CN114397205A - A kind of impact force testing device and method - Google Patents
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Abstract
Description
技术领域technical field
本发明涉及冲击测试技术领域,尤其涉及一种冲击力测试装置及方法。The invention relates to the technical field of impact testing, in particular to an impact force testing device and method.
背景技术Background technique
数显悬臂梁、简支梁主要用于硬质热塑性模塑和挤塑材料,硬质热固性模塑材料以及纤维增强的热固性和热塑性复合材料等非金属材料冲击韧性的测定。由机身、冲击摆锤、试样支座、测量装置、操纵机构等部分组成。Digital cantilever beams and simply supported beams are mainly used for the determination of the impact toughness of non-metallic materials such as rigid thermoplastic molding and extrusion materials, rigid thermosetting molding materials, and fiber-reinforced thermosetting and thermoplastic composite materials. It consists of fuselage, impact pendulum, sample support, measuring device, operating mechanism and other parts.
这种技术的缺点在于:一般现有仪器适用于只用冲击强度表征冲击行为,仅获得冲击强度或冲击断裂能;并且要求冲击试验机的势能要与待测试样的断裂能近似匹配。最终手动查表或数显只能得到一个表示材料断裂韧性的结果值,无法获得全过程中的载荷-挠度、冲击能量-时间等关键信息参数的同时,造成原位获取材料在从接触载荷-产生弹性形变-塑性损伤-完全断裂过程的应力-应变、挠度-载荷等关键数据与信息缺失。传统的冲击测试断裂方法,更是无法高精度获得冲击过程中微裂纹萌发、裂纹延伸、分层和贯穿以及纤维拉断、基体压缩变形、界面脱粘滑移等重要变化信息,亦不能在细观图像上和动态录像上对材料的失效机制展开全面、客观和深入的分析与研究。The disadvantage of this technique is that: the existing instruments are generally suitable for characterizing impact behavior with impact strength only, and only impact strength or impact fracture energy are obtained; and the potential energy of the impact testing machine is required to approximately match the fracture energy of the sample to be tested. In the end, the manual look-up table or digital display can only obtain a result value representing the fracture toughness of the material, and it is impossible to obtain the key information parameters such as load-deflection, impact energy-time and other key information parameters in the whole process. Key data and information such as stress-strain, deflection-load, etc., which produce elastic deformation-plastic damage-complete fracture process, are missing. The traditional impact test fracture method cannot obtain the important change information such as microcrack initiation, crack extension, delamination and penetration, fiber breaking, matrix compression deformation, interface debonding slip and so on during the impact process with high precision, nor can it be obtained in the fine Conduct a comprehensive, objective and in-depth analysis and research on the failure mechanism of the material on the viewing image and dynamic video.
因此,亟需一种冲击力测试装置及方法,以解决上述问题。Therefore, there is an urgent need for an impact force testing device and method to solve the above problems.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提出一种冲击力测试装置及方法,能够提高对试样的冲击力测试的采集参数范围,便于实现对试样的失效机制展开全面、客观和深入的分析与研究。The purpose of the present invention is to provide an impact force testing device and method, which can improve the collection parameter range of the impact force test on the sample, and facilitate the comprehensive, objective and in-depth analysis and research on the failure mechanism of the sample.
为实现上述技术效果,本发明的技术方案如下:For realizing above-mentioned technical effect, technical scheme of the present invention is as follows:
一种冲击力测试装置,包括:机架;安装组件,所述安装组件设在所述机架上,所述安装组件用于安装试样;冲击件,所述冲击件可转动地设在所述机架上;第一检测件,所述第一检测件设在所述冲击件上,所述第一检测件用于获取所述冲击件施加于所述试样上的作用力;第二检测件,所述第二检测件与所述冲击件连接,所述第二检测件用于获取所述冲击件的转速;图像采集组件,所述图像采集组件设在所述机架上,所述图像采集组件能够同时获取所述试样的图像信息。An impact force testing device, comprising: a frame; an installation assembly, the installation assembly is arranged on the frame, the installation assembly is used for installing a sample; an impact piece, the impact piece is rotatably arranged on the on the frame; a first detection piece, the first detection piece is arranged on the impact piece, and the first detection piece is used to obtain the force exerted by the impact piece on the sample; the second detection piece A detection piece, the second detection piece is connected with the impact piece, and the second detection piece is used to obtain the rotational speed of the impact piece; an image acquisition component, the image acquisition component is arranged on the frame, and the The image acquisition component can simultaneously acquire image information of the sample.
进一步地,所述冲击件的第一侧朝向所述安装组件设置,所述冲击件的第二侧背离所述安装组件设置,所述第一检测件设在所述冲击件的第二侧。Further, the first side of the impact piece is disposed toward the mounting assembly, the second side of the impact piece is disposed away from the mounting assembly, and the first detection piece is disposed on the second side of the impact piece.
进一步地,所述安装组件包括两个间隔设置的安装件,两个所述安装件上分别设有多个安装部,两个所述安装件上的多个所述安装部分别一一对应设置。Further, the mounting assembly includes two mounting parts arranged at intervals, a plurality of mounting parts are respectively provided on the two mounting parts, and the plurality of the mounting parts on the two mounting parts are respectively arranged in a one-to-one correspondence .
进一步地,所述安装件包括安装架和锁紧件,所述安装部沿两个所述安装件的分布方向可活动地设在所述安装架上,所述锁紧件用于将所述安装部锁紧在所述安装架上。Further, the mounting member includes a mounting frame and a locking member, the mounting portion is movably arranged on the mounting frame along the distribution direction of the two mounting members, and the locking member is used to lock the mounting member. The mounting portion is locked on the mounting bracket.
进一步地,所述试样的第一侧朝向所述冲击件设置,所述试样的第二侧背离所述冲击件设置;所述图像采集组件包括:第一采集件,所述第一采集件设在所述机架上并用于获取所述试样的第一侧的图像信息;第二采集件,所述第二采集件设在所述机架上并用于获取所述试样的第二侧的图像信息;第三采集件,所述第三采集件设在所述机架上并能够获取所述试样的底侧的图像信息。Further, the first side of the sample is disposed toward the impact member, and the second side of the sample is disposed away from the impact member; the image acquisition assembly includes: a first acquisition member, the first acquisition A second collection piece is arranged on the rack and used to acquire the image information of the first side of the sample; the second collection piece is arranged on the rack and used to acquire the first side of the sample. The image information of the two sides; the third collecting part, the third collecting part is arranged on the rack and can acquire the image information of the bottom side of the sample.
进一步地,所述图像采集组件还包括反射件,所述反射件设在所述机架上并位于所述试样的下方,所述反射件能够将所述试样的底侧的图像信息反射至所述第三采集件。Further, the image acquisition assembly further includes a reflective member, the reflective member is arranged on the rack and located below the sample, and the reflective member can reflect the image information on the bottom side of the sample to the third collection piece.
进一步地,所述冲击力测试装置还包括补光组件,所述补光组件用于向所述试样照射光线。Further, the impact force testing device further includes a supplementary light component, and the supplementary light component is used for irradiating light to the sample.
进一步地,所述机架包括:本体,所述本体限定有容纳腔,所述冲击件和所述安装组件均设置于所述容纳腔内;防护门,所述防护门可活动地设在所述容纳腔的敞开端。Further, the rack includes: a main body, the main body defines an accommodating cavity, and the impact piece and the mounting assembly are both arranged in the accommodating cavity; a protective door, the protective door is movably arranged in the accommodating cavity the open end of the accommodating cavity.
进一步地,所述冲击件包括:驱动件,所述驱动件设在所述机架上;摆动杆,所述摆动杆的一端连接于所述驱动件的输出端,所述驱动件能够带动所述摆动杆转动并使所述摆动杆与水平方向的夹角保持固定;冲击刃,所述冲击刃连接于所述摆动杆的另一端;电磁阀,所述电磁阀用于控制所述驱动件释放所述摆动杆以使所述摆动杆带动所述冲击刃冲击所述试样。Further, the impact member includes: a driving member, which is arranged on the frame; a swing rod, one end of the swing rod is connected to the output end of the driving member, and the driving member can drive the The swing rod rotates and keeps the angle between the swing rod and the horizontal direction fixed; the impact blade is connected to the other end of the swing rod; the solenoid valve is used to control the driving member The swing lever is released so that the swing lever drives the impact blade to impact the specimen.
一种冲击力测试方法,基于前文所述的冲击力测试装置,包括:第一检测件、第二检测件和图像采集组件分别获取工作信号并分别开始采集作用力、转速和图像信息;冲击件获取工作信号并转动冲击试样;获取冲击件受到的冲击能量与时间的关系曲线;第一检测件、第二检测件和图像采集组件在预设时间后分别停止采集作用力、转速和图像信息。An impact force testing method, based on the aforementioned impact force testing device, includes: a first detection part, a second detection part and an image acquisition component respectively acquire working signals and start to collect force, rotational speed and image information respectively; Obtain the working signal and rotate the impact sample; obtain the relationship curve between the impact energy and time received by the impact piece; the first detection piece, the second detection piece and the image acquisition component respectively stop collecting the force, speed and image information after a preset time .
本发明的有益效果为:The beneficial effects of the present invention are:
安装组件能够稳定可靠地承载试样,使得冲击件在冲击试样时能够保持位置不变,以便于第一检测件、第二检测件和图像采集组件采集到试样的可靠信息。第一检测件能够获取冲击件施加于试样上的作用力,第二检测件能够获取冲击件的转速,图像采集组件能够同时获取试样不同方位的图像信息。由此,在整个冲击过程中,通过第一检测件和第二检测件所记录的作用力和转速以及冲击件、试样的自身参数,能够较为可靠地计算出试样受到的挠度、力值、应力、应变等参数的变化,从而记录下整个冲击过程中挠度-力值、应力-应变或力-时间的曲线;同时,图像采集组件又能获得在整个冲击过程中试样的形变或断裂形貌的照片,并能够获取试样在受到冲击时各个侧面的断裂特征,例如微裂纹萌发、裂纹延伸、分层和贯穿以及纤维拉断、基体压缩变形、界面脱粘滑移等重要变化信息,再例如侧向冲击、贯层冲击、垂直方向和平行冲击的断裂特征。由此,通过获取的冲击挠度-载荷曲线的变化,再结合图像采集组件所采集的同步断裂形貌特征,从而能够更加客观全面地分析出试样的断裂方式和断裂特征,例如快速判断韧性断裂、脆性断裂和碎性断裂。The mounting assembly can carry the sample stably and reliably, so that the impact member can keep its position unchanged when impacting the sample, so that the first detection member, the second detection member and the image acquisition assembly can collect reliable information of the sample. The first detection part can acquire the force exerted by the impact part on the sample, the second detection part can acquire the rotational speed of the impact part, and the image acquisition component can simultaneously acquire image information of the sample in different orientations. Therefore, in the whole impact process, the deflection and force value of the sample can be calculated more reliably through the force and rotational speed recorded by the first detection piece and the second detection piece, as well as the parameters of the impact piece and the sample itself. , stress, strain and other parameters, so as to record the deflection-force value, stress-strain or force-time curve during the entire impact process; at the same time, the image acquisition component can obtain the deformation or fracture of the sample during the entire impact process. Photographs of the morphology, and can obtain the fracture characteristics of each side of the sample when it is impacted, such as microcrack initiation, crack extension, delamination and penetration, as well as fiber breaking, matrix compressive deformation, interface debonding slip and other important change information , another example is the fracture characteristics of lateral impact, through-layer impact, vertical direction and parallel impact. As a result, the change of the obtained impact deflection-load curve, combined with the synchronous fracture morphology characteristics collected by the image acquisition component, can more objectively and comprehensively analyze the fracture mode and fracture characteristics of the sample, such as rapid judgment of ductile fracture. , brittle fracture and crush fracture.
本发明的附加方面和优点将在下面的描述中部分给出,部分将从下面的描述中变得明显,或通过本发明的实践了解到。Additional aspects and advantages of the present invention will be set forth, in part, from the following description, and in part will be apparent from the following description, or may be learned by practice of the invention.
附图说明Description of drawings
图1是本发明具体实施方式提供的冲击力测试装置的结构示意图;1 is a schematic structural diagram of an impact force testing device provided by a specific embodiment of the present invention;
图2是本发明具体实施方式提供的冲击力测试装置的部分分解结构示意图;2 is a schematic diagram of a partially exploded structure of an impact force testing device provided by a specific embodiment of the present invention;
图3是本发明具体实施方式提供的机架的部分结构示意图;3 is a schematic diagram of a partial structure of a rack provided by a specific embodiment of the present invention;
图4是本发明具体实施方式提供的安装组件的局部结构示意图;FIG. 4 is a schematic diagram of a partial structure of a mounting assembly provided by a specific embodiment of the present invention;
图5是本发明具体实施方式提供的冲击力测试方法的试验结果图之一;5 is one of the test result diagrams of the impact force testing method provided by the specific embodiment of the present invention;
图6是本发明具体实施方式提供的冲击力测试方法的试验结果图之二;6 is the second test result diagram of the impact force test method provided by the specific embodiment of the present invention;
图7是本发明具体实施方式提供的冲击力测试方法的试验结果图之三。FIG. 7 is the third test result diagram of the impact force testing method provided by the specific embodiment of the present invention.
附图标记reference number
1、机架;11、本体;12、防护门;13、立柱;14、采集支撑件;15、支脚;2、安装组件;21、安装件;211、安装架;212、锁紧件;22、安装部;221、安装槽;3、冲击件;31、驱动件;32、摆动杆;33、冲击刃;34、电磁阀;4、第一检测件;5、图像采集组件;51、第一采集件;52、第二采集件;53、第三采集件;54、反射件;6、补光灯。1. Rack; 11. Main body; 12. Protective door; 13. Upright column; 14. Collection support; 15. Support foot; 2. Mounting assembly; 21. Mounting piece; 211. Mounting frame; 212. Locking piece; 22 , installation part; 221, installation groove; 3, impact piece; 31, drive piece; 32, swing rod; 33, impact blade; 34, solenoid valve; 4, first detection piece; 5, image acquisition component; 51, first A collection piece; 52, a second collection piece; 53, a third collection piece; 54, a reflector; 6, a fill light.
具体实施方式Detailed ways
为使本发明解决的技术问题、采用的技术方案和达到的技术效果更加清楚,下面结合附图并通过具体实施方式来进一步说明本发明的技术方案。In order to make the technical problems solved by the present invention, the technical solutions adopted and the technical effects achieved more clearly, the technical solutions of the present invention are further described below with reference to the accompanying drawings and through specific embodiments.
在本发明的描述中,除非另有明确的规定和限定,术语“相连”、“连接”、“固定”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或成一体;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通或两个元件的相互作用关系。对于本领域的普通技术人员而言,可以具体情况理解上述术语在本发明中的具体含义。In the description of the present invention, unless otherwise expressly specified and limited, the terms "connected", "connected" and "fixed" should be understood in a broad sense, for example, it may be a fixed connection, a detachable connection, or an integrated ; It can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, and it can be the internal connection of two elements or the interaction relationship between the two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood in specific situations.
在本发明中,除非另有明确的规定和限定,第一特征在第二特征之“上”或之“下”可以包括第一和第二特征直接接触,也可以包括第一和第二特征不是直接接触而是通过它们之间的另外的特征接触。而且,第一特征在第二特征“之上”、“上方”和“上面”包括第一特征在第二特征正上方和斜上方,或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”包括第一特征在第二特征正下方和斜下方,或仅仅表示第一特征水平高度小于第二特征。In the present invention, unless otherwise expressly specified and limited, a first feature "on" or "under" a second feature may include the first and second features in direct contact, or may include the first and second features Not directly but through additional features between them. Also, the first feature being "above", "over" and "above" the second feature includes the first feature being directly above and obliquely above the second feature, or simply means that the first feature is level higher than the second feature. The first feature is "below", "below" and "below" the second feature includes the first feature being directly below and diagonally below the second feature, or simply means that the first feature has a lower level than the second feature.
需要理解的是,术语“中心”、“纵向”、“横向”、“长度”、“宽度”、“厚度”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”、“顺时针”、“逆时针”、“轴向”、“径向”、“周向”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。在本发明的描述中,除非另有说明,“多个”的含义是两个或两个以上。此外,术语“第一”、“第二”仅仅用于在描述上加以区分,并没有特殊的含义。It is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "top", "bottom", "front", "rear", "left", "Right", "Vertical", "Horizontal", "Top", "Bottom", "Inner", "Outer", "Clockwise", "Counterclockwise", "Axial", "Radial", " The orientation or positional relationship indicated such as "circumferential direction" is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the indicated device or element must have a specific orientation, It is constructed and operated in a particular orientation and is therefore not to be construed as a limitation of the present invention. In the description of the present invention, unless otherwise specified, "plurality" means two or more. In addition, the terms "first" and "second" are only used for distinction in description, and have no special meaning.
下面参考图1-图4描述本发明实施例的冲击力测试装置的具体结构。The specific structure of the impact force testing device according to the embodiment of the present invention will be described below with reference to FIG. 1 to FIG. 4 .
如图1-图4所示,图1公开了一种冲击力测试装置,其包括机架1、安装组件2、冲击件3、第一检测件4、第二检测件和图像采集组件5。安装组件2设在机架1上,安装组件2用于安装试样。冲击件3可转动地设在机架1上。第一检测件4设在冲击件3上,第一检测件4用于获取冲击件3施加于试样上的作用力。第二检测件与冲击件3连接,第二检测件用于获取冲击件3的转速。图像采集组件5设在机架1上,图像采集组件5能够同时获取试样的的图像信息。As shown in FIGS. 1-4 , FIG. 1 discloses an impact force testing device, which includes a frame 1 , a mounting
可以理解的是,安装组件2能够稳定可靠地承载试样,使得冲击件3在冲击试样时能够保持位置不变,以便于第一检测件4、第二检测件和图像采集组件5采集到试样的可靠信息。第一检测件4能够获取冲击件3施加于试样上的作用力,第二检测件能够获取冲击件3的转速,图像采集组件5能够同时获取试样不同方位的图像信息。由此,在整个冲击过程中,通过第一检测件4和第二检测件所记录的作用力和转速以及冲击件3、试样的自身参数,能够较为可靠地计算出试样受到的挠度、力值、应力、应变等参数的变化,从而记录下整个冲击过程中挠度-力值、应力-应变或力-时间的曲线;同时,图像采集组件5又能获得在整个冲击过程中试样的形变或断裂形貌的照片,并能够获取试样在受到冲击时各个侧面的断裂特征,例如微裂纹萌发、裂纹延伸、分层和贯穿以及纤维拉断、基体压缩变形、界面脱粘滑移等重要变化信息,再例如侧向冲击、贯层冲击、垂直方向和平行冲击的断裂特征。由此,通过获取的冲击挠度-载荷曲线的变化,再结合图像采集组件5所采集的同步断裂形貌特征,从而能够更加客观全面地分析出试样的断裂方式和断裂特征,例如快速判断韧性断裂、脆性断裂和碎性断裂。It can be understood that the mounting
根据本实施例的冲击力测试装置,能够较好地提高对试样的冲击力测试的采集参数范围,在细观图像和动态录像上获取试样的各个冲击面的重要变化信息,便于实现对试样的失效机制展开全面、客观和深入的分析与研究。According to the impact force testing device of this embodiment, the acquisition parameter range of the impact force test on the sample can be better improved, and the important change information of each impact surface of the sample can be obtained on the mesoscopic image and dynamic video recording, which is convenient to realize the impact force test of the sample. A comprehensive, objective and in-depth analysis and study of the failure mechanism of the sample is carried out.
在一些实施例中,如图1所示,冲击件3的第一侧朝向安装组件2设置,冲击件3的第二侧背离安装组件2设置,第一检测件4设在冲击件3的第二侧。In some embodiments, as shown in FIG. 1 , the first side of the
可以理解的是,如将第一检测件4设置于冲击件3的第一侧,当冲击件3冲击试样时,第一检测件4虽然能够获取到试样受到的冲击力,但是同时也有可能对第一检测件4造成损坏,同时其获取的冲击力的误差也较大。在本实施例中,设置于第二侧的第一检测件4能够通过冲击件3的反作用力获取冲击力作用到试样上的冲击力,从而能够保证第一检测件4检测到冲击力的准确性,又能防止第一检测件4在检测过程中损坏的问题。It can be understood that, if the
具体地,在本实施例中,第一检测件4可以设置为力传感器。Specifically, in this embodiment, the
在一些实施例中,如图1和图2所示,安装组件2包括两个间隔设置的安装件21,两个安装件21上分别设有多个安装部22,两个安装件21上的多个安装部22分别一一对应设置。In some embodiments, as shown in FIG. 1 and FIG. 2 , the mounting
可以理解的是,试样的两端能够分别安装在一个安装件21上的一个安装部22上,从而实现试样在安装组件2上的稳固安装,同时安装部22设有多个,多个安装部22能够实现试样在安装组件2上的不同位置的安装,以提高测试的适用范围。此外,由于两个安装件21间隔设置,使得图像采集组件5能够采集到位于两个安装件21之间的试样的图像信息,便于实现试样的图像信息采集。It can be understood that the two ends of the sample can be respectively installed on one mounting
具体地,每个安装件21上的多个安装部22在竖直方向上间隔设置。Specifically, the plurality of mounting
具体地,如图4所述,安装部22的侧面开设有安装槽221,以便于安装固定试样的端部,当冲击件3冲击试样时,试样的上侧、下侧以及背离冲击件3的一侧也能在安装槽221的限位下,从而防止试样在冲击作用下脱落。Specifically, as shown in FIG. 4 , a mounting
在一些实施例中,如图1和图2所示,安装件21包括安装架211和锁紧件212,安装部22沿两个安装件21的分布方向可活动地设在安装架211上,锁紧件212用于将安装部22锁紧在安装架211上。In some embodiments, as shown in FIGS. 1 and 2 , the mounting
可以理解的是,由于安装部22能够活动设置,从而使得不同长度的试样均能够安装在安装组件2上,且锁紧件212能够将安装部22锁紧在安装架211上,以保证在实现长度可调节时又能保证试样的可靠安装。It can be understood that since the mounting
具体地,锁紧件212包括锁紧扳手,锁紧扳手螺纹连接于安装架211和安装部22,以起到锁紧效果。Specifically, the locking
在一些实施例中,如图1和图2所示,试样的第一侧朝向冲击件3设置,试样的第二侧背离冲击件3设置。图像采集组件5包括第一采集件51、第二采集件52和第三采集件53。第一采集件51设在机架1上并用于获取试样的第一侧的图像信息。第二采集件52设在机架1上并用于获取试样的第二侧的图像信息。第三采集件53设在机架1上并能够获取试样的底侧的图像信息。In some embodiments, as shown in FIGS. 1 and 2 , the first side of the sample is positioned toward the
可以理解的是,通过第一采集件51、第二采集件52和第三采集件53的设置,即可实时获取试样在冲击件3的入射面、出射面和断裂面等三个典型位置的形变的高清视频图像。It can be understood that, by setting the first collecting
具体地,在本实施例中,第一采集件51、第二采集件52和第三采集件53均能够设置为CCD相机或高速摄像头等。Specifically, in this embodiment, the
具体地,如图1和图2所示,机架1还包括采集支撑件14,采集支撑件14用于支撑第一采集件51、第二采集件52和第三采集件53。Specifically, as shown in FIG. 1 and FIG. 2 , the rack 1 further includes a
在一些实施例中,如图1和图2所示,图像采集组件5还包括反射件54,反射件54设在机架1上并位于试样的下方,反射件54能够将试样的底侧的图像信息反射至第三采集件53。In some embodiments, as shown in FIG. 1 and FIG. 2 , the image acquisition assembly 5 further includes a
可以理解的是,通过反射件54的设置,使得第三采集件53无须设置于试样的下方就能获取试样的底侧的图像信息,从而有效减少第三采集件53在试样下方的占用空间,提高整个装置的集成度,同时也能够防止冲击件3意外破坏第三采集件53的问题,延长装置的使用寿命。It can be understood that, through the setting of the
具体地,反射件54包括能够实现90°折射的高清棱镜,例如45°棱镜。Specifically, the
在一些实施例中,如图1和图2所示,冲击力测试装置还包括补光组件,补光组件用于向试样照射光线。In some embodiments, as shown in FIG. 1 and FIG. 2 , the impact force testing device further includes a supplementary light component, and the supplementary light component is used for irradiating light to the sample.
可以理解的是,补光组件能够提供较佳的图像采集环境,从而有效提高图像采集组件5采集到试样的图像的清晰程度,便于对试样进行数据分析。It can be understood that the supplementary light component can provide a better image acquisition environment, thereby effectively improving the clarity of the image of the sample collected by the image acquisition component 5 and facilitating the data analysis of the sample.
具体地,如图2所示,补光组件包括多个补光灯6,多个补光灯6根据试样的实际需求环设于试样的周围。Specifically, as shown in FIG. 2 , the supplementary light assembly includes a plurality of
在一些实施例中,如图1和图3所示,机架1包括本体11和防护门12。本体11限定有容纳腔,冲击件3和安装组件2均设置于容纳腔内。防护门12可活动地设在容纳腔的敞开端。In some embodiments, as shown in FIGS. 1 and 3 , the rack 1 includes a
可以理解的是,防护门12能够起到可靠的防护效果,从而较好地保证冲击力试验的安全性。It can be understood that the
具体地,机架1还包括支脚15,支脚15设在本体11的底壁上。Specifically, the rack 1 further includes
在一些实施例中,如图2所示,冲击件3包括驱动件31、摆动杆32、冲击刃33和电磁阀34。驱动件31设在机架1上。摆动杆32的一端连接于驱动件31的输出端,驱动件31能够带动摆动杆32转动并使摆动杆32与水平方向的夹角保持固定。冲击刃33连接于摆动杆32的另一端。电磁阀34用于控制驱动件31释放摆动杆32以使摆动杆32带动冲击刃33冲击试样。In some embodiments, as shown in FIG. 2 , the
可以理解的是,通过电磁阀34的设置,能够较好地实现对驱动件31的控制,并能够使驱动件31带动摆动杆32保持在预设角度,从而实现冲击刃33在不同角度的条件下落下,并完成对试样的冲击。It can be understood that the setting of the
具体地,如图1和图3所示,机架1还包括立柱13,驱动件31和电磁阀34均设置于立柱13上。Specifically, as shown in FIG. 1 and FIG. 3 , the rack 1 further includes a
在一些具体的实施例中,第二检测件为光电编码器。光电编码器连接于驱动件31,以获取驱动件31的输出转速,进而获取摆动杆32和冲击刃33的转速。In some specific embodiments, the second detection element is a photoelectric encoder. The photoelectric encoder is connected to the driving
本发明还公开了一种冲击力测试方法,基于前文所述的冲击力测试装置,包括:第一检测件4、第二检测件和图像采集组件5分别获取工作信号并分别开始采集作用力、转速和图像信息;冲击件3获取工作信号并转动冲击试样;获取冲击件3受到的冲击能量与时间的关系曲线;第一检测件4、第二检测件和图像采集组件5在预设时间后分别停止采集作用力、转速和图像信息。The present invention also discloses an impact force testing method, which is based on the aforementioned impact force testing device, comprising: the
根据本发明实施例的冲击力测试方法,由于具有前文所述的冲击力测试装置,能够较好地提高对试样的冲击力测试的采集参数范围,在细观图像和动态录像上获取试样的各个冲击面的重要变化信息,便于实现对试样的失效机制展开全面、客观和深入的分析与研究。According to the impact force testing method of the embodiment of the present invention, due to the impact force testing device described above, the acquisition parameter range of the impact force test on the sample can be better improved, and the sample can be obtained on the mesoscopic image and dynamic video recording. The important change information of each impact surface is easy to carry out a comprehensive, objective and in-depth analysis and research on the failure mechanism of the sample.
具体地,采用前文所述的冲击力测试装置的冲击力测试方法包括:Specifically, the impact force testing method using the aforementioned impact force testing device includes:
在人机交互界面点击软件开始按钮,软件发出信号继电器。继电器发出同步工作信号,使图像采集组件5、第一检测件4和第二检测件同时工作采集数据。图像采集组件5实时获取冲击时试样的撞击形变的视频图像。高速信号采集器开始采集第一检测件4和第二检测件的信号。冲击件3下摆并冲击试样。Click the software start button on the man-machine interface, and the software sends a signal relay. The relay sends out a synchronous working signal, so that the image acquisition component 5, the
利用光电编码器获取冲击速度,利用力传感器获取冲击力。绘制出力与时间的曲线图,可以通过下面公式一对力-时间曲线二次积分计算得出挠度,绘制出力-挠度的曲线。Use the photoelectric encoder to obtain the impact speed, and use the force sensor to obtain the impact force. To draw the curve graph of force and time, the deflection can be calculated by the quadratic integral of a pair of force-time curves by the following formula, and the curve of force-deflection can be drawn.
具体地,冲击件3的挠度根据公式一:计算而得,其中,t为冲击后用于计算挠度的时间,单位为秒(s);s(t)为冲击后在t时试样的挠度,单位为米(m);ν0为冲击速度,单位为米每秒(m/s);LP为冲击件3的摆长,单位为米(m);MH为冲击件3的水平力矩,单位为牛顿米(N·s);F(t)为冲击后在t时测得的力,单位为牛顿(N);mc为载能体的质量,单位为千克(kg);g为当地的重力加速度,单位为米每二次方秒(m/s2)。Specifically, the deflection of the
获取试样的力-挠度曲线后,通过公式二即可计算在达到一定挠度所消耗的能力,最后根据试样的尺寸获取试样的冲击能量,Wj为规定挠度下的能量,单位为焦耳(J);sj为力-挠度曲线上的某个点;s为挠度,单位为米(m);F为力,单位为牛顿(N)。After obtaining the force-deflection curve of the specimen,
数据采集1秒后停止采集。Data collection stops after 1 second.
应用软件导入数据和视频图片。由于图像采集组件5、第一检测件4和第二检测件均为同步采集,其数据起始点是一致的,曲线和视频图片都是带有时间标记。软件通过第一采集件51的曲线波形找到撞击初始时间点,然后自动匹配第二采集件52的冲击力曲线和撞击视频图像,使曲线上的特征点和图像一一对应。人工可以进行微调干预,便于更好地分析材料的脆性和韧性。The application software imports data and video pictures. Since the image acquisition component 5, the
具体地,在本实施例中,冲击速度为2.9~3.8m/s,冲击件3的仰角为150°,冲击能量为1J~22.5J,冲击件3的中心与冲击点距离为230mm或395mm;第一检测件4和第二检测件的精度均为0.1%,图像采集组件5的第一采集件51、第二采集件52和第三采集件53的型号为MIKROTRON Gmbh所生产的4FIBER Camera,其拍摄速度为3000帧/s,分辨率为896×328。Specifically, in this embodiment, the impact speed is 2.9-3.8m/s, the elevation angle of the
如图5-图7所示,根据本实施例的冲击力测试方法的一个具体实施过程及结论如下:As shown in Figures 5-7, a specific implementation process and conclusion of the impact force testing method according to the present embodiment are as follows:
图5(b),5(c)分别为竹束单板层积复合材料(IBLVL)和重组竹(RB)的冲击破坏模式。冲击载荷下,IBLVL表现出典型的继层积剪切后的拉伸破坏模式,裂纹呈“Z”字形穿层扩展。而RB主要破环模式为多层的剪切破环,其裂纹也呈现明显的分层扩展。Figures 5(b) and 5(c) show the impact failure modes of bamboo bundle veneer laminate (IBLVL) and reconstituted bamboo (RB), respectively. Under impact load, IBLVL exhibits a typical tensile failure mode after lamination shearing, and the crack propagates through the layer in a "Z" shape. The main rupture mode of RB is multi-layer shear rupture, and its cracks also show obvious delamination propagation.
图5(d)为二者的断裂能-时间曲线,两条曲线均显示达到最大断裂能前的线弹性和弹塑性变形行为。IBLVL的冲击断裂时间为10.85ms,较RB(6.32ms)延长了71.7%,表明IBLVL比RB有较多的冲击持续时间和更多的能量吸收。IBLVL断裂能和冲击韧性分别为90.5J和13.8(J/cm2),较RB(6.07J/cm2)分别提高了109%和127%,如图5(e)和5(f)所示。Figure 5(d) shows the fracture energy-time curves of the two, both of which show the linear elastic and elastoplastic deformation behaviors before reaching the maximum fracture energy. The impact rupture time of IBLVL is 10.85ms, which is 71.7% longer than that of RB (6.32ms), indicating that IBLVL has more impact duration and more energy absorption than RB. The fracture energy and impact toughness of IBLVL are 90.5J and 13.8 (J/cm2), respectively, which are 109% and 127% higher than RB (6.07J/cm2), respectively, as shown in Figures 5(e) and 5(f).
图6和图7分别展示了动态冲击作用下(冲击速度2.9m/s),IBLVL和RB典型的动态变形和失效过程。整个变形过程可以分为三个典型阶段:1)由一端中心局部冲击形成的弯曲荷载向另一端传递;2)材料在冲击/弯曲下开始发生结构整体变形;3)试件缓冲破坏失效。Figures 6 and 7 show the typical dynamic deformation and failure processes of IBLVL and RB under dynamic impact (impact velocity 2.9 m/s), respectively. The whole deformation process can be divided into three typical stages: 1) The bending load formed by the local impact in the center of one end is transferred to the other end; 2) The material begins to deform as a whole under the impact/bending; 3) The buffer failure of the specimen fails.
1)0ms时,冲击件3冲头与试样刚接触。1.32ms时,二者均有不同程度的破环,细小裂纹和楔形豁口分别在IBLVL和RB试样的冲击受拉侧最外端呈零星状萌生和扩展。2)2.64ms,两种材料的变形不断增大,裂纹向芯层扩展,IBLVL有纤维拔出和分层“藕断丝连”的拉断;而RB的最外侧主裂纹已向中层扩展明显,多处断裂空隙出现,进入失稳型扩展阶段,将对材料造成不可逆的损伤。3)3.96ms时,IBLVL变形继续增加,细小裂纹成Z字汇聚成主裂纹现象明显;而此时RB已达到最大破坏变形量,大量纤维被拉断。4)5.28ms时,IBLVL达到最大变形量,裂纹前段已抵达试样2/3宽度截面处;此时RB出现试样回弹现象。5)6.27ms时,RB试样冲击件3回弹脱离试样,冲击完成,而IBLVL依然处于试样回弹状态;6)到10.56ms时,IBLVL冲击件3脱离试样,冲击完成,IBLVL和RB整个冲击响应阶段的持续时间分别为10.56ms和6.27ms。1) At 0ms, the punch of the
综上,与RB相比,IBLVL具有更好的冲击韧性,这取决于上、下层与芯层在抵抗冲击和能量吸收过程中相互之间的协同作用。In conclusion, compared with RB, IBLVL has better impact toughness, which depends on the synergy between the upper and lower layers and the core layer in the process of impact resistance and energy absorption.
在本说明书的描述中,参考术语“有些实施例”、“其他实施例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施例或示例中。在本说明书中,对上述术语的示意性表述不一定指的是相同的实施例或示例。而且,描述的具体特征、结构、材料或者特点可以在任何的一个或多个实施例或示例中以合适的方式结合。In the description of this specification, description with reference to the terms "some embodiments," "other embodiments," etc. means that a particular feature, structure, material, or characteristic described in connection with that embodiment or example is included in at least one embodiment of the present invention or in the example. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
以上内容仅为本发明的较佳实施例,对于本领域的普通技术人员,依据本发明的思想,在具体实施方式及应用范围上均会有改变之处,本说明书内容不应理解为对本发明的限制。The above contents are only preferred embodiments of the present invention. For those of ordinary skill in the art, according to the idea of the present invention, there will be changes in the specific embodiments and application scope. limits.
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115415174A (en) * | 2022-08-05 | 2022-12-02 | 宁波德昌电器有限公司 | An automatic detection device and detection method for a fan |
CN118090117A (en) * | 2024-04-17 | 2024-05-28 | 江苏天宇设计研究院有限公司 | Impact test device for protective door |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040103713A1 (en) * | 2002-11-18 | 2004-06-03 | Voon Wong Shaw | Pendulum impact test rig |
CN1719225A (en) * | 2004-07-08 | 2006-01-11 | 日东电工株式会社 | Impact test apparatus and impact test method |
CN104897357A (en) * | 2015-04-08 | 2015-09-09 | 东北大学 | Metal sheet spot-welding joint impact performance test device and method |
CN206057106U (en) * | 2016-08-24 | 2017-03-29 | 深圳市靖邦电子有限公司 | The swing impact experiment apparatus of pcb board |
CN108072579A (en) * | 2017-11-23 | 2018-05-25 | 吉林大学 | The impact indentation test device and method of variable bit rate |
CN208672465U (en) * | 2018-08-29 | 2019-03-29 | 樊金淼 | A kind of Charpy impact machine tester of the automatic centering applied to high molecular material |
CN210533852U (en) * | 2019-07-03 | 2020-05-15 | 华南农业大学 | A swing impact test device for evaluating the mechanical behavior of fruit collision and damage |
CN112116855A (en) * | 2020-03-02 | 2020-12-22 | 四川大学 | Multifunctional skull and maxillofacial bone impact mechanics experimental device |
-
2022
- 2022-01-27 CN CN202210100272.3A patent/CN114397205B/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040103713A1 (en) * | 2002-11-18 | 2004-06-03 | Voon Wong Shaw | Pendulum impact test rig |
CN1719225A (en) * | 2004-07-08 | 2006-01-11 | 日东电工株式会社 | Impact test apparatus and impact test method |
CN104897357A (en) * | 2015-04-08 | 2015-09-09 | 东北大学 | Metal sheet spot-welding joint impact performance test device and method |
CN206057106U (en) * | 2016-08-24 | 2017-03-29 | 深圳市靖邦电子有限公司 | The swing impact experiment apparatus of pcb board |
CN108072579A (en) * | 2017-11-23 | 2018-05-25 | 吉林大学 | The impact indentation test device and method of variable bit rate |
CN208672465U (en) * | 2018-08-29 | 2019-03-29 | 樊金淼 | A kind of Charpy impact machine tester of the automatic centering applied to high molecular material |
CN210533852U (en) * | 2019-07-03 | 2020-05-15 | 华南农业大学 | A swing impact test device for evaluating the mechanical behavior of fruit collision and damage |
CN112116855A (en) * | 2020-03-02 | 2020-12-22 | 四川大学 | Multifunctional skull and maxillofacial bone impact mechanics experimental device |
Non-Patent Citations (1)
Title |
---|
王金元 等: "熔断器撞击器冲击实验研究", 高压电器, no. 04 * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115415174A (en) * | 2022-08-05 | 2022-12-02 | 宁波德昌电器有限公司 | An automatic detection device and detection method for a fan |
CN118090117A (en) * | 2024-04-17 | 2024-05-28 | 江苏天宇设计研究院有限公司 | Impact test device for protective door |
CN118090117B (en) * | 2024-04-17 | 2024-06-28 | 江苏天宇设计研究院有限公司 | Impact test device for protective door |
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