CN203894096U - Disc spring stiffness calibration testing device - Google Patents

Disc spring stiffness calibration testing device Download PDF

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Publication number
CN203894096U
CN203894096U CN201420339593.XU CN201420339593U CN203894096U CN 203894096 U CN203894096 U CN 203894096U CN 201420339593 U CN201420339593 U CN 201420339593U CN 203894096 U CN203894096 U CN 203894096U
Authority
CN
China
Prior art keywords
circular base
disc spring
testing device
disk spring
spring stiffness
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
CN201420339593.XU
Other languages
Chinese (zh)
Inventor
王燕洁
赵文华
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.)
Xi'an Desheng non-standard equipment manufacturing Co., Ltd.
Original Assignee
AVIC Aircraft Strength Research Institute
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 AVIC Aircraft Strength Research Institute filed Critical AVIC Aircraft Strength Research Institute
Priority to CN201420339593.XU priority Critical patent/CN203894096U/en
Application granted granted Critical
Publication of CN203894096U publication Critical patent/CN203894096U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model belongs to the field of aerial test tools and fixtures and relates to a disc spring stiffness calibration testing device. The disc spring stiffness calibration testing device comprises an upper circular base, a lower circular base and a positioning shaft, wherein cylindrical sections of the upper circular base and the lower circular base are respectively connected with an upper chuck and a lower chuck in a material testing machine; the positioning shaft is positioned between the upper circular base and the lower circular base and is positioned on a central axis of the cylindrical sections of the upper circular base and the lower circular base; a disc spring is positioned at a positioning hole of the lower base by virtue of the positioning shaft. According to the testing device, the disc spring stiffness testing precision is improved, the working efficiency is improved, and the testing device has the characteristics of compact structure, convenience in use and low manufacturing cost.

Description

A kind of disk spring rigidity rating test device
Technical field
The utility model belongs to Aviation Test frock clamp field, relates to a kind of device for disk spring rigidity rating test.
Background technology
At undercarriage, fall, in shimmy test, some testing requirements Reality simulation fuselage mode and the local rigidity of supporting, this just needs application simulation device simulation rigidity, contain a lot of different size disk springs, and most of criteria of right and wrong part needs processing in simulator.And disk spring is after processing, need in Material Testing Machine, to each disk spring, carry out rigidity demarcation, owing to there is no the caliberating device of special-purpose fixedly disk spring in Material Testing Machine, at timing signal, easily there is bias in disk spring, the rigidity test data of measuring have error, be difficult to warranty test quality, and install take a lot of work, time-consuming, inefficiency.
Utility model content
The purpose of this utility model: a kind of easy adjusting, disk spring rigidity rating test device that precision is higher are provided.
The technical solution of the utility model: a kind of disk spring rigidity rating test device, it comprises circular upper bed-plate, circular lower bottom base, locating shaft, wherein, the cylindrical section part of circular upper bed-plate and circular lower bottom base is connected with lower chuck with the upper chuck in Material Testing Machine respectively, described locating shaft is positioned in the middle of circular upper bed-plate and circular lower bottom base, on axis in the two cylindrical section, and disk spring is positioned at the pilot hole place of circular lower bottom base by locating shaft.
The beneficial effects of the utility model: the utility model disk spring rigidity rating test device is by changing the locating shaft of different size, can realize a covering device rigidity demarcation that just can complete plurality of specifications disk spring is once installed in Material Testing Machine, for the rigidity of disk spring in demarcation, occur and computational data error amount larger, can find in time and do rational adjustment.This device can make the trueness error of disk spring rigidity test be reduced in 3% by 10% original left and right, to guarantee the high-quality test that completes.The utility model has not only improved the precision of disk spring rigidity test but also has improved work efficiency, also has compact conformation, easy to use, the feature of low cost of manufacture.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation;
Structural representation when Fig. 2 is the utility model work.
Wherein, the circular upper bed-plate of 1-, 2-locating shaft, the circular lower bottom base of 3-, 4-butterfly spring, 5-upper chuck, 6-lower chuck.
Embodiment
Below by embodiment, the utility model is described in further detail:
Refer to Fig. 1, it is that the utility model is for the apparatus structure schematic diagram of butterfly spring rigidity rating test.Described disk spring rigidity rating test device comprises circular upper bed-plate 1, circular lower bottom base 3, locating shaft 2, wherein, the cylindrical section part of circular upper bed-plate 1 and circular lower bottom base 3 is connected with lower chuck 6 with the upper chuck 5 in Material Testing Machine respectively, to guarantee the location of disk spring 4 in Material Testing Machine.Described locating shaft 2 is positioned in the middle of circular upper bed-plate 1 and circular lower bottom base 3, and on the axis in the two cylindrical section, disk spring 4 is positioned at the pilot hole place of lower bottom base 2 by locating shaft 2.
Described locating shaft 2 is made into multiple different specification according to the specification of butterfly spring.
It is motionless that the circular upper bed-plate 1 of the utility model timing signal and circular lower bottom base 3 are connected with Material Testing Machine, only need can realize the covering device rigidity that once installation just can complete plurality of specifications disk spring in Material Testing Machine by the locating shaft of replacing different size and demarcate.For the rigidity of disk spring in demarcation, occur and computational data error amount larger, can find in time and do rational adjustment.This device can make the trueness error of disk spring rigidity test be reduced in 3% by 10% original left and right, to guarantee the high-quality test that completes.The utility model has not only improved the precision of disk spring rigidity test but also has improved work efficiency, also has compact conformation, easy to use, the feature of low cost of manufacture.

Claims (1)

1. a disk spring rigidity rating test device, it is characterized in that: comprise circular upper bed-plate (1), circular lower bottom base (3), locating shaft (2), wherein, the cylindrical section part of circular upper bed-plate (1) and circular lower bottom base (3) is connected with lower chuck with the upper chuck in Material Testing Machine respectively, described locating shaft (2) is positioned in the middle of circular upper bed-plate (1) and circular lower bottom base (3), on axis in the two cylindrical section, and disk spring (4) is positioned at the pilot hole place of circular lower bottom base (3) by locating shaft (2).
CN201420339593.XU 2014-06-24 2014-06-24 Disc spring stiffness calibration testing device Expired - Fee Related CN203894096U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420339593.XU CN203894096U (en) 2014-06-24 2014-06-24 Disc spring stiffness calibration testing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420339593.XU CN203894096U (en) 2014-06-24 2014-06-24 Disc spring stiffness calibration testing device

Publications (1)

Publication Number Publication Date
CN203894096U true CN203894096U (en) 2014-10-22

Family

ID=51720486

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420339593.XU Expired - Fee Related CN203894096U (en) 2014-06-24 2014-06-24 Disc spring stiffness calibration testing device

Country Status (1)

Country Link
CN (1) CN203894096U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105527079A (en) * 2015-12-03 2016-04-27 北京机械设备研究所 Dynamic calibration method for springs

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105527079A (en) * 2015-12-03 2016-04-27 北京机械设备研究所 Dynamic calibration method for springs

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
EE01 Entry into force of recordation of patent licensing contract

Assignee: Xi'an Desheng non-standard equipment manufacturing Co., Ltd.

Assignor: China Plane Intensity Research Institute

Contract record no.: 2015610000110

Denomination of utility model: Disc spring stiffness calibration testing device

Granted publication date: 20141022

License type: Exclusive License

Record date: 20151224

LICC Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model
EC01 Cancellation of recordation of patent licensing contract

Assignee: Xi'an Desheng non-standard equipment manufacturing Co., Ltd.

Assignor: China Plane Intensity Research Institute

Contract record no.: 2015610000110

Date of cancellation: 20160222

LICC Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model
C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20160310

Address after: 710065, No. two, No. 3, Yanta District, Shaanxi, Xi'an

Patentee after: Xi'an Desheng non-standard equipment manufacturing Co., Ltd.

Address before: 710065 box 86, Xi'an, Shaanxi, Xi'an

Patentee before: China Plane Intensity Research Institute

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

Granted publication date: 20141022

Termination date: 20200624