CN204630905U - The proving installation of circular ring structure hardware friction factor - Google Patents

The proving installation of circular ring structure hardware friction factor Download PDF

Info

Publication number
CN204630905U
CN204630905U CN201420818170.6U CN201420818170U CN204630905U CN 204630905 U CN204630905 U CN 204630905U CN 201420818170 U CN201420818170 U CN 201420818170U CN 204630905 U CN204630905 U CN 204630905U
Authority
CN
China
Prior art keywords
compressing member
ring structure
circular ring
pressing plate
structure hardware
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
CN201420818170.6U
Other languages
Chinese (zh)
Inventor
谢林君
任欣
沈明学
林绍萱
张明
薛国宏
梁叶佳
姚伟达
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhejiang University of Technology ZJUT
Shanghai Nuclear Engineering Research and Design Institute Co Ltd
Original Assignee
Zhejiang University of Technology ZJUT
Shanghai Nuclear Engineering Research and Design Institute Co Ltd
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 Zhejiang University of Technology ZJUT, Shanghai Nuclear Engineering Research and Design Institute Co Ltd filed Critical Zhejiang University of Technology ZJUT
Priority to CN201420818170.6U priority Critical patent/CN204630905U/en
Application granted granted Critical
Publication of CN204630905U publication Critical patent/CN204630905U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

A kind of proving installation of circular ring structure hardware friction factor, comprise the testing machine that load is provided, the clutch end of testing machine is fixedly connected with the upper end of cover clamp, compressing member is installed in the lower end of cover clamp, sensor support base is installed in the side of cover clamp, the end face cloth displacement sensor of cover clamp, the lower disposed lower cover pressing plate of cover clamp, lower cover pressing plate is arranged in the frame of testing machine, lower compressing member is installed in the upper end of lower cover pressing plate, upper compressing member and lower compressing member are all ringwise, lower compressing member to be positioned at immediately below compressing member and test station between the two for placing for circular ring structure hardware to be tested, lower sensor bearing is installed in the side of lower cover pressing plate, lower sensor bearing and upper sensor bearing are arranged in pairs, and between lower sensor bearing and upper sensor bearing, deformation-sensor is installed.The utility model structure is simple, easy to operate, rational in infrastructure, effectively measure friction factor, data stabilization is reliable.

Description

The proving installation of circular ring structure hardware friction factor
Technical field
The utility model relates to material property-compress the fields such as resilient ring resiliency test, PVvalue testing as pad and nuclear-power reactor in-pile component, especially a kind of proving installation of circular ring structure hardware friction factor.
Background technology
Pressure vessel that is large-scale or that work under harsh working condition is very strict to the performance requirement of the hermetically-sealed construction of circular ring metal pad.Work normally to make gasket seal, ensure that sealing property often needs to carry out resiliency test to circular ring metal pad, simultaneously in install operation process, in order to compress gasket often needs to apply pretightning force, and the impact that there is friction force due to gasket surface and flange causes the pretightning force that applies and design load to there is gap, therefore also needs to calculate its friction factor.Thus there is not seal leakage in guarantee equipment, safe and reliable operation.
In addition, the compression resilient ring of CAP1400 and AP1000 nuclear reactor in-pile component is a kind of circular compression type springs, and it has certain elastic rebound ability and can keep necessary snap-in force.It is between upper support flange and cradle cylinder body flange, when top cover of reactor pressure vessel tools for bolts ' pretension, resilient ring can be compressed predetermined deflection, its pretightning force produced makes cradle cylinder body assembly and upper support board component location, under accidental conditions, cradle cylinder body assembly can not make the contacted pine between itself and two flange interfaces because the pretightning force of resilient ring is too small, thus the Flow vibration causing cradle cylinder body assembly excessive.Meanwhile, resilient ring pretightning force can not be excessive and exceed its elastic range, thus cause resilient ring deformation resilience amount to reduce, and cradle cylinder body assembly Flow vibration amplitude also can be caused for a long time to increase and frequency reduction.But find when resilient ring design analysis, resilient ring and the friction force up and down between flange contact facings can directly affect its axial rigidity.When friction factor increases, its axial rigidity value is corresponding can increase, and the axial pre tightening force needed under making identical initial deformation condition increases, and also makes its ring inner-stress value increase.Because the friction factor of reality can not obtain from analysis; For this reason, need the side amount of carrying out resilient ring being carried out to friction factor, to obtain the relation between the parameters such as the axial force of resilient ring and axial displacement, finally calculate the friction factor on surface of contact.Therefore, resilient ring friction factor compresses resilient ring mounting design to nuclear reactor and plays vital effect, also runs important impact reliably to nuclear reactor safety.
Utility model content
In order to overcome the deficiency effectively cannot measuring the friction factor of circular ring structure hardware in prior art, the utility model provides the proving installation that a kind of structure is simple, easy to operate, rational in infrastructure, effectively measure friction factor, data stabilization reliable circular ring structure hardware friction factor.
The utility model solves the technical scheme that its technical matters adopts:
A kind of proving installation of circular ring structure hardware friction factor, comprise the testing machine in order to imposed load, the stationary end of described testing machine is fixedly connected with the upper end of cover clamp, compressing member is installed in the lower end of described cover clamp, sensor support base is installed in the side of described cover clamp, the end face of described cover clamp arranges the displacement transducer of the axial displacement for detecting circular ring structure hardware to be tested, the lower disposed lower cover pressing plate of described cover clamp, described lower cover pressing plate is arranged in the frame of described testing machine, lower compressing member is installed in the upper end of described lower cover pressing plate, described upper compressing member and lower compressing member are all ringwise, described lower compressing member to be positioned at immediately below compressing member and test station between the two for placing for circular ring structure hardware to be tested, lower sensor bearing is installed in the side of described lower cover pressing plate, described lower sensor bearing and upper sensor bearing are arranged in pairs, and the sensor of the axial deformation for detecting circular ring structure hardware to be tested is installed between described lower sensor bearing and upper sensor bearing.
Further, described cover clamp comprises cylinder arc and multidiameter pressing plate, the upper end of described cylinder arc is provided with the link with threaded hole, and described link is connected with the clutch end of described testing machine, and the lower end of described cylinder arc is fixedly connected with described multidiameter pressing plate.
The described bottom pressing down cover plate with spherical coordinate to pad be connected, described spherical cooperation pad coordinates with the spherical base in testing machine frame.
Institute's displacement sensors is milscale, and described deformation-sensor is extensometer.
Institute's displacement sensors has at least two, and the circular arc intervals such as at least two displacement transducers are arranged on a circle; Describedly extend in respect of at least two, the circular arc intervals such as at least two extensometers are arranged on a circle.
The first order axial end of described multidiameter pressing plate is for placing clock gauge, and described upper compressing member is placed in the axle lower surface, the second level of described multidiameter pressing plate.
Described lower cover pressing plate has multidiameter shape, and first end mask requires smooth surface and parallels with upper press cover plate end face; Second end face places described lower compressing member; Second level axle periphery fixes described lower sensor bearing; Be cylindrical hole in the middle part of third level axle lower surface, in described cylindrical hole, place described spherical cooperation pad.
Described upper compressing member and lower compressing member are annulus, and two end faces of described annulus are parallel to each other.
Match with the lower surface of upper press cover plate second level axle in the upper surface of described upper compressing member, the lower surface of described upper compressing member contacts with circular ring structure hardware to be tested; The thickness of described upper compressing member is identical with the thickness of cover clamp third level axle, and the internal diameter of described upper compressing member is identical with the diameter of third level axle, and the external diameter of described upper compressing member is then consistent with second level shaft diameter;
The upper surface of described lower compressing member contacts with circular ring structure hardware to be tested, the lower surface of described lower compressing member coordinates with the upper surface of the second level axle of lower cover pressing plate, the thickness of described lower compressing member is identical with the thickness of lower cover pressing plate first order axle, the internal diameter of described lower compressing member is identical with the diameter of second level axle, and the external diameter of described lower compressing member is then consistent with first order shaft diameter.Described spherical cooperation pad comprises cylindrical bottom and spherical head, the top of described cylindrical bottom is arranged on and presses down in the cylindrical groove of cover plate, the bottom of described cylindrical bottom and spherical head, described spherical base has the concave sphere mated with described spherical head.
The beneficial effects of the utility model are mainly manifested in: structure is simple, easy to operate, rational in infrastructure, effectively measure friction factor, data stabilization is reliable.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of the proving installation of circular ring structure hardware friction factor.
Fig. 2 is the schematic diagram of cover clamp.
Fig. 3 is the schematic diagram of lower cover pressing plate.
Fig. 4 is the schematic diagram of upper compressing member and lower compressing member.
Fig. 5 is the schematic diagram of circular ring structure hardware.
Fig. 6 is the spherical schematic diagram coordinating pad.
Fig. 7 is the schematic diagram of upper sensor bearing and lower sensor bearing.
Embodiment
Below in conjunction with accompanying drawing, the utility model is further described.
With reference to Fig. 1 ~ Fig. 7, the proving installation of circular ring structure hardware friction factor, comprise the testing machine 1 that load is provided, the stationary end of described testing machine 1 is fixedly connected with the upper end of cover clamp 2, compressing member 3 is installed in the lower end of described cover clamp 2, sensor support base 4 is installed in the side of described cover clamp 3, the end face of described cover clamp 2 arranges the displacement transducer 5 of the axial displacement for detecting circular ring structure hardware to be tested, the lower disposed lower cover pressing plate 6 of described cover clamp 2, described lower cover pressing plate 6 is arranged in the frame of described testing machine 1, lower compressing member 7 is installed in the upper end of described lower cover pressing plate 6, described upper compressing member 3 and lower compressing member 7 are all ringwise, described lower compressing member 7 to be positioned at immediately below compressing member 3 and test station between the two for placing for circular ring structure hardware 8 to be tested, lower sensor bearing 9 is installed in the side of described lower cover pressing plate 6, described lower sensor bearing 9 and upper sensor bearing 4 are arranged in pairs, and the deformation-sensor 10 of the axial deformation for detecting circular ring structure hardware to be tested is installed between described lower sensor bearing 9 and upper sensor bearing 4.
Further, described cover clamp 2 comprises cylinder arc and multidiameter pressing plate, the upper end of described cylinder arc is provided with the link with threaded hole, and described link is connected with the clutch end of described testing machine 1, and the lower end of described cylinder arc is fixedly connected with described multidiameter pressing plate.
The described bottom pressing down cover plate 6 is connected with spherical cooperation pad 11, and described spherical cooperation pad 11 coordinates with the spherical base in testing machine 1 frame.
Institute's displacement sensors 5 is milscale, and described deformation-sensor 10 is extensometer.
Institute's displacement sensors 5 has at least two, and at least two intervals such as displacement transducer 5 circular arc such as grade are arranged on a circle; Describedly extend in respect of at least two, the circular arc intervals such as at least two extensometers are arranged on a circle.
The first order axial end of described multidiameter pressing plate is for placing clock gauge, and described upper compressing member is placed in the axle lower surface, the second level of described multidiameter pressing plate.
Described lower cover pressing plate 6 has multidiameter shape, and first end mask requires smooth surface and parallels with upper press cover plate end face; Second end face places described lower compressing member; Second level axle periphery fixes described lower sensor bearing; Be cylindrical hole in the middle part of third level axle lower surface, in described cylindrical hole, place described spherical cooperation pad.
Described upper compressing member 3 and lower compressing member 7 are annulus, and two end faces of described annulus are parallel to each other.
Match with the lower surface of upper press cover plate 2 second level axle in the upper surface of described upper compressing member 3, the lower surface of described upper compressing member 3 contacts with circular ring structure hardware 8 to be tested; The thickness of described upper compressing member 3 is identical with the thickness of cover clamp third level axle, and the internal diameter of described upper compressing member 3 is identical with the diameter of third level axle, and the external diameter of described upper compressing member 3 is then consistent with second level shaft diameter;
The upper surface of described lower compressing member 7 contacts with circular ring structure hardware 8 to be tested, the lower surface of described lower compressing member 7 coordinates with the upper surface of the second level axle of lower cover pressing plate 6, the thickness of described lower compressing member 7 is identical with the thickness of lower cover pressing plate first order axle, the internal diameter of described lower compressing member 7 is identical with the diameter of second level axle, and the external diameter of described lower compressing member 7 is then consistent with first order shaft diameter.
Described spherical cooperation pad 11 comprises cylindrical bottom and spherical head, the top of described cylindrical bottom is arranged on and presses down in the cylindrical groove of cover plate, the bottom of described cylindrical bottom and spherical head, described spherical base has the concave sphere mated with described spherical head.
In the present embodiment, first cover clamp 2 is fixed by bolt and testing machine, thus hang on testing machine 1, and upper compressing member 3 is fixed on the below of upper press cover plate 2 by sunk screw, upper sensor bearing 4 is fixed on outside upper press cover plate 2; In addition, spherical cooperation pad 11 is positioned over the centre below testing machine, lower cover pressing plate 6 is assembled with thereon; The outside cylinder of lower cover pressing plate 6 is bolted 4 lower sensor bearings 9, and lower compressing member 7 is inserted in the upper end of lower cover pressing plate 6, and is mounted thereon by sunk screw.Thereafter the circular ring structure hardware 8 to be tested of circular ring structure is placed on the inner ring surface of lower compressing member 7; Finally, 4 extensometers are bundled between upper sensor bearing 4 and lower sensor bearing 9,4 clock gauges are placed on the second ladder axial plane of cover clamp 2.
After described device installation, progressively loaded by the circular ring structure hardware 8 to be tested of testing machine 1 to test, often load the clock gauge and extensometer data that once record load p and correspondence, be loaded into setting load from 0 load after, start to be unloaded to 0 load; To 4 clock gauges get its mean value as its test member average displacement, get the average deformation of 4 extensometers as average deformation δ, thus can draw and obtain deformation under load (P-δ) data and compactibility curve.
Further again, described drafting obtains deformation under load (P-δ) data, and also P is horizontal ordinate, and δ is that ordinate carries out matching according to least square method, thus obtains its softness factor λ; Test member friction factor f can be obtained by carrying out mechanics derivation to ring component,
Described derivation formula is as follows:
f = a h - 2 π J x E ahc · δ p
Wherein, a is the annular width of circular ring structure hardware; C is the inside radius of circular ring structure hardware; H is the thickness of circular ring structure hardware; J xfor the moment of inertia of circular ring structure hardware; E is elastic modulus; δ is (displacement) deflection; P is load.

Claims (10)

1. the proving installation of a circular ring structure hardware friction factor, it is characterized in that: described proving installation comprises the testing machine in order to imposed load, the stationary end of described testing machine is fixedly connected with the upper end of cover clamp, compressing member is installed in the lower end of described cover clamp, sensor support base is installed in the side of described cover clamp, the end face of described cover clamp arranges the displacement transducer of the axial displacement for detecting circular ring structure hardware to be tested, the lower disposed lower cover pressing plate of described cover clamp, described lower cover pressing plate is arranged in the frame of described testing machine, lower compressing member is installed in the upper end of described lower cover pressing plate, described upper compressing member and lower compressing member are all ringwise, described lower compressing member to be positioned at immediately below compressing member and test station between the two for placing for circular ring structure hardware to be tested, lower sensor bearing is installed in the side of described lower cover pressing plate, described lower sensor bearing and upper sensor bearing are arranged in pairs, and the sensor of the axial deformation for detecting circular ring structure hardware to be tested is installed between described lower sensor bearing and upper sensor bearing.
2.2 .the proving installation of circular ring structure hardware friction factor as claimed in claim 1, it is characterized in that: described cover clamp comprises cylinder arc and multidiameter pressing plate, the upper end of described cylinder arc is provided with the link with threaded hole, described link is connected with the clutch end of described testing machine, and the lower end of described cylinder arc is fixedly connected with described multidiameter pressing plate.
3.3 .the proving installation of circular ring structure hardware friction factor as claimed in claim 1 or 2, is characterized in that: described in press down cover plate bottom with spherical coordinate to pad be connected, described spherical cooperation pad coordinates with the spherical base in testing machine frame.
4.4 .the proving installation of circular ring structure hardware friction factor as claimed in claim 1 or 2, is characterized in that: institute's displacement sensors is milscale, and described deformation-sensor is extensometer.
5.5 .the proving installation of circular ring structure hardware friction factor as claimed in claim 4, is characterized in that: institute's displacement sensors has at least two, and the circular arc intervals such as at least two displacement transducers are arranged on a circle; Describedly extend in respect of at least two, the circular arc intervals such as at least two extensometers are arranged on a circle.
6.6 .the proving installation of circular ring structure hardware friction factor as claimed in claim 2, is characterized in that: the first order axial end of described multidiameter pressing plate is for placing clock gauge, and described upper compressing member is placed in the axle lower surface, the second level of described multidiameter pressing plate.
7.7 .the proving installation of circular ring structure hardware friction factor as claimed in claim 3, is characterized in that: described lower cover pressing plate has multidiameter shape, and first end mask requires smooth surface and parallels with upper press cover plate end face; Second end face places described lower compressing member; Second level axle periphery fixes described lower sensor bearing; Be cylindrical hole in the middle part of third level axle lower surface, in described cylindrical hole, place described spherical cooperation pad.
8.8 .the proving installation of circular ring structure hardware friction factor as claimed in claim 1 or 2, is characterized in that: described upper compressing member and lower compressing member are annulus, and two end faces of described annulus are parallel to each other.
9.9 .the proving installation of circular ring structure hardware friction factor as claimed in claim 8, it is characterized in that: match with the lower surface of upper press cover plate second level axle in the upper surface of described upper compressing member, the lower surface of described upper compressing member contacts with circular ring structure hardware to be tested; The thickness of described upper compressing member is identical with the thickness of cover clamp third level axle, and the internal diameter of described upper compressing member is identical with the diameter of third level axle, and the external diameter of described upper compressing member is then consistent with second level shaft diameter;
The upper surface of described lower compressing member contacts with circular ring structure hardware to be tested, the lower surface of described lower compressing member coordinates with the upper surface of the second level axle of lower cover pressing plate, the thickness of described lower compressing member is identical with the thickness of lower cover pressing plate first order axle, the internal diameter of described lower compressing member is identical with the diameter of second level axle, and the external diameter of described lower compressing member is then consistent with first order shaft diameter.
10.10 .the proving installation of circular ring structure hardware friction factor as claimed in claim 3, it is characterized in that: described spherical cooperation pad comprises cylindrical bottom and spherical head, the top of described cylindrical bottom is arranged on and presses down in the cylindrical groove of cover plate, the bottom of described cylindrical bottom and spherical head, described spherical base has the concave sphere mated with described spherical head.
CN201420818170.6U 2014-12-22 2014-12-22 The proving installation of circular ring structure hardware friction factor Expired - Fee Related CN204630905U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420818170.6U CN204630905U (en) 2014-12-22 2014-12-22 The proving installation of circular ring structure hardware friction factor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420818170.6U CN204630905U (en) 2014-12-22 2014-12-22 The proving installation of circular ring structure hardware friction factor

Publications (1)

Publication Number Publication Date
CN204630905U true CN204630905U (en) 2015-09-09

Family

ID=54049922

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420818170.6U Expired - Fee Related CN204630905U (en) 2014-12-22 2014-12-22 The proving installation of circular ring structure hardware friction factor

Country Status (1)

Country Link
CN (1) CN204630905U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106680199A (en) * 2017-01-24 2017-05-17 浙江工业大学 Hydraulic driving-based frictional resistance coefficient testing device
CN110006821A (en) * 2019-05-09 2019-07-12 北京长城华冠汽车技术开发有限公司 A kind of steel plate and bushing friction coefficient measuring apparatus and measurement method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106680199A (en) * 2017-01-24 2017-05-17 浙江工业大学 Hydraulic driving-based frictional resistance coefficient testing device
CN106680199B (en) * 2017-01-24 2023-10-20 浙江工业大学 Friction resistance coefficient testing device based on hydraulic drive
CN110006821A (en) * 2019-05-09 2019-07-12 北京长城华冠汽车技术开发有限公司 A kind of steel plate and bushing friction coefficient measuring apparatus and measurement method
CN110006821B (en) * 2019-05-09 2021-08-17 北京长城华冠汽车技术开发有限公司 Device and method for measuring friction coefficient of steel plate and bushing

Similar Documents

Publication Publication Date Title
CN104132805A (en) Multifunctional pneumatic reciprocating sealing performance test bench
CN207798567U (en) A kind of airtight and watertight padding compression recovery performance experimental rig
CN204630905U (en) The proving installation of circular ring structure hardware friction factor
CN104006939A (en) Device for measuring nonlinear characteristic of spring
CN204964302U (en) Flexible material compression stress and strain digital display formula testing arrangement
CN203785964U (en) Digital portable press
CN104535491A (en) Device for testing friction coefficient of circular ring structure metal component
CN208083739U (en) Pressure sensitive collet
CN201967132U (en) Discrete test fixture for mobile phone electron-phonon
CN211477021U (en) Device for detecting elongation dispersity of whole-circle fastening bolt of large pump gland
CN110672436B (en) Compression-shear testing machine
CN205918703U (en) External displacement sensor is used to pneumatic cylinder dynamic testing
CN208840838U (en) For the press fitting of engine spindle Front oil seal and displacement sensor gradient device
CN203732249U (en) Disc spring test device
CN105486436A (en) Circular load sensor
CN109341983A (en) A kind of pressure measuring tool
CN209166771U (en) A kind of spring test device
CN204757854U (en) Measurement device for it preloads to be used for angular contact ball bearing to apply
CN203894014U (en) Device for measuring non-linear characteristics of spring
CN103439044A (en) System and method for testing yaw clamping force
CN220339620U (en) Mattress elasticity test equipment
CN203275193U (en) Track-gauge block detecting device
CN209727456U (en) A kind of device for survey aircraft undercarriage bearing radial gap
CN220438024U (en) Bellows bearing capacity test device
CN201434672Y (en) Device for testing irregular compression permanent deformation of seal strip

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150909

Termination date: 20171222

CF01 Termination of patent right due to non-payment of annual fee