CN103383311A - Three crank-rocker mechanism joint bearing high-speed testing machine - Google Patents
Three crank-rocker mechanism joint bearing high-speed testing machine Download PDFInfo
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Abstract
本发明公开一种三曲柄摇杆机构关节轴承高速试验机,所述曲轴的三个曲拐上安装滑动轴瓦Ⅰ、Ⅱ、Ⅲ,三根高频摆动轴Ⅰ、Ⅱ、Ⅲ各支承在两个滚动轴承上,三根高频摆动轴Ⅰ、Ⅱ、Ⅲ与其它零部件连接方式均相同,其中,高频摆动轴Ⅰ的一端与试验关节轴承Ⅰ的内圈固联,试验关节轴承Ⅰ的外圈均与加载液压缸Ⅰ固联,高频摆动轴Ⅰ的另一端与摇杆Ⅰ固联。本发明的带有三个曲拐的曲轴设计成动平衡结构,冲击小、噪音低。该发明同时对三个关节轴承进行疲劳试验,也可对不同批次、不同厂家的产品进行比对疲劳试验,工作效率高。该发明的摆动频率可达70~80Hz,可满足高频摆动航空关节轴承疲劳试验的要求。
The invention discloses a high-speed testing machine for joint bearings of a three-crank rocker mechanism. The three cranks of the crankshaft are equipped with sliding bearing bushes I, II, and III, and the three high-frequency swing shafts I, II, and III are each supported on two rolling bearings. Above, the three high-frequency oscillating shafts Ⅰ, Ⅱ, and Ⅲ are connected in the same way as other components. Among them, one end of the high-frequency oscillating shaft Ⅰ is firmly connected to the inner ring of the test spherical plain bearing Ⅰ, and the outer ring of the test spherical plain bearing Ⅰ is connected to the The loading hydraulic cylinder I is fixedly connected, and the other end of the high-frequency swing shaft I is fixedly connected with the rocker I. The crankshaft with three crank throws of the present invention is designed as a dynamic balance structure with small impact and low noise. The invention carries out fatigue tests on three joint bearings at the same time, and can also carry out comparison fatigue tests on products of different batches and different manufacturers, and has high working efficiency. The oscillating frequency of the invention can reach 70-80 Hz, which can meet the requirements of high-frequency oscillating aviation joint bearing fatigue test.
Description
技术领域 technical field
本发明涉及一种三曲柄摇杆机构关节轴承高速试验机。 The invention relates to a high-speed testing machine for joint bearings of a three-crank rocker mechanism.
背景技术 Background technique
关节轴承是一种特殊结构的滑动轴承,主要是由一个带外球面的内圈和一个带内球面的外圈组成。关节轴承因具有转动灵活、免维护、结构紧凑、易于装拆、承载能力大、寿命长等诸多优点,被广泛应用于航空飞行器摆动构件连接。 Spherical joint bearing is a kind of sliding bearing with special structure, which is mainly composed of an inner ring with an outer spherical surface and an outer ring with an inner spherical surface. Joint bearings are widely used in the connection of swing components of aviation vehicles because of their flexible rotation, maintenance-free, compact structure, easy assembly and disassembly, large load-carrying capacity, and long life.
航空飞行器在飞行过程中,任何组成构件的失效都会造成灾难性后果。因此对航空飞行器组成构件服役寿命的确定是一项非常严肃而重要的工作。为了准确的确定航空飞行器组成构件的服役寿命,通常做法是对航空飞行器组成构件进行模拟真实工况条件下的疲劳试验,再把通过试验求得的疲劳寿命除以一个安全系数即为航空飞行器组成构件的服役寿命。 During the flight of an aircraft, the failure of any component will cause catastrophic consequences. Therefore, it is a very serious and important work to determine the service life of the components of the aircraft. In order to accurately determine the service life of the components of the aircraft, the usual practice is to carry out fatigue tests on the components of the aircraft under simulated real working conditions, and then divide the fatigue life obtained through the test by a safety factor, which is the component of the aircraft. Component service life.
关节轴承作为航空飞行器的重要组成构件之一,也必须进行模拟真实工况条件下的疲劳试验。有些航空飞行器上的关节轴承摆动频率很高(30~70Hz),而我国目前使用的关节轴承疲劳试验机多采用曲柄滑块机构,因该机构难以实现运动构件的动平衡,故其最高摆动频率一般不超过20Hz,无法满足高频摆动航空关节轴承疲劳试验的要求,严重制约了国产高频摆动航空关节轴承的发展。 As one of the important components of aerospace vehicles, spherical plain bearings must also undergo fatigue tests under simulated real working conditions. The oscillating frequency of joint bearings on some aviation vehicles is very high (30-70 Hz), while the joint bearing fatigue testing machines currently used in my country mostly use crank slider mechanisms, because it is difficult for this mechanism to achieve dynamic balance of moving components, so its highest oscillating frequency Generally, it does not exceed 20Hz, which cannot meet the requirements of the fatigue test of high-frequency oscillating aviation joint bearings, which seriously restricts the development of domestic high-frequency oscillating aviation joint bearings.
发明内容 Contents of the invention
为了克服现有的采用曲柄滑块机构的关节轴承疲劳试验机存在的上述不足,本发明提供一种三曲柄摇杆机构关节轴承高速试验机。该发明带有三个曲拐的曲轴为动平衡结构,三个曲柄摆杆机构的运动方式近似对称,三根连杆运动过程中产生的惯性载荷得到部分相互抵消,因此,冲击小、噪音低。 In order to overcome the above-mentioned shortcomings of the existing joint bearing fatigue testing machine using a crank slider mechanism, the present invention provides a high-speed testing machine for joint bearings with a three-crank rocker mechanism. In this invention, the crankshaft with three crank throws is a dynamic balance structure, and the movement mode of the three crank swing rod mechanisms is approximately symmetrical, and the inertial loads generated during the movement of the three connecting rods are partially canceled out, so the impact is small and the noise is low.
本发明解决其技术问题所采用的技术方案是:一种三曲柄摇杆机构关节轴承高速试验机,包括连杆Ⅰ、Ⅱ、Ⅲ、摇杆Ⅰ、Ⅱ、Ⅲ、销轴Ⅰ、Ⅱ、Ⅲ、滑动轴瓦Ⅰ、Ⅱ、Ⅲ、滚动轴承Ⅰ、Ⅱ、Ⅲ、Ⅳ 、Ⅴ、 Ⅵ、 Ⅶ 、Ⅷ、联轴器和电机。所述支承在滚动轴承ⅠⅡ上的一个带有三个曲拐的曲轴的一端通过联轴器与电机相连,曲轴的三个曲拐上安装三个滑动轴瓦Ⅰ、Ⅱ、Ⅲ,滑动轴瓦与曲拐轴构成转动动连接;三根高频摆动轴Ⅰ、Ⅱ、Ⅲ各支承在两个滚动轴承上。三根高频摆动轴Ⅰ、Ⅱ、Ⅲ的一端与三个试验关节轴承Ⅰ、Ⅱ、Ⅲ、三个试验关节轴承Ⅰ、Ⅱ、Ⅲ、与三个加载液压缸Ⅰ、Ⅱ、Ⅲ、以及三根高频摆动轴Ⅰ、Ⅱ、Ⅲ、的另一端与三个摇杆Ⅰ、Ⅱ、Ⅲ、的连接方式均相同,其中,高频摆动轴Ⅰ的一端与试验关节轴承Ⅰ的内圈固联,试验关节轴承Ⅰ的外圈均与加载液压缸Ⅰ固联,高频摆动轴Ⅰ的另一端与摇杆Ⅰ固联;三根摇杆Ⅰ、Ⅱ、Ⅲ的结构、尺寸也相同,三根连杆Ⅰ、Ⅱ、Ⅲ的结构、尺寸也相同,其中,连杆Ⅰ的两端各有一个圆柱孔,一个圆柱孔固联在曲轴上的滑动轴瓦Ⅱ的外圆上,另一个圆柱孔通过销轴Ⅰ与摇杆Ⅰ的圆柱孔构成转动动连接。 The technical solution adopted by the present invention to solve the technical problem is: a high-speed testing machine for joint bearings of a three-crank rocker mechanism, including connecting rods I, II, III, rockers I, II, III, pin shafts I, II, III , Sliding bearings Ⅰ, Ⅱ, Ⅲ, rolling bearings Ⅰ, Ⅱ, Ⅲ, Ⅳ, Ⅴ, Ⅵ, Ⅶ, Ⅷ, couplings and motors. One end of the crankshaft with three crankshafts supported on the rolling bearing III is connected to the motor through a coupling, and three sliding bearing bushes I, II, III are installed on the three crankshafts of the crankshaft, and the sliding bearing bushes and the crankshaft It constitutes a rotating dynamic connection; three high-frequency swing shafts I, II, and III are supported on two rolling bearings. One end of three high-frequency swing shafts I, II, III and three test joint bearings I, II, III, three test joint bearings I, II, III, and three loading hydraulic cylinders I, II, III, and three high The other ends of the high-frequency oscillating shafts Ⅰ, Ⅱ, and Ⅲ are connected in the same way to the three rockers Ⅰ, Ⅱ, and Ⅲ. Among them, one end of the high-frequency oscillating shaft Ⅰ is firmly connected with the inner ring of the test joint bearing Ⅰ. The outer ring of the joint bearing Ⅰ is fixedly connected with the loading hydraulic cylinder Ⅰ, and the other end of the high-frequency oscillating shaft Ⅰ is connected with the rocker Ⅰ; the structure and size of the three rockers I, II, and III are also the same, and the three connecting rods The structure and size of Ⅱ and Ⅲ are also the same. Among them, there is a cylindrical hole at both ends of the connecting rod Ⅰ, one cylindrical hole is fixedly connected to the outer circle of the sliding bearing bush Ⅱ on the crankshaft, and the other cylindrical hole passes through the pin shaft Ⅰ and The cylindrical hole of the rocking rod I constitutes a rotational connection.
所述曲轴的三个曲拐交错布置,第一个曲拐向上,即曲拐轴线与曲轴轴线的偏心距朝上;第二个曲拐向下,即曲拐轴线与曲轴轴线的偏心距朝下;第三个曲拐向上,即曲拐轴线与曲轴轴线的偏心距朝上。 The three crank throws of the crankshaft are arranged alternately, the first crank throw is upward, that is, the eccentric distance between the crank throw axis and the crankshaft axis is upward; the second crank throw is downward, that is, the eccentric distance between the crank throw axis and the crankshaft axis is upward. Down; the third crankshaft is up, that is, the eccentric distance between the crankshaft axis and the crankshaft axis is upward.
所述三根高频摆动轴Ⅰ、Ⅱ、Ⅲ的轴线均与曲轴轴线位于同一平面内,且彼此平行。 The axes of the three high-frequency oscillating shafts I, II and III are all located in the same plane as the axis of the crankshaft and parallel to each other.
本发明与现有技术相比具有如下优点:1、本发明的带有三个曲拐的曲轴能设计成动平衡结构,即在曲轴高速转动过程中,曲轴本身产生的离心惯性力和离心惯性力矩在曲轴本身得到平衡,曲轴的支承轴承不会受到该离心惯性力和离心惯性力矩作用。2、三个曲柄摆杆机构的运动方式近似对称,即当左右连杆垂直于纸面向上摆动时,中间连杆垂直于纸面向下摆动;当左右连杆沿纸面向上平动时,中间连杆沿纸面向下平动,这样三根连杆运动过程中产生的惯性载荷得到部分相互抵消,故冲击小、噪音低。3、可以同时对三个关节轴承进行疲劳试验,提高了工作效率。4、由于同时进行疲劳试验的关节轴承的工况条件完全相同,故可对不同生产批次、不同生产厂家的关节轴承进行比对疲劳试验。该发明的摆动频率可达70~80Hz,可满足高频摆动航空关节轴承疲劳试验的要求。 Compared with the prior art, the present invention has the following advantages: 1. The crankshaft with three crank throws of the present invention can be designed into a dynamic balance structure, that is, in the high-speed rotation process of the crankshaft, the centrifugal inertial force and centrifugal moment of inertia produced by the crankshaft itself When the crankshaft itself is balanced, the supporting bearings of the crankshaft will not be subjected to the centrifugal inertial force and centrifugal inertial moment. 2. The movement mode of the three crank swing rod mechanisms is approximately symmetrical, that is, when the left and right connecting rods swing upward perpendicular to the paper, the middle connecting rod swings downward perpendicular to the paper; when the left and right connecting rods move upward along the paper, the middle The connecting rods move downward along the plane of the paper, so that the inertial loads generated during the movement of the three connecting rods are partially offset by each other, so the impact is small and the noise is low. 3. The fatigue test can be carried out on three joint bearings at the same time, which improves the work efficiency. 4. Since the working conditions of the spherical plain bearings undergoing fatigue tests at the same time are exactly the same, it is possible to carry out comparative fatigue tests on spherical plain bearings of different production batches and different manufacturers. The oscillating frequency of the invention can reach 70-80 Hz, which can meet the requirements of high-frequency oscillating aviation joint bearing fatigue test.
附图说明 Description of drawings
图1为三曲柄摇杆机构关节轴承高速试验机工作状态俯视剖面示意图; Fig. 1 is a top view sectional schematic diagram of the working state of the three-crank rocker mechanism joint bearing high-speed testing machine;
图2为图1的A-A剖视示意图; Fig. 2 is a schematic sectional view of A-A of Fig. 1;
图3为图1的B-B剖视示意图; Fig. 3 is the B-B sectional schematic diagram of Fig. 1;
图4为图2的C-C剖面示意图; Fig. 4 is the C-C sectional schematic diagram of Fig. 2;
图5为带有三个曲拐曲轴零件的三维示意图。 Figure 5 is a three-dimensional schematic view of a crankshaft component with three crank throws.
在上述附图中,1.摇杆Ⅰ,2、4.滚动轴承Ⅲ、Ⅳ,3.高频摆动轴Ⅰ,5.加载液压缸Ⅰ,6.试验关节轴承Ⅰ,7、13.滚动轴承Ⅰ、Ⅱ,8.滑动轴瓦Ⅰ,9.滑动轴瓦Ⅱ,10.连杆Ⅰ,11连杆Ⅱ,12.曲轴,14.联轴器,15.电机,16.连杆Ⅲ,17.滑动轴瓦Ⅲ,18、22.滚动轴承Ⅴ、Ⅵ,19.试验关节轴承Ⅱ,20.加载液压缸Ⅱ,21.高频摆动轴Ⅱ,23.摇杆Ⅱ,24.摇杆Ⅲ,25、29.滚动轴承Ⅶ、Ⅷ,26.高频摆动轴Ⅲ,27.加载液压缸Ⅲ,28.试验关节轴承Ⅲ,30.销轴Ⅰ,31.销轴Ⅱ,32.销轴Ⅲ, In the above drawings, 1. Rocker I, 2, 4. Rolling bearings III, IV, 3. High-frequency swing shaft I, 5. Loading hydraulic cylinder I, 6. Test joint bearing I, 7, 13. Rolling bearings I, Ⅱ, 8. Sliding bearing Ⅰ, 9. Sliding bearing Ⅱ, 10. Connecting rod Ⅰ, 11 Connecting rod Ⅱ, 12. Crankshaft, 14. Coupling, 15. Motor, 16. Connecting rod Ⅲ, 17. Sliding bearing Ⅲ , 18, 22. Rolling bearing Ⅴ, Ⅵ, 19. Test joint bearing Ⅱ, 20. Loading hydraulic cylinder Ⅱ, 21. High-frequency swing shaft Ⅱ, 23. Rocker Ⅱ, 24. Rocker Ⅲ, 25, 29. Rolling bearing Ⅶ , Ⅷ, 26. High-frequency swing shaft Ⅲ, 27. Loading hydraulic cylinder Ⅲ, 28. Test joint bearing Ⅲ, 30. Pin shaft Ⅰ, 31. Pin shaft Ⅱ, 32. Pin shaft Ⅲ,
具体实施方式 Detailed ways
实施例 Example
在图1~图4所示的一种三曲柄摇杆机构关节轴承高速试验机工作状态示意图。支承在两个滚动轴承Ⅰ、Ⅱ(7、13)上的带有三个曲拐的曲轴12的一端通过联轴器14与电机(或液压马达)15相连,曲轴12的三个曲拐交错布置,即第一个曲拐向上(曲拐轴线与曲轴轴线的偏心距朝上)、第二个曲拐向下(曲拐轴线与曲轴轴线的偏心距朝下)、第三个曲拐向上(曲拐轴线与曲轴轴线的偏心距朝上)。在带有三个曲拐的曲轴12的左侧第一个曲拐轴上安装滑动轴瓦Ⅰ8,在带有三个曲拐的曲轴8的左侧第二个曲拐轴上安装滑动轴瓦Ⅱ9,在带有三个曲拐的曲轴8的左侧第三个曲拐轴上安装滑动轴瓦Ⅲ17,滑动轴瓦Ⅰ、Ⅱ、Ⅲ(8、9、17)与各自配合的曲拐轴构成转动动连接(两者间可相对转动,但不能相对轴向移动)。高频摆动轴Ⅰ3支承在两个滚动轴承Ⅲ、Ⅳ(2、4)上;高频摆动轴Ⅱ21支承在两个滚动轴承Ⅴ、Ⅵ(18、22)上;高频摆动轴26Ⅲ支承在两个滚动轴承Ⅶ、Ⅷ(25、29)上。三根高频摆动轴Ⅰ、Ⅱ、Ⅲ(3、21、26)的轴线均与带有三个曲拐的曲轴12的轴线位于同一平面内,且彼此平行。高频摆动轴Ⅰ3的一端与试验关节轴承Ⅰ6的内圈固联,试验关节轴承6的外圈与加载液压缸Ⅰ5固联;高频摆动轴Ⅱ21的一端与试验关节轴承Ⅱ19的内圈固联,试验关节轴承Ⅱ19的外圈与加载液压缸Ⅱ20固联;高频摆动轴Ⅲ26的一端与试验关节轴承Ⅲ28的内圈固联,试验关节轴承Ⅲ28的外圈与加载液压缸Ⅲ27固联。摇杆Ⅰ1的两端各有一个圆柱孔,其中一个圆柱孔与高频摆动轴Ⅰ3的一端固联;摇杆Ⅱ23的两端各有一个圆柱孔,其中一个圆柱孔与高频摆动轴Ⅱ21的一端固联;摇杆Ⅲ24的两端各有一个圆柱孔,其中一个圆柱孔与高频摆动轴Ⅲ26的一端固联。连杆Ⅱ11的两端各有一个圆柱孔,一个圆柱孔固联在滑动轴瓦Ⅲ17外圆上,另一个圆柱孔通过销轴Ⅱ31与摇杆Ⅱ23的圆柱孔构成转动动连接(两者间可相对转动,但不能相对轴向移动);连杆Ⅰ10的两端各有一个圆柱孔,一个圆柱孔固联在滑动轴瓦Ⅱ9外圆上,另一个圆柱孔通过销轴Ⅰ30与摇杆Ⅰ1的圆柱孔构成转动动连接(两者间可相对转动,但不能相对轴向移动);连杆Ⅲ16的两端各有一个圆柱孔,一个圆柱孔固联在滑动轴瓦Ⅰ8外圆上,另一个圆柱孔通过销轴Ⅲ32与摇杆Ⅱ22的圆柱孔构成转动动连接(两者间可相对转动,但不能相对轴向移动)。
A schematic diagram of the working state of a three-crank rocker mechanism joint bearing high-speed testing machine shown in Figures 1 to 4. One end of the
本发明的工作过程如下:曲轴、曲轴上的一个曲拐、一根连杆、一根摇杆、一个销轴、一根高频摆动轴和与它们配合的滚动轴承、滑动轴瓦共同构成一个曲柄摆杆机构,其中曲轴、曲轴上的一个曲拐构成曲柄摆杆机构的曲柄。曲轴12、三根连杆Ⅰ、Ⅱ、Ⅲ(10、11、16)、三根摇杆Ⅰ、Ⅱ、Ⅲ(1、23、24)、三个销轴Ⅰ、Ⅱ、Ⅲ(30、31、32)、三根高频摆动轴Ⅰ、Ⅱ、Ⅲ(3、21、26)和与它们配合的滚动轴承、滑动轴瓦共同构成三个曲柄摆杆机构。当电机(或液压马达)15通过联轴器14带动曲轴12高速转动时,通过三个曲柄摆杆机构使三根高频摆动轴Ⅰ、Ⅱ、Ⅲ(3、21、26)绕自身轴线高频往复回转摆动,固联在三根高频摆动轴Ⅰ、Ⅱ、Ⅲ(3、21、26)端部的三个试验关节轴承Ⅰ、Ⅱ、Ⅲ(6、19、28)的内圈也将随之高频往复回转摆动,与三个加载液压缸Ⅰ、Ⅱ、Ⅲ(5、20、27)固联的三个试验关节轴承Ⅰ、Ⅱ、Ⅲ(6、19、28)的外圈由于受到加载液压缸的限制而固定不动,这样就实现了试验关节轴承的内圈相对于外圈的高频往复回转摆动,三个加载液压缸Ⅰ、Ⅱ、Ⅲ(5、20、27)给三个试验关节轴承Ⅰ、Ⅱ、Ⅲ(6、19、28)的外圈施加拉力或压力,所施加的拉力或压力的大小由液压系统控制。
The working process of the present invention is as follows: the crankshaft, a crank throw on the crankshaft, a connecting rod, a rocker, a pin shaft, a high-frequency oscillating shaft, and rolling bearings and sliding bushes cooperating with them form a crank pendulum Rod mechanism, wherein the crankshaft and a crank throw on the crankshaft constitute the crank of the crank pendulum mechanism.
Claims (3)
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| CN2013103066114A CN103383311A (en) | 2013-07-22 | 2013-07-22 | Three crank-rocker mechanism joint bearing high-speed testing machine |
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| CN106908242A (en) * | 2017-02-28 | 2017-06-30 | 浙江大学 | Connecting rod synchronous belt type oscillating bearing experimental rig |
| CN106969914A (en) * | 2017-02-28 | 2017-07-21 | 浙江大学 | Crank and synchronous belt type oscillating bearing experimental rig |
| CN107782555A (en) * | 2017-11-22 | 2018-03-09 | 华中科技大学 | A kind of testing large rotating machinery bearing shell performance and the multi-function test stand in life-span |
| CN109163904A (en) * | 2018-10-11 | 2019-01-08 | 吉林大学 | Multi-load movable joint bearing fatigue marginal test machine |
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| CN107782555A (en) * | 2017-11-22 | 2018-03-09 | 华中科技大学 | A kind of testing large rotating machinery bearing shell performance and the multi-function test stand in life-span |
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| CN109163904A (en) * | 2018-10-11 | 2019-01-08 | 吉林大学 | Multi-load movable joint bearing fatigue marginal test machine |
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