to the technical field of rubber hose detection, and particularly discloses an anti-drawing fatigue detection device and method based on rubber hose production, and the device comprises installation mechanisms which are arranged at the inner side of a frame body and are symmetrically distributed with respect to the central point of the frame body, and are used for fixing a rubber hose from the end part. According to the invention, the symmetrically arranged mounting mechanisms are arranged in the frame body, so that the two ends of the rubber hose are synchronously stretched, the internal stress distribution of the rubber hose is more uniform, and the overall tensile property of a material can be reflected more truly; and the fluid circularly flows in the rubber hose through the flow guide mechanism, so that the actual conditions such as high-temperature fluid or low-temperature fluid conveyed in the rubber hose are simulated, the anti-drawing fatigue performance of the rubber hose is detected, and the detection accuracy and authenticity are improved according to the actual application scene.

The application discloses a kind of air pressure-temperature-damage coupling's flexible material air tightness test system and method, test system includes tensile fatigue device, sample holder, high-pressure permeation device, fixed support device and holder, the two ends of sample are fixed by sample holder, first fixed in tensile fatigue device to carry out cyclic tension test with sample holder, to obtain the sample with different fatigue damage degree;Through holder, the sample after cyclic tension is transferred and fixed on fixed support device, so that the center test area of sample is located in the high-pressure sealed box permeation region formed by upper box assembly and lower box assembly in high-pressure permeation device, so as to carry out air tightness detection under different temperature and different air pressure, to obtain the gas permeation rate and gas permeation coefficient of sample, realize the overall evaluation of flexible material air tightness and fatigue resistance.

The utility model discloses a fatigue test fixture and equipment, including a first clamp assembly and a second clamp assembly, the first clamp assembly moves along a first direction, the first clamp assembly includes a first clamp seat and a first sample fixing table, the first sample fixing table is installed on the first clamp seat through a first rotating shaft, and the second clamp assembly is installed on the second clamp seat through a second rotating shaft. The second clamp assembly comprises a second clamp seat, the second clamp seat is mounted on the base, a force sensor is arranged between the second clamp seat and the base, and the second clamp seat is provided with a second sample fixing table and a third sample fixing table; the first sample fixing table and the second sample fixing table can limit a test sample between the first clamp assembly and the second clamp assembly in the first direction, and the first sample fixing table and the third sample fixing table can limit the test sample between the first clamp assembly and the second clamp assembly in the second direction. According to the utility model, the test sample can be tested in two fatigue test modes, namely single tensile fatigue and plane bending fatigue.

The invention discloses a method for improving the tensile fatigue performance of a thin-wall Ti6Al4V titanium alloy, and belongs to the technical field of metal material processing, and the method comprises the following steps: S1, determining femtosecond laser shock peening parameters based on material performance parameters; s2, setting a laser processing path through a laser processing system control end; according to the method, the ultrahigh pressure shock waves generated by the femtosecond laser shock peening technology initiate strong plastic deformation on the surface layer of the material, the plastic deformation forms a dislocation structure with higher density by inducing dislocation motion and proliferation, the strength and hardness of the material are further improved, in addition, the plastic deformation can cause the surface layer of the material to generate compressive residual stress, and the mechanical property of the material is improved. According to the invention, due to the existence of the residual stress, the external tensile stress is effectively resisted, the damage accumulation of the material in high-cycle fatigue is delayed, and the proliferation and slippage of dislocation are delayed, so that the fatigue resistance of the material is further improved.

The utility model belongs to the technical field of tensile fatigue testing, and particularly relates to tensile fatigue testing equipment which comprises a frame body, a testing table, a first tensile seat, a second tensile seat and a driving assembly, the testing table is connected with the frame body, the first tensile seat and the second tensile seat are both connected with the testing table, and the driving assembly is connected with the first tensile seat and the second tensile seat. The first stretching seat is provided with a first locking structure, the first locking structure is used for locking one end of a headband on the first stretching seat, the second stretching seat is provided with a second locking structure, the second locking structure is used for locking the other end of the headband on the second stretching seat, and the driving assembly is connected with the test board. The driving assembly can drive the first stretching base to move in the direction close to or away from the second stretching base. The driving assembly can accurately adjust the distance between the first stretching seat and the second stretching seat according to design requirements, the stretching distance of each time can be accurately controlled, and the accuracy of the measured stretching frequency limit is improved.

The utility model relates to a wire tensile fatigue strength detection device, which comprises a mounting platform, a fastening end, a moving end, a tension output part and an operation and display panel, the fastening end and the moving end are each provided with an annular clamping structure, and the operation and display panel is electrically connected with the fastening end, the moving end and the tension output part. According to the device provided by the utility model, the wire rod is clamped by the clamping structure through operation on the operation and display panel, and then the tension output part pulls the movable end to move along the axis direction of the wire rod, so that a tensile test is carried out on the wire rod, and the tension output part transmits a tension output value of the tension output part to the operation and display panel for display; the clamping structure is simple in structure and convenient for experimenters to observe numerical value changes and record test data, the clamping structure in the embodiment can adapt to wire rods with different diameters, meanwhile, after the wire rods are clamped, the wire rods are not prone to falling off in the test process, the test can be conducted for a long time, more accurate test results can be obtained, and the test efficiency is improved. And the door of the mounting platform can protect the safety of experimenters.

The present invention relates to the technical field of testing equipment, and in particular to an anti-fatigue detection device for a suspension structure of an automobile chassis, comprising two discs and a group of power units, wherein one disc is fixed in position, and the other disc is driven to move by the power unit, and each disc is provided with a support plate, and the two support plates are located between the two discs, and each support plate is provided with a plug post, and the two plug posts are used to pass through two round holes on a rubber ear, so as to fix the rubber ear; the device can not only simulate the torsional fatigue of the rubber ear under a dynamic load, but also perform elastic reciprocating tensile fatigue test, thereby realizing multiple test tasks on the rubber ear, thereby obtaining more accurate test results, and by causing the rubber ear to reciprocate in torsion and stretching, the device can better simulate the complex working conditions of the automobile during actual use, thereby improving the practical significance of the test.

The invention belongs to the technical field of metallurgy, and particularly relates to a 420 MPa-grade wind power steel welded joint with the fatigue grade of DC112 and a preparation method. According to the 420 MPa grade wind power steel welded joint, under the tension-tension fatigue test condition that the stress ratio R is equal to 0.5, after 2 * 106 times of cyclic loading, the fatigue strength of the 420 MPa grade wind power steel welded joint reaches 112 MPa, and the strict requirement for the DC112 grade fatigue grade in the international standard DNV-ST-0126 is completely met. The performance index is obviously superior to the prior art level, and key technical support is provided for high-reliability design and light-weight manufacturing of a wind power tower tube structure.

The invention discloses a high-temperature fatigue test system and a high-temperature fatigue test method for a composite casing mounting seat, and belongs to the technical field of fatigue test of casing mounting seats. The system comprises a biaxial fatigue test device, a test piece, a heating device, a data acquisition assembly and a controller, the test piece is installed on the biaxial fatigue test device, and the heating device and the data acquisition assembly are both connected with the test piece. The controller is electrically connected with the biaxial fatigue test device, the heating device and the data acquisition assembly. The heating device is used for heating the test piece to simulate the high-temperature working condition of the test piece, the biaxial fatigue test device is used for performing biaxial loading on the test piece, and the data acquisition component is used for acquiring strain data of the test piece in the test process, so that the biaxial tensile fatigue test on the composite casing mounting seat is realized. Therefore, the high-temperature fatigue performance of the composite material outer culvert casing mounting seat under the dual effects of the internal pressure and the axial force can be verified.

The invention belongs to the field of fatigue strength testing of metal materials, and particularly relates to a clamping device suitable for tension-tension fatigue performance testing of a linear material and a testing method. A fatigue machine connecting piece is fixed to a fatigue machine, and the load is reset; the long-rod bolt, the springs and the sample upper clamp are assembled, so that the resultant force of the pre-pressure of the two springs is the amplitude of the fatigue load, and the pre-pressure of the springs is reserved; fixing two ends of the linear material by using a winding clamp, and loading to an average value of a fatigue load; mounting the assembled long-rod bolt, spring and sample upper clamp on the sample, and connecting with a fatigue machine connecting sheet; loading to the maximum value of the fatigue load; a sample lower clamp is hung on the sample; the distance between the linear material and the fatigue machine stand column is measured, a tensioner and a U-shaped bolt baffle assembly are installed, and it is ensured that the distance between the linear material and the fatigue machine stand column is not changed; and unloading until the wire rod is bent, clearing the load, and then starting a fatigue test. According to the invention, effective tension-tension fatigue test can be carried out on the linear material, and accurate wire fatigue performance data can be obtained.

To predict a fatigue life of a thermoplastic resin capable of improving prediction accuracy in a range where a stress ratio R is 0 to 1.SOLUTION: A fatigue life prediction method comprising a step of creating a fatigue life prediction diagram of a thermoplastic resin having a stress ratio R of 0 to 1 based on the following formula (1). Where σ a is a stress amplitude, σ m is a mean stress, σ B is a value based on a rupture strength calculated from a result of a tensile test with a stress ratio R of 1, an index x is a value of more than 0 and less than 1.0, and σ w is an intercept obtained by substituting, into the above formula (1), a stress amplitude and a mean stress calculated from a result of a pulsating tensile fatigue test with a stress ratio R of 0 as σ a and σ m, respectively, a value based on the rupture strength as σ B, and a value of more than 0 and less than 1.0 as x. ) SELECTED DRAWING: Figure 2

The invention discloses a high-strength and high-conductivity copper alloy wire which comprises the following components in percentage by mass: 0.10-1.0% of Sn and the balance of Cu and inevitable impurities, in the microstructure of the cross section of the copper alloy wire, 1t; 100 gt; , lt; 110gt, 110gt; and lt; 111gt, 111gt; the area percentage S100, the area percentage S110 and the area percentage S111 of the silk texture meet the condition that S100 / (S110 + S111) is larger than or equal to 0.8; the preparation process comprises the steps of casting, hot working, rough cold working, intermediate heat treatment and fine cold working. By controlling the texture structure condition of the Cu-Sn alloy wire, the tensile strength can be 400 MPa or above, and the electric conductivity can be 65% IACS or above; a load of stress of 1% strain is circularly applied to the wire and unloaded until the wire is broken, and the number of cycles is more than 10000; the wire has high strength, high conductivity and excellent tensile fatigue performance, and can be applied to the fields of automobile wire harnesses, medical wire harnesses, industrial robots, consumer electronics and the like.

The present invention relates to a wedge-shaped clamp suitable for axial tensile fatigue test, which can realize the application of tensile fatigue load to a flat test piece whose side of the clamping section is a wedge surface. The clamping section of the test piece is placed in the groove of the wedge block, and the side of the clamping section is connected to the inner wedge surface of the wedge block; the outer wedge surface of the wedge block is connected to the wedge surface of the wedge groove in the groove block, and presses the vertical surface on the other side of the wedge groove when subjected to tensile load; the protruding part at the bottom of the wedge block cooperates with the longitudinal notch of the groove block; the groove block is connected to the fatigue testing machine clamp through a threaded hole. The present invention can realize the clamping of a flat test piece under tensile fatigue load, and has the following advantages: less processing requirements for the clamping section of the flat test piece; the clamp has no indentation on the test piece to avoid affecting the test results; the test piece is guaranteed not to bend in the width direction during the clamping process; the test piece is clamped by the tensile load of the fatigue testing machine, and no bolts or the like are required for clamping, and the structure is compact; it is easy to disassemble and assemble; and it has good interchangeability.

The utility model relates to a kind of metal composite material high-frequency fatigue test device, including support frame, testing device, protective cover and fixing device, testing device is installed on the support frame, the testing device is used to further test the tensile fatigue strength of metal by constantly increasing the force of stretching;The protective cover is installed on the testing device outside;The fixing device is installed on the testing device, and the fixing device is used to fix the metal to be tested.By the closed transmission chain of motor-reducer-screw integrated in test support, cooperate with the symmetrical limiting rod in displacement groove and displacement block limiting hole, the loading axis and the sample center line always keep high-precision coaxial, avoid eccentric error;Motor support supports reducer independently, suppresses bending deformation and resonance, improves long-term stability;Fixing device realizes sample trace eccentricity compensation, quick plug-in clamping and double-groove limiting positioning with the laminated structure of fixed block-adjusting disc-clamping block-mounting block, and different size samples can be replaced by a person.

The invention discloses a wave-resistant structure for an oil tank in the field of wave resistance of oil tanks. The N supporting assemblies are distributed at intervals in the length direction of the oil tank and fixed in the oil tank; each wave-proof plate is arranged between every two adjacent supporting assemblies and can move up and down in the height direction of the supporting assemblies; the supporting assembly comprises a hollow stand column, a perforated plate is arranged in the stand column and divides the interior of the stand column into an upper cavity and a lower cavity, a plurality of liquid inlets corresponding to the lower cavity are formed in the periphery of the stand column, a floating piece capable of moving up and down along with the oil surface is arranged in the upper cavity, and the floating piece is connected with the wave-proof plate into a whole through a connecting piece. The periphery of the stand column is provided with a limiting groove corresponding to the upper cavity and allowing the connecting piece to penetrate through. Through the three core advantages of replacing material dependence with hydraulic damping, eliminating tensile fatigue through rigid linkage and preventing clamping stagnation through accurate guiding, the reliability problem caused by material aging, repeated stretching and motion instability in a comparison structure is solved.

The utility model relates to the technical field of mechanical clamps, and discloses a pin plate sample tension fatigue clamp for a full-temperature environment, which comprises a clamping rod, the outer wall of the clamping rod is slidably connected with a protective cover, the outer wall of the right end of the protective cover is rotatably connected with a connecting mechanism, the outer wall of the right end of the clamping rod is provided with a fixing mechanism, and the fixing mechanism is connected with the protective cover. The fixing mechanism comprises a cylindrical pin, a limiting assembly is arranged on the inner wall of the right end of the cylindrical pin, a cylindrical pin fixing seat is clamped to the outer wall of the right end of the cylindrical pin through the limiting assembly, a clamping groove A is formed in the outer wall of the cylindrical pin fixing seat, and a supporting mechanism is arranged on the outer wall of the inner wall of the right end of the clamping rod. And a pin plate sample is detachably mounted on the outer wall of the right end of the clamping rod. According to the utility model, the cylindrical pin and the cylindrical pin fixing seat as well as the cotter pin and the cotter pin fixing seat can be fixed through the limiting assembly, so that the pin plate sample is clamped and fixed more conveniently and quickly.

The invention discloses a stud tensile fatigue test fixture and an assembly method, and relates to the technical field of test fixtures, the stud tensile fatigue test fixture comprises a first fixture and a second fixture which are symmetrically arranged at the two ends of a test bolt, the second fixture and the first fixture each comprise a fixture body, and the bottom of each fixture body is penetrated by the test bolt; a centering assembly is arranged between the test bolt and the clamp body; a fixing assembly is arranged at the end, penetrating through the clamp body, of the testing bolt. By adopting the stud tensile fatigue test fixture and the assembly method, automatic centering of the test bolt and the fixture can be realized, and the accuracy of a test result is improved.

The utility model discloses a clamp structure and a tensile fatigue testing device, and relates to the technical field of material performance tests.The clamp structure comprises a mounting seat, and a groove structure is arranged on the mounting seat; the two clamping pieces are symmetrically arranged in the groove structure; the driving structure comprises a first connecting piece and a second connecting piece, the first connecting piece is rotationally arranged on the mounting base, the second connecting piece is arranged in the groove structure, the second connecting piece can slide from one end of the groove structure to the other end of the groove structure, the second connecting piece is movably connected with the clamping piece, and the first connecting piece and the second connecting piece are connected through a first transmission structure; the first transmission structure is used for converting rotation of the first connecting piece into linear motion of the second connecting piece, and in the process that the two clamping pieces move along with the second connecting piece, the groove structure can make the two clamping pieces close to each other oppositely. The whole clamp structure is humanized in design and convenient to operate, the two clamping pieces can be close to each other in the opposite direction only by rotating the first connecting piece, and the to-be-tested piece is rapidly clamped and fixed.

The application discloses a high-temperature tensile-tensile fatigue test system and method, and designs a clamping device which can adapt to thickness change of a sample and ensure accurate centering of the sample based on a cold clamping mode; a movable thermocouple device is also designed, the thermocouple contacts the sample in the heating and heat preservation stage, and the thermocouple is slid to a position 3-6 mm away from the surface of the sample when the fatigue loading is formally started; and a silica aerogel composite material is selected to make a heat insulation felt which is arranged at the upper opening of a high-temperature furnace to block the hot air flow continuously rising from the high-temperature furnace, eliminate the risk of overheating of the chuck and the sensor system above the testing machine in a long-time fatigue test, and improve the stability and uniformity of the temperature field of the high-temperature furnace. The application makes technical innovations from three aspects of the clamping device, temperature measurement and control and heat insulation of the high-temperature furnace, effectively solves the technical problems of the high-temperature tensile-tensile fatigue test, and improves the technical level of the high-temperature tensile-tensile fatigue test of SiC-based composite materials.

The invention relates to the field of material testing, and discloses a notch cantilever beam-based small sample bending fatigue testing method, which is characterized by comprising the following steps: S1, applying a low-frequency bending symmetric cyclic loading test to the tail end of a beam to obtain a tail end load-displacement curve; s2, establishing a corresponding relation between load-displacement and the true strain amplitude epsilon m and stress amplitude sigma m of the fatigue source RVE through an energy method; s3, a fatigue life estimation model is established according to epsilon m and sigma m, and the fatigue performance of the material is obtained. The Manson-Coffin fatigue life prediction is completed by establishing the relation between epsilon eq (average strain amplitude)-epsilon m (real stress amplitude) and epsilon eq (average strain amplitude)-sigma m (stress amplitude), the traditional experience method that the bending fatigue performance is equivalently replaced by tensile fatigue is overcome, and the test method for detecting the bending fatigue performance of the material is further provided.

The invention relates to the field of material science and fracture mechanics, in particular to a technical method for characterizing a fracture microstructure. Specifically, the invention provides a characterization method for directly obtaining fracture cleavage plane orientation by using an EBSD technology, and the characterization method can be used for orientation analysis of a smooth cleavage plane or a quasi-cleavage plane on a fracture of a tensile, fatigue or impact sample. According to the method, direct characterization of a cleavage plane is realized through combination of an EBSD (electron back scattering diffraction) technology and a fracture three-dimensional orientation characterization method, so that the characterization precision of microscopic features of the fracture plane is improved, the characterization cost is greatly reduced, and visual characterization of space orientation information of the facet is realized by utilizing crystallographic calculation.

The application provides a full-electric instrumented tensile impact fatigue test system, and mainly solves the problems of stress wave pulse transmission in a rod back and forth, non-repeated cyclic loading test and automatic test. The application uses a Hopkinson rod system, a stress wave riveting gun module, a screw drive and a comprehensive detection and controller to realize single repeated impact loading of a test piece, control of the emission and recovery of a projectile body, and closed-loop control of loading force. The application realizes the single loading impact fatigue function of the test piece by energy absorption and a stopper and a screw drive, and realizes instrumented and full-automatic impact tensile fatigue test.

The invention discloses a high-tensile fatigue-resistant adhesive tape material and a preparation method thereof. The core of the high-tensile fatigue-resistant adhesive tape material is to construct a dynamic ionic bond and bio-based coordination bond dual-crosslinking adhesive layer system. The adhesive layer is prepared by taking modified polylactic acid-cellulose nanocrystals as a bio-based matrix, matching with an ionic liquid modifier, introducing modified tea polyphenol and zinc acetate to form a bio-based coordination bond according to a molar ratio of 1: 3-1: 5 through solvent-free melt blending. The bio-based content of the adhesive tape is 50%-70%, the tensile strength is 15-18 MPa, the self-repairing efficiency is 85%-95% at the room temperature for 10-15 min, the 50% strain cycle fatigue resistance frequency is 10000-15000, the problem that the strength and self-repairing of an existing bio-based adhesive cannot be achieved at the same time is solved, and the adhesive tape is suitable for medical and flexible electronic scenes.