CN205002759U - Automatic mechanism of proofreading of deep groove ball bearing inner circle standard component - Google Patents
Automatic mechanism of proofreading of deep groove ball bearing inner circle standard component Download PDFInfo
- Publication number
- CN205002759U CN205002759U CN201520718178.XU CN201520718178U CN205002759U CN 205002759 U CN205002759 U CN 205002759U CN 201520718178 U CN201520718178 U CN 201520718178U CN 205002759 U CN205002759 U CN 205002759U
- Authority
- CN
- China
- Prior art keywords
- standard component
- bearing inner
- transfer passage
- test aircraft
- survey
- 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
Links
Abstract
The utility model discloses an automatic mechanism of proofreading of deep groove ball bearing inner circle standard component, transfer passage on the base is used for the conveying bearing inner circle, the bearing inner race that the positioner that sets for position department in the transfer passage can fixed position reachs this position, survey frame one end vertically can be moved and is positioned on the base, it is equipped with the ditch position gauge head that just can tightly support side surface on the bearing inner race channel on the positioner to survey frame one end downside, surveying the pen can carry out the survey measurements and deliver a letter in the controller surveying frame one end upside apparent height, survey the drive of frame drive arrangement and survey frame one end longitudinal motion, standard component material feeding unit can send the inner circle standard component to positioner and go up the location, standard component material feeding unit can also tak eoff the standard component on the positioner away, controller control transfer passage, positioner, survey frame drive arrangement, survey the action of pen and standard component material feeding unit, the utility model discloses an automated inspection and automatic correction of, it is high to rectify frequency, measurement accuracy and measurement of efficiency, does not have the influence to equipment life.
Description
Technical field
The utility model relates to a kind of checkout equipment, particularly a kind of deep groove ball bearing inner ring standard component automatic Proofreading mechanism.
Background technology
Bearing before assembling, need to measure each part of bearing, as measured bearing inner race raceway groove, measuring equipment is measured bearing inner race raceway groove to be detected online one by one, after the measurement carrying out some, use standard component to proofread measuring equipment, avoid measuring equipment measuring error, the check and correction of current bearing inner race measuring equipment is all manually carried out, during artificial check and correction, need first to shut down, then standard component is put into, drive into again and measure, carry out error compensation setting, shut down again after having proofreaded and take out standard component, on-line measurement is carried out in start again, such frequent shutdown is answered a pager's call and is affected service life of equipment, and cause on-line measurement efficiency low, also there is potential safety hazard in shutdown operation check and correction flow process, again also easily there is dimensional discrepancy during start, cause measuring accuracy low, and manually place inconvenience.
Utility model content
In order to overcome above-mentioned defect, the utility model provides a kind of deep groove ball bearing inner ring standard component automatic Proofreading mechanism, and this deep groove ball bearing inner ring standard component automatic Proofreading mechanism can realize the on-line Full measurement of bearing inner race raceway groove and on-line automatic check and correction.
The utility model in order to the technical scheme solving its technical matters and adopt is: a kind of deep groove ball bearing inner ring standard component automatic Proofreading mechanism, comprise base, transfer passage, survey pen, test aircraft, test aircraft drive unit, standard component pay-off and controller, transfer passage is positioned on base, transfer passage is for carrying bearing inner race to be detected, in transfer passage, setting position is provided with locating device, this locating device stationary positioned can arrive the bearing inner race of this position, test aircraft one end longitudinally can motion positions on base, and on the downside of test aircraft one end, be provided with ditch position gauge head, this ditch position gauge head be able to be tight against the bearing inner race raceway groove uper side surface on locating device, survey pen can carry out survey measurements to test aircraft one end uper side surface height and be messaging in controller, test aircraft drive unit drives the lengthwise movement of test aircraft one end, the locating device that inner ring standard component can be sent to transfer passage by standard component pay-off is located, and the standard component on the locating device of transfer passage can be taken away by standard component pay-off, controller controls transfer passage, locating device, test aircraft drive unit, survey pen and the action of standard component pay-off.
As further improvement of the utility model, described transfer passage is the ramp way that width only can roll through for a bearing inner race, and the feed end height of this ramp way is higher than discharge end height.
As further improvement of the utility model, described locating device comprises the first limited block and the first limit driving device, first limited block can extend into transfer passage and be positioned at the side of ditch position gauge head towards conveying front, first limited block sidewall be able to stop that the bearing inner race in transfer passage moves on, and the first limit driving device drives the first limited block to-and-fro movement.
As further improvement of the utility model, material inductor, the second limited block and the second spacing driving are also provided with, described have material inductor can sense that in transfer passage, bearing inner race to be detected has been transported to assigned address and has been messaging in controller, second limited block can to extend in transfer passage and to stop in transfer passage and be continued conveying by the bearing being had material inductor to sense, second limit driving device drives the second limited block motion, and controller controls the second limit driving device action.
As further improvement of the utility model, the described test aircraft other end is articulated with on base, is also provided with an elastic component, and this elastic component provides the confining force longitudinally moved upward can to test aircraft one end.
As further improvement of the utility model, described elastic component is a pair V-arrangement shell fragment, base is provided with inverted v-shaped hinged seat, the test aircraft other end forms V-shaped hinged end, the tip of described hinged seat and hinged end is hinged, two V-arrangement shell fragments lay respectively in the V-arrangement opening that hinged seat and hinged end both sides are formed, and each V-arrangement shell fragment both sides are tight against hinged seat and hinged end sidewall respectively.
As further improvement of the utility model, described standard component pay-off comprises fixed frame, fork, rotating driving device, clamp system and driving clamping device, described fixed mount is fixedly installed on base, fork one end can be rotated and is installed on fixed frame, rotating driving device drives the fork other end around one end reciprocally swinging, clamp system is fixedly installed in the fork other end, clamp system is provided with can a pair jaw of relative motion, jaw is provided with the supporting rod of prolongation, supporting rod end be able to arrive above locating device, described supporting rod and jaw exist and set angle, driving clamping device drives the jaw relative sliding of clamp system.
As further improvement of the utility model, described rotating driving device is upset cylinder, and driving clamping device is gripper cylinder, and clamp system is a pair handgrip, and a pair handgrip is fixedly connected with two tache motorices of gripper cylinder respectively.
The beneficial effects of the utility model are: the utility model realizes positioning the bearing inner race in transfer passage by locating device, then bearing inner race raceway groove is pushed against by test aircraft, sidewall carries out survey measurements to test aircraft height and then indirectly measures bearing inner race raceway groove, after measuring the product of some, transfer passage stops conveying products, standard component is sent to location survey on locating device by standard component pay-off automatically, and then corrected by the auto-compensation realizing surveying a reading to the measurement of standard component, and then output measures numerical value accurately, the utility model achieves the online check and correction of bearing inner race on-line checkingi and pick-up unit, effectively increase the frequency of check and correction, ensure the stability that product size is measured, simultaneously owing to automatically completing in machine, so do not have a significant impact the production efficiency of product, during due to check and correction, without the need to shutting down, handling safety, avoid start again and occur dimensional discrepancy, and avoid frequent shutdown and answer a pager's call and affect service life of equipment.
Accompanying drawing explanation
Fig. 1 is front view of the present utility model;
Fig. 2 is right view of the present utility model;
Fig. 3 is vertical view of the present utility model.
Embodiment
Embodiment: a kind of deep groove ball bearing inner ring 6 standard component automatic Proofreading mechanism, comprise base 1, transfer passage 2, survey pen 3, test aircraft 4, test aircraft drive unit 5, standard component pay-off and controller, transfer passage 2 is positioned on base 1, transfer passage 2 is for carrying bearing inner race 6 to be detected, in transfer passage 2, setting position is provided with locating device, this locating device stationary positioned can arrive the bearing inner race 6 of this position, test aircraft 4 one end longitudinally can motion positions on base 1, and be provided with ditch position gauge head 19 on the downside of test aircraft 4 one end, this ditch position gauge head 19 be able to be tight against the bearing inner race 6 raceway groove uper side surface on locating device, survey pen 3 can carry out survey measurements to test aircraft 4 one end uper side surface height and be messaging in controller, test aircraft drive unit 5 drives test aircraft 4 one end lengthwise movement, the locating device that inner ring standard component can be sent to transfer passage 2 by standard component pay-off is located, and the standard component on the locating device of transfer passage 2 can be taken away by standard component pay-off, controller controls transfer passage 2, locating device, test aircraft drive unit 5, survey pen 3 and the action of standard component pay-off.
Motion flow:
Bearing inner race 6 batch transportation in transfer passage 2, arrive one by one on locating device and position, now test aircraft drive unit 5 drives test aircraft 4 one end longitudinally to decline, the ditch position gauge head 19 on it is made to be tight against bearing inner race 6 raceway groove uper side surface, now survey pen 3 to start to carry out survey measurements to the height of test aircraft 4 one end uper side surface, measure numerical value is certified products in specialized range, is unacceptable product not in specialized range, after online bear inner ring grooved railway detects certain hour, controller control transfer passage 2 stops treating detection bearing inner race 6 and carries, the locating device that now bearing inner race 6 standard component is sent to transfer passage 2 by standard component pay-off positions test aircraft 4 one end longitudinally decline, ditch position gauge head 19 is against on the raceway groove of bearing inner race 6 standard component, survey pen 3 now to test aircraft 4 one end uper side surface elevation carrection reading, controller carries out correction check and correction according to this logarithm to measurement data, and then output measures numerical value accurately, then, bearing inner race 6 standard component is taken away by standard component pay-off, transfer passage 2 continues conveying bearing standard part to be detected and detects, circulation like this, achieve the online check and correction of bearing inner race 6 on-line checkingi and pick-up unit, effectively increase the frequency of check and correction, ensure the stability that product size is measured, simultaneously owing to automatically completing in machine, so do not have a significant impact the production efficiency of product, during due to check and correction, without the need to shutting down, handling safety, avoid start again and occur dimensional discrepancy, and avoid frequent shutdown and answer a pager's call and affect service life of equipment.
Described transfer passage 2 is the ramp way that width only can roll through for a bearing inner race 6, the feed end height of this ramp way is higher than discharge end height, bearing inner race 6 carries out automatic transport under Gravitative Loads, saving the energy, also can be undertaken carrying by conveying belt or cylinder mechanism carries out carrying etc. in addition.
Described locating device comprises the first limited block 7 and the first limit driving device 8, first limited block 7 can extend into transfer passage 2 and be positioned at the side of ditch position gauge head 19 towards conveying front, first limited block 7 sidewall be able to stop that the bearing inner race 6 in transfer passage 2 moves on, first limit driving device 8 drives the first limited block 7 to-and-fro movement, after bearing inner race 6 is rolled into desired location, first limited block 7 stretches out and just stops that it moves forward, and then achieve the stop location of bearing inner race 6, be convenient to measure its raceway groove, can be that other locating device is as jaw clamping position in addition.
Also be provided with material inductor 9, second limited block 10 and the second spacing driving 11, described have material inductor 9 can sense that in transfer passage 2, bearing inner race 6 to be detected has been transported to assigned address and has been messaging in controller, second limited block 10 can to extend in transfer passage 2 and to stop in transfer passage 2 and be continued conveying by the bearing being had material inductor 9 to sense, second spacing driving 11 device drives the second limited block 10 to move, controller controls the second spacing driving 11 device action, detecting front, position by induction has bearing inner race 6 to be detected to enter, stopped by the second limited block 10 in advance, it is avoided to collide the bearing inner race 6 of measuring position, cause product to clash into damage and measuring error.
Described test aircraft 4 other end is articulated with on base 1, also be provided with an elastic component, this elastic component provides the confining force longitudinally moved upward can to test aircraft 4 one end, test aircraft 4 one end swings around the other end, ditch position, the test aircraft 4 one end gauge head 19 that elastic component is automatically disengages bearing inner race 6 after measurement completes, during measurement, test aircraft drive unit 5 drives the decline of test aircraft 4 one end to overcome elastic force, and certain test aircraft 4 also can be that longitudinal sliding motion is positioned on base 1.
Described elastic component is a pair V-arrangement shell fragment 12, base 1 is provided with inverted v-shaped hinged seat, test aircraft 4 other end forms V-shaped hinged end, the tip of described hinged seat and hinged end is hinged, two V-arrangement shell fragments 12 lay respectively in the V-arrangement opening that hinged seat and hinged end both sides are formed, each V-arrangement shell fragment 12 both sides are tight against hinged seat and hinged end sidewall respectively, realize test aircraft 4 one end height remain on desired location by V-arrangement shell fragment 12.
Described standard component pay-off comprises fixed frame 13, fork 14, rotating driving device, clamp system and driving clamping device, described fixed mount is fixedly installed on base 1, fork 14 one end can be rotated and is installed on fixed frame 13, rotating driving device drives fork 14 other end around one end reciprocally swinging, clamp system is fixedly installed in fork 14 other end, clamp system is provided with can a pair jaw of relative motion, jaw is provided with the supporting rod 18 of prolongation, supporting rod 18 end be able to arrive above locating device, described supporting rod 18 and jaw exist and set angle, driving clamping device drives the jaw relative sliding of clamp system, the supporting rod 18 that bearing inner race 6 standard component is clamped mechanism clamps, swung by fork 14, bearing inner race 6 standard component is extend into check and correction locating device positioning and measures and then realize measuring equipment, after detection completes, supporting rod 18 picks up bearing inner race 6 standard component again, get out of the way transfer passage 2, wait for and proofreading next time, this standard component pay-off can realize inner ring standard component and accurately be sent on locating device, the supporting rod 18 extended and can not be surveyed pen 3 and interferes with transfer passage 2 and test aircraft 4.
Described rotating driving device is upset cylinder 15, and driving clamping device is gripper cylinder 16, and clamp system is that a pair handgrip 17, a pair handgrip 17 is fixedly connected with two tache motorices of gripper cylinder 16 respectively.
Claims (8)
1. a deep groove ball bearing inner ring standard component automatic Proofreading mechanism, it is characterized in that: comprise base (1), transfer passage (2), survey pen (3), test aircraft (4), test aircraft drive unit (5), standard component pay-off and controller, transfer passage is positioned on base, transfer passage is for carrying bearing inner race to be detected, in transfer passage, setting position is provided with locating device, this locating device stationary positioned can arrive the bearing inner race of this position, test aircraft one end longitudinally can motion positions on base, and on the downside of test aircraft one end, be provided with ditch position gauge head (19), this ditch position gauge head be able to be tight against the bearing inner race raceway groove uper side surface on locating device, survey pen can carry out survey measurements to test aircraft one end uper side surface height and be messaging in controller, test aircraft drive unit drives the lengthwise movement of test aircraft one end, the locating device that inner ring standard component can be sent to transfer passage by standard component pay-off is located, and the standard component on the locating device of transfer passage can be taken away by standard component pay-off, controller controls transfer passage, locating device, test aircraft drive unit, survey pen and the action of standard component pay-off.
2. deep groove ball bearing inner ring standard component automatic Proofreading mechanism according to claim 1, is characterized in that: described transfer passage is the ramp way that width only can roll through for a bearing inner race, and the feed end height of this ramp way is higher than discharge end height.
3. deep groove ball bearing inner ring standard component automatic Proofreading mechanism according to claim 2, it is characterized in that: described locating device comprises the first limited block (7) and the first limit driving device (8), first limited block can extend into transfer passage and be positioned at the side of ditch position gauge head towards conveying front, first limited block sidewall be able to stop that the bearing inner race in transfer passage moves on, and the first limit driving device drives the first limited block to-and-fro movement.
4. deep groove ball bearing inner ring standard component automatic Proofreading mechanism according to claim 3, it is characterized in that: be also provided with material inductor (9), second limited block (10) and the second spacing driving (11), described have material inductor can sense that in transfer passage, bearing inner race to be detected has been transported to assigned address and has been messaging in controller, second limited block can to extend in transfer passage and to stop in transfer passage and be continued conveying by the bearing being had material inductor to sense, second limit driving device drives the second limited block motion, controller controls the second limit driving device action.
5. deep groove ball bearing inner ring standard component automatic Proofreading mechanism according to claim 1, is characterized in that: the described test aircraft other end is articulated with on base, is also provided with an elastic component, and this elastic component provides the confining force longitudinally moved upward can to test aircraft one end.
6. deep groove ball bearing inner ring standard component automatic Proofreading mechanism according to claim 5, it is characterized in that: described elastic component is a pair V-arrangement shell fragment (12), base is provided with inverted v-shaped hinged seat, the test aircraft other end forms V-shaped hinged end, the tip of described hinged seat and hinged end is hinged, two V-arrangement shell fragments lay respectively in the V-arrangement opening that hinged seat and hinged end both sides are formed, and each V-arrangement shell fragment both sides are tight against hinged seat and hinged end sidewall respectively.
7. deep groove ball bearing inner ring standard component automatic Proofreading mechanism according to claim 1, it is characterized in that: described standard component pay-off comprises fixed frame (13), fork (14), rotating driving device, clamp system and driving clamping device, described fixed frame is fixedly installed on base, fork one end can be rotated and is installed on fixed frame, rotating driving device drives the fork other end around one end reciprocally swinging, clamp system is fixedly installed in the fork other end, clamp system is provided with can a pair jaw of relative motion, jaw is provided with the supporting rod (18) of prolongation, supporting rod end be able to arrive above locating device, described supporting rod and jaw exist and set angle, driving clamping device drives the jaw relative sliding of clamp system.
8. deep groove ball bearing inner ring standard component automatic Proofreading mechanism according to claim 7, it is characterized in that: described rotating driving device is upset cylinder (15), driving clamping device is gripper cylinder (16), clamp system is a pair handgrip (17), and a pair handgrip is fixedly connected with two tache motorices of gripper cylinder respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520718178.XU CN205002759U (en) | 2015-09-16 | 2015-09-16 | Automatic mechanism of proofreading of deep groove ball bearing inner circle standard component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520718178.XU CN205002759U (en) | 2015-09-16 | 2015-09-16 | Automatic mechanism of proofreading of deep groove ball bearing inner circle standard component |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205002759U true CN205002759U (en) | 2016-01-27 |
Family
ID=55159643
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520718178.XU Expired - Fee Related CN205002759U (en) | 2015-09-16 | 2015-09-16 | Automatic mechanism of proofreading of deep groove ball bearing inner circle standard component |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205002759U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108731618A (en) * | 2018-05-02 | 2018-11-02 | 无锡诚石轴承有限公司 | Miniature bearing outer ring raceway dimension automatic detection device |
| CN113686292A (en) * | 2021-08-12 | 2021-11-23 | 吉林北方捷凯传动轴有限公司 | Automatic detection grouping machine for inner ring of movable end section of transmission shaft |
| CN114043393A (en) * | 2021-11-10 | 2022-02-15 | 首都航天机械有限公司 | Small-sized part comparison detection clamping device and method |
| CN114619302A (en) * | 2022-03-21 | 2022-06-14 | 芜湖伦比轴承有限公司 | Bearing inner race grinding mistake proofing device |
-
2015
- 2015-09-16 CN CN201520718178.XU patent/CN205002759U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108731618A (en) * | 2018-05-02 | 2018-11-02 | 无锡诚石轴承有限公司 | Miniature bearing outer ring raceway dimension automatic detection device |
| CN113686292A (en) * | 2021-08-12 | 2021-11-23 | 吉林北方捷凯传动轴有限公司 | Automatic detection grouping machine for inner ring of movable end section of transmission shaft |
| CN113686292B (en) * | 2021-08-12 | 2023-11-07 | 吉林北方捷凯传动轴有限公司 | Automatic detection grouping machine for inner ring of movable end section of transmission shaft |
| CN114043393A (en) * | 2021-11-10 | 2022-02-15 | 首都航天机械有限公司 | Small-sized part comparison detection clamping device and method |
| CN114043393B (en) * | 2021-11-10 | 2023-08-11 | 首都航天机械有限公司 | Small part comparison detection clamping device and method |
| CN114619302A (en) * | 2022-03-21 | 2022-06-14 | 芜湖伦比轴承有限公司 | Bearing inner race grinding mistake proofing device |
| CN114619302B (en) * | 2022-03-21 | 2023-11-10 | 芜湖伦比轴承有限公司 | Bearing inner race grinding error proofing device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205002753U (en) | Automatic mechanism of proofreading of deep groove ball bearing outer lane standard component | |
| CN205002759U (en) | Automatic mechanism of proofreading of deep groove ball bearing inner circle standard component | |
| CN102608201B (en) | Clamp system is automatically positioned in the flaw detection of bell housing, cleaning all-in-one loading and unloading | |
| CN104444289A (en) | Automatic feeding mechanism | |
| CN204240972U (en) | The positive clearance detector of bearing | |
| CN209117604U (en) | A kind of piston pin detection machine | |
| CN106584128A (en) | Automatic assembly production line of spool | |
| CN105158329A (en) | Full-automatic eddy-current flaw-detection hardness tester | |
| CN105716562A (en) | Device for detecting positive clearance of bearing | |
| CN204416447U (en) | A kind of automatic feed mechanism | |
| CN204963823U (en) | Outer spherical bearing outer diameter , circularity detect machine | |
| CN106563743B (en) | A kind of automatic corrector of wheel rim flatness | |
| CN202967515U (en) | Feeding device for steel pipe flaw detector | |
| CN205346254U (en) | Automatic lifting device of two roll tables of elongated shape article | |
| CN204666084U (en) | Semi-automatic linearity testing apparatus | |
| CN205002762U (en) | Automatic mechanism of proofreading of deep groove ball bearing inner circle internal diameter standard component | |
| CN206074046U (en) | A kind of lithium battery welds testing equipment | |
| CN211412791U (en) | Spherical roller penetrating profiling eddy current flaw detection device | |
| CN209689586U (en) | A kind of wall-hung boiler left and right correction piecing devices automatically | |
| CN105415172B (en) | The wear-resistant detection means of phone housing with automatic loading and unloading device | |
| CN216815391U (en) | Monocrystalline silicon detection table device | |
| CN207917977U (en) | A kind of conveyance drawing material device of bearing outer ring inner diameter measurement machine | |
| CN102944606A (en) | Steel pipe eddy current inspection feed mechanism | |
| CN206609580U (en) | The code-reading apparatus of steel cylinder water press testing machine | |
| CN205966873U (en) | Bicycle rims automatic correction equipment |
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: 20160127 Termination date: 20200916 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |