WO2019173995A1 - 一种法兰盘拉弯扭复合加载多螺栓松脱试验机 - Google Patents

一种法兰盘拉弯扭复合加载多螺栓松脱试验机 Download PDF

Info

Publication number
WO2019173995A1
WO2019173995A1 PCT/CN2018/079092 CN2018079092W WO2019173995A1 WO 2019173995 A1 WO2019173995 A1 WO 2019173995A1 CN 2018079092 W CN2018079092 W CN 2018079092W WO 2019173995 A1 WO2019173995 A1 WO 2019173995A1
Authority
WO
WIPO (PCT)
Prior art keywords
fixed
test piece
plate
bearing
clamping plate
Prior art date
Application number
PCT/CN2018/079092
Other languages
English (en)
French (fr)
Inventor
孙清超
张豹
林清源
孙伟
杨斌
Original Assignee
大连理工大学
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 大连理工大学 filed Critical 大连理工大学
Priority to PCT/CN2018/079092 priority Critical patent/WO2019173995A1/zh
Priority to US16/613,759 priority patent/US10598567B1/en
Publication of WO2019173995A1 publication Critical patent/WO2019173995A1/zh

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M13/00Testing of machine parts
    • G01M13/02Gearings; Transmission mechanisms
    • G01M13/022Power-transmitting couplings or clutches
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M13/00Testing of machine parts
    • G01M13/02Gearings; Transmission mechanisms
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes

Definitions

  • the invention belongs to the technical field of mechanical testing equipment, and relates to a flange bending and twisting composite loading multi-bolt loosening testing machine.
  • the bolt loosening test machine can be used to study the looseness of the bolt under load.
  • the bolts currently used are loaded into the loose test machine and are divided into the following types:
  • the Junker Loose Tester primarily produces lateral movement by applying alternating lateral loads to the preloaded fasteners. This lateral movement causes the bolts and nuts to oscillate relative to each other, resulting in a micro-slip of the larger thread contact surface, causing the fastener to quickly loosen. It loosens the fasteners faster than any previous test method.
  • the tested fasteners are tightened on the clamping gantry, and a predetermined pre-tightening force is generated.
  • the servo hydraulic cylinder causes an alternating lateral displacement between the clamped two metal plates, resulting in a reduction of the clamping force. Even lost. The moment of the clamping force is continuously recorded, and the anti-loosening performance of the fastener is judged by comparison.
  • test piece is screwed into the test sleeve, and the position mark is made on the part and the sleeve, and then the sleeve is placed on the vibration test stand for reciprocation. After the start-up, the sleeve reciprocates against both ends of the guide groove in the guide groove, causing a large impact force, causing the test piece to loosen. During the test, the position of the test piece was recorded during the stop of the test, and the anti-loosening performance of the test piece was determined accordingly.
  • test benches are not for the loose test bench of single bolts, and the load is single, but in the multi-bolt structure such as analysis flange, the load on the bolt cannot be simple and accurate due to the interaction between the bolts.
  • the ground is equivalent to a single bolt, and in the actual use of the bolt, the load is generally more complicated in the case of multiple bolts. It is not a single lateral load. Therefore, the test bench is designed to effectively simulate the actual load condition of the multi-bolt flange, and it is more appropriate to obtain the looseness of each bolt when the multi-bolt is subjected to the load. At present, there is no relevant patent in the multi-bolt loose test machine.
  • the object of the present invention is to provide a flange bending and torsion composite loading multi-bolt loosening test machine, which can simultaneously apply a tensile bending and torsion composite load to a multi-bolt connection flange to study the looseness characteristics of the bolt.
  • the utility model relates to a flange pulling bending and twisting composite loading multi-bolt loosening testing machine, which is composed of three parts, namely an axial load transmitting part, a lateral load transmitting part and a torque load transmitting part;
  • the axial load transmitting portion includes a lower clamping plate 18, a thin test piece 19, a thick test piece 20, a test piece bolt 21, a bearing cover 23, a thrust ball bearing 24, an upper clamping plate 25, and an axial loading support 26 And the hydraulic puller 27; the lower clamping plate 18 and the axial loading support 26 are both fixed on the base 35; the thin test piece 19 and the thick test piece 20 are correspondingly assembled together, through the test piece The bolt 21 is assembled in the corresponding bolt hole; the thin test piece 19 and the thick test piece 20 are integrally mounted between the lower clamping plate 18 and the upper clamping plate 25, and the outer hexagon of the thin test piece 19 is mounted under the clamping.
  • the inner hexagon of the plate 18 is fixed by a hexagonal bolt; the end of the thick test piece 20 is mounted in the inner ring of the upper clamping plate 25 and fixed by a hexagon socket bolt; the bearing cover 23 passes through the upper clamping plate. 25, and the thrust ball bearing 24 is sandwiched between the bearing cover 23 and the upper clamping plate 25; one end of the hydraulic starting rod of the hydraulic puller 27 is placed in a cylinder on the axial loading support 26, on which The claw hook hooks the edge of the bearing cover 23;
  • the lateral load transmitting portion includes an eccentric coupling 1, a camshaft 2, an end cap 3, a cam link 4, a hinge pin 5, a U-shaped connecting rod 6, a first linear bearing 7-1, and a second linear bearing 7-2, the first support plate 8-1, the second support plate 8-2, the first ⁇ 8.5 pin 9-1, the second ⁇ 8.5 pin 9-2, and the third 8.5 pin 9 -3, elastic rod 10, short-head threaded member 11, adjusting ring 12, S-type column tension sensor 13, long-end threaded member 14, rotating head 15, tension plate 16, limit plate 17 and three-phase asynchronous motor 34;
  • the first support plate 8-1, the second support plate 8-2 and the three-phase asynchronous motor 34 are both fixed on the base 35; the eccentric coupling 1 is fixed at one end to the motor of the three-phase asynchronous motor 34.
  • the other end is fixed with the camshaft 2; the camshaft 2 is coupled to the cam link 4 via a ball bearing, and is sealed against dust by the end cap 3; the cam link 4 is connected with the U-shaped
  • the rod 6 is connected by a hinge pin 5; the first linear bearing 7-1 is fixed in the first support plate 8-1, and the U-shaped link 6 passes through the first linear bearing 7-1;
  • One end of the rod 10 is hinged to the U-shaped link 6 by the first ⁇ 8.5 pin 9-1, and the other One end of the end and short head screw 11 is hinged by a second ⁇ 8.5 pin 9-2; the other end of the short head screw 11 is screwed to one end of the S-type column tension sensor 13 and is in between
  • the adjusting ring 12 is mounted, and the other end of the S-type column tension sensor 13 is screwed with one end of the long-end screw member 14; the second linear bearing 7-2 is fixed in the second supporting plate 8-2, the long-end thread The other end of the member 14 passes through the second
  • the torque load transmitting portion includes a torsion arm 22, a reducer support frame 28, a guide rail slider 29, a bearing outer casing 30, a torque eccentric coupling 31, a speed reducer 32, and a servo motor 33; the reducer support frame 28 Fixed on the base 35, the servo motor 33 externally connected to the reducer 32 is fixed on the reducer support frame 28; the output shaft of the reducer 32 is coupled with the torque eccentric coupling 31, and the torque eccentric coupling 31
  • the upper end surface of the bearing sleeve 30 is fixed to the upper end surface of the bearing sleeve 30, and the lower end surface of the bearing sleeve 30 is fixed on the slider of the guide rail slider 29.
  • the guide rail of the guide rail slider 29 is fixed to the torsion arm 22, and the end portion of the torsion arm 22 is provided with a hexagon socket. On the outer hexagon of the thick test piece 20, it is located on the tension plate 16.
  • the invention has the beneficial effects that the three composite loads can be isolated from each other without interfering with each other, and the applied load magnitude is displayed in real time.
  • Figure 1 is a positive triaxial view of the test rig.
  • 6U type connecting rod 7-1 first linear bearing; 7-2 second linear bearing; 8-1 first supporting plate;
  • 13S type column tension sensor 14 long head threaded parts; 15 rotating head; 16 tension plate; 17 limit plate;
  • the utility model relates to a flange pulling bending and twisting composite loading multi-bolt loosening testing machine, which is composed of three parts, namely an axial load transmitting part, a lateral load transmitting part and a torque load transmitting part;
  • the axial load transmitting portion includes a lower clamping plate 18, a thin test piece 19, a thick test piece 20, a test piece bolt 21, a bearing cover 23, a thrust ball bearing 24, an upper clamping plate 25, and an axial loading support 26 And the hydraulic puller 27; the lower clamping plate 18 and the axial loading support 26 are both fixed on the base 35; the thin test piece 19 and the thick test piece 20 are correspondingly assembled together, through the test piece The bolt 21 is assembled in the corresponding bolt hole; the thin test piece 19 and the thick test piece 20 are integrally mounted between the lower clamping plate 18 and the upper clamping plate 25, and the outer hexagon of the thin test piece 19 is mounted under the clamping.
  • the inner hexagon of the plate 18 is fixed by a hexagonal bolt; the end of the thick test piece 20 is mounted in the inner ring of the upper clamping plate 25 and fixed by a hexagon socket bolt; the bearing cover 23 passes through the upper clamping plate. 25, and the thrust ball bearing 24 is sandwiched between the bearing cover 23 and the upper clamping plate 25; one end of the hydraulic starting rod of the hydraulic puller 27 is placed in a cylinder on the axial loading support 26, on which The claw hook hooks the edge of the bearing cover 23;
  • the lateral load transmitting portion includes an eccentric coupling 1, a camshaft 2, an end cap 3, a cam link 4, a hinge pin 5, a U-shaped connecting rod 6, a first linear bearing 7-1, and a second linear bearing 7-2, the first support plate 8-1, the second support plate 8-2, the first ⁇ 8.5 pin 9-1, the second ⁇ 8.5 pin 9-2, and the third 8.5 pin 9 -3, elastic rod 10, short-head threaded member 11, adjusting ring 12, S-type column tension sensor 13, long-end threaded member 14, rotating head 15, tension plate 16, limit plate 17 and three-phase asynchronous motor 34;
  • the first support plate 8-1, the second support plate 8-2 and the three-phase asynchronous motor 34 are both fixed on the base 35; the eccentric coupling 1 is fixed at one end to the motor of the three-phase asynchronous motor 34.
  • the other end is fixed with the camshaft 2; the camshaft 2 is coupled to the cam link 4 via a ball bearing, and is sealed against dust by the end cap 3; the cam link 4 is connected with the U-shaped
  • the rod 6 is connected by a hinge pin 5; the first linear bearing 7-1 is fixed in the first support plate 8-1, and the U-shaped link 6 passes through the first linear bearing 7-1;
  • One end of the rod 10 is hinged to the U-shaped link 6 by the first ⁇ 8.5 pin 9-1, and the other One end of the end and short head screw 11 is hinged by a second ⁇ 8.5 pin 9-2; the other end of the short head screw 11 is screwed to one end of the S-type column tension sensor 13 and is in between
  • the adjusting ring 12 is mounted, and the other end of the S-type column tension sensor 13 is screwed with one end of the long-end screw member 14; the second linear bearing 7-2 is fixed in the second supporting plate 8-2, the long-end thread The other end of the member 14 passes through the second
  • the torque load transmitting portion includes a torsion arm 22, a reducer support frame 28, a guide rail slider 29, a bearing outer casing 30, a torque eccentric coupling 31, a speed reducer 32, and a servo motor 33; the reducer support frame 28 Fixed on the base 35, the servo motor 33 externally connected to the reducer 32 is fixed on the reducer support frame 28; the output shaft of the reducer 32 is coupled with the torque eccentric coupling 31, and the torque eccentric coupling 31
  • the upper end surface of the bearing sleeve 30 is fixed to the upper end surface of the bearing sleeve 30, and the lower end surface of the bearing sleeve 30 is fixed on the slider of the guide rail slider 29.
  • the guide rail of the guide rail slider 29 is fixed to the torsion arm 22, and the end portion of the torsion arm 22 is provided with a hexagon socket. On the outer hexagon of the thick test piece 20, it is located on the tension plate 16.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

一种法兰盘拉弯扭复合加载多螺栓松脱试验机,用一个三相异步电机(34)产生的横向载荷作为对法兰盘施加的弯矩载荷,用液压拉马(27)产生的拉力作为轴向的拉力载荷,用伺服电机(33)产生的扭矩作为对法兰盘施加的扭矩载荷。该试验机可以将三种复合载荷互相隔离开,互不干扰,并且实时显示所施加的载荷大小,并同时对多螺栓连接法兰盘施加拉弯扭复合载荷,研究螺栓松脱特性。

Description

一种法兰盘拉弯扭复合加载多螺栓松脱试验机 技术领域
本发明属于机械试验设备技术领域,涉及一种法兰盘拉弯扭复合加载多螺栓松脱试验机。
背景技术
螺栓松脱试验机可以用来研究螺栓在承受载荷的情况下松脱的情况,现在使用的螺栓受载松脱试验机分为以下几种:
1、    是Junker式松脱试验方法
如GB/T 10431-2008。Junker式松脱试验机主要是通过对加预紧力的紧固件施加交变的横向载荷使之产生横向移动。这种横向移动使螺栓螺母之间相对摇摆,从而导致更大的螺纹接触面微观滑移,使紧固件迅速出现松转。它比以往任何一种试验法都能更快地使紧固件松转。
2、    电-液伺服控制式振动法
试验时将被试紧固件拧紧在装夹台架上,并产生规定的预紧力,通过伺服液压缸使被夹紧的两金属板之间产生交变横向位移,导致夹紧力减少,甚至丧失。连续记录夹紧力的瞬时,通过对比判断紧固件的防松性能。
3、    NAS振动试验法
将试件拧紧在试验套筒内,并在零件和套筒上做出位置标记,然后将套筒置于振动试验台上作往复运动。开机后,套筒在导槽内往复冲击导槽的两端,产生较大的冲击力,致使试件松动。在试验过程中定时停机记录试件位置变化,并据此判定试件的防松性能。
以上实验台无一不是针对单螺栓的松脱试验台,而且所承受的载荷单一,但是在分析法兰盘等多螺栓结构中,由于螺栓之间相互作用的存在,螺栓上的载荷无法简单精确地的等效到单螺栓上,并且在螺栓的实际使用过程中,在涉及多螺栓的情况下,载荷一般较为复杂。并非单一的横向载荷,因此设计出此试验台,可以有效的模拟多螺栓法兰盘的实际受载情况,更加贴切的得出多螺栓承受载荷的时候各螺栓的松脱情况。目前在多螺栓松脱试验机方面尚无相关专利。
技术问题
本发明的目的是提供了一种法兰盘拉弯扭复合加载多螺栓松脱试验机,能够同时对多螺栓连接法兰盘施加拉弯扭复合载荷,研究螺栓松脱特性的试验机。
技术解决方案
本发明的技术方案:
一种法兰盘拉弯扭复合加载多螺栓松脱试验机,由三个部分组成,分别为轴向载荷传递部分、横向载荷传递部分和扭矩载荷传递部分;
所述的轴向载荷传递部分包括下夹持板18、薄试件19、厚试件20、试件螺栓21、轴承盖23、推力球轴承24、上夹持板25、轴向加载支撑26和液压拉马27;所述的下夹持板18和轴向加载支撑26均固定在基台35上;所述的薄试件19和厚试件20止口对应装配在一起,通过试件螺栓21装配在对应螺栓孔中固定;薄试件19和厚试件20整体安装于下夹持板18与上夹持板25之间,所述的薄试件19的外六角安装在下夹持板18的内六角中,并用内六角螺栓固定;所述的厚试件20末端安装在上夹持板25内圈中,并用内六角螺栓固定;所述的轴承盖23穿过上夹持板25,并将推力球轴承24夹在轴承盖23与上夹持板25之间;所述的液压拉马27的油压起动杆一端置于轴向加载支撑26上的圆筒内,其上的爪勾勾住轴承盖23边缘;
所述的横向载荷传递部分包括偏心联轴器1、凸轮轴2、端盖3、凸轮连杆4、铰接销5、U型连杆6、第一直线轴承7-1、第二直线轴承7-2、第一支撑板8-1、第二支撑板8-2、第一Ф8.5柱销9-1、第二Ф8.5柱销9-2、第三Ф8.5柱销9-3、弹性杆10、短头螺纹件11、调节环12、S型柱式拉力传感器13、长头螺纹件14、旋转头15、拉力板16、限位板17和三相异步电机34;所述的第一支撑板8-1、第二支撑板8-2与三相异步电机34均固定在基台35上;所述的偏心联轴器1一端固定在三相异步电机34的电机轴上,另一端与凸轮轴2固定在一起;所述的凸轮轴2通过滚珠轴承与凸轮连杆4连接在一起,并用端盖3密封防尘;所述的凸轮连杆4与U型连杆6用铰接销5连接;所述的第一直线轴承7-1固定在第一支撑板8-1中,U型连杆6穿过第一直线轴承7-1;所述的弹性杆10一端用第一Ф8.5柱销9-1与U型连杆6铰接,另一端与短头螺纹件11的一端通过第二Ф8.5柱销9-2铰接;所述的短头螺纹件11的另一端与S型柱式拉力传感器13一端螺纹连接,并在两者中间安装调节环12,S型柱式拉力传感器13的另一端与长头螺纹件14的一端螺纹连接;所述的第二直线轴承7-2固定在第二支撑板8-2中,长头螺纹件14的另一端穿过第二直线轴承7-2,与旋转头15用第三Ф8.5柱销9-3铰接;所述的旋转头15置于拉力板16的U型槽内,通过限位板17限制旋转头15在拉力板16的U型槽内的移动;所述的拉力板16套在厚试件20中轴上;
所述的扭矩载荷传递部分包括扭力臂22、减速器支撑架28、导轨滑块29、轴承外套30、扭矩偏心联轴器31、减速器32和伺服电机33;所述的减速器支撑架28固定在基台35上,伺服电机33外接减速器32共同固定在减速器支撑架28上;所述的减速器32的输出轴与扭矩偏心联轴器31连接在一起,扭矩偏心联轴器31与轴承外套30上端面固定在一起,轴承外套30下端面固定在导轨滑块29的滑块上,导轨滑块29的导轨固定在扭力臂22,扭力臂22上设有内六角头的一端套在厚试件20的外六角上,位于拉力板16上。
有益效果
本发明的有益效果:本发明可以将三种复合载荷互相隔离开,互不干扰,并且实时显示所施加的载荷大小。
附图说明
图1为试验台的正三轴测图。
图中:1偏心联轴器;2凸轮轴;3端盖;4凸轮连杆;5铰接销;
6U型连杆;7-1第一直线轴承;7-2第二直线轴承;8-1第一支撑板;
8-2第二支撑板;9-1第一Ф8.5柱销;9-2第二Ф8.5柱销;
9-3第三Ф8.5柱销;10弹性杆;11短头螺纹件;12调节环;
13S型柱式拉力传感器;14长头螺纹件;15旋转头;16拉力板;17限位板;
8下夹持板;19薄试件;20厚试件;21试件螺栓;22扭力臂;23轴承盖;
24推力球轴承;25上夹持板;26轴向加载支撑;27液压拉马;
28减速器支撑架;29导轨加滑块;30轴承外套;31扭矩偏心联轴器;
32减速器;33伺服电机;34三相异步电机;35基台。
本发明的实施方式
以下结合附图和技术方案,进一步说明本发明的具体实施方式。
如图1所示:
一种法兰盘拉弯扭复合加载多螺栓松脱试验机,由三个部分组成,分别为轴向载荷传递部分、横向载荷传递部分和扭矩载荷传递部分;
所述的轴向载荷传递部分包括下夹持板18、薄试件19、厚试件20、试件螺栓21、轴承盖23、推力球轴承24、上夹持板25、轴向加载支撑26和液压拉马27;所述的下夹持板18和轴向加载支撑26均固定在基台35上;所述的薄试件19和厚试件20止口对应装配在一起,通过试件螺栓21装配在对应螺栓孔中固定;薄试件19和厚试件20整体安装于下夹持板18与上夹持板25之间,所述的薄试件19的外六角安装在下夹持板18的内六角中,并用内六角螺栓固定;所述的厚试件20末端安装在上夹持板25内圈中,并用内六角螺栓固定;所述的轴承盖23穿过上夹持板25,并将推力球轴承24夹在轴承盖23与上夹持板25之间;所述的液压拉马27的油压起动杆一端置于轴向加载支撑26上的圆筒内,其上的爪勾勾住轴承盖23边缘;
所述的横向载荷传递部分包括偏心联轴器1、凸轮轴2、端盖3、凸轮连杆4、铰接销5、U型连杆6、第一直线轴承7-1、第二直线轴承7-2、第一支撑板8-1、第二支撑板8-2、第一Ф8.5柱销9-1、第二Ф8.5柱销9-2、第三Ф8.5柱销9-3、弹性杆10、短头螺纹件11、调节环12、S型柱式拉力传感器13、长头螺纹件14、旋转头15、拉力板16、限位板17和三相异步电机34;所述的第一支撑板8-1、第二支撑板8-2与三相异步电机34均固定在基台35上;所述的偏心联轴器1一端固定在三相异步电机34的电机轴上,另一端与凸轮轴2固定在一起;所述的凸轮轴2通过滚珠轴承与凸轮连杆4连接在一起,并用端盖3密封防尘;所述的凸轮连杆4与U型连杆6用铰接销5连接;所述的第一直线轴承7-1固定在第一支撑板8-1中,U型连杆6穿过第一直线轴承7-1;所述的弹性杆10一端用第一Ф8.5柱销9-1与U型连杆6铰接,另一端与短头螺纹件11的一端通过第二Ф8.5柱销9-2铰接;所述的短头螺纹件11的另一端与S型柱式拉力传感器13一端螺纹连接,并在两者中间安装调节环12,S型柱式拉力传感器13的另一端与长头螺纹件14的一端螺纹连接;所述的第二直线轴承7-2固定在第二支撑板8-2中,长头螺纹件14的另一端穿过第二直线轴承7-2,与旋转头15用第三Ф8.5柱销9-3铰接;所述的旋转头15置于拉力板16的U型槽内,通过限位板17限制旋转头15在拉力板16的U型槽内的移动;所述的拉力板16套在厚试件20中轴上;
所述的扭矩载荷传递部分包括扭力臂22、减速器支撑架28、导轨滑块29、轴承外套30、扭矩偏心联轴器31、减速器32和伺服电机33;所述的减速器支撑架28固定在基台35上,伺服电机33外接减速器32共同固定在减速器支撑架28上;所述的减速器32的输出轴与扭矩偏心联轴器31连接在一起,扭矩偏心联轴器31与轴承外套30上端面固定在一起,轴承外套30下端面固定在导轨滑块29的滑块上,导轨滑块29的导轨固定在扭力臂22,扭力臂22上设有内六角头的一端套在厚试件20的外六角上,位于拉力板16上。
一种法兰盘拉弯扭复合加载多螺栓松脱试验机的实验方法,步骤如下:
(1)对液压拉马27加压,液压拉马27的油压起动杆伸出,带动液压拉马27的爪勾向上移动,油压起动杆抵住轴向加载支撑26,爪勾勾紧轴承盖23边缘,从而产生一个轴向的拉力。
(2)启动三相异步电机34,由于偏心联轴器1偏心距的存在,电机的转动便可以输出周期性横向载荷,由于弹性杆10的存在,不会发生电机抱死的情况。
(3)启动伺服电机33,由于扭矩偏心联轴器31偏心距的存在,会使扭力臂摆动,从而对厚试件施加循环的扭矩载荷。

Claims (2)

  1. 一种法兰盘拉弯扭复合加载多螺栓松脱试验机,其特征在于,所述的法兰盘拉弯扭复合加载多螺栓松脱试验机由三个部分组成,分别为轴向载荷传递部分、横向载荷传递部分和扭矩载荷传递部分;
    所述的轴向载荷传递部分包括下夹持板(18)、薄试件(19)、厚试件(20)、试件螺栓(21)、轴承盖(23)、推力球轴承(24)、上夹持板(25)、轴向加载支撑(26)和液压拉马(27);所述的下夹持板(18)和轴向加载支撑(26)均固定在基台(35)上;所述的薄试件(19)和厚试件(20)止口对应装配在一起,通过试件螺栓(21)装配在对应螺栓孔中固定;薄试件(19)和厚试件(20)整体安装于下夹持板(18)与上夹持板(25)之间,所述的薄试件(19)的外六角安装在下夹持板(18)的内六角中,并用内六角螺栓固定;所述的厚试件(20)末端安装在上夹持板(25)内圈中,并用内六角螺栓固定;所述的轴承盖(23)穿过上夹持板(25),并将推力球轴承(24)夹在轴承盖(23)与上夹持板(25)之间;所述的液压拉马(27)的油压起动杆一端置于轴向加载支撑(26)上的圆筒内,其上的爪勾勾住轴承盖(23)边缘;
    所述的横向载荷传递部分包括偏心联轴器(1)、凸轮轴(2)、端盖(3)、凸轮连杆(4)、铰接销(5)、U型连杆(6)、第一直线轴承(7-1)、第二直线轴承(7-2)、第一支撑板(8-1)、第二支撑板(8-2)、第一Ф8.5柱销(9-1)、第二Ф8.5柱销(9-2)、第三Ф8.5柱销(9-3)、弹性杆(10)、短头螺纹件(11)、调节环(12)、S型柱式拉力传感器(13)、长头螺纹件(14)、旋转头(15)、拉力板(16)、限位板(17)和三相异步电机(34);所述的第一支撑板(8-1)、第二支撑板(8-2)与三相异步电机(34)均固定在基台(35)上;所述的偏心联轴器(1)一端固定在三相异步电机(34)的电机轴上,另一端与凸轮轴(2)固定在一起;所述的凸轮轴(2)通过滚珠轴承与凸轮连杆(4)连接在一起,并用端盖(3)密封防尘;所述的凸轮连杆(4)与U型连杆(6)用铰接销(5)连接;所述的第一直线轴承(7-1)固定在第一支撑板(8-1)中,U型连杆(6)穿过第一直线轴承(7-1);所述的弹性杆(10)一端用第一Ф8.5柱销(9-1)与U型连杆(6)铰接,另一端与短头螺纹件(11)的一端通过第二Ф8.5柱销(9-2)铰接;所述的短头螺纹件(11)的另一端与S型柱式拉力传感器(13)一端螺纹连接,并在两者中间安装调节环(12),S型柱式拉力传感器(13)的另一端与长头螺纹件(14)的一端螺纹连接;所述的第二直线轴承(7-2)固定在第二支撑板(8-2)中,长头螺纹件(14)的另一端穿过第二直线轴承(7-2),与旋转头(15)用第三Ф8.5柱销(9-3)铰接;所述的旋转头(15)置于拉力板(16)的U型槽内,通过限位板(17)限制旋转头(15)在拉力板(16)的U型槽内的移动;所述的拉力板(16)套在厚试件(20)中轴上;
    所述的扭矩载荷传递部分包括扭力臂(22)、减速器支撑架(28)、导轨滑块(29)、轴承外套(30)、扭矩偏心联轴器(31)、减速器(32)和伺服电机(33);所述的减速器支撑架(28)固定在基台(35)上,伺服电机(33)外接减速器(32)共同固定在减速器支撑架(28)上;所述的减速器(32)的输出轴与扭矩偏心联轴器(31)连接在一起,扭矩偏心联轴器(31)与轴承外套(30)上端面固定在一起,轴承外套(30)下端面固定在导轨滑块(29)的滑块上,导轨滑块(29)的导轨固定在扭力臂(22),扭力臂(22)上设有内六角头的一端套在厚试件(20)的外六角上,位于拉力板(16)上。
  2. 根据权利要求1所述的法兰盘拉弯扭复合加载多螺栓松脱试验机,其特征在于,所述的调节环(12)的厚度根据需求进行调节。
PCT/CN2018/079092 2018-03-15 2018-03-15 一种法兰盘拉弯扭复合加载多螺栓松脱试验机 WO2019173995A1 (zh)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PCT/CN2018/079092 WO2019173995A1 (zh) 2018-03-15 2018-03-15 一种法兰盘拉弯扭复合加载多螺栓松脱试验机
US16/613,759 US10598567B1 (en) 2018-03-15 2018-03-15 Multi-bolt loosening test machine for flange with tension, bending and torsion compound loading

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2018/079092 WO2019173995A1 (zh) 2018-03-15 2018-03-15 一种法兰盘拉弯扭复合加载多螺栓松脱试验机

Publications (1)

Publication Number Publication Date
WO2019173995A1 true WO2019173995A1 (zh) 2019-09-19

Family

ID=67908737

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2018/079092 WO2019173995A1 (zh) 2018-03-15 2018-03-15 一种法兰盘拉弯扭复合加载多螺栓松脱试验机

Country Status (2)

Country Link
US (1) US10598567B1 (zh)
WO (1) WO2019173995A1 (zh)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112014087A (zh) * 2020-08-26 2020-12-01 株洲时代新材料科技股份有限公司 一种基于拉杆的橡胶节点三向疲劳试验装置
CN112014017A (zh) * 2020-07-30 2020-12-01 南京安润朴新能源科技有限公司 一种新型工业机器人伺服电机齿槽转矩试验台及实验方法
CN112461525A (zh) * 2020-11-20 2021-03-09 中国直升机设计研究所 一种无人直升机发动机安装支架试验装置
CN113390730A (zh) * 2021-06-30 2021-09-14 深圳市优瑞特检测技术有限公司 一种电器板材测试用自动循环弯折实验装置
CN116294467A (zh) * 2023-03-15 2023-06-23 绿能纤材(重庆)科技有限公司 一种羧甲基纤维素锂接枝聚丙烯酸锂的烘干粉碎装置
CN117302540A (zh) * 2023-09-14 2023-12-29 成都飞机工业(集团)有限责任公司 一种飞机机翼折叠插销作动器试验测试装置及方法
CN117705449A (zh) * 2024-02-06 2024-03-15 聊城大学 一种向心关节轴承磨损寿命试验系统及试验方法

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107621361B (zh) * 2017-08-02 2019-03-05 大连理工大学 一种基于精确控制螺栓横向载荷松脱试验机的闭环控制方法
WO2020014852A1 (zh) * 2018-07-17 2020-01-23 大连理工大学 一种多螺栓松脱试验机横向载荷幅值闭环控制方法
US11073455B2 (en) * 2018-07-17 2021-07-27 Dalian University Of Technology Transverse load stepless amplitude modulation device of multiple bolt loosing tester
CN111638117B (zh) * 2020-07-01 2024-08-06 北京信息科技大学 一种单驱动圆周多向同步拉伸机构
CN114076651B (zh) * 2020-08-20 2024-04-26 上海飞机制造有限公司 一种复合材料临时紧固件验证装置及其使用方法
CN113203651B (zh) * 2021-03-19 2022-05-31 国家海洋局南海调查技术中心(国家海洋局南海浮标中心) 一种浮标锚链磨损测试用试验台
CN112857785B (zh) * 2021-03-26 2024-05-07 重庆双禾科技有限公司 一种铰链扭力自动检测调试装置
CN113959695B (zh) * 2021-10-12 2024-09-17 吉林大学 一种数控机床卡盘可靠性试验装置
CN114166516B (zh) * 2021-12-06 2022-12-27 北京化工大学 一种圆弧端齿连接的转子系统的应力试验装置和系统
CN114778103B (zh) * 2022-06-17 2022-10-28 深圳市永达电子信息股份有限公司 一种检测部件结构紧密度的自动化测试装置及方法
CN115235767B (zh) * 2022-07-26 2023-04-07 中国航发沈阳发动机研究所 一种连杆形式的主轴试验用支点固定装置
CN117548289B (zh) * 2024-01-09 2024-04-02 宁波欧达光电有限公司 一种用于电磁屏蔽光伏组件的制备装置

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1200148A1 (ru) * 1983-11-25 1985-12-23 Petrov Evgenij N Приспособление дл испытани резьбового соединени на самоотвинчивание под действием раст гивающей нагрузки
DE4311956A1 (de) * 1993-04-10 1994-10-13 Inst Mikrostrukturtechnologie Anordnung zur Bestimmung des Belastungszustandes von Verbindungselementen
JP2011047687A (ja) * 2009-08-25 2011-03-10 Nichiyu Giken Kogyo Co Ltd 引張荷重記録装置
CN103512745A (zh) * 2013-10-12 2014-01-15 无锡创明传动工程有限公司 一种扭矩加载机构
KR20160064636A (ko) * 2014-11-28 2016-06-08 현대위아 주식회사 체결형 볼트의 풀림특성 검출장치
CN107621361A (zh) * 2017-08-02 2018-01-23 大连理工大学 一种基于精确控制螺栓横向载荷松脱试验机的闭环控制方法
CN108444686A (zh) * 2018-03-15 2018-08-24 大连理工大学 一种法兰盘拉弯扭复合加载多螺栓松脱试验机

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2286642A (en) * 1939-05-12 1942-06-16 Henry L Scott Company Magnetically controlled load testing machine
US3440869A (en) * 1966-11-04 1969-04-29 Standard Pressed Steel Co Threaded fastener testing apparatus
US3643501A (en) * 1969-11-18 1972-02-22 Ingersoll Rand Co Wrenching system and method
US3866463A (en) * 1973-11-19 1975-02-18 Smithkline Corp Device for testing the torque required to release a screw cap from its tightened position
US5597964A (en) * 1995-06-06 1997-01-28 Air Industries Corporation Torque measuring device for free running self-locking nut and bolt combination
AU6609598A (en) * 1997-02-12 1998-09-08 Thomas Loffler Method and device for producing screw assemblies
ATE430264T1 (de) * 2000-03-22 2009-05-15 Ronald C Clarke Gerät mit variabler verstärkung der bolzenlastanzeige sowie verfahren zur herstellung und zum gebrauch des geräts
JP5465404B2 (ja) 2007-10-31 2014-04-09 一般財団法人小林理学研究所 インナナットの緩み及び損傷の検知方法とその装置
JP5910971B2 (ja) 2013-05-24 2016-04-27 イナバゴム株式会社 締付固定部材の緩み検出装置
CN103512803B (zh) * 2013-09-26 2016-08-17 吉林大学 多载荷多物理场耦合材料微观力学性能原位测试仪器
US9702797B2 (en) * 2014-09-01 2017-07-11 ScienBiziP Consulting(Shenzhen)Co., Ltd. Supporting apparatus and torsion test measuring device using same
CN104655379B (zh) 2015-03-13 2017-09-29 武汉理工大学 一种用于测试螺纹紧固件防松性能的装置
KR101823118B1 (ko) 2016-03-09 2018-03-08 (주)삼호정기 피스톤핀 검사장치 및 이를 포함하는 피스톤핀 조립시스템
CN105784304B (zh) 2016-05-05 2018-04-10 大连理工大学 一种多功能紧固件测试试验机
CN106769038B (zh) 2016-12-12 2019-04-16 中机试验装备股份有限公司 一种组合加载运动关节轴承试验机
CN107271166B (zh) 2017-06-30 2019-08-23 武汉理工大学 螺纹连接接口防松性能试验装置及其检测方法
CN107505124B (zh) * 2017-08-02 2018-09-04 大连理工大学 一种精确控制横向载荷松脱试验机

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1200148A1 (ru) * 1983-11-25 1985-12-23 Petrov Evgenij N Приспособление дл испытани резьбового соединени на самоотвинчивание под действием раст гивающей нагрузки
DE4311956A1 (de) * 1993-04-10 1994-10-13 Inst Mikrostrukturtechnologie Anordnung zur Bestimmung des Belastungszustandes von Verbindungselementen
JP2011047687A (ja) * 2009-08-25 2011-03-10 Nichiyu Giken Kogyo Co Ltd 引張荷重記録装置
CN103512745A (zh) * 2013-10-12 2014-01-15 无锡创明传动工程有限公司 一种扭矩加载机构
KR20160064636A (ko) * 2014-11-28 2016-06-08 현대위아 주식회사 체결형 볼트의 풀림특성 검출장치
CN107621361A (zh) * 2017-08-02 2018-01-23 大连理工大学 一种基于精确控制螺栓横向载荷松脱试验机的闭环控制方法
CN108444686A (zh) * 2018-03-15 2018-08-24 大连理工大学 一种法兰盘拉弯扭复合加载多螺栓松脱试验机

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112014017A (zh) * 2020-07-30 2020-12-01 南京安润朴新能源科技有限公司 一种新型工业机器人伺服电机齿槽转矩试验台及实验方法
CN112014087A (zh) * 2020-08-26 2020-12-01 株洲时代新材料科技股份有限公司 一种基于拉杆的橡胶节点三向疲劳试验装置
CN112461525A (zh) * 2020-11-20 2021-03-09 中国直升机设计研究所 一种无人直升机发动机安装支架试验装置
CN113390730A (zh) * 2021-06-30 2021-09-14 深圳市优瑞特检测技术有限公司 一种电器板材测试用自动循环弯折实验装置
CN113390730B (zh) * 2021-06-30 2022-10-11 深圳市优瑞特检测技术有限公司 一种电器板材测试用自动循环弯折实验装置
CN116294467A (zh) * 2023-03-15 2023-06-23 绿能纤材(重庆)科技有限公司 一种羧甲基纤维素锂接枝聚丙烯酸锂的烘干粉碎装置
CN117302540A (zh) * 2023-09-14 2023-12-29 成都飞机工业(集团)有限责任公司 一种飞机机翼折叠插销作动器试验测试装置及方法
CN117705449A (zh) * 2024-02-06 2024-03-15 聊城大学 一种向心关节轴承磨损寿命试验系统及试验方法
CN117705449B (zh) * 2024-02-06 2024-04-26 聊城大学 一种向心关节轴承磨损寿命试验系统及试验方法

Also Published As

Publication number Publication date
US20200080914A1 (en) 2020-03-12
US10598567B1 (en) 2020-03-24

Similar Documents

Publication Publication Date Title
WO2019173995A1 (zh) 一种法兰盘拉弯扭复合加载多螺栓松脱试验机
WO2019173994A1 (zh) 一种法兰盘拉弯复合加载多螺栓松脱试验机
WO2020014851A1 (zh) 一种多螺栓松脱试验机横向载荷无级调幅装置
CN105784304B (zh) 一种多功能紧固件测试试验机
CN104655379B (zh) 一种用于测试螺纹紧固件防松性能的装置
WO2016141761A1 (zh) 一种提升机用钢丝绳、摩擦衬垫综合摩擦检测装置及方法
CN105043976A (zh) 一种动态测量微动疲劳过程中微动副摩擦系数的试验装置及试验方法
CN208155713U (zh) 用于弯扭振动疲劳试验的加载装置
CN108444687B (zh) 一种法兰盘拉弯复合加载多螺栓松脱试验机
CN204988981U (zh) 一种动态测量微动疲劳过程中微动副摩擦系数的试验装置
CN108444686B (zh) 一种法兰盘拉弯扭复合加载多螺栓松脱试验机
CN115420494A (zh) 一种集成式刹车油管螺纹接头和螺栓紧固性能测试机
CN206488994U (zh) 拉伸疲劳‑四点弯曲疲劳原位力学测试装置
CN209910965U (zh) 一种螺栓临界松动载荷测定的实验装置
CN204008309U (zh) 一种拉压-扭转复合加载试验机
EP2812156A1 (en) Pretensioning tool and method for tightening a nut
CN108332897B (zh) 一种检测螺栓预紧力高温变化的试验装置
CN114459757B (zh) 一种滚动摩擦副润滑性能测试装置及其测试方法
CN109489976A (zh) 新主轴轴承试验机
CN114018732A (zh) 一种滚动微动疲劳试验装置及试验方法
CN111633602B (zh) 一种发动机离合器安装辅助压紧装置及安装方法
CN108801623B (zh) 一种多螺栓松脱试验机横向载荷无级调幅装置
CN113447369A (zh) 一种针对扭剪型螺栓的扭矩系数试验机
CN204434163U (zh) 一种葫芦限载器调试装置
CN209280313U (zh) 新主轴轴承试验机

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 18909708

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 18909708

Country of ref document: EP

Kind code of ref document: A1