CN101819114A - Ultrasonic bending fatigue experimental device - Google Patents
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Abstract
一种超声弯曲疲劳实验装置,换能器位于传力器内,并与连接器连接。传力器位于本发明的中部;传力器的垫板与上连接板和下连接板之间通过传力杆固连。连接器一端穿过传力器下端的下连接板与位移放大器连接;另一端穿过上连接板,与换能器连接。支承装置位于位移放大器下方;静载荷加力装置穿过垫板的中心孔与垫板固连。本发明的换能器、连接器、位移放大器和压头构成纵向谐振系统,并通过压头将纵向振动载荷传递到弯曲疲劳试样,使弯曲疲劳试样产生弯曲振动。定位丝杠能实现自动调节弯曲疲劳试样支承点的位置,从而实现超声弯曲疲劳实验,能实现不同加载载荷、不同几何尺寸试样的超声弯曲疲劳实验,适于利用轴向加载超声疲劳实验机进行弯曲疲劳实验。
An ultrasonic bending fatigue test device, the transducer is located in the force transmitter and connected with the connector. The power transmission device is located in the middle of the present invention; the backing plate of the power transmission device is fixedly connected with the upper connecting plate and the lower connecting plate by a dowel rod. One end of the connector passes through the lower connecting plate at the lower end of the force transmitter and is connected with the displacement amplifier; the other end passes through the upper connecting plate and is connected with the transducer. The supporting device is located under the displacement amplifier; the static load reinforcing device passes through the center hole of the backing plate and is fixedly connected with the backing plate. The transducer, connector, displacement amplifier and indenter of the present invention constitute a longitudinal resonance system, and the longitudinal vibration load is transmitted to the bending fatigue sample through the indenter, so that the bending fatigue sample generates bending vibration. The positioning screw can automatically adjust the position of the support point of the bending fatigue specimen, so as to realize the ultrasonic bending fatigue experiment, and can realize the ultrasonic bending fatigue experiment of samples with different loading loads and different geometric sizes, and is suitable for using axial loading ultrasonic fatigue testing machine Perform bending fatigue tests.
Description
技术领域technical field
本发明涉及结构材料疲劳、耐久性测试领域,具体是一种超声弯曲疲劳实验装置。The invention relates to the fields of structural material fatigue and durability testing, in particular to an ultrasonic bending fatigue test device.
背景技术Background technique
疲劳失效是在交变载荷下结构件的主要失效形式,如曲轴、齿轮、连杆、弹簧、螺栓等构件以及压力容器、车辆、飞机、海洋平台、焊接钢桥等结构的主要失效形式都是疲劳破坏。疲劳破坏导致的工程构件失效事故占总事故的比例达80%。由于疲劳断裂发生突然,并导致灾难性的事故,因此,材料的疲劳破坏问题一直是国内外学者和工程界研究和关心的课题。Fatigue failure is the main failure mode of structural parts under alternating loads, such as crankshafts, gears, connecting rods, springs, bolts and other components, as well as pressure vessels, vehicles, aircraft, offshore platforms, welded steel bridges and other structures. fatigue damage. The failure accidents of engineering components caused by fatigue damage account for 80% of the total accidents. Because fatigue fracture occurs suddenly and leads to catastrophic accidents, the fatigue failure of materials has always been a subject of research and concern by scholars and engineering circles at home and abroad.
在航空航天、汽车、铁路、核工业、机械等工业领域,一些结构零部件在工作过程中要承受高频、低幅循环载荷作用,承受循环载荷次数高达109-1011周,这种高频循环载荷虽然应力幅值小,但其频率很高,可达数千赫兹,尤其这种高频、低幅载荷与其它载荷叠加时,造成的复合损伤会大大地加速结构部件的损坏,严重威胁到结构部件的工作安全和可靠。所以国外在研究高速运转结构件的疲劳寿命中,特别重视低幅、超高周疲劳寿命的研究。近几年来,有关工程材料107周次以上的超高周疲劳行为的研究已成为疲劳研究的一个新课题,引起工程界的高度重视。In aerospace, automobile, railway, nuclear industry, machinery and other industrial fields, some structural parts have to bear high-frequency and low-amplitude cyclic loads during the working process, and the number of cyclic loads is as high as 10 9 -10 11 weeks. Although the stress amplitude of high-frequency cyclic load is small, its frequency is very high, up to thousands of hertz, especially when this high-frequency, low-amplitude load is superimposed with other loads, the composite damage caused will greatly accelerate the damage of structural components, seriously Threats to the safety and reliability of structural components. Therefore, foreign countries pay special attention to the research of low-amplitude and ultra-high-cycle fatigue life in the study of fatigue life of high-speed operating structural parts. In recent years, the research on the ultra-high cycle fatigue behavior of engineering materials with more than 10 7 cycles has become a new subject of fatigue research, which has attracted great attention from the engineering community.
超声疲劳(Ultrasonic Fatigue)实验技术采用共振原理,将超声发生器产生的高频电信号通过换能器转化为同频率的振动位移输出,这种振动位移经过位移放大器放大,将高频循环应力加载于试样,从而实现结构材料的超声高频循环加载,进而实现结构材料的超高周疲劳性能的实验研究。超声疲劳实验技术已成为有效、可靠的获得工程材料超高周疲劳性能的实验手段。Ultrasonic fatigue (Ultrasonic Fatigue) experimental technology adopts the resonance principle to convert the high-frequency electrical signal generated by the ultrasonic generator into a vibration displacement output with the same frequency through the transducer. This vibration displacement is amplified by the displacement amplifier to load the high-frequency cyclic stress In order to realize the ultrasonic high-frequency cyclic loading of structural materials, and then realize the experimental research on the ultra-high cycle fatigue performance of structural materials. Ultrasonic fatigue test technology has become an effective and reliable experimental method to obtain the ultra-high cycle fatigue performance of engineering materials.
现有的超声疲劳实验装置主要由超声发生器、换能器、高倍位移放大器、拉压疲劳试样组成(如图1),通过超声发生器提供激振电源和交频电信号,超声换能器将交频电信号转换为同样频率的振动信号,高倍位移放大器将换能器输出的振动位移放大,并传递给拉压疲劳试样,形成对试样的轴向循环应力加载。由于现有的超声疲劳实验装置没有能够将纵向波转换为横向波的实验装置,同时,由于在现有轴向加载超声疲劳实验装置中,拉压疲劳试样所承受的动载荷预与静载荷方向一致,不需要考虑静载荷对动载荷的影响,故在结构上没有静载荷加力装置,所以现有技术中的轴向加载超声疲劳实验装置只能实现对疲劳试样的轴向加载。The existing ultrasonic fatigue test device is mainly composed of an ultrasonic generator, a transducer, a high-magnification displacement amplifier, and a tension-compression fatigue sample (as shown in Figure 1). The transducer converts the alternating-frequency electrical signal into a vibration signal of the same frequency, and the high-magnification displacement amplifier amplifies the vibration displacement output by the transducer, and transmits it to the tension-compression fatigue specimen to form axial cyclic stress loading on the specimen. Since the existing ultrasonic fatigue test device does not have an experimental device that can convert the longitudinal wave into a transverse wave, at the same time, because in the existing axially loaded ultrasonic fatigue test device, the dynamic load preload and static load of the tension and compression fatigue specimen The direction is the same, and there is no need to consider the influence of static load on dynamic load, so there is no static load adding device in the structure, so the axial loading ultrasonic fatigue test device in the prior art can only realize axial loading of fatigue samples.
发明内容Contents of the invention
为克服现有技术中存在的只能实现对疲劳试样轴向加载的不足,本发明提出了一种超声弯曲疲劳实验装置。In order to overcome the deficiency in the prior art that only the axial loading of fatigue samples can be achieved, the present invention proposes an ultrasonic bending fatigue test device.
本发明包括低倍位移放大器、连接器、支承装置、传力器和换能器;换能器的下端与连接器通过螺杆连接。并且The invention includes a low-magnification displacement amplifier, a connector, a supporting device, a force transmitter and a transducer; the lower end of the transducer is connected to the connector through a screw. and
换能器位于传力器内;传力器位于超声弯曲疲劳实验装置的中部;传力器包括下连接板、上连接板、传力杆和垫板,并且垫板位于传力器的顶端,上连接板和下连接板位于传力器的下端。垫板与上连接板和下连接板之间通过传力杆固连。连接器一端穿过传力器下端的下连接板与低倍位移放大器连接;另一端穿过上连接板,与换能器连接。The transducer is located in the force transmitter; the force transmitter is located in the middle of the ultrasonic bending fatigue test device; the force transmitter includes a lower connecting plate, an upper connecting plate, a dowel rod and a backing plate, and the backing plate is located on the top of the force transmitting device, The upper connecting plate and the lower connecting plate are located at the lower end of the power transmission device. The backing plate is fixedly connected with the upper connecting plate and the lower connecting plate by a dowel rod. One end of the connector passes through the lower connecting plate at the lower end of the force transmitter to connect with the low-magnification displacement amplifier; the other end passes through the upper connecting plate to connect with the transducer.
支承装置位于低倍位移放大器下方;静载荷加力装置穿过垫板的中心孔与垫板固连。The supporting device is located under the low-magnification displacement amplifier; the static load reinforcing device passes through the center hole of the backing plate and is fixedly connected with the backing plate.
支承装置为对称结构,包括压块、调节滑块、纵向调节螺钉、滑块、支承盖、定位套筒、定位丝杠、手柄、底座、横向调节螺钉、支承条压块、支承条和滑块固定板;两个滑块对称的安装在底座台面的中心,两个调节滑块分别位于滑块表面的导向滑槽内;两个支承盖分别位于底座台面的两端;定位丝杠穿过横贯底座台面的定位丝杠安装槽,并通过定位套筒定位;支承条安装在滑块上的支承条安装槽中,压块、支承条压块分别固定支承条的两端。The supporting device is a symmetrical structure, including a pressing block, an adjusting slider, a longitudinal adjusting screw, a sliding block, a supporting cover, a positioning sleeve, a positioning screw, a handle, a base, a horizontal adjusting screw, a supporting bar pressing block, a supporting bar and a sliding block Fixed plate; two sliders are symmetrically installed in the center of the base table, and two adjustment sliders are respectively located in the guide chute on the surface of the slider; two support covers are respectively located at both ends of the base table; the positioning screw passes through the The positioning lead screw installation groove on the base table is positioned through the positioning sleeve; the support bar is installed in the support bar installation groove on the slider, and the two ends of the support bar are respectively fixed by the pressing block and the support bar pressing block.
所述的隔离块套装在下连接板和上连接板之间的传力杆上。传力杆一端与垫板连接,另一端先后穿过上连接板、隔离块和下连接板后,用螺母固定。The spacer block is set on the dowel bar between the lower connecting plate and the upper connecting plate. One end of the dowel rod is connected with the backing plate, and the other end passes through the upper connecting plate, the isolation block and the lower connecting plate successively, and is fixed with a nut.
所述的底座的底板中心有与实验台定位轴配合的通孔;底座的台面中心有滑块的导向滑槽,导向滑槽的中心位置有凸出滑槽内表面的定位块,在定位块的两侧,由内向外是相互连通的滑块的导向滑槽和定位丝杠安装槽。The center of the bottom plate of the base has a through hole that matches the positioning shaft of the test bench; the center of the table top of the base has a guide chute for the slider, and the center of the guide chute has a positioning block that protrudes from the inner surface of the chute. The two sides of the guide chute and the positioning lead screw installation groove of the slider communicate with each other from the inside to the outside.
所述滑块的连接块位于底座的导向滑槽内,并且该连接块上有定位丝杠连接孔;滑块的安装块表面有与连接块上的定位丝杠连接孔平行的安装调节滑块的导向滑槽,并且该导向滑槽的中心与定位丝杠连接孔的中心在同一垂直面上;在滑块安装块表面一边,有与导向滑槽垂直的支承条安装槽。The connecting block of the slider is located in the guide chute of the base, and the connecting block has a positioning screw connecting hole; the surface of the mounting block of the sliding block has an installation adjusting slider parallel to the positioning screw connecting hole on the connecting block The guide chute, and the center of the guide chute and the center of the positioning screw connection hole are on the same vertical plane; on one side of the surface of the slider mounting block, there is a support bar installation groove perpendicular to the guide chute.
所述的定位丝杠中部外表面有两段旋向相反的外螺纹;两段外螺纹分别与一个滑块连接后一同安放在底座的导向滑槽中;定位丝杠两端有定位套筒的安装孔;定位丝杠的两端套装有定位套筒,并且使定位套筒的一端面紧贴底座的侧壁;限位螺钉穿过定位套筒侧面的定位槽,装入定位丝杠上的螺孔中;定位套筒通过内孔与定位丝杠间隙配合。The outer surface of the middle part of the positioning screw has two sections of external threads with opposite rotation directions; the two sections of external threads are respectively connected with a slider and placed in the guide chute of the base together; there are positioning sleeves at both ends of the positioning screw Mounting holes; the two ends of the positioning screw are fitted with a positioning sleeve, and one end of the positioning sleeve is close to the side wall of the base; the limit screw passes through the positioning groove on the side of the positioning sleeve and is inserted into the positioning screw on the positioning screw. In the screw hole; the positioning sleeve is clearance matched with the positioning lead screw through the inner hole.
所述的支承盖两侧底边的中心有半圆形的定位丝杠的过孔;在支承盖的盖表面两端有连接孔;当定位丝杠与滑块连接并一同安放在底座的导向滑槽中后,将支承盖固定在底座上,支承盖下表面的半圆槽与底座上表面的半圆定位丝杠安装槽,构成了支承定位丝杠自由转动的丝杠支承座。There is a semicircular through hole for the positioning screw at the center of the bottom edge on both sides of the support cover; there are connecting holes at both ends of the cover surface of the support cover; when the positioning screw is connected with the slider and placed on the guide of the base together After being in the chute, the support cover is fixed on the base, and the semicircle groove on the lower surface of the support cover and the semicircle positioning lead screw installation groove on the base upper surface constitute a lead screw support seat for supporting the positioning lead screw to rotate freely.
所述的调节滑块的两侧分别有开口槽,该开口槽对称于调节滑块的中心,并且开口方向一致;调节滑块的中心有纵向调节螺钉的安装孔。The two sides of the adjusting slider are respectively provided with opening grooves, which are symmetrical to the center of the adjusting slider and have the same opening direction; the center of the adjusting slider has a mounting hole for a longitudinal adjusting screw.
所述的压块的侧边中部有横向调节螺钉的安装孔;在横向调节螺钉安装孔的下方、压块侧边的底部,有与压紧支承条配合的凹槽;压块上表面调节螺钉安装孔的两侧,有中心线与横向调节螺钉安装孔的中心线相互垂直的滑块的连接孔。支承条压块上的连接孔位于压紧支承条压紧槽的两侧。滑块与底座台面上的导向滑槽之间滑动配合;定位丝杠安装槽的直径同定位丝杠外径。There is a mounting hole for the horizontal adjustment screw in the middle of the side of the pressure block; below the mounting hole for the horizontal adjustment screw and at the bottom of the side of the pressure block, there is a groove for matching the compression support bar; the adjustment screw on the upper surface of the pressure block On both sides of the mounting hole, there are connecting holes of the slide block whose center line is perpendicular to the center line of the horizontal adjustment screw mounting hole. The connecting holes on the support bar pressing block are located on both sides of the pressing groove of the support bar. The sliding block is slidingly matched with the guide chute on the table top of the base; the diameter of the positioning lead screw installation groove is the same as the outer diameter of the positioning lead screw.
本发明应用共振原理,保证弯曲疲劳试样与超声疲劳实验系统具有相同的谐振频率,实现不同静载荷与动载荷的复合加载。弯曲疲劳实验装置支承部分采用丝杠传动,导向滑槽导向,从而实现弯曲疲劳试样的准确定位和加载。由于超声弯曲疲劳实验过程中系统保持共振,因此必须准确计算各组件在20kHz振动频率下的谐振尺寸,并使弯曲疲劳试样准确定位。在弯曲疲劳实验装置中,应设置纵向自动对心装置,以及保证横向定位的横向定位装置。纵向、横向定位装置,都由丝杠装置控制,从而实现任意几何尺寸弯曲疲劳试样的疲劳实验。The invention applies the principle of resonance to ensure that the bending fatigue sample and the ultrasonic fatigue test system have the same resonance frequency, and realizes composite loading of different static loads and dynamic loads. The supporting part of the bending fatigue test device is driven by a screw and guided by a guide chute, so as to realize accurate positioning and loading of the bending fatigue test specimen. Since the system maintains resonance during the ultrasonic bending fatigue test, it is necessary to accurately calculate the resonance size of each component at a vibration frequency of 20kHz and accurately position the bending fatigue specimen. In the bending fatigue test device, a longitudinal automatic centering device and a lateral positioning device to ensure lateral positioning should be installed. Both the longitudinal and lateral positioning devices are controlled by the lead screw device, so as to realize the fatigue experiment of bending fatigue specimens of any geometric size.
本发明的换能器、连接器、低倍位移放大器和压头构成纵向谐振系统,并通过压头将纵向振动载荷传递到弯曲疲劳试样,使弯曲疲劳试样产生弯曲振动。弯曲疲劳试样的几何尺寸、支承点的位置经过严格计算使其满足与纵向振动载荷同频率的弯曲谐振条件,因而使弯曲疲劳试样产生弯曲共振。超声弯曲疲劳实验装置中,设计了连接器,传力杆与上、下连接板、隔离块构成传力器,传力器的上、下连接板与连接器的零位移面连接,静载荷通过连接器的零位移面施加于弯曲试样,以避免静载荷对系统振动波的影响,保证超声弯曲疲劳系统的共振条件。超声弯曲疲劳实验支承装置中定位丝杠可实现自动调节弯曲疲劳试样支承点的位置,并保证弯曲疲劳试样自动对中,从而实现超声弯曲疲劳实验。The transducer, connector, low-magnification displacement amplifier and indenter of the present invention constitute a longitudinal resonance system, and the longitudinal vibration load is transmitted to the bending fatigue sample through the indenter, so that the bending fatigue sample generates bending vibration. The geometric dimensions of the bending fatigue specimen and the position of the support point are strictly calculated to meet the bending resonance condition of the same frequency as the longitudinal vibration load, thus causing the bending fatigue specimen to generate bending resonance. In the ultrasonic bending fatigue test device, a connector is designed. The dowel bar, the upper and lower connecting plates, and the isolation block constitute a force transmitting device. The upper and lower connecting plates of the force transmitting device are connected with the zero-displacement surface of the connector. The static load passes through the The zero displacement surface of the connector is applied to the bending sample to avoid the influence of the static load on the vibration wave of the system and ensure the resonance condition of the ultrasonic bending fatigue system. The positioning lead screw in the supporting device of the ultrasonic bending fatigue test can automatically adjust the position of the supporting point of the bending fatigue sample, and ensure the automatic centering of the bending fatigue sample, so as to realize the ultrasonic bending fatigue test.
本发明的连接器是根据振动波波动理论设计的。连接器上有零振动位移面,静载荷加力装置与连接器的零振动位移面相连接,外加静载荷通过此零振动位移面,将静载荷传递给弯曲疲劳试样,同时连接器也将动载荷传递给弯曲疲劳试样,动载荷与静载荷之间的传递互不影响。弯曲疲劳试样设计根据横向波波动理论,设计加载点和支承点。加载点和支承点的准确位置通过调节支承装置实现。本发明将支承条固定在滑块上,滑块内螺纹与定位丝杠形成螺旋运动,旋转定位丝杠即可推动滑块,滑块通过螺杆传力,使其沿底座中的导向滑槽滑动,进而确定了纵向位移。通过双向螺杆滑动装置实现弯曲试样的自动对心。同时,本发明采用的横向定位是通过单边双导柱加螺杆侧推装置定位,压块的内螺纹与调节螺钉形成螺旋传动,旋转调节螺钉即可推动弯曲疲劳试样,保证弯曲疲劳试样的横向定位。支承条安装在滑块上,磨损后可卸下更换。The connector of the present invention is designed according to the vibration wave theory. There is a zero-vibration displacement surface on the connector, and the static load force device is connected to the zero-vibration displacement surface of the connector. The load is transmitted to the bending fatigue specimen, and the transmission between the dynamic load and the static load does not affect each other. The design of the bending fatigue specimen is based on the transverse wave wave theory, and the loading point and support point are designed. The exact position of the loading point and the supporting point is achieved by adjusting the supporting device. In the present invention, the support bar is fixed on the slider, and the internal thread of the slider and the positioning screw form a spiral motion, and the positioning screw can be rotated to push the slider, and the slider transmits force through the screw to make it slide along the guide chute in the base , and then determine the longitudinal displacement. The automatic centering of the curved specimen is realized by the two-way screw sliding device. At the same time, the lateral positioning adopted by the present invention is positioned by a single-side double guide post plus a screw side pusher device. The internal thread of the pressing block and the adjusting screw form a helical transmission, and the rotating adjusting screw can push the bending fatigue sample to ensure that the bending fatigue sample horizontal orientation. The support bar is installed on the slider and can be removed for replacement after wear and tear.
超声弯曲疲劳实验装置的应用可有效地实现不同加载载荷、不同几何尺寸弯曲疲劳试样的超声弯曲疲劳实验。它适于利用轴向加载超声疲劳实验机进行弯曲疲劳实验。The application of the ultrasonic bending fatigue test device can effectively realize the ultrasonic bending fatigue test of bending fatigue samples with different loads and different geometric sizes. It is suitable for bending fatigue experiments using an axially loaded ultrasonic fatigue testing machine.
附图说明Description of drawings
附图1是现有技术中的超声疲劳实验装置结构示意图;Accompanying
附图2是超声弯曲疲劳实验装置的结构示意图;Accompanying drawing 2 is the structural representation of ultrasonic bending fatigue test device;
附图3是超声弯曲疲劳实验装置的结构轴测图;Accompanying drawing 3 is the structural axonometric view of ultrasonic bending fatigue test device;
附图4是两种实验装置下振动位移的分布情况,其中a是轴向加载超声疲劳实验装置的轴向振动位移曲线,b是超声弯曲疲劳实验装置的轴向振动位移与弯曲疲劳试样弯曲振动位移曲线;Accompanying drawing 4 is the distribution of vibration displacement under two kinds of experimental devices, wherein a is the axial vibration displacement curve of the axially loaded ultrasonic fatigue test device, b is the axial vibration displacement of the ultrasonic bending fatigue test device and the bending fatigue specimen bending Vibration displacement curve;
附图5是连接器的结构示意图;Accompanying drawing 5 is the structural representation of connector;
附图6是隔离块的结构示意图;Accompanying drawing 6 is the structural representation of isolation block;
附图7是连接板的结构示意图;Accompanying drawing 7 is the structural representation of connecting plate;
附图8是垫板的结构示意图;Accompanying drawing 8 is the structural representation of backing plate;
附图9是低倍位移放大器的结构示意图;Accompanying drawing 9 is the structural representation of low power displacement amplifier;
附图10是压头的结构示意图;Accompanying drawing 10 is the structural representation of pressure head;
附图11是支承装置的轴测图;Accompanying drawing 11 is the axonometric view of supporting device;
附图12是支承装置的俯视图;Accompanying drawing 12 is the top view of supporting device;
附图13是支承装置的主视图;Accompanying drawing 13 is the front view of supporting device;
附图14是底座的结构示意图;Accompanying drawing 14 is the structural representation of base;
附图15是支承盖的结构示意图;Accompanying drawing 15 is the structural representation of support cover;
附图16是滑块的结构示意图;Accompanying drawing 16 is the structural representation of slider;
附图17是调节滑块的结构示意图;Accompanying drawing 17 is the structural representation of adjusting slider;
附图18是压块的结构示意图;Accompanying drawing 18 is the structural representation of briquetting;
附图19是支承条压块的结构示意图;Accompanying drawing 19 is the structural representation of support bar briquetting block;
附图20是定位丝杠的结构示意图;Accompanying drawing 20 is the structural representation of positioning screw;
附图21是定位套筒的结构示意图;Accompanying drawing 21 is the structural representation of positioning sleeve;
附图22是手柄的结构示意图;Accompanying drawing 22 is the structural representation of handle;
附图23是滑块固定板的结构示意图。其中:Accompanying drawing 23 is the structural representation of slider fixing plate. in:
1.拉压疲劳试样 2.高倍位移放大器 3.导向滑槽 4.支承装置 5.弯曲疲劳试样1. Tension and
6.低倍位移放大器 7.连接器 8.下连接板 9.上连接板 10.换能器6. Low
11.传力杆 12.垫板 13.静载荷加力装置 14.隔离块 15.压头11.
16.压块 17.调节滑块 18.纵向调节螺钉 19.滑块 20.支承盖16.
21.定位套筒 22.定位丝杠 23.手柄 24.底座 25.横向调节螺钉21. Positioning
26.支承条压块 27.支承条 28.滑块固定板 29.支承条安装槽 30.定位丝杠安装槽26. Support
具体实施方式Detailed ways
本实施例是一种超声弯曲疲劳实验装置,用于金属材料20kHz频率下的三点弯曲疲劳实验,可完成应力比R>0的弯曲疲劳实验。根据该超声弯曲疲劳试验装置中连接器以及低倍位移放大器的设计,弯曲疲劳试样的应力幅值加载范围在250-850MPa之间。超声弯曲疲劳试样须满足20kHz的弯曲谐振条件,弯曲疲劳试样的最小长度应大于30mm。This embodiment is an ultrasonic bending fatigue test device, which is used for a three-point bending fatigue test of metal materials at a frequency of 20 kHz, and can complete a bending fatigue test with a stress ratio R>0. According to the design of the connector and the low-magnification displacement amplifier in the ultrasonic bending fatigue test device, the stress amplitude loading range of the bending fatigue specimen is between 250-850 MPa. The ultrasonic bending fatigue specimen must meet the bending resonance condition of 20kHz, and the minimum length of the bending fatigue specimen should be greater than 30mm.
超声弯曲疲劳实验装置包括支承装置4、弯曲疲劳试样5、低倍位移放大器6、连接器7、换能器10、传力器、静载荷加力装置13、隔离块14和压头15。传力器为由杆件和板件组成的框架结构,包括下连接板8、上连接板9、传力杆11、垫板12构成,位于本实施例的中部;换能器10位于传力器内。传力器顶端的平板为安装静载荷加力装置的垫板12;换能器10的下端与连接器7通过螺杆连接,连接器7穿过传力器下端的下连接板8和上连接板9,并与低倍位移放大器6连接。支承装置4位于低倍位移放大器6下方,用于安放弯曲疲劳试样5。静载荷加力装置为机械式拉压装置,传力器连接到静载荷加力装置上,通过传力器将静载荷加载到弯曲疲劳试样。The ultrasonic bending fatigue test device includes a supporting
如图5所示。连接器7为铝合金回转体,外圆周为阶梯状,其中部外径最大,形成了连接器7的凸缘;在凸缘的两侧,分别是不同外径的下连接板8和上连接板9的配合段。连接器7两端端面中心分别有螺纹孔,连接器直径较小一端通过螺杆与低倍位移放大器6螺接,较大一端通过螺杆与换能器10螺接,换能器10通过通信电缆与外接的超声发生器连接,连接器7的几何尺寸满足20kHz沿轴向振动的谐振条件。As shown in Figure 5. The
传力器包括下连接板8、上连接板9、传力杆11和垫板12。其中,垫板12位于传力器的顶端,上连接板9和下连接板8位于传力器的下端;垫板12与上连接板9和下连接板8之间通过三根传力杆11固连。静载荷加力装置13穿过垫板12的中心孔,并通过螺母与垫板12固连,从而将垫板12连接到静载荷加力装置13上。The power transmission device includes a lower connecting
垫板12为圆形板件,中心有通孔。下连接板8和上连接板9均为圆形板件,在下连接板8和上连接板9中心有连接器7的安装通孔,并且该连接器7安装通孔的内径小于连接器7中部外圆周上凸缘的直径。连接器7凸缘一侧的大端穿过上连接板9的中心孔,连接器7凸缘一侧的小端穿过下连接板8的中心孔,使连接器7中部的凸缘位于下连接板8和上连接板9之间。传力杆11的两端均有外螺纹;传力杆11的一端通过垫板12边缘的连接孔与垫板12固连,另一端分别穿过位于下连接板8和上连接板9边缘的三个连接孔,并用螺母固定。The
如图10所示。压头15为横截面近似锥形的杆件。在压头15平面的中部有连接螺孔,通过该连接螺孔,用螺杆与低倍位移放大器6的小端端面上的螺孔相连,实现压头15与低倍位移放大器6的连接。形成压头15锥形的锥尖部呈圆弧,在疲劳实验时该圆弧形的锥尖部与弯曲疲劳试样5接触。As shown in Figure 10. The indenter 15 is a rod with an approximately tapered cross section. There is connecting screw hole in the middle part of pressure head 15 planes, by this connection screw hole, links to each other with the screw hole on the small end face of low
如图9所示。低倍位移放大器6是用钛合金材料加工而成的回转体,根据实验需求,低倍位移放大器的放大倍数为6.3,低倍位移放大器的几何尺寸满足20kHz沿轴向振动的谐振条件。低倍位移放大器6的外圆周为阶梯状;在低倍位移放大器两端面中心加工有螺孔,直径小的一端通过螺杆与压头15连接,直径大的一端通过螺杆与连接器7相连接。As shown in Figure 9. The low-
如图6所示。三个隔离块14均为中空回转体,被套装在位于下连接板8和上连接板9之间的各传力杆11上。隔离块14的内径略大于传力杆11的外径,当隔离块14套装在传力杆11上后,两者之间间隙配合。隔离块14壳体的高度同连接器7凸缘的厚度。当传力杆11与上连接板9和下连接板8连接时,通过隔离块将上连接板9和下连接板8隔离分开。隔离块14的高度相对于连接器7凸缘厚度的公差为+0.1mm,以保证连接器7可以在上连接板9和下连接板8之间转动。As shown in Figure 6. The three
传力杆11为两端加工有螺纹的圆柱形长钢杆,传力杆一端穿过垫板12边缘上的小孔由螺母将其与垫板12连接,另一端先后穿过上连接板9、隔离块14、下连接板8由螺母将它们连接在一起。在传力杆11与上连接板9、隔离块14、下连接板8连接之前,应先将连接器7的大小两端分别穿过上连接板9和下连接板8的中心孔,使得传力杆与连接板连接的同时,将连接器7的凸缘固定在上、下两个连接板之间。在连接器7、上连接板9、隔离块14、下连接板8以及垫板12的相对位置确定好后,用同样的3根传力杆将其连接。The
如图11-13所示。支承装置4为对称结构,包括压块16、调节滑块17、纵向调节螺钉18、滑块19、支承盖20、定位套筒21、定位丝杠22、手柄23、底座24、横向调节螺钉25、支承条压块26、支承条27和滑块固定板28。支承装置4安装在静载荷加力装置的实验台面上,并位于实验台面的中心。定位丝杠22分别穿过两个滑块19的中心螺纹孔,并且支承在横贯底座24台面的定位丝杠安装槽30上。两个滑块19对称地安装在底座24台面中心的导向滑槽3内,两个调节滑块17分别位于滑块19表面的导向滑槽内。两个支承盖20分别安装于底座24台面的两端,并且使定位丝杠22穿过支承盖20下端的半圆与底座台面两端的半圆形定位丝杠安装槽30构成的支承座中。两个滑块19初始位置确定后,通过定位套筒21确定定位丝杠22在底座24台面上的位置。两个支承条27分别安放于两个滑块台面上的半圆支撑条安装槽29中,支承条的两端分别安装压块16和支承条压块26,压块16和支承条压块26将支承条固定在滑块上面的半圆支撑条安装槽29中。纵向调节螺钉18分别穿过调节滑块17中部的螺孔安装于两个调节滑块上,横向调节螺钉25分别穿过压块16中部的螺纹孔安装于两个压块上。两个滑块位置确定后,分别由两个滑块固定板28将滑块固定在底座24上。As shown in Figure 11-13. The
如图14所示。底座24由平板和一个叵字形的台架焊接而成。在底座平板的中部有通孔,该通孔的直径同静载荷加力装置实验台面上的定位轴直径,两者之间为间隙配合;叵字形的台架位于平板中部、通孔的上方。叵字形台架的台面中心有沿该台面长度方向的导向滑槽3,用于安装滑块19,并使滑块19能够在导向滑槽3内滑动。导向滑槽3的中心位置有凸出导向滑槽3内表面的定位块,用于确定滑块的初始位置。在定位块的两侧是用于安装滑块19的导向滑槽3,滑槽由内向外是相互连通的。底座24的导向滑槽3的宽度同滑块19下表面连接块的宽度,两者之间为间隙配合,当滑块19的连接块安放在导向滑槽3内时,两者之间滑动配合;定位丝杠安装槽30为圆弧形,其直径同定位丝杠22外径,两者为间隙配合。底座24的底板上有用于将底座与静载荷加力装置实验台固定的连接孔。As shown in Figure 14.
如图16所示。滑块19有两个,由安装块和与之相互垂直的连接块组成,其外形呈“T”字形。滑块19的连接块位于底座24的导向滑槽3内;在滑块19的连接块上有贯通该连接块的定位丝杠22的连接孔。滑块19的安装块表面有与滑块的连接块上的定位丝杠22连接孔平行的用于安装调节滑块17的导向滑槽3,并且该导向滑槽3的中心与定位丝杠22连接孔的中心在同一垂直面上。在滑块19安装块表面一边,还有导向滑槽3垂直的圆弧形支承条安装槽29,用于安装支承条27;支承条27的安装槽29贯穿滑块19安装块的宽度方向。As shown in Figure 16.
如图20所示。定位丝杠22中部外表面有两段不连贯的外螺纹,并且两段外螺纹旋向相反。定位丝杠22的两段螺纹分别与两个滑块19连接后,一同安放在底座24的导向滑槽3中。当旋转定位丝杠22时,两个滑块19分别向相反的方向沿导向滑槽3移动。定位丝杠两端的光杆部分加工有螺孔,用于安装两个定位套筒。定位丝杠的一端与手柄23连接。装配时,将两个滑块旋入定位丝杠22中,两个滑块的连接段分别安放在底座24内的导向滑槽3中,定位丝杠22安放在底座24上的两个半圆形定位丝杠安装槽30中,通过旋转定位丝杠使得滑块沿底座24内的导向滑槽3移动。滑块上面的矩形槽用于安装调节滑块17。滑块上面的半圆支承条安装槽29用于安装支承条27。滑块上销钉的位置,表示安装定位销的销钉孔,其余8个小孔均为安装紧固螺钉的螺钉孔。As shown in Figure 20. There are two sections of incoherent external threads on the outer surface of the middle part of the
如图15所示。支承盖20有两个,均为矩形带槽壳体;在支承盖20长度方向两侧底边的中心有半圆形的定位丝杠22的过孔;在支承盖20的盖表面两端各有一个连接孔,并且该连接孔与底座24上面的螺钉孔相对应。当定位丝杠22与滑块连接并一同安放在底座24的导向滑槽3中后,将支承盖20通过连接螺钉安装在底座24上,支承盖下表面的半圆槽与底座24上表面的半圆形定位丝杠安装槽30,构成了支承定位丝杠22自由转动的丝杠支承座,用于安装定位丝杠22。As shown in Figure 15. There are two support covers 20, both of which are rectangular grooved housings; there are
如图21所示。定位套筒21有两个,均为两个侧面加工有平台的圆柱形壳体,在圆柱形壳体侧面平台上加工有定位槽。定位套筒21的内孔为圆形,其孔径同定位丝杠22的外径,两者为间隙配合。当定位丝杠22、滑块19以及支承盖20安装好之后,旋转定位丝杠,调节滑块的位置,使得两个滑块的连接块分别靠紧底座24导向滑槽3中间定位块的两边,并将此时滑块的位置确定为初始位置。将两个定位套筒21分别从定位丝杠22的两端装入,并且使定位套筒21的一端面紧贴底座24的侧壁,限位螺钉穿过定位套筒侧面的定位槽,装入定位丝杠22上的螺孔中,限制了定位丝杠在滑槽中的轴向移动。As shown in Figure 21. There are two positioning
如图17所示。调节滑块17为块状体。调节滑块17有两个,其结构相同、方向相反。调节滑块17为对称结构,其截面呈十字形。调节滑块17的水平块的两侧分别有一个贯通该水平块厚度的开口槽;调节滑块17沿滑块19上面的导向滑槽3移动,当调节滑块17位置确定后,紧固螺钉穿过该开口槽将调节滑块17固定在滑块上,该开口槽沿调节滑块17中心对称。在调节滑块17的中部,有贯通的螺纹孔;该螺纹孔与纵向调节螺钉18配合。调节滑块17沿滑块19上面的矩形槽滑动,以调整安放弯曲疲劳试样的空间。As shown in Figure 17. The
如图18所示。压块16为块状体。压块16有2个。压块16的侧边中部有贯通的横向调节螺钉25的安装孔;在横向调节螺钉25安装孔的下方、压块16侧边的底部,有半圆形凹槽,用于压紧支承条27的一端。压块16的上表面有两个螺纹孔,该螺纹孔的中心线与横向调节螺钉25安装孔的中心线相互垂直,并且分布在横向调节螺钉25安装孔的两侧。通过压块16上表面的螺纹孔与滑块19连接。As shown in Figure 18. The
如图19所示。块状的支承条压块26亦有2个,用于压紧支承条27的另一端。支承条压块26中心下表面有与压紧支承条27配合的圆弧形凹槽。支承条压块26上有两个连接孔,该连接孔的中心线与压紧支承条27压紧槽的中心线相互垂直,并且分布在压紧支承条27压紧槽的两侧,通过该连接孔将支承条压块26与滑块19连接。As shown in Figure 19. There are also 2 block-shaped support
如图23所示。滑块固定板28为矩形块,其中部有螺纹孔,用于滑块固定板28与滑块19的连接。当滑块19位置确定后,用紧固螺钉穿过滑块固定板28中部的螺纹孔与滑块19连接,将滑块19通过滑块固定板固定在底座24上。As shown in Figure 23. The
支承条27安装在滑块19上的支承条安装槽29内,压块16、支承条压块26分别固定支承条的两端。
手柄23一端加工有矩形内孔,用于连接定位丝杠,手柄23有助于定位丝杠的旋转。纵向调节螺钉18安装在调节滑块17中部的螺孔中,安装弯曲疲劳试样5时,旋转纵向调节螺钉18,以确定试样的纵向位置。横向调节螺钉25安装在压块16中部的螺孔中,安装弯曲疲劳试样时,旋转横向调节螺钉,以确定试样的横向位置。One end of the
超声弯曲疲劳实验时,首先将传力器连同换能器10、连接器7、低倍位移放大器6、压头15连接到静载荷加力装置上,然后将超声弯曲疲劳实验装置支承部分安装于静载荷加力装置13的实验台面上,并将弯曲疲劳试样5安放于支承装置4的支承条27上;调节好弯曲疲劳试样5的位置,旋转传力器上的连接器7,使得压头15的锥尖位于弯曲疲劳试样5的中心线上,便可加力,启动疲劳实验。During the ultrasonic bending fatigue test, first connect the force transducer together with the
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103217347A (en) * | 2013-04-17 | 2013-07-24 | 河南理工大学 | Ultrasonic vibration three-point bending test device suitable for observing crisp and hard material on line |
| CN104458253A (en) * | 2014-12-31 | 2015-03-25 | 华侨大学 | Contact pair part fatigue test device based on ultrasonic vibration |
| CN104483218A (en) * | 2014-04-25 | 2015-04-01 | 华侨大学 | Material fatigue characteristic testing method based on supersonic vibration under microscale |
| CN104483216A (en) * | 2014-12-31 | 2015-04-01 | 华侨大学 | Ultrasonic-vibration based microscale testing device for material impact fatigue |
| CN105890902A (en) * | 2016-06-12 | 2016-08-24 | 西北工业大学 | Fatigue test device for ultrasonic high-frequency rolling bearing |
| CN106404566A (en) * | 2016-12-13 | 2017-02-15 | 天津旁耘科技有限公司 | Bed fatigue test controller for light, mechanical and electronic integration medical instrument |
| CN106680083A (en) * | 2016-12-26 | 2017-05-17 | 中国电力科学研究院 | Testing device for treading fatigue of tension composite insulator |
| CN107941624A (en) * | 2017-12-13 | 2018-04-20 | 吉林大学 | High-temperature high-frequency material mechanical property in-situ test device |
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| CN108562505A (en) * | 2018-05-25 | 2018-09-21 | 吉林大学 | Combined load and the material high-frequency fatigue test device and method under high temperature-atmosphere |
| CN109175112A (en) * | 2018-07-27 | 2019-01-11 | 沈阳航空航天大学 | A kind of aperture synchronizes the thin plate bending experimental rig of symmetrical adjustment and punch-pin quick change |
| CN109765129A (en) * | 2019-03-22 | 2019-05-17 | 吉林大学 | A resonant system that can realize multi-axis ultrasonic fatigue test |
| CN110411872A (en) * | 2019-07-29 | 2019-11-05 | 杭州嘉振超声波科技有限公司 | Ultrasonic wave fatigue tester |
| CN110579404A (en) * | 2019-09-12 | 2019-12-17 | 吉林大学 | Instrument and method for in-situ testing of mechanical properties of materials under high temperature and complex mechanical loads |
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| CN111125952A (en) * | 2019-12-17 | 2020-05-08 | 吉林大学 | Static prestretching-ultrasonic bending fatigue sample and design method |
| CN114323996A (en) * | 2021-12-28 | 2022-04-12 | 浙江工业大学 | Tiny sample bending fatigue test device and method based on acoustic radiation force |
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| CN103217347A (en) * | 2013-04-17 | 2013-07-24 | 河南理工大学 | Ultrasonic vibration three-point bending test device suitable for observing crisp and hard material on line |
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| CN104483218B (en) * | 2014-04-25 | 2017-05-03 | 华侨大学 | Material fatigue characteristic testing method based on supersonic vibration under microscale |
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| CN104483216A (en) * | 2014-12-31 | 2015-04-01 | 华侨大学 | Ultrasonic-vibration based microscale testing device for material impact fatigue |
| CN105890902A (en) * | 2016-06-12 | 2016-08-24 | 西北工业大学 | Fatigue test device for ultrasonic high-frequency rolling bearing |
| CN106404566A (en) * | 2016-12-13 | 2017-02-15 | 天津旁耘科技有限公司 | Bed fatigue test controller for light, mechanical and electronic integration medical instrument |
| CN106680083A (en) * | 2016-12-26 | 2017-05-17 | 中国电力科学研究院 | Testing device for treading fatigue of tension composite insulator |
| CN107957448B (en) * | 2017-11-21 | 2020-06-26 | 西南石油大学 | Ultrasonic fatigue average stress loading device |
| CN107957448A (en) * | 2017-11-21 | 2018-04-24 | 西南石油大学 | A kind of ultrasonic fatigue mean stress loading device |
| CN107941624A (en) * | 2017-12-13 | 2018-04-20 | 吉林大学 | High-temperature high-frequency material mechanical property in-situ test device |
| CN107941624B (en) * | 2017-12-13 | 2023-12-22 | 吉林大学 | High-temperature high-frequency material mechanical property in-situ testing device |
| CN108562505A (en) * | 2018-05-25 | 2018-09-21 | 吉林大学 | Combined load and the material high-frequency fatigue test device and method under high temperature-atmosphere |
| CN109175112A (en) * | 2018-07-27 | 2019-01-11 | 沈阳航空航天大学 | A kind of aperture synchronizes the thin plate bending experimental rig of symmetrical adjustment and punch-pin quick change |
| CN109765129A (en) * | 2019-03-22 | 2019-05-17 | 吉林大学 | A resonant system that can realize multi-axis ultrasonic fatigue test |
| CN110411872A (en) * | 2019-07-29 | 2019-11-05 | 杭州嘉振超声波科技有限公司 | Ultrasonic wave fatigue tester |
| CN110579404A (en) * | 2019-09-12 | 2019-12-17 | 吉林大学 | Instrument and method for in-situ testing of mechanical properties of materials under high temperature and complex mechanical loads |
| CN110579404B (en) * | 2019-09-12 | 2021-10-15 | 吉林大学 | Instrument and method for in-situ testing of mechanical properties of materials under high temperature and complex mechanical loads |
| US11635359B2 (en) | 2019-09-12 | 2023-04-25 | Jilin University | Instrument and method for mechanical properties in situ testing of materials under high temperature and complex mechanical loads |
| CN110608873A (en) * | 2019-09-25 | 2019-12-24 | 吉林大学 | Reliability test device for high-speed electric spindle based on ultrasonic vibrator loading |
| CN111125952A (en) * | 2019-12-17 | 2020-05-08 | 吉林大学 | Static prestretching-ultrasonic bending fatigue sample and design method |
| CN114323996A (en) * | 2021-12-28 | 2022-04-12 | 浙江工业大学 | Tiny sample bending fatigue test device and method based on acoustic radiation force |
| CN114323996B (en) * | 2021-12-28 | 2024-04-09 | 浙江工业大学 | A device and method for testing the bending fatigue of a small sample based on acoustic radiation force |
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