CN204718898U - High-temp in-situ stretching-fatigue test system - Google Patents

Abstract

The utility model relates to a kind of high-temp in-situ stretching-fatigue test system, belongs to scientific instrument and Material Testing Technology field.Test macro comprises tensile loads and detecting unit, fatigue loading and detecting unit, in-situ observation unit, high temperature load and detecting unit etc.Wherein tensile loads and detecting unit provide power by motor, and being slowed down by worm and gear, ball-screw realizes semi-static load; Order about flexible hinge by piezoelectric ceramics and realize the medium and low frequency to-and-fro movement upwards of test specimen tensile axis, realize fatigue loading; By optical microscope, dynamic monitoring is carried out to test process, realize in-situ observation.This test principle is reliable, has important scientific meaning and good using value, can the mechanical property of material for test and the correlativity rule of microstructure and deformation damage mechanism under testing and analysis hot environment accurately.

Description

High temperature in situ tension-fatigue test system

technical field

The utility model relates to the technical field of scientific instruments and material testing, in particular to a high-temperature in-situ stretching-fatigue testing system. It is used to accurately detect the mechanical properties of the specimen in high temperature environment and the correlation law between its microstructure and deformation damage mechanism.

Background technique

The application of in-situ testing technology has played a role in promoting the development of materials science. In the process of material testing, the microscopic deformation and damage of materials under load are monitored dynamically through optical microscopes and other instruments, which can reveal various materials and their properties more deeply. The micro-mechanical behavior of its products, the damage mechanism and the correlation law between the material properties and the applied load.

It is well known that the mechanical properties of materials usually change with the compound action of the temperature field and stress field in which they are located. In particular, with the rapid development of high-tech industries such as aerospace and microelectronics, the industry has put forward new requirements for the performance of materials. Therefore, to explore the mechanical properties of materials under multi-field coupling conditions such as temperature field and mechanical field The mechanism of evolution is particularly important. The temperature-controllable tensile fatigue test can realize the precise test of the micro-mechanical properties of materials under different temperatures, different tensile loads, and different fatigue loads, and analyze the mechanical properties and denatured damage of materials under high temperature conditions and composite load modes. The mechanism has practical significance that cannot be ignored.

At present, the existing high-temperature tensile equipment cannot perform tensile-fatigue composite load tests in high-temperature environments, and cannot fully monitor the microscopic deformation and damage of materials under load. Therefore, the development of high-temperature in-situ tensile-fatigue The test system is of great significance to the study of the mechanical properties of materials under tensile-fatigue composite loads and the deformation and damage mechanisms of materials under different temperature fields.

Contents of the invention

The purpose of the utility model is to provide a high-temperature in-situ tension-fatigue testing system, which solves the above-mentioned problems existing in the prior art. The utility model realizes the uniaxial stretching or uniaxial stretching-fatigue test in the range of high temperature 500°C-1700°C by adjusting the temperature, and combines the optical microscope to observe the material mechanical property test process in real time, such as the crack of the material In situ monitoring of initiation, crack growth and material failure and destruction processes to achieve in situ testing. In addition, the mechanical and deformation signal detection unit collects signals such as the tensile force and tensile deformation of the test piece during the test process, which can fit the stress-strain history of the tested material under the corresponding load, and then analyze the Conduct in-depth research on the micromechanical behavior and deformation damage mechanism of materials under high temperature environment and tensile-fatigue load. The variable temperature field is applied through a high-temperature furnace, the high-temperature environment is provided by silicon-molybdenum rods, and the temperature is adjusted through a control system. It can be integrated in the vacuum chamber to realize the tensile-fatigue test of the micromechanical properties of materials under vacuum conditions or high temperatures in special gas environments.

Above-mentioned purpose of the utility model is realized through the following technical solutions:

High-temperature in-situ tensile-fatigue testing system, including tensile loading and detection unit, fatigue loading and detection unit, in-situ observation unit, high-temperature loading and The detection units are respectively installed on both sides of the high temperature furnace, and the directions of the tensile loading and fatigue loading are on the same axis, the tensile loading and detection unit, fatigue loading and detection unit are installed on the base 14, and the in-situ observation unit is placed It is above the high temperature loading and detection unit and installed on the base 14 through the bracket 1 .

The tensile loading and detection unit is powered by the servo motor 12, and the tensile load is applied to the test piece through the worm wheel II9, the worm II10, the worm I5, the worm I7, the lead screw 28, and the nut 27; the servo motor 12 passes The motor seat 11 is installed on the base 14, and the worm I7 is installed on the output shaft of the motor; the worm wheel II9 and the worm I7 are installed on the shaft 31, and the shaft is installed through the bearing I30, the bearing seat I6, the bearing II32, and the bearing seat II8 to the base 14; the worm gear I5 is installed on the screw 28, and the screw 28 is installed on the bottom plate 29 through the screw seat 42; the nut 27 is installed on the nut seat 3, and the nut seat 3 passes through the slider Ⅰb 24 and slider Ⅰc 34 are installed on the guide rail Ⅰa 25 and guide rail Ⅰb33 respectively, and the guide rail Ⅰa25 and guide rail Ⅰb 33 are installed on the bottom plate 29; the two ends of the tension sensor 13 are respectively connected with the nut seat 3 and the clamp body 2, and the clamp body 2 passes through The slider Ⅰa23 and the slider Ⅰd 35 are installed on the guide rail Ⅰa 25 and the guide rail Ⅰb 33 respectively; the displacement sensor Ⅰ4 adopts a separate LVDT, the main part of the sensor is installed on the bottom plate Ⅰ29, and the core of the sensor is installed on the top plate Ⅰ22 through threads, and the top plate I22 is installed on the clamp body 2, and the base plate 29 is fixed on the base 14 through the support block I26.

The fatigue loading and detection unit includes a flexible hinge 18, a piezoelectric ceramic 19, a clamp body II41 and a displacement sensor II20. The piezoelectric ceramic 19 is installed in the flexible hinge 18, and the fixed end of the flexible hinge 18 is fixed on the bottom plate II17 by screws. Above, the movable end of the flexible hinge 18 is connected to the clamp body II41, the clamp body II41 is respectively installed on the guide rail IIa38 and the guide rail IIb44 through the slider II37 and the slider II45, and the guide rail IIa38 and the guide rail IIb44 are installed on the bottom plate II17; the displacement sensor II20 is installed on the base plate II17, and is used to measure the displacement of the clamp body II41 during the fatigue test; the base plate II17 is fixed on the base 14 through the support block II15.

The in-situ observation unit includes an optical microscope 21 and a support 1. The working distance of the optical microscope 21 is large enough to cover the surface to be observed of the test piece from the window 46 above the high-temperature furnace, and the position of the optical microscope 21 is adjusted by the support 1 .

According to different observation purposes, the in-situ observation unit can choose an optical microscope to monitor the crack initiation, expansion, and fracture process of the test piece in a high-temperature environment; a Raman spectrometer can be selected to detect the micro-area on the surface of the test piece, and carry out durability testing. Phase structure research, grain and grain boundary changes, crack initiation, etc. of high-temperature materials; X-ray diffractometer can be selected to analyze the phase of the specimen, determine the grain size and stress distribution, study the special properties of the material and its atomic arrangement, The relationship between crystal phase changes, etc.; or choose to use infrared thermal imaging cameras to check material defects, etc.; some observation equipment can be used in conjunction, such as optical microscopes and Raman spectrometers. The test conditions in the high-temperature furnace can be checked through the window 46, and the surface conditions of the test pieces at different temperatures can be observed by using an optical microscope; The corresponding laser, X-ray, etc. need to be emitted in the high-temperature furnace, and a suitable window is processed on the high-temperature furnace.

The high-temperature loading and detection unit includes a high-temperature furnace 16 and its control system. The heating element of the high-temperature furnace 16 is a silicon-molybdenum rod. The silicon-molybdenum rod is powered to generate heat, and the high-temperature silicon-molybdenum rod radiates to make the furnace chamber The temperature inside the high temperature furnace rises rapidly, and the temperature of the inner cavity of the high temperature furnace can be as high as 1700°C. The temperature of the outer surface of the high temperature furnace can be maintained at room temperature through water cooling. A thermocouple is installed in the inner cavity of the high temperature furnace to monitor the actual temperature of the inner cavity of the high temperature furnace. Temperature: the high temperature furnace 16 is equipped with a corresponding control cabinet for controlling the temperature of the inner cavity of the high temperature furnace.

The high-temperature loading and detection unit can choose different heating methods according to different requirements. For example, according to the required temperature and the type of high-temperature furnace, the heating element in the high-temperature furnace can choose resistance wire, silicon carbide rod, silicon molybdenum rod, Or use infrared halogen lamps with spherical reflectors to create more concentrated areas of high heat flux.

The clamp body I2 is connected with the pressure plate I36 through screws, and the test piece is clamped by tightening the screws; the clamp body I2 is processed with grooves for positioning the test piece; the clamp body I2, Knurls are processed on the pressure plate I36 to ensure the reliability of clamping.

The clamp body II41 is connected with the pressure plate II40 by screws, and the test piece is clamped by tightening the screws; the clamp body II41 is processed with grooves for positioning the test piece; the clamp body II41 , Pressure plate Ⅱ40 are processed with knurling to ensure the reliability of clamping.

With the change of temperature, the elastoplastic deformation ability of the material all changes to a certain extent. According to the test system of the utility model, the change law of the mechanical properties of different materials at different temperatures can be studied, such as the sensitivity of stress to temperature, whether the strain rate has Obvious temperature softening effect, etc. The utility model can be integrated in a vacuum box to realize high-temperature in-situ stretching-fatigue tests in a vacuum environment or a special gas environment, and can selectively avoid problems such as oxidation of test pieces.

The beneficial effects of the utility model are: the testing system is reliable in principle, simple and compact in structure, and can accurately detect the micromechanical properties and denatured damage mechanisms of materials and their products under the action of tensile-fatigue loading mode in high-temperature environments . The test system can observe the test process in real time with the help of part of the optical microscope to realize in-situ observation. To sum up, the utility model not only has good scientific research and application value, but also has great significance for the development of in-situ testing technology and devices, and the progress of research on the microscopic mechanical properties of materials.

Description of drawings

The accompanying drawings described here are used to provide a further understanding of the utility model and constitute a part of the application. The schematic examples and descriptions of the utility model are used to explain the utility model and do not constitute improper limitations to the utility model.

Fig. 1 is the overall structural representation of the utility model;

Fig. 2 is the control principle block diagram of the utility model;

Fig. 3 is a structural schematic diagram of the tensile loading and detection unit of the present invention;

Fig. 4 is a structural schematic diagram of the fatigue loading and detection unit of the present invention;

Fig. 5 is the partial structural representation of the testing system of the present utility model;

Fig. 6 is the schematic diagram of the testing system of the present utility model;

Fig. 7 is the schematic diagram of the in-situ observation of the relative position of the test piece and the microscope before the test;

Fig. 8 is a schematic diagram of the in-situ observation of the relative position of the test piece and the microscope after the test.

In the figure: 1. bracket; 2. clip body Ⅰ; 3. nut seat; 4. displacement sensor Ⅰ; 5. worm wheel Ⅰ; 6. bearing seat Ⅰ; 7. worm screw Ⅰ; 8. bearing seat Ⅱ; 9. worm wheel Ⅱ ;10. Worm II; 11. Motor base; 12. Servo motor; 13. Tension sensor; 14. Base; 15. Support block II; 16. High temperature furnace; 17. Base plate II; 18. Flexible hinge; 19. Press Electric ceramic; 20. Displacement sensor II; 21. Optical microscope; 22. Top plate I; 23. Slider Ia; 24. Slider Ib; 25. Guide rail Ia; 26. Support block I; 27. Nut; 28. Lead screw ;29, bottom plate I; 30, bearing I; 31, shaft; 32 bearing II; 33, guide rail Ib; 34, slider Ic; 35, slider Id; 36, pressure block I; 37, slider IIa; Guide rail Ⅱa; 39. Top plate Ⅱ; 40. Pressure plate Ⅱ; 41. Clamp body Ⅱ; 42. Screw seat; 43. Block Ⅲ; 44. Guide rail Ⅱb; 45. Slider Ⅱb; Ⅰ; 48, block Ⅱ.

Detailed ways

Further illustrate the detailed content of the utility model and its specific implementation below in conjunction with accompanying drawing.

Referring to Figures 1 to 8, the high-temperature in-situ tensile-fatigue testing system of the present invention includes a tensile loading and detection unit, a fatigue loading and detection unit, an in-situ observation unit, a high-temperature loading and detection unit, etc., and the device Horizontally arranged, where the tensile loading and testing unit, fatigue loading and testing unit are respectively installed on both sides of the high temperature furnace, and the directions of tensile loading and fatigue loading are on the same axis. The uniaxial tension-fatigue mechanical performance test of the material was realized under the thermal field with adjustable temperature from 500°C to 1700°C, and the full dynamic monitoring of the microscopic deformation damage of the material under load was realized based on the optical microscope.

Referring to Fig. 3, the tensile loading and detection unit described in the utility model is powered by the servo motor 12, and stretches the test piece through the worm gear II9 worm, II10, worm gear I5, worm I7, lead screw 28, and nut 27. Load; the servo motor 12 is installed on the base 14 through the motor base 11, and the worm I7 is installed on the output shaft of the motor; the worm wheel II9 and the worm I7 are installed on the shaft 31, and the shaft passes through the bearing I30, the bearing seat I6, bearing II32, and bearing seat II8 are installed on the base 14; the worm gear I5 is installed on the screw 28, and the screw 28 is installed on the bottom plate 29 through the screw seat 42; the nut 27 is installed on the nut seat 3, the nut seat 3 is respectively installed on the guide rail Ia25 and the guide rail Ib33 through the slider Ib24 and the slider Ic34, and the guide rail Ia25 and the guide rail Ib33 are installed on the bottom plate 29; the two ends of the tension sensor 13 are respectively connected with the nut seat 3 and the clamp body I2 , the clamp body I2 is installed on the guide rail Ia25 and the guide rail Ib33 respectively through the slider Ia23 and the slider dI35; the displacement sensor I4 adopts a separate LVDT, the main part of the sensor is installed on the bottom plate I29, and the core of the sensor is installed on the top plate I22 through threads , the top plate I22 is installed on the clamp body I2, and the bottom plate 29 is fixed on the base 14 through the support block I26.

Referring to Fig. 4, the fatigue loading and detection unit described in the present invention includes a flexible hinge 18 piezoelectric ceramic 19, a clamp body II 41 and a displacement sensor II 20, etc.; the piezoelectric ceramic 19 is installed in the flexible hinge 18, and the flexible The fixed end of the hinge 18 is fixed on the bottom plate II17 by screws, the movable end of the flexible hinge 18 is connected with the clamp body II41, and the clamp body II41 is respectively installed on the guide rail IIa38 and the guide rail IIb44 through the slider IIa37 and the slider IIb45, and the guide rail IIa38 and the guide rail IIb44 Installed on the base plate II17; the displacement sensor II20 is used to measure the displacement of the clamp body II41 during the fatigue test, the fixed end of the displacement sensor II20 is installed on the base plate II17, the movable end is connected with the top plate II39, and the top plate II39 is installed on the clamp Specifically on II41; said bottom plate II17 is fixed on the base 14 through the support block II15.

The in-situ observation unit includes an optical microscope 21 and a support 1; the working distance of the optical microscope 21 is large enough to cover the surface to be observed of the test piece from the window 46 above the high temperature furnace, and the position of the optical microscope 21 can be passed Bracket 1 adjustment.

The high-temperature loading and detection unit is composed of a high-temperature furnace 16 and its control system; the heating element of the high-temperature furnace 16 is a silicon-molybdenum rod, which is heated by supplying power to the silicon-molybdenum rod, and the high-temperature silicon-molybdenum rod is radiated to make it The temperature in the furnace cavity rises rapidly, and the temperature in the inner cavity of the high-temperature furnace can reach as high as 1700°C. The high-temperature furnace includes an insulation layer and a water-cooled layer from the inside to the outside, and the temperature on the outer surface of the high-temperature furnace can be maintained at room temperature through water cooling. A thermocouple is installed in the chamber for monitoring the actual temperature of the inner chamber of the high-temperature furnace; the high-temperature furnace 16 is equipped with a corresponding control cabinet for controlling the temperature of the inner chamber of the high-temperature furnace.

The clamp body I2 and the clamp body II41 are respectively connected to the pressure plate I36 and the pressure plate II40 through screws, and the specimen is clamped by tightening the screws; the clamp body I2 and the clamp body II41 are both processed with grooves, It is used to locate the test piece; the clamp body I2, the pressure plate I36, the clamp body II41, and the pressure plate II40 are all processed with knurling to ensure the reliability of clamping.

The high-temperature furnace 16 is positioned and adjusted by surrounding blocks, such as block I47, block II48, and block III43.

Referring to Figures 1 to 5, before the test system is installed, it is necessary to calibrate and calibrate the tension sensor 13, displacement sensor I4, and displacement sensor II20 used in the test system, and then install and debug the test system. Before installing the test piece, it is necessary to adjust the position of the clamp body I2 so that the test piece can pass through the high-temperature furnace; contact with the test piece so as not to create additional friction.

According to the purpose of the experiment, choose the appropriate measurement method, that is, uniaxial tensile test or tensile-fatigue composite load test. The fatigue test involved mainly refers to the low-cycle fatigue test, and it is carried out on the basis of the specimen being stretched. That is, the specimen is pre-deformed or under a certain load condition for medium and low frequency tensile tests. Therefore, the test research carried out with the invented test system mainly analyzes the material elastic modulus E , yield strength , strength limit , elongation after fracture A , reduction of area Z and other mechanical properties parameters. in,

Elastic Modulus ,

Yield Strength ,

strength limit ,

elongation after break ,

rate of reduction in area ;

in, : stress of the material, : the strain of the material, : material load corresponding to the lower yield point, : the maximum load of the material, : the original cross-sectional area of the material, : Cross-sectional area of the material after fracture, : material original gauge length, : Gauge length after material breakage.

The mechanical properties of materials are mainly reflected in the deformation and failure properties of materials under load. The elastic modulus, fracture limit, fatigue strength and other parameters of the material are the most important test objects in the mechanical performance test of the material. The elastic modulus, yield strength, strength limit, elongation after fracture and section shrinkage of the material can be measured through tensile testing. rate, thereby measuring the mechanical properties of the material under tensile load. The yield and failure process of the material under the action of bidirectional tensile load is studied through the load-displacement curve. The alternating stress generated by the cyclic loading force will cause permanent damage to the local material, and induce the initiation, expansion and instability of cracks. The effect of fatigue loading on the mechanical properties of materials can be measured by tensile-fatigue testing. However, different materials show different responses to temperature, such as the difference in the sensitivity of stress to temperature, the difference in the temperature softening effect of strain rate, and so on. The mechanical properties of materials at different temperatures are even quite different, that is, the elastic modulus, yield strength, strength limit, elongation after fracture and reduction of area of the same material measured at different temperatures are different.

If the temperature is When , the mechanical property parameters of some materials change with temperature as follows:

,

,

;

in : modulus of elasticity at temperature, : modulus of elasticity at room temperature, : yield strength at temperature, : Yield strength at room temperature, , , , and : coefficient related to material; : The total strain at temperature, : the instantaneous strain resulting from the stress, : creep, : Strain due to thermal expansion.

However, when the temperature reaches a higher level, such as when the temperature reaches the recrystallization temperature of the material, the mechanical property parameters of the material may show another trend as the temperature changes.

The high temperature tensile-fatigue test can measure the mechanical performance parameters of materials under different temperature fields under tensile and fatigue loads.

In the whole process of testing, in order to monitor the crack initiation, propagation and instability of the tested piece in real time, the test piece needs to be polished and corroded before the test, and the optical microscope imaging system is used for dynamic monitoring, and the image can be recorded at the same time. Combined with the debugging software, the engineering stress-strain curve and other mechanical parameters that characterize the mechanical properties of the material can also be obtained in real time.

As shown in Figure 7 and Figure 8, the position of the microscope before the test corresponds to the observation area. With the application of the tensile load, crack initiation and crack expansion gradually appear in the observation area until the specimen breaks. At the same time, The lens is adjusted following the movement of the specimen observation area to ensure full dynamic monitoring of the microscopic deformation and damage of the material.

The above descriptions are only preferred examples of the utility model, and are not intended to limit the utility model. For those skilled in the art, the utility model can have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made to the utility model shall be included in the protection scope of the utility model.

Claims (7)

1. A high-temperature in-situ tensile-fatigue testing system, characterized in that: it comprises a tensile loading and detection unit, a fatigue loading and detection unit, an in-situ observation unit, a high-temperature loading and detection unit, and is arranged horizontally as a whole, wherein the tensile The loading and testing unit, fatigue loading and testing unit are respectively installed on both sides of the high temperature furnace, and the directions of tensile loading and fatigue loading are on the same axis, and the tensile loading and testing unit, fatigue loading and testing unit are installed on the base On (14), the in-situ observation unit is placed above the high-temperature loading and detection unit, and is installed on the base (14) through the bracket (1). 2. The high-temperature in-situ tensile-fatigue testing system according to claim 1, characterized in that: said tensile loading and detection unit is powered by a servo motor (12), through worm wheel II (9), worm II (10), worm wheel I (5), worm screw I (7), leading screw (28), nut (27) apply tensile load to the test piece; described servo motor (12) is installed on the On the base (14), the worm I (7) is installed on the output shaft of the motor; the worm gear II (9) and the worm I (7) are installed on the shaft (31), and the shaft passes through the bearing I (30), Bearing seat I (6), bearing II (32), and bearing seat II (8) are installed on the base (14); the worm wheel I (5) is installed on the lead screw (28), and the lead screw (28) Installed on the base plate (29) through the screw seat (42); the nut (27) is installed on the nut seat (3), and the nut seat (3) passes through the slider Ib (24), the slider Ic (34) Installed on the guide rail Ia (25) and the guide rail Ib (33) respectively, the guide rail Ia (25) and the guide rail Ib (33) are installed on the bottom plate (29); the two ends of the tension sensor (13) are connected with the nut seat (3) and The clamp body Ⅰ (2) is connected, and the clamp body Ⅰ (2) is installed on the guide rail Ⅰa (25) and the guide rail Ⅰb (33) respectively through the slider Ⅰa (23) and the slider Ⅰd (35); the displacement sensor Ⅰ (4) Separate LVDT is used, the main part of the sensor is installed on the bottom plate I (29), the core of the sensor is installed on the top plate I (22) through threads, and the top plate I (22) is installed on the clamp body I (2). Base plate (29) is fixed on the base (14) by support block I (26). 3. The high-temperature in-situ tensile-fatigue testing system according to claim 1, characterized in that: the fatigue loading and detection unit includes a flexible hinge (18), piezoelectric ceramics (19), clamp body II (41 ) and displacement sensor II (20), the piezoelectric ceramic (19) is installed in the flexible hinge (18), the fixed end of the flexible hinge (18) is fixed on the bottom plate II (17) by screws, and the flexible hinge (18) The movable end is connected with the clamp body II (41), and the clamp body II (41) is respectively installed on the guide rail IIa (38) and the guide rail IIb (44) through the slider II (37) and the slider II (45), and the guide rail IIa ( 38) and the guide rail IIb (44) are installed on the base plate II (17); the displacement sensor II (20) is installed on the base plate II (17) to measure the displacement of the clamp body II (41) during the fatigue test; The bottom plate II (17) is fixed on the base (14) through the support block II (15). 4. The high-temperature in-situ tensile-fatigue testing system according to claim 1, characterized in that: the in-situ observation unit includes an optical microscope (21) and a support (1), and the optical microscope (21) The working distance is large enough to cover the surface to be observed of the test piece from the window (46) above the high-temperature furnace, and the position of the optical microscope (21) is adjusted through the bracket (1). 5. The high-temperature in-situ tensile-fatigue testing system according to claim 1, characterized in that: the high-temperature loading and detection unit comprises a high-temperature furnace (16), and the heating element of the high-temperature furnace (16) is silicon Molybdenum rods are heated by supplying power to the silicon-molybdenum rods. The high-temperature silicon-molybdenum rods cause the temperature in the furnace cavity to rise rapidly through radiation. The temperature in the high-temperature furnace cavity can be as high as 1700 ° C. Maintaining at room temperature, a thermocouple is installed in the inner cavity of the high-temperature furnace to monitor the actual temperature of the inner cavity of the high-temperature furnace; the high-temperature furnace (16) is equipped with a control cabinet for controlling the temperature of the inner cavity of the high-temperature furnace. 6. The high-temperature in-situ tensile-fatigue testing system according to claim 2, characterized in that: the clamp body I (2) is connected to the pressure plate I (36) by screws, and the test piece is tightened by tightening the screws. Clamping; grooves are processed on the clamp body I (2) for positioning the test piece; knurls are processed on the clamp body I (2) and the pressure plate I (36) to ensure that the clamping Sustained reliability. 7. The high-temperature in-situ tensile-fatigue testing system according to claim 3, characterized in that: the clamp body II (41) is connected to the pressure plate II (40) by screws, and the test piece is tightened by tightening the screws. Clamping; grooves are processed on the clamp body II (41) for positioning the test piece; knurls are processed on the clamp body II (41) and the pressure plate II (40) to ensure Clamping reliability.