CN207095542U - A kind of vehicular four wheels position indicator calibrating installation - Google Patents

A kind of vehicular four wheels position indicator calibrating installation Download PDF

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Publication number
CN207095542U
CN207095542U CN201721012108.8U CN201721012108U CN207095542U CN 207095542 U CN207095542 U CN 207095542U CN 201721012108 U CN201721012108 U CN 201721012108U CN 207095542 U CN207095542 U CN 207095542U
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China
Prior art keywords
fuselage
pillar
plc
support
vehicular
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CN201721012108.8U
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Chinese (zh)
Inventor
李念强
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Shandong Group Is Still Network Polytron Technologies Inc
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Shandong Group Is Still Network Polytron Technologies Inc
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Abstract

The utility model discloses a kind of vehicular four wheels position indicator calibrating installation,Including fuselage,The top of the fuselage is provided with geometrical clamp,The top of the geometrical clamp is provided with display,The display nesting is arranged at the inside of the geometrical clamp,The display is fixedly connected with the fuselage by the geometrical clamp,The offside of the display is provided with the pillar of column,The top of the pillar is provided with warning light,The warning light insertion is arranged at the inside of the pillar,And it is screwed and is connected with the pillar,The side of the branch outer surface of column is provided with turn-button,The turn-button is disposed through the inside of the pillar,And it is fixedly connected with the pillar,The end of the turn-button is provided with support,The end of the support is provided with fixed plate,This kind of vehicular four wheels position indicator calibrating installation,Bracket end is provided with CM05 imaging sensors,Reach measurement purpose based on graphical analysis is carried out after optical imagery,Enable users to quickly obtain visual effect.

Description

A kind of vehicular four wheels position indicator calibrating installation
Technical field
Wheel alignment collimation technique field is the utility model is related to, specially a kind of vehicular four wheels position indicator calibrating installation.
Background technology
So-called wheel alignment calibration, course refer to whether shift or distorted now with vehicle body in side automotive check wheel As instructing user to adjust accordingly wheel alignment parameter, complying with former design requirement, to reach preferable garage Performance is sailed, that is, manipulates that light, driving stability is reliable, reduces the fine measuring instrument of tire partial wear, everybody most commonly draws Line position indicator, CCD position indicators, laser orientation instru-ment etc..
But existing wheel alignment calibrating installation volume is big, quality weight, it is impossible to there will be the problem of be exposed directly to user, Poor intuition, stability are poor, it is impossible to arbitrarily adjust test side, reduce applicability, due to being frequently used for outwork, reduce Service life adds the operating time of user, it is necessary to the artificial detection end position of regulation one by one, complicated, cumbersome, clearly Clean difficulty is big.
So how to design a kind of vehicular four wheels position indicator calibrating installation, turning into us will currently solve the problems, such as.
Utility model content
The purpose of this utility model is to provide a kind of vehicular four wheels position indicator calibrating installation, to solve above-mentioned background technology The problem of middle proposition.
To achieve the above object, the utility model provides following technical scheme:A kind of vehicular four wheels position indicator calibrating installation, Including fuselage, the top of the fuselage is provided with geometrical clamp, and the top of the geometrical clamp is provided with display, and the display nesting is set The inside of the geometrical clamp is placed in, the display is fixedly connected with the fuselage by the geometrical clamp, the display Offside is provided with the pillar of column, and the top of the pillar is provided with warning light, and the warning light insertion is arranged at the interior of the pillar Portion, and be screwed and be connected with the pillar, the side of the branch outer surface of column is provided with turn-button, and the turn-button is through setting It is fixedly connected in the inside of the pillar, and with the pillar, the end of the turn-button is provided with support, and the end of the support is set There is fixed plate, the side of the fixed plate is provided with fixing hole, and the fixed plate nesting is arranged on the surface of the support, described Fixed plate is fixedly connected with the support by the fixing hole, and the end of the fixed plate is equipped with camera, the shooting Head is embedded to be arranged at the end of the fixed plate, and is fixedly connected with the fixed plate, and the inside of the pillar is provided with drive link, The adjacent side of the drive link is provided with telescopic mast, and the end of the telescopic mast is equipped with sliding shoe, the pillar and the telescopic mast It is flexibly connected by the sliding shoe, the lateral surface of the fuselage is locked provided with case, and the case lock is disposed through the fuselage Inside, and be fixedly connected with the fuselage by nut, the adjacent side of the case lock is provided with chamber door, and the bottom of the fuselage is provided with rolling Wheel, roller insertion is arranged at the inside of the fuselage, and is bolted to connection with the fuselage, the fuselage it is interior Portion is provided with dual-mode antenna, and the offside of the dual-mode antenna is provided with plc, and the dual-mode antenna is compiled with described The centre position of journey cyclelog is provided with data wire, and the data wire is disposed through the dual-mode antenna and may be programmed with described The inside of cyclelog, the dual-mode antenna are connected with the plc by the data line signal, institute The bottom for stating plc is provided with battery, and the battery is set in parallel in the plc Bottom, and be electrically connected with the plc, the centre of the battery and the plc Position is provided with backing plate.
Further, the side of the branch outer surface of column is provided with loudspeaker, and the loudspeaker nesting is arranged at the table of the pillar On face, and it is screwed and is connected with the pillar.
Further, the end of the support is equipped with CM05 imaging sensors, and the CM05 imaging sensors insertion is set The end of the support is placed in, and is fixedly connected with the support.
Further, the side of the fuselage is provided with solar panels, and the solar panels are set in parallel in the fuselage Side, and bonded with the fuselage by glue.
Further, the end of the chamber door is provided with rotating shaft, and the shaft parallel is arranged at the end of the chamber door, and with The chamber door welding.
Further, the adjacent side of the plc is provided with coldplate, and the coldplate tiling is arranged at institute The side of plc is stated, and is fixedly connected with the plc by spiral shell button.
Compared with prior art, the beneficial effects of the utility model are:This kind of vehicular four wheels position indicator calibrating installation, volume Small, light weight, bracket end is provided with CM05 imaging sensors, reaches measurement mesh based on graphical analysis is carried out after optical imagery , enable users to quickly obtain visual effect, pillar lateral surface is provided with loudspeaker, can read the result drawn after scanning, convenient User goes and finds out what's going on, and solar panels can effectively absorb heat and provide operating power source for fuselage, so that user is used for outwork, Chamber door can reduce the noise of fuselage interior device work, while facilitate user to be cleaned, and reduce maintenance cost, may be programmed journey The coldplate of sequence controller neighbour side can effectively absorb plc work caused by heat, prevent programmable program Controller because there is auto-ignition in high temperature, plc can in time there will be the problem of calibrated, export simultaneously Figure after problem figure and calibration is made comparisons to user, enhances using effect, the turn-button of pillar lateral surface can facilitate user according to Need to rotate support, improve applicability, the telescopic mast inside pillar can carry out extension work as needed, reduce The operating time of user, stability is good, service life length, simple in construction, simple and quick.
Brief description of the drawings
Fig. 1 is overall structure diagram of the present utility model;
Fig. 2 is fuselage interior structural representation of the present utility model;
Fig. 3 is pillar partial structural diagram of the present utility model;
In figure:1- fuselages;2- geometrical clamps;3- displays;4- pillars;5- warning lights;6- loudspeaker;7- turn-buttons;8- fixed plates; 9- cameras;10- fixing holes;11-CM05 imaging sensors;12- solar panels;13- casees are locked;14- chamber doors;15- rotating shafts;16- Roller;17- dual-mode antennas;18- data wires;19- coldplates;20- plcs;21- backing plates;22- batteries; 23- drive links;24- telescopic masts;25- sliding shoes;26- supports.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made The every other embodiment obtained, belong to the scope of the utility model protection.
Fig. 1-3 are referred to, the utility model provides a kind of technical scheme:A kind of vehicular four wheels position indicator calibrating installation, bag Fuselage 1 is included, the top of the fuselage 1 is provided with geometrical clamp 2, and the top of the geometrical clamp 2 is provided with display 3, and the display 3 is embedding Set is arranged at the inside of the geometrical clamp 2, and the display 3 is fixedly connected with the fuselage 1 by the geometrical clamp 2, described The offside of display 3 is provided with the pillar 4 of column, and the top of the pillar 4 is provided with warning light 5, and the insertion of warning light 5 is arranged at The inside of the pillar 4, and be screwed and be connected with the pillar 4, the side of the outer surface of pillar 4 is provided with turn-button 7, The turn-button 7 is disposed through the inside of the pillar 4, and is fixedly connected with the pillar 4, and the end of the turn-button 7 is provided with Support 26, the end of the support 26 are provided with fixed plate 8, and the side of the fixed plate 8 is provided with fixing hole 10, the fixed plate 8 Nesting is arranged on the surface of the support 26, and the fixed plate 8 is fixedly connected with the support 26 by the fixing hole 10, The end of the fixed plate 8 is equipped with camera 9, and the camera 9 is embedded in the end for being arranged at the fixed plate 8, and with institute Fixed plate 8 to be stated to be fixedly connected, the inside of the pillar 4 is provided with drive link 23, and the adjacent side of the drive link 23 is provided with telescopic mast 24, The end of the telescopic mast 24 is equipped with sliding shoe 25, and the pillar 4 passes through the activity of sliding shoe 25 with the telescopic mast 24 Connection, the lateral surface of the fuselage 1 are provided with case lock 13, and the case lock 13 is disposed through the inside of the fuselage 1, and with it is described Fuselage 1 is fixedly connected by nut, and the adjacent side of the case lock 13 is provided with chamber door 14, and the bottom of the fuselage 1 is provided with roller 16, institute State roller 16 and be embedded in and be arranged at the inside of the fuselage 1, and be bolted to connection with the fuselage 1, the fuselage 1 it is interior Portion is provided with dual-mode antenna 17, and the offside of the dual-mode antenna 17 is provided with plc 20, the dual-mode antenna 17 with The centre position of the plc 20 is provided with data wire 18, and the data wire 18 is disposed through the transmitting-receiving day The inside of line 17 and the plc 20, the dual-mode antenna 17 pass through with the plc 20 The signal of data wire 18 connection, the bottom of the plc 20 are provided with battery 22, and the battery 22 is flat Row is arranged at the bottom of the plc 20, and is electrically connected with the plc 20, described The centre position of battery 22 and the plc 20 is provided with backing plate 21.
Further, the side of the outer surface of pillar 4 is provided with loudspeaker 6, and the nesting of loudspeaker 6 is arranged at the pillar 4 Surface on, and be screwed and be connected with the pillar 4, the loudspeaker 6 can read the result drawn after scanning, convenient User goes and finds out what's going on.
Further, the end of the support 26 is equipped with CM05 imaging sensors 11, the CM05 imaging sensors 11 It is embedded to be arranged at the end of the support 26, and be fixedly connected with the support 26, the CM05 imaging sensors 11 are based on light Study and graphical analysis is carried out as after to reach measurement purpose, enable users to quickly obtain visual effect.
Further, the side of the fuselage 1 is provided with solar panels 12, and the solar panels 12 are set in parallel in the machine The side of body 1, and bonded with the fuselage 1 by glue, the solar panels 12 can effectively absorb heat and be provided for fuselage Operating power source, so that user is used for outwork.
Further, the end of the chamber door 14 is provided with rotating shaft 15, and the rotating shaft 15 is set in parallel in the chamber door 14 End, and being welded with the chamber door 14, can the chamber door 14 reduce the noise of the internal components of fuselage 1 work, while conveniently User is cleaned, and reduces maintenance cost
Further, the adjacent side of the plc 20 is provided with coldplate 19, and the tiling of coldplate 19 is set The side of the plc 20 is placed in, and is fixedly connected with the plc 20 by spiral shell button, The coldplate 19 can effectively absorb the plc work 20 and make caused heat, prevent the programmable journey There is auto-ignition because of high temperature in sequence controller 20.
Operation principle:First, fuselage 1 is completed and confirms errorless rear startup fuselage 1, when vehicle entrance can scan model When enclosing, CM05 imaging sensors 11 coordinate camera 9 to work simultaneously, and the wheel information collected is sent into programmable program control Handled in device 20 processed, then the result after processing is delivered in display 3 by plc 20, obtained for user Visual effect is obtained, while loudspeaker 6 will be explained in detail for user, facilitate user to go and find out what's going on, because being set in the side of fuselage 1 There are solar panels 12, such words solar panels 12, which can effectively absorb heat and be converted to electric energy, to be flowed into battery 22, is made 1 sustainable work of fuselage is obtained, if larger problem be present, warning light 5, which can flash, to be reminded the user that, because in the outer of pillar 4 Side is provided with turn-button 7, like this user can be facilitated to be rotated as needed to support 26 so that support 26 improves applicable Property, dual-mode antenna 17 can be that plc 20 upgrade in time algorithm data, and plc 20 can be in time There will be the problem of calibrated, while export problem figure and calibration after figure made comparisons to user, enhance using effect, prop up Telescopic mast 24 inside post 4 can carry out extension work to pillar 4 as needed, reduce the operating time of user.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art, It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.

Claims (6)

1. a kind of vehicular four wheels position indicator calibrating installation, including fuselage (1), it is characterised in that:The top of the fuselage (1) is provided with Geometrical clamp (2), the top of the geometrical clamp (2) are provided with display (3), and display (3) nesting is arranged at the geometrical clamp (2) inside, the display (3) are fixedly connected with the fuselage (1) by the geometrical clamp (2), the display (3) Offside is provided with the pillar (4) of column, and the top of the pillar (4) is provided with warning light (5), and warning light (5) insertion is arranged at The inside of the pillar (4), and be screwed and be connected with the pillar (4), the side of pillar (4) outer surface is provided with Turn-button (7), the turn-button (7) is disposed through the inside of the pillar (4), and is fixedly connected with the pillar (4), described turn The end of button (7) is provided with support (26), and the end of the support (26) is provided with fixed plate (8), and the side of the fixed plate (8) is set Have fixing hole (10), fixed plate (8) nesting is arranged on the surface of the support (26), the fixed plate (8) with it is described Support (26) is fixedly connected by the fixing hole (10), and the end of the fixed plate (8) is equipped with camera (9), described to take the photograph The end of the fixed plate (8) is arranged at as head (9) is embedded, and is fixedly connected with the fixed plate (8), the pillar (4) Inside is provided with drive link (23), and the adjacent side of the drive link (23) is provided with telescopic mast (24), and the end of the telescopic mast (24) is equal Provided with sliding shoe (25), the pillar (4) is flexibly connected with the telescopic mast (24) by the sliding shoe (25), the fuselage (1) lateral surface is provided with case lock (13), and case lock (13) is disposed through the inside of the fuselage (1), and with the fuselage (1) it is fixedly connected by nut, the adjacent side of the case lock (13) is provided with chamber door (14), and the bottom of the fuselage (1) is provided with roller (16), the roller (16) is embedded is arranged at the inside of the fuselage (1), and is bolted to connection with the fuselage (1), The inside of the fuselage (1) is provided with dual-mode antenna (17), and the offside of the dual-mode antenna (17) is provided with plc (20), the dual-mode antenna (17) and the centre position of the plc (20) are provided with data wire (18), described Data wire (18) is disposed through the inside of the dual-mode antenna (17) and the plc (20), the transmitting-receiving Antenna (17) is connected with the plc (20) by the data wire (18) signal, the programmable program control The bottom of device (20) processed is provided with battery (22), and the battery (22) is set in parallel in the plc (20) Bottom, and be electrically connected with the plc (20), the battery (22) and the programmable program control The centre position of device (20) processed is provided with backing plate (21).
A kind of 2. vehicular four wheels position indicator calibrating installation according to claim 1, it is characterised in that:The pillar (4) is outside The side on surface is provided with loudspeaker (6), and loudspeaker (6) nesting is arranged on the surface of the pillar (4), and with the pillar (4) it is screwed connection.
A kind of 3. vehicular four wheels position indicator calibrating installation according to claim 1, it is characterised in that:The support (26) End is equipped with CM05 imaging sensors (11), the embedded end for being arranged at the support (26) of the CM05 imaging sensors (11) Portion, and be fixedly connected with the support (26).
A kind of 4. vehicular four wheels position indicator calibrating installation according to claim 1, it is characterised in that:The fuselage (1) Side is provided with solar panels (12), and the solar panels (12) are set in parallel in the side of the fuselage (1), and with the fuselage (1) bonded by glue.
A kind of 5. vehicular four wheels position indicator calibrating installation according to claim 1, it is characterised in that:The chamber door (14) End is provided with rotating shaft (15), and the rotating shaft (15) is set in parallel in the end of the chamber door (14), and is welded with the chamber door (14) Connect.
A kind of 6. vehicular four wheels position indicator calibrating installation according to claim 1, it is characterised in that:The programmable program The adjacent side of controller (20) is provided with coldplate (19), and coldplate (19) tiling is arranged at the plc (20) side, and be fixedly connected with the plc (20) by spiral shell button.
CN201721012108.8U 2017-08-14 2017-08-14 A kind of vehicular four wheels position indicator calibrating installation Active CN207095542U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721012108.8U CN207095542U (en) 2017-08-14 2017-08-14 A kind of vehicular four wheels position indicator calibrating installation

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Application Number Priority Date Filing Date Title
CN201721012108.8U CN207095542U (en) 2017-08-14 2017-08-14 A kind of vehicular four wheels position indicator calibrating installation

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020143573A1 (en) * 2019-01-07 2020-07-16 深圳市道通科技股份有限公司 Method for aligning calibration apparatus with vehicle based on wheel aligner

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020143573A1 (en) * 2019-01-07 2020-07-16 深圳市道通科技股份有限公司 Method for aligning calibration apparatus with vehicle based on wheel aligner

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: Vehicle four -wheel aligner calibrating device

Effective date of registration: 20200618

Granted publication date: 20180313

Pledgee: Dongying rural commercial bank Limited by Share Ltd. Dongcheng sub branch

Pledgor: SHANDONG TUANSHANG NETWORK TECHNOLOGY Co.,Ltd.

Registration number: Y2020980003243

PE01 Entry into force of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20210520

Granted publication date: 20180313

Pledgee: Dongying rural commercial bank Limited by Share Ltd. Dongcheng sub branch

Pledgor: SHANDONG TUANSHANG NETWORK TECHNOLOGY Co.,Ltd.

Registration number: Y2020980003243

PC01 Cancellation of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: A calibration device for vehicle four wheel aligner

Effective date of registration: 20210601

Granted publication date: 20180313

Pledgee: Dongying rural commercial bank Limited by Share Ltd. Dongcheng sub branch

Pledgor: SHANDONG TUANSHANG NETWORK TECHNOLOGY Co.,Ltd.

Registration number: Y2021980004268

PE01 Entry into force of the registration of the contract for pledge of patent right