CN105675412A - Bending fretting fatigue experimental equipment and experimental method - Google Patents
Bending fretting fatigue experimental equipment and experimental method Download PDFInfo
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Abstract
本发明公开了一种弯曲微动疲劳实验装置,包括试样、试样夹持固定部、法向接触载荷施加部、弯曲疲劳载荷施加部和数据采集控制系统,试样的一端固定在试样夹持固定部,另一端设置弯曲疲劳载荷施加部且通过法向接触载荷施加部压紧,试样夹持固定部与弯曲疲劳载荷施加部均与数据采集控制系统电连接。本发明还公开了一种弯曲微动疲劳实验方法,该方法为:组装好该装置,安装上试样,对圆棒试样施加法向接触载荷,当载荷施加到设定条件时,操控电液伺服疲劳试验机,使圆棒试样按设定的参数进行实验。该实验装置与方法操作简单,真实模拟了构件在交变载荷下的弯曲微动疲劳损伤,控制与测试精度高,实验数据重现性好,实验结果准确可靠。
The invention discloses a bending fretting fatigue experiment device, which comprises a sample, a sample clamping and fixing part, a normal contact load applying part, a bending fatigue load applying part and a data acquisition control system. One end of the sample is fixed on the sample The fixed part is clamped, and the other end is provided with a bending fatigue load applying part, which is pressed by the normal contact load applying part. Both the sample clamping fixed part and the bending fatigue load applying part are electrically connected to the data acquisition and control system. The invention also discloses a bending fretting fatigue test method, the method is as follows: assemble the device, install the sample, apply a normal contact load to the round bar sample, and when the load is applied to the set condition, control the electric The hydraulic servo fatigue testing machine enables the round bar sample to be tested according to the set parameters. The experimental device and method are simple to operate, truly simulate the bending fretting fatigue damage of components under alternating loads, have high control and test precision, good reproducibility of experimental data, and accurate and reliable experimental results.
Description
技术领域technical field
本发明属于微动疲劳技术研究领域,尤其涉及一种弯曲微动疲劳实验装置及实验方法。The invention belongs to the technical research field of fretting fatigue, and in particular relates to a bending fretting fatigue experimental device and an experimental method.
背景技术Background technique
微动是指在机械振动、疲劳载荷、电磁振动或热循环等交变载荷作用下,两个接触表面之间(如紧配合面)发生的极小振幅(微米量级)的相对运动,这些接触表面通常名义上静止,即微动发生在“紧固”配合的机械部件中。Fretting refers to the relative motion of extremely small amplitude (micron level) between two contact surfaces (such as tight fitting surfaces) under the action of alternating loads such as mechanical vibration, fatigue load, electromagnetic vibration or thermal cycle. The contacting surfaces are usually nominally stationary, i.e. fretting occurs in mechanical parts that are "tightly" fitted.
微动疲劳是指接触体由于承受外界交变疲劳应力产生不同的变形引起接触界面发生微幅相对运动(通常在微米级),促使疲劳裂纹早期萌生和加速扩展,从而导致构件过早失效破坏的现象,它是一种伴随微动磨损的疲劳强度和疲劳寿命问题。研究表明,微动疲劳能使构件的疲劳寿命降低20%~80%,甚至更低。Fretting fatigue refers to the phenomenon that the contact interface undergoes slight relative motion (usually at the micron level) due to the different deformations of the contact body due to the external alternating fatigue stress, which promotes the early initiation and accelerated growth of fatigue cracks, resulting in premature failure of the component. Phenomenon, it is a fatigue strength and fatigue life problem accompanied by fretting wear. Studies have shown that fretting fatigue can reduce the fatigue life of components by 20% to 80%, or even lower.
微动疲劳损伤普遍存在于机械、铁路、汽车、船舶、航空航天、桥梁工程、核反应堆、电力工业等领域的紧配合部件中,随着工程领域对高精度、长寿命和高可靠性的要求日渐提升,以及更加复杂恶劣的工况条件,微动疲劳损伤的危害日益凸显。微动会加速零部件的疲劳裂纹萌生与扩展,从而使零部件的服役寿命明显降低。据调查,微动疲劳现已成为一些关键零部件失效的主要原因之一,被称作工业中的“癌症”。Fretting fatigue damage generally exists in tight fitting parts in machinery, railways, automobiles, ships, aerospace, bridge engineering, nuclear reactors, power industry and other fields. With the increasing requirements for high precision, long life and high reliability in the engineering field The hazards of fretting fatigue damage are becoming more and more prominent in the increasingly complex and harsh working conditions. Fretting will accelerate the initiation and growth of fatigue cracks in parts, which will significantly reduce the service life of parts. According to the survey, fretting fatigue has become one of the main reasons for the failure of some key components, and it is called "cancer" in the industry.
弯曲微动疲劳损伤普遍存在于旋转类零部件中,大大降低了这些零部件的服役寿命。对弯曲微动疲劳进行试验与分析,以搞清其弯曲微动疲劳特性和损伤机理,可为相关零部件的设计、制造与维护提供准确、可靠的试验依据,对降低其疲劳裂纹的萌生与扩展,提高零部件的服役寿命具有重要意义。目前,尚无专门为弯曲微动疲劳实验量身设计的实验装备与实验方法。Bending fretting fatigue damage generally exists in rotating parts, which greatly reduces the service life of these parts. The bending fretting fatigue test and analysis are carried out to clarify its bending fretting fatigue characteristics and damage mechanism, which can provide accurate and reliable test basis for the design, manufacture and maintenance of related parts, and help reduce the initiation and damage of fatigue cracks. It is of great significance to extend and improve the service life of components. At present, there are no experimental equipment and experimental methods specially designed for bending fretting fatigue experiments.
发明内容Contents of the invention
本发明的目的在于提供一种弯曲微动疲劳实验装置及实验方法,该装置结构简单,易于操作,能够进行各种不同工况与规格材料试样的弯曲微动疲劳实验,控制与测试精度高,实验数据更准确、可靠,重现性好。The object of the present invention is to provide a bending fretting fatigue experiment device and experimental method. The device has a simple structure and is easy to operate, and can perform bending fretting fatigue experiments on various working conditions and specifications of material samples, and has high control and testing accuracy. , the experimental data is more accurate, reliable and reproducible.
为实现上述目的,本发明采用如下技术方案:To achieve the above object, the present invention adopts the following technical solutions:
本发明提供了一种弯曲微动疲劳实验装置,包括试样(2)、试样夹持固定部、法向接触载荷施加部、弯曲疲劳载荷施加部和数据采集控制系统,所述试样(2)的一端固定在所述试样夹持固定部,另一端设置有所述弯曲疲劳载荷施加部且通过所述法向接触载荷施加部上下垂直压紧,所述试样夹持固定部上设置有力传感器(12),所述力传感器(12)与所述弯曲疲劳载荷施加部均与所述数据采集控制系统电连接,由所述数据采集控制系统控制实验条件并采集实验数据。The invention provides a bending fretting fatigue experimental device, comprising a sample (2), a sample clamping and fixing part, a normal contact load applying part, a bending fatigue load applying part and a data acquisition control system, the sample ( 2) One end is fixed on the sample clamping and fixing part, the other end is provided with the bending fatigue load applying part and is pressed vertically up and down by the normal contact load applying part, and the sample clamping and fixing part A force sensor (12) is provided, and both the force sensor (12) and the bending fatigue load application part are electrically connected to the data acquisition control system, and the data acquisition control system controls the experimental conditions and collects experimental data.
所述试样夹持固定部包括固定在疲劳实验台底座上的基座(1)、设置在所述基座(1)中间的长槽、设置所述基座(1)上的方孔、设置在所述方孔内的夹持块(3)、固定螺钉一(4),所述试样(2)左端通过所述基座(1)方孔内的所述夹持块(3)以及所述固定螺钉一(4)固定在所述基座(1)上。The sample clamping and fixing part includes a base (1) fixed on the base of the fatigue test bench, a long groove arranged in the middle of the base (1), a square hole arranged on the base (1), The clamping block (3) and fixing screw one (4) arranged in the square hole, the left end of the sample (2) passes through the clamping block (3) in the square hole of the base (1) And the fixing screw one (4) is fixed on the base (1).
所述法向接触载荷施加部包括承载台(7)、上微动垫夹持座(11)、加载板(15)、直线导轨(17),所述直线导轨(17)穿过所述上微动垫夹持座(11)、底端固定在所述承载台(7)上、顶端固定在所述加载板(15)上,所述承载台(7)通过固定螺钉二(5)和固定板(6)固定在所述基座(1)中间的长槽内,其位置根据实验需要可在一定距离内调整,所述承载台(7)中间设置有下微动垫(8),所述上微动垫夹持座(11)上设置有上微动垫(10),所述试样(2)设置在所述上微动垫(10)与所述下微动垫(8)之间,所述上微动垫夹持座(11)的上部设置有槽,所述槽内设置有力传感器(12),实时测量加载的法向接触载荷大小,所述加载板(15)上设置有加载螺钉(16),所述加载螺钉(16)与所述上微动垫夹持座(11)之间设置钢珠球(14),通过加载螺钉(16)和钢珠球(14)向所述上微动垫夹持座(11)施加法向接触载荷。The normal contact load applying part includes a bearing platform (7), an upper fretting pad clamping seat (11), a loading plate (15), and a linear guide rail (17), and the linear guide rail (17) passes through the upper The micro-movement pad clamping seat (11), the bottom end is fixed on the bearing platform (7), and the top is fixed on the loading plate (15), and the bearing platform (7) is fixed by fixing screws two (5) and The fixed plate (6) is fixed in the long groove in the middle of the base (1), and its position can be adjusted within a certain distance according to the experimental requirements. The lower fretting pad (8) is arranged in the middle of the bearing platform (7). The upper fretting pad holder (11) is provided with an upper fretting pad (10), and the sample (2) is arranged between the upper fretting pad (10) and the lower fretting pad (8). ), the upper part of the upper fretting pad clamping seat (11) is provided with a groove, and a force sensor (12) is arranged in the groove to measure the normal contact load loaded in real time. The loading plate (15) A loading screw (16) is arranged on the top, and a steel ball (14) is set between the loading screw (16) and the upper fretting pad clamping seat (11), and the loading screw (16) and the steel ball (14) A normal contact load is applied to the upper fretting pad clamping seat (11).
所述弯曲疲劳载荷施加部为电液伺服疲劳试验机(9)。The bending fatigue load applying part is an electro-hydraulic servo fatigue testing machine (9).
进一步,所述上微动垫夹持座(11)通过两个直线轴承(18)安装在所述直线导轨(17)上,所述力传感器(12)上下两面各设置有一片用于保护所述力传感器(12)本体的垫片(13),所述的上微动垫夹持座(11)两边安装直线轴承(18),使其在直线导轨(17)上运动的摩擦力几乎为零。Further, the upper fretting pad clamping seat (11) is installed on the linear guide rail (17) through two linear bearings (18), and the upper and lower sides of the force sensor (12) are respectively provided with a piece for protecting the The gasket (13) of the force sensor (12) body, the linear bearings (18) are installed on both sides of the upper fretting pad clamping seat (11), so that the frictional force of its movement on the linear guide rail (17) is almost zero.
本发明还提供了一种弯曲微动疲劳实验方法,该方法包括如下步骤:The present invention also provides a bending fretting fatigue test method, the method comprising the following steps:
a、将基座(1)固定在疲劳实验台上的合适位置上,然后将安装有下微动垫(8)和直线导轨(17)的承载台(7)固定在基座(1)中间的长槽内,其在长槽内的位置根据实验条件需要来确定,再然后将试样(2)左端固定在基座(1)的左侧方孔内,右端置于下微动垫(8)之上,随后将安装有上微动垫(10)的上微动垫夹持座(11)穿过直线导轨(17)垂直滑下,使上微动垫(10)与试样(2)垂直正交,实现良好的点接触;a. Fix the base (1) at a suitable position on the fatigue test bench, and then fix the bearing platform (7) with the lower fretting pad (8) and the linear guide rail (17) in the middle of the base (1) Its position in the long groove is determined according to the needs of the experimental conditions, and then the left end of the sample (2) is fixed in the left square hole of the base (1), and the right end is placed on the lower fretting pad ( 8), then the upper fretting pad holder (11) with the upper fretting pad (10) is vertically slid down through the linear guide rail (17), so that the upper fretting pad (10) and the sample ( 2) Vertical and orthogonal to achieve good point contact;
b、拧动加载螺钉(16),所施加的法向接触载荷会通过力传感器(12)的测量显示在与数据采集控制系统相连的计算机上,当法向接触载荷施加到设定的实验条件时,停止拧动加载螺钉(16),然后通过数据采集控制系统来操控电液伺服疲劳试验机(9),使试样(2)按设定的参数(振幅、频率等)进行弯曲微动疲劳实验。在此过程中,各项实验数据会通过传感器反馈给数据采集控制系统进行分析,绘制出各种参数的变化曲线。b. Turn the loading screw (16), the applied normal contact load will be displayed on the computer connected to the data acquisition control system through the measurement of the force sensor (12), when the normal contact load is applied to the set experimental conditions , stop screwing the loading screw (16), and then control the electro-hydraulic servo fatigue testing machine (9) through the data acquisition control system, so that the sample (2) performs bending micro-motion according to the set parameters (amplitude, frequency, etc.) Fatigue experiment. During this process, various experimental data will be fed back to the data acquisition and control system for analysis through sensors, and the change curves of various parameters will be drawn.
本发明的有益效果:Beneficial effects of the present invention:
第一、圆棒试样与圆柱形上微动垫成正交点接触模式,由电液伺服疲劳试验机施加弯曲微动疲劳载荷,而且此电液伺服疲劳试验机激振幅度小,频率高,精度高,准确地实现了对圆棒试样的弯曲微动疲劳实验,真实有效地对弯曲微动疲劳进行了测试与分析;First, the round bar sample and the cylindrical upper fretting pad form an orthogonal point contact mode, and the bending fretting fatigue load is applied by the electro-hydraulic servo fatigue testing machine, and the electro-hydraulic servo fatigue testing machine has a small vibration amplitude and a high frequency , high precision, accurately realized the bending fretting fatigue experiment of the round bar sample, and truly and effectively tested and analyzed the bending fretting fatigue;
第二、使用了直线轴承与直线导轨的组合,使上微动垫夹持座上下滑动时与导轨之间的摩擦力几乎为零,而且使力传感器测到的法向接触载荷与真实施加到试样上的载荷偏差几乎为零,大大保证了实验数据的精确度与实验结果的可信度;Second, the combination of linear bearings and linear guide rails is used to make the friction force between the upper fretting pad clamping seat and the guide rail almost zero when sliding up and down, and to make the normal contact load measured by the force sensor and the actual applied to the The load deviation on the sample is almost zero, which greatly guarantees the accuracy of the experimental data and the credibility of the experimental results;
第三、力传感器、电液伺服疲劳试验机与数据采集控制系统相结合,精确设定输出各项实验参数(法向接触载荷、弯曲疲劳载荷、实验频率等),精确采集各项实验结果数据,能实现各种复杂工况下的弯曲微动疲劳实验。Third, the force sensor, electro-hydraulic servo fatigue testing machine is combined with the data acquisition and control system to accurately set and output various experimental parameters (normal contact load, bending fatigue load, experimental frequency, etc.), and accurately collect various experimental result data , which can realize bending fretting fatigue experiments under various complex working conditions.
总之,采用本发明的实验装置与实验方法,可以方便地、精确地按设定条件进行各种不同工况与规格材料的弯曲微动疲劳实验,较真实地模拟出构件在交变载荷作用下的弯曲微动疲劳损伤,控制与测试精度高,实验结果更准确可靠,实验数据重现性好,克服了现有实验方法精度差、结果单一、数据重现性差等缺陷。In a word, by adopting the experimental device and experimental method of the present invention, it is possible to conveniently and accurately carry out bending fretting fatigue experiments of various working conditions and specifications of materials according to the set conditions, and more realistically simulate the components under alternating loads. The bending fretting fatigue damage has high control and test precision, more accurate and reliable experimental results, and good reproducibility of experimental data, which overcomes the shortcomings of existing experimental methods such as poor precision, single results, and poor data reproducibility.
附图说明Description of drawings
下面结合附图和具体实施方式对本发明作进一步详细的说明。The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
图1为本发明实施例结构示意图;Fig. 1 is the structural representation of the embodiment of the present invention;
图2为本发明实施例主视结构示意图;Fig. 2 is a schematic diagram of the front view structure of an embodiment of the present invention;
图3为本发明实施例左视结构示意图;Fig. 3 is a left view structural schematic diagram of an embodiment of the present invention;
图4为本发明实施例7075铝合金弯曲微动疲劳S~N曲线,其中,▲为弯曲微动疲劳法向应力=368.4MPa,为弯曲微动疲劳断裂寿命超过106次;Fig. 4 is the bending fretting fatigue S-N curve of the 7075 aluminum alloy of the embodiment of the present invention, where ▲ is the bending fretting fatigue normal stress = 368.4MPa, For bending fretting fatigue fracture life more than 10 6 times;
图5为本发明实施例接触载荷对S-N曲线的影响图,其中,为弯曲微动疲劳法向载荷250N,为与之相对应的弯曲微动疲劳断裂寿命超过106次的情况;▲为弯曲微动疲劳法向载荷500N,为与之相对应的弯曲微动疲劳断裂寿命超过106次的情况;■为弯曲微动疲劳法向载荷750N,为与之相对应的弯曲微动疲劳断裂寿命超过106次的情况;Fig. 5 is the impact diagram of the contact load on the SN curve of the embodiment of the present invention, wherein, Bending fretting fatigue normal load 250N, is the case where the corresponding bending fretting fatigue fracture life exceeds 10 6 times; ▲ is the bending fretting fatigue normal load of 500N, is the case where the corresponding bending fretting fatigue fracture life exceeds 10 6 times; ■ is the bending fretting fatigue normal load of 750N, It is the case where the corresponding bending fretting fatigue fracture life exceeds 10 6 times;
图6为本发明实施例接触载荷对弯曲微动疲劳寿命的影响图,其中W=6.0kN,σa,max=305.6MPa。Fig. 6 is a graph showing the influence of contact load on bending fretting fatigue life according to an embodiment of the present invention, where W=6.0kN, σ a,max =305.6MPa.
具体实施方式detailed description
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
本实施例以7075铝合金挤压成型的棒材作为试验材料,系统研究了其弯曲微动疲劳损伤行为。7075-T651铝合金是一种高强度铝合金,具有普通抗腐蚀性能和良好机械性能,并可阳极反应,广泛应用于航空航天等关键结构的零部件。由于其应用领域普遍存在微动损伤,因此开展针对该合金的研究,不仅具有深化微动疲劳基础理论的科学意义,更有在工程应用领域指导抗微动疲劳损伤的实际意义。In this example, the extruded 7075 aluminum alloy bar was used as the test material, and its bending fretting fatigue damage behavior was systematically studied. 7075-T651 aluminum alloy is a high-strength aluminum alloy with general corrosion resistance and good mechanical properties, and can be anodized. It is widely used in key structural parts such as aerospace. Because fretting damage is common in its application fields, the research on this alloy not only has the scientific significance of deepening the basic theory of fretting fatigue, but also has practical significance in guiding the anti-fretting fatigue damage in the field of engineering applications.
如图1~图3所示,为本发明的实施例,包括试样夹持固定部分、法向接触载荷施加部分、弯曲疲劳载荷施加部分以及数据采集控制系统部分,其中,试样夹持固定部分的构成是:基座1安装固定在疲劳实验台底座上,试样2左端通过基座1左侧方孔内的上下两片夹持块3以及其上的固定螺钉一4固定于基座1之上。法向接触载荷施加部分的构成是:承载台7通过固定螺钉二5和固定板6固定于基座1中间的长槽内,其位置根据实验需要可在一定距离内调整。承载台7中间安装有下微动垫8,两边是两根直线导轨17,上微动垫夹持座11通过两个直线轴承18安装在直线导轨17上,上微动垫10安装在上微动垫夹持座11上,上微动垫10与下微动垫8之间夹着的便是试样2。加载板15固定在直线导轨17顶端,通过加载螺钉16和钢珠球14施加法向接触载荷。力传感器12放置在上微动垫夹持座11的上部孔槽内,实时测量加载的法向接触载荷大小。弯曲疲劳载荷施加部分的构成是:弯曲疲劳载荷由日产岛津EHF-UM100k2-040-0A型电液伺服疲劳试验机9施加。电液伺服疲劳试验机9和力传感器12均与数据采集控制系统连接,由其控制实验条件并采集实验数据。As shown in Figures 1 to 3, it is an embodiment of the present invention, including a sample clamping and fixing part, a normal contact load applying part, a bending fatigue load applying part and a data acquisition control system part, wherein the sample is clamped and fixed Part of the composition is: the base 1 is installed and fixed on the base of the fatigue test bench, and the left end of the sample 2 is fixed to the base through the upper and lower clamping blocks 3 in the square hole on the left side of the base 1 and the fixing screw 4 on it. 1 above. The composition of the normal contact load application part is: the bearing platform 7 is fixed in the long groove in the middle of the base 1 through the fixing screw 2 5 and the fixing plate 6, and its position can be adjusted within a certain distance according to the experimental requirements. The lower micro-movement pad 8 is installed in the middle of the bearing platform 7, and two linear guide rails 17 are installed on both sides. The sample 2 is sandwiched between the upper fretting pad 10 and the lower fretting pad 8 on the moving pad clamping seat 11 . The loading plate 15 is fixed on the top of the linear guide rail 17, and the normal contact load is applied through the loading screw 16 and the steel ball 14. The force sensor 12 is placed in the upper hole of the upper fretting pad holder 11 to measure the normal contact load applied in real time. The composition of the bending fatigue load application part is: the bending fatigue load is applied by the Nissan Shimadzu EHF-UM100k2-040-0A electro-hydraulic servo fatigue testing machine 9 . Both the electro-hydraulic servo fatigue testing machine 9 and the force sensor 12 are connected with the data acquisition control system, which controls the experimental conditions and collects the experimental data.
该装置的使用方法及工作过程为:The use method and working process of this device are:
将基座1固定在疲劳实验台上的合适位置上,然后将安装有下微动垫8和直线导轨17的承载台7固定在基座1中间的长槽内,其在长槽内的位置根据实验条件需要来确定,再然后将试样2左端固定在基座1的左侧方孔内,右端置于下微动垫8之上,随后将安装有上微动垫10的上微动垫夹持座11穿过直线导轨17垂直滑下,使上微动垫10与试样2垂直正交,实现良好的点接触。Fix the base 1 at a suitable position on the fatigue test bench, and then fix the bearing platform 7 with the lower fretting pad 8 and the linear guide rail 17 in the long groove in the middle of the base 1, and its position in the long groove Determined according to the needs of the experimental conditions, then fix the left end of the sample 2 in the left square hole of the base 1, place the right end on the lower fretting pad 8, and then place the upper fretting pad 10 on the The pad clamping seat 11 slides down vertically through the linear guide rail 17, so that the upper fretting pad 10 is perpendicular to the sample 2 and achieves good point contact.
拧动加载螺钉16,所施加的法向接触载荷会通过力传感器12的测量显示在与数据采集控制系统相连的计算机上,当法向接触载荷施加到设定的实验条件时,停止拧动加载螺钉16,然后通过数据采集控制系统来操控电液伺服疲劳试验机9,使试样2按设定的参数振幅、频率等进行弯曲微动疲劳实验。在此过程中,各项实验数据会通过传感器反馈给数据采集控制系统进行分析,绘制出各种参数的变化曲线。Turn the loading screw 16, the applied normal contact load will be displayed on the computer connected to the data acquisition control system through the measurement of the force sensor 12, when the normal contact load is applied to the set experimental conditions, stop the twisting and loading Screw 16, and then control the electro-hydraulic servo fatigue testing machine 9 through the data acquisition control system, so that the sample 2 can be subjected to bending fretting fatigue test according to the set parameters such as amplitude and frequency. During this process, various experimental data will be fed back to the data acquisition and control system for analysis through sensors, and the change curves of various parameters will be drawn.
弯曲微动疲劳S~N曲线Bending fretting fatigue S-N curve
由于弯曲微动疲劳局部接触应力的作用,试样的疲劳强度呈现急剧的减少趋势,如果没有在试样的微动垫位置施加法向载荷,样品在弯曲应力为611.21MPa时经过1.0×106次循环都未断裂,但是当在微动垫位置施加500N(接触应力为368.4MPa)的法向载荷时,弯曲疲劳强度急剧减小为大约240MPa。从图4中可以清晰看到:S~N曲线均呈现“C”型曲线特征,在高弯曲疲劳应力作用下,随着疲劳应力的下降,试样断裂寿命明显下降,在331.0MPa的弯曲应力作用下,弯曲微动疲劳寿命降低到最低值,这个最低值可称作“C”型曲线的“鼻子”。如果弯曲应力继续降低到更低值,弯曲微动疲劳寿命又呈现迅速增加趋势。Due to the local contact stress of bending fretting fatigue, the fatigue strength of the sample shows a sharp decrease trend. If no normal load is applied to the fretting pad position of the sample, the sample passes through 1.0×106 times when the bending stress is 611.21MPa None of the cycles failed, but when a normal load of 500N (contact stress of 368.4MPa) was applied at the fretting pad location, the bending fatigue strength decreased sharply to about 240MPa. It can be clearly seen from Figure 4 that the S-N curves all present the characteristics of a "C" curve. Under the action of high bending fatigue stress, as the fatigue stress decreases, the fracture life of the sample decreases significantly. Under the action of , the bending fretting fatigue life is reduced to the lowest value, which can be called the "nose" of the "C" curve. If the bending stress continues to decrease to a lower value, the bending fretting fatigue life shows a trend of rapid increase again.
一般情况下,在微动磨损研究中发现:不同的测试条件下微动运行存在3个不同的区域,即部分滑移区(Partialslipregime,PSR)、混合区(Mixedfrettingregime,MFR)和滑移区(Slipregime,SR)。根据前人的有关微动疲劳的研究工作,发现一个普遍的变化规律,即随着法向压力、位移幅值的增加,微动疲劳寿命的变化曲线出现一个凹区。实际上,凹区与混合区直接相关,是局部接触疲劳最为强烈的区域。据此,可以推断弯曲微动疲劳S~N曲线呈现“C”型曲线特征是由于微动运行于不同的区域,而通常混合区是一个最危险的区域,微观裂纹在该区域最容易萌生和扩展,因此,“C”型曲线的“鼻子”可以认为是微动运行于混合区的结果。这种与微动磨损现象的一致性,在不同角度反映了局部磨损与局部疲劳,以及局部疲劳与整体疲劳的相互作用关系。当弯曲疲劳应力高于“C”型曲线的“鼻子”时,由于接触区的相对位移较大而进入滑移区;当弯曲疲劳应力低于“鼻子”时,微动相应的运行于部分滑移区。在滑移区,磨损率高于裂纹萌生速率,导致裂纹在形核阶段由于材料磨损而被消除,这样微动疲劳寿命呈现更长的趋势。在部分滑移区,通常情况下接触区呈现轻微的损伤,而中心黏着区几乎没有损伤,微观裂纹被抑制而不易萌生和扩展,使得微动疲劳寿命大大增加。In general, in the study of fretting wear, it is found that there are three different regions in the fretting operation under different test conditions, namely the partial slip region (Partialslipregime, PSR), the mixed region (Mixedfrettingregime, MFR) and the slip region ( Slipregime, SR). According to previous research work on fretting fatigue, a general change law is found, that is, with the increase of normal pressure and displacement amplitude, a concave area appears in the change curve of fretting fatigue life. In fact, the concave area is directly related to the mixed area, which is the most intense area of local contact fatigue. Based on this, it can be inferred that the bending fretting fatigue S-N curve presents a "C"-shaped curve characteristic because the fretting runs in different regions, and usually the mixed region is the most dangerous region, where microscopic cracks are most likely to initiate and Extended, therefore, the "nose" of the "C"-shaped curve can be considered the result of fretting operating in the mixed region. This consistency with the fretting wear phenomenon reflects the interaction between local wear and local fatigue, as well as local fatigue and overall fatigue from different angles. When the bending fatigue stress is higher than the "nose" of the "C" curve, it enters the slip zone due to the relatively large relative displacement of the contact area; when the bending fatigue stress is lower than the "nose", the fretting correspondingly operates in the partial sliding Move area. In the slip zone, the wear rate is higher than the crack initiation rate, resulting in cracks being eliminated due to material wear during the nucleation stage, so that the fretting fatigue life tends to be longer. In the partial slip area, the contact area usually shows slight damage, while the central adhesion area has almost no damage, and the microscopic cracks are suppressed and are not easy to initiate and expand, so that the fretting fatigue life is greatly increased.
综上所述,可以总结为弯曲微动疲劳寿命与接触区的微动运行区域密切相关。当接触界面运行于部分滑移区和滑移区的时候,试样的微动疲劳寿命相对的高于混合区,但在鼻子区域的上方,虽然微动疲劳寿命增加了,但整体疲劳寿命降低的倾向也增加了,换句话说,当试验参数控制在“C”型曲线下方时,试样运行于安全区域,是适合工程应用的范围。In summary, it can be concluded that the bending fretting fatigue life is closely related to the fretting operation area of the contact zone. When the contact interface operates in the partial slip zone and the slip zone, the fretting fatigue life of the sample is relatively higher than that in the mixed zone, but above the nose region, although the fretting fatigue life increases, the overall fatigue life decreases The tendency of is also increased, in other words, when the test parameters are controlled below the "C" curve, the sample runs in a safe area, which is a range suitable for engineering applications.
接触载荷对S-N曲线的影响Influence of Contact Load on S-N Curve
图5显示了7075铝合金弯曲微动疲劳S~N曲线在改变微动垫上的法向载荷(接触应力)而出现的相应变化。在微动垫上的法向载荷为250N时,7075铝合金弯曲微动疲劳强度大约为320MPa,其微动疲劳寿命随着疲劳应力的增加呈现先减小,后反而出现增大的特征,微动疲劳S~N曲线呈现“C”型曲线特征。当法向载荷增加到500N时,疲劳强度急剧减小为约240MPa,微动疲劳S~N曲线同样呈现“C”型曲线特征,在低弯曲疲劳应力作用下,随着疲劳应力的增加,试样断裂寿命明显下降,在331.0MPa弯曲应力作用下,微动疲劳寿命降低到最低值,这个最低值即“C”型曲线的“鼻子”。随着疲劳应力的进一步增加,疲劳寿命由出现增加趋势,如果弯曲应力继续增加到更高值,微动疲劳寿命又呈现减小趋势。当法向载荷为750N时,7075铝合金弯曲微动疲劳强度大约为280MPa,相比500N时反而出现明显上升,而弯曲微动疲劳寿命同样随着疲劳应力的增加而先减小后呈现增大,最后又减小,微动疲劳S~N曲线同样呈现“C”型曲线特征。因此,以上三种载荷下都有“C”型曲线特征,如同前面的解释,这种微动疲劳寿命变化曲线出现的凹区与混合区的存在有关。在相同弯曲疲劳载荷下,随着法向载荷的增加,微动垫与试样间的相对位移是呈现减小趋势的,微动运行区表现为从滑移区朝混合区和部分滑移区方向转变。Figure 5 shows the corresponding changes in the bending fretting fatigue S-N curve of 7075 aluminum alloy when the normal load (contact stress) on the fretting pad is changed. When the normal load on the fretting pad is 250N, the bending fretting fatigue strength of 7075 aluminum alloy is about 320MPa, and its fretting fatigue life decreases firstly with the increase of fatigue stress, and then increases instead. The fatigue S-N curve presents the characteristic of "C" type curve. When the normal load increases to 500N, the fatigue strength decreases sharply to about 240MPa, and the fretting fatigue S-N curve also presents a "C"-shaped curve feature. Under the action of low bending fatigue stress, with the increase of fatigue stress, the test The fracture life of the samples decreased significantly. Under the bending stress of 331.0MPa, the fretting fatigue life decreased to the lowest value, which is the "nose" of the "C" curve. With the further increase of the fatigue stress, the fatigue life shows an increasing trend, and if the bending stress continues to increase to a higher value, the fretting fatigue life shows a decreasing trend. When the normal load is 750N, the bending fretting fatigue strength of 7075 aluminum alloy is about 280MPa, which is significantly increased compared with 500N, and the bending fretting fatigue life also decreases first and then increases with the increase of fatigue stress , and finally decreased, the fretting fatigue S-N curve also presents the characteristic of "C" type curve. Therefore, under the above three loads, there are "C" curve characteristics. As explained above, the concave area of the fretting fatigue life change curve is related to the existence of the mixed area. Under the same bending fatigue load, as the normal load increases, the relative displacement between the fretting pad and the sample shows a decreasing trend, and the fretting operation area is from the slip zone to the mixed zone and partial slip zone change of direction.
接触载荷对弯曲微动疲劳寿命的影响Effect of Contact Load on Bending Fretting Fatigue Life
如图6所示,在最大弯曲疲劳载荷为6.0kN时,随着接触载荷的增加,微动疲劳寿命呈现先减小后增大的趋势发展。这个结果进一步表明微动混合区的存在,即随着接触载荷的增加,微动运行区域从滑移区朝混合区和部分滑移区转移,这样根据微动损伤区的损伤特性:完全滑移区磨损比较严重,几乎不会发现裂纹;而混合区微观裂纹是其主要损伤特征,磨损相对轻微;在部分滑移区,磨损最轻微,一般不曾见微观裂纹。与此同时,随着微动垫接触载荷的增加,局部的接触损伤是一个增加的趋势。综合以上的分析情况可知,完全滑移区尽管有磨损但是其接触应力较小从而寿命最长;混合区有微观裂纹导致微动疲劳寿命最短;部分滑移区尽管微动位移较小,但是接触应力较大从而微动疲劳寿命相对比混合区大而比部分滑移区小。As shown in Figure 6, when the maximum bending fatigue load is 6.0kN, as the contact load increases, the fretting fatigue life presents a trend of first decreasing and then increasing. This result further indicates the existence of the fretting mixed zone, that is, as the contact load increases, the fretting operation area shifts from the slip zone to the mixed zone and the partial slip zone, so that according to the damage characteristics of the fretting damage zone: complete slip The wear in the slip zone is relatively serious, and almost no cracks can be found; the microscopic cracks in the mixed zone are the main damage characteristics, and the wear is relatively slight; in the partial slip zone, the wear is the slightest, and generally no microscopic cracks are seen. At the same time, with the increase of the contact load of the fretting pad, the local contact damage is an increasing trend. Based on the above analysis, it can be seen that although there is wear in the complete slip area, the contact stress is small and the service life is the longest; the microscopic cracks in the mixed area lead to the shortest fretting fatigue life; although the partial slip area has small fretting displacement, the contact stress is the longest. The stress is larger so that the fretting fatigue life is relatively larger than that in the mixed region and smaller than that in the partial slip region.
本发明的实验装置与实验方法,可以方便地、精确地按设定条件进行各种不同工况与规格材料的弯曲微动疲劳实验,较真实地模拟出构件在交变载荷作用下的弯曲微动疲劳损伤,控制与测试精度高,实验结果更准确可靠,实验数据重现性好。The experimental device and experimental method of the present invention can conveniently and accurately carry out bending fretting fatigue experiments of various working conditions and specifications of materials according to the set conditions, and more realistically simulate the bending fretting fatigue of components under alternating loads. Dynamic fatigue damage, high control and testing precision, more accurate and reliable experimental results, and good reproducibility of experimental data.
以上所述仅为本发明的较佳实施例而已,并不用以限制本发明,凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included in the scope of the present invention. within the scope of protection.
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CN113720590A (en) * | 2021-07-30 | 2021-11-30 | 中国航发沈阳发动机研究所 | Fretting fatigue simulation test device and method |
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