CN205691441U - A kind of laser positioning cold punching automatic test equipment - Google Patents

A kind of laser positioning cold punching automatic test equipment Download PDF

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Publication number
CN205691441U
CN205691441U CN201620485394.9U CN201620485394U CN205691441U CN 205691441 U CN205691441 U CN 205691441U CN 201620485394 U CN201620485394 U CN 201620485394U CN 205691441 U CN205691441 U CN 205691441U
Authority
CN
China
Prior art keywords
support
jump bit
laser
fuselage
guide pipe
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
CN201620485394.9U
Other languages
Chinese (zh)
Inventor
边焕燕
王伟珍
刘伟
陈松
吴兴华
黄小军
唐宝刚
曹轲
乔辉
李创
叶武君
李明海
刘永涛
张力天
王新
张选花
肖会会
江鹏
刘江林
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 ZHONGCAI PROFILES CO Ltd
Original Assignee
XI'AN ZHONGCAI PROFILES 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 XI'AN ZHONGCAI PROFILES CO Ltd filed Critical XI'AN ZHONGCAI PROFILES CO Ltd
Priority to CN201620485394.9U priority Critical patent/CN205691441U/en
Application granted granted Critical
Publication of CN205691441U publication Critical patent/CN205691441U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of laser positioning cold punching automatic test equipment, including support, assembly pulley, jump bit, guide pipe, jump bit capture unit, generating laser, DC electromagnet, jump bit stay cord, described support includes fuselage support, it is arranged on the supporting fuselage bar above fuselage support, it is arranged on the pulley bracket in supporting fuselage masthead portion, top locating rack that side is connected with supporting fuselage bar and laser support, described DC electromagnet is arranged on the locating rack of top, its lower end connects guide pipe, the lower end of described guide pipe arranges laser support, generating laser is set gradually below described laser support, jump bit capture unit, jump bit, one end of described jump bit stay cord is connected with jump bit and on the assembly pulley being set on pulley bracket, the other end is connected with the tup reset machine being arranged on fuselage support side.This utility model simple in construction, improves positioning precision, improves the verity of test data.

Description

A kind of laser positioning cold punching automatic test equipment
Technical field
This utility model belongs to the test field of measuring technique of plastic-steel section bar, is specifically related to a kind of laser positioning cold punching automatic Assay device.
Background technology
In plastic-steel section bar production process, for the control to product quality, under freezing state to be carried out to some kinds Impact test is measured, and traditional equipment availability is the most time-consuming takes a lot of work again, simultaneously it is impossible to ensure that shock point is on cavity of sectional material, causes Test data is inaccurate, causes finished products quality to be not sufficiently stable.
Utility model content
In view of this, main purpose of the present utility model is to provide a kind of laser positioning cold punching automatic test equipment.
For reaching above-mentioned purpose, the technical solution of the utility model is achieved in that
This utility model embodiment provides a kind of laser positioning cold punching automatic test equipment, and this device includes support, pulley Group, jump bit, guide pipe, jump bit capture unit, generating laser, DC electromagnet, jump bit stay cord, described support includes Fuselage support, be arranged on the supporting fuselage bar above fuselage support, be arranged on the pulley bracket in supporting fuselage masthead portion, side with The top locating rack of supporting fuselage bar connection and laser support, described DC electromagnet is arranged on the locating rack of top, its lower end Connecting guide pipe, the lower end of described guide pipe arranges laser support, sets gradually generating laser, punching below described laser support Hammer capture unit, jump bit, one end of described jump bit stay cord is connected with jump bit and around being set on pulley bracket On assembly pulley, the other end is connected with the tup reset machine being arranged on fuselage support side.
In such scheme, the upper end of described guide pipe is connected with top locating rack by positioning sleeve.
In such scheme, described fuselage support is provided above impacting platform.
Compared with prior art, the beneficial effects of the utility model:
This utility model simple in construction, reduces testing crew and reduces to 1 people, improve positioning precision and stop personnel and testing Anthropic factor in journey, improves the verity of test data.
Accompanying drawing explanation
Fig. 1 provides the structural representation of a kind of laser positioning cold punching automatic test equipment for this utility model embodiment.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with accompanying drawing and enforcement Example, is further elaborated to this utility model.Should be appreciated that specific embodiment described herein is only in order to explain This utility model, is not used to limit this utility model.
This utility model embodiment provides a kind of laser positioning cold punching automatic test equipment, as it is shown in figure 1, this device includes Support, assembly pulley 10, jump bit 16, guide pipe 5, jump bit capture unit 14, generating laser 12, DC electromagnet 2, impact Hammer stay cord 11, described support includes fuselage support 8, is arranged on the supporting fuselage bar 6 above fuselage support 8, is arranged on fuselage and props up Top locating rack 3 that the pulley bracket 1 at strut 6 top, side are connected with supporting fuselage bar 6 and laser support 13, described direct current Electric magnet 2 is arranged on top locating rack 3, and its lower end connects guide pipe 5, and the lower end of described guide pipe 5 arranges laser support 13, Setting gradually generating laser 12, jump bit capture unit 14, jump bit 16 below described laser support 13, described jump bit draws Rope 11 one end be connected with jump bit 16 and on the assembly pulley 10 being set on pulley bracket 1, the other end be arranged on machine The tup reset machine 17 of body support 8 side connects.
The upper end of described guide pipe 5 is connected with top locating rack 3 by positioning sleeve 4.
Described fuselage support 8 is provided above impacting platform 7.
Described top locating rack 3 and jump bit capture unit 14 be respectively arranged below photoswitch 18, lower photoelectricity Switch 15.
Detection sample section is placed on impact platform 7, shock surface alignment generating laser 12.Opening on push platform 9 The signal testing machine that dynamic button performs program to PLC mono-is started working according to program, and described jump bit 16 freely falls to be pounded On shock surface, described jump bit 16 is upspring and is detected by lower photoswitch 15, and described jump bit capture unit 14 starts will impact Hammer 16 seizure, the SR on push 9, described tup reset machine 17 starts the location that jump bit 16 is promoted to 1.5m In set 4, going up photoswitch 18 simultaneously and detect jump bit 16, described DC electromagnet 2 is energized and jump bit 16 is fixed on 1.5m Position, jump bit capture unit 14 resets simultaneously, and single test completes.Whole process is by PLC control.
The above, preferred embodiment the most of the present utility model, it is not intended to limit protection of the present utility model Scope.

Claims (3)

1. a laser positioning cold punching automatic test equipment, it is characterised in that this device includes support, assembly pulley, jump bit, leads Xiang Guan, jump bit capture unit, generating laser, DC electromagnet, jump bit stay cord, described support includes fuselage support, sets Put the supporting fuselage bar above fuselage support, be arranged on the pulley bracket in supporting fuselage masthead portion, side and supporting fuselage bar The top locating rack connected and laser support, described DC electromagnet is arranged on the locating rack of top, and its lower end connects guide pipe, The lower end of described guide pipe arranges laser support, sets gradually generating laser, jump bit seizure list below described laser support Unit, jump bit, one end of described jump bit stay cord is connected with jump bit and on the assembly pulley being set on pulley bracket, separately One end is connected with the tup reset machine being arranged on fuselage support side.
A kind of laser positioning cold punching automatic test equipment the most according to claim 1, it is characterised in that: described guide pipe Upper end is connected with top locating rack by positioning sleeve.
A kind of laser positioning cold punching automatic test equipment the most according to claim 1 and 2, it is characterised in that: described fuselage Support is provided above impacting platform.
CN201620485394.9U 2016-05-25 2016-05-25 A kind of laser positioning cold punching automatic test equipment Expired - Fee Related CN205691441U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620485394.9U CN205691441U (en) 2016-05-25 2016-05-25 A kind of laser positioning cold punching automatic test equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620485394.9U CN205691441U (en) 2016-05-25 2016-05-25 A kind of laser positioning cold punching automatic test equipment

Publications (1)

Publication Number Publication Date
CN205691441U true CN205691441U (en) 2016-11-16

Family

ID=57262842

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620485394.9U Expired - Fee Related CN205691441U (en) 2016-05-25 2016-05-25 A kind of laser positioning cold punching automatic test equipment

Country Status (1)

Country Link
CN (1) CN205691441U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108827765A (en) * 2018-08-20 2018-11-16 信义汽车部件(芜湖)有限公司 Glass nailing formula shock machine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108827765A (en) * 2018-08-20 2018-11-16 信义汽车部件(芜湖)有限公司 Glass nailing formula shock machine

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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: 20161116

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