CN205002753U - Automatic mechanism of proofreading of deep groove ball bearing outer lane standard component - Google Patents
Automatic mechanism of proofreading of deep groove ball bearing outer lane standard component Download PDFInfo
- Publication number
- CN205002753U CN205002753U CN201520770045.7U CN201520770045U CN205002753U CN 205002753 U CN205002753 U CN 205002753U CN 201520770045 U CN201520770045 U CN 201520770045U CN 205002753 U CN205002753 U CN 205002753U
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- China
- Prior art keywords
- standard component
- bearing outer
- outer ring
- transfer passage
- deep groove
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Abstract
The utility model discloses an automatic mechanism of proofreading of deep groove ball bearing outer lane standard component, a positioner enables bearing inner race and keeps quiescent condition for in the transfer passage of conveying bearing outer lane, measurement mounting panel on the bottom plate can slide along perpendicular transfer passage direction of delivery, activity side bearer one end vertically can be moved and is positioned to measure on the mounting panel, fixed side bearer all is equipped with ditch position gauge head with activity side bearer one end, and the bearing inner race channel surface that ditch position gauge head on the activity side bearer and the ditch position gauge head on the fixed side bearer can tightly support on the positioner just respectively, surveying the pen can carry out the survey measurements and deliver a letter in the controller activity survey frame one end height, survey frame drive arrangement drive activity and survey frame one end longitudinal motion, standard component material feeding unit fixes a position and taks eoff away on sending the outer lane standard component into positioner, each part action of controller control, the utility model discloses a bearing inner race on -line measuring and detection device's online check and correction.
Description
Technical field
The utility model relates to a kind of checkout equipment, particularly a kind of deep groove ball bearing outer ring standard component automatic Proofreading mechanism.
Background technology
Bearing before assembling, need to measure each part of bearing, as measured bearing outer ring channel, measuring equipment is measured bearing outer ring channel 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 outer ring 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 outer ring standard component automatic Proofreading mechanism, and this deep groove ball bearing outer ring standard component automatic Proofreading mechanism can realize the on-line Full measurement of bearing outer ring channel 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 outer ring standard component automatic Proofreading mechanism, comprise base plate, measure installing plate, translation driving device, activity test aircraft, test aircraft drive unit, fixing side frame, transfer passage, survey pen, standard component pay-off and controller, transfer passage is positioned on base plate, transfer passage is for carrying bearing outer ring to be detected, in transfer passage, setting position is provided with locating device, this locating device can make the bearing outer ring of this position of arrival keep stationary state, measuring installing plate can be located on base plate along the horizontal slip of vertical transport passage throughput direction, translation driving device drives measures installing plate motion, fixing test aircraft is fixedly installed in be measured on installing plate, movable side frame one end longitudinally can motion positions on measurement installing plate, fixing side frame and movable side frame one end are equipped with ditch position gauge head, and the ditch position gauge head on movable side frame and the ditch position gauge head on fixing side frame can be tight against the bearing outer ring channel surface on locating device just respectively, survey pen can carry out survey measurements to activity test aircraft one end uper side surface height and be messaging in controller, one end lengthwise movement of test aircraft drive unit driving activity test aircraft, the locating device that outer ring standard component can be sent to transfer passage by standard component pay-off is located, and the outer ring 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, translation driving device, 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 outer ring, 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 measuring position towards conveying front, first limited block sidewall be able to stop that the bearing outer ring 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, also be provided with pan feeding inductor, the second limited block and the second spacing driving, described pan feeding inductor can sense that transfer passage inflow point needs detection axis bearing outer-ring and enters and be 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 that pan feeding inductor senses, 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 activity test aircraft other end is articulated with to be measured on installing plate, is also provided with an elastic component, and this elastic component provides the confining force longitudinally moved downward can to test aircraft one end.
As further improvement of the utility model, described elastic component is a pair V-arrangement shell fragment, measure installing plate and be provided with inverted v-shaped hinged seat, the activity 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 fixing side frame is two, is symmetrically distributed in movable side frame both sides.
As further improvement of the utility model, described standard component pay-off comprises fixed head, rocking arm, clamping device and first, two drive units, described fixed head is fixedly installed on transfer passage sidewall, one end can rotate and be installed on fixed head, first drive unit drives rocking arm reciprocally swinging, the rocking arm other end is provided with clamping device, clamping device can clamp standard component, second drive unit drives clamping device clamping and unclamps, standard component can be sent into locating device place and position by the clamping device of the rocking arm other end, controller controls first, two drive unit actions.
As further improvement of the utility model, described first drive unit is upset cylinder.
As further improvement of the utility model, described second drive unit is gripper cylinder, clamping device be two can relative sliding arrange handgrip, two handgrips are fixedly connected with the tache motorice of gripper cylinder respectively.
The beneficial effects of the utility model are: the utility model makes the bearing outer ring in transfer passage stop conveying by locating device, static etc. to be detected, then by raceway groove gauge head on movable side frame and fixing side frame location is pushed against to bearing outer ring channel, survey measurements is carried out to activity test aircraft height and indirectly can measure bearing outer ring channel, 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 outer ring 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 outer ring standard component automatic Proofreading mechanism, comprise base plate 1, measure installing plate 2, translation driving device 3, activity test aircraft 4, test aircraft drive unit 5, fixing side frame 6, transfer passage 7, survey pen 8, standard component pay-off and controller, transfer passage 7 is positioned on base plate 1, transfer passage 7 is for carrying bearing outer ring 9 to be detected, in transfer passage 7, setting position is provided with locating device, this locating device can make the bearing outer ring 9 of this position of arrival keep stationary state, measuring installing plate 2 can be located on base plate 1 along the horizontal slip of vertical transport passage 7 throughput direction, translation driving device 3 drives measurement installing plate 2 to move, fixing test aircraft is fixedly installed in be measured on installing plate 2, movable side frame one end longitudinally can motion positions on measurement installing plate 2, fixing side frame 6 and movable side frame one end are equipped with ditch position gauge head, and the ditch position gauge head on movable side frame and the ditch position gauge head on fixing side frame 6 can be tight against bearing outer ring 9 channel surface on locating device just respectively, survey pen 8 can carry out survey measurements to activity test aircraft 4 one end uper side surface height and be messaging in controller, one end lengthwise movement of test aircraft drive unit 5 driving activity test aircraft 4, the locating device that outer ring standard component can be sent to transfer passage 7 by standard component pay-off is located, and the outer ring standard component on the locating device of transfer passage 7 can be taken away by standard component pay-off, controller controls transfer passage 7, locating device, test aircraft drive unit 5, translation driving device 3, survey pen 8 and the action of standard component pay-off.
Motion flow:
Bearing outer ring 9 batch transportation in transfer passage 7, arrive one by one on locating device and position, now translation driving device 3 drives and measures installing plate 2 horizontal feed, the ditch position gauge head of realization activity side frame and fixing side frame 6 one end extend in bearing outer ring 9, then longitudinally rise in test aircraft drive unit 5 driving activity test aircraft 4 one end, the ditch position gauge head on it is made to be tight against on the surface of bearing outer ring 9 raceway groove, achieve bearing outer ring 9 raceway groove like this and push against location, channel dimensions can be obtained by raceway groove gauge head distance on raceway groove gauge head on computational activity side frame and fixing side frame 6, realize bearing outer ring 9 raceway groove to measure, survey the height of pen 8 to activity test aircraft 4 one end uper side surface and carry out survey measurements, measure numerical value is certified products in specialized range, is unacceptable product not in specialized range, after online outer ring raceway detects certain hour, controller control transfer passage 7 stops treating detection axis bearing outer-ring 9 and carries, now bearing outer ring 9 standard component is sent on the locating device of transfer passage 7 by standard component pay-off, ditch position gauge head on movable side frame and fixing side frame 6 to stretch in standard component and is against on the raceway groove of bearing outer ring 9, survey pen 8 now to test aircraft 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 outer ring 9 standard component is taken away by standard component pay-off, transfer passage 7 continues conveying bearing standard part to be detected and detects, circulation like this, achieve the online check and correction of bearing outer ring 9 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 7 is the ramp way that width only can roll through for a bearing outer ring 9, the feed end height of this ramp way is higher than discharge end height, bearing outer ring 9 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 10 and the first limit driving device 11, first limited block 10 can extend into transfer passage 7 and be positioned at the side of measuring position towards conveying front, first limited block 10 sidewall be able to stop that the bearing outer ring 9 in transfer passage 7 moves on, first limit driving device 11 drives the first limited block 10 to-and-fro movement, after bearing outer ring 9 is rolled into the measuring position of setting, first limited block 10 stretches out and just stops that it moves forward, and then achieve the stop location of bearing outer ring 9, be convenient to measure its raceway groove, can be that other locating device such as detent realizes its transfixion in addition.
Also be provided with pan feeding inductor 12, second limited block 13 and the second spacing driving 14, described pan feeding inductor 12 can sense that transfer passage 7 inflow point needs detection axis bearing outer-ring 9 and enters and be messaging in controller, second limited block 13 can to extend in transfer passage 7 and to stop in transfer passage 7 and be continued conveying by the bearing that pan feeding inductor 12 senses, second spacing driving 14 device drives the second limited block 13 to move, controller controls the second spacing driving 14 device action, by arranging pan feeding inductor 12 and the second limited block 13 in detection front, position, bearing outer ring 9 to be detected is entered after in transfer passage 7 stopped in advance by the second limited block 13 before arrival detection position, it is avoided to collide the bearing outer ring 9 of measuring position, cause product to clash into damage and measuring error.
Described activity test aircraft 4 other end is articulated with to be measured on installing plate 2, also be provided with an elastic component, this elastic component provides the confining force longitudinally moved downward can to test aircraft one end, test aircraft one end swings around the other end, elastic component makes ditch position, test aircraft one end gauge head after measurement completes, automatically disengage bearing outer ring 9 raceway groove, during measurement, test aircraft drive unit 5 drives liter on test aircraft one end to overcome elastic force, and certain activity test aircraft 4 also can be that longitudinal sliding motion is positioned to measure on installing plate 2.
Described elastic component is a pair V-arrangement shell fragment 15, measure installing plate 2 and be provided with inverted v-shaped hinged seat, activity 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 15 lay respectively in the V-arrangement opening that hinged seat and hinged end both sides are formed, each V-arrangement shell fragment 15 both sides are tight against hinged seat and hinged end sidewall respectively, realize activity test aircraft 4 one end height remain on desired location by V-arrangement shell fragment 15, and can upper and lower elastic movement.
Described fixing side frame 6 is two, is symmetrically distributed in movable side frame both sides, and three points realize outer ring raceway stable position, ensures that measuring accuracy is high, and certainly fixing side frame 6 also can be one and be positioned at immediately below movable side frame.
Described standard component pay-off comprises fixed head 16, rocking arm 17, clamping device 18 and first, two drive units 19, 20, described fixed head 16 is fixedly installed on transfer passage 7 sidewall, rocking arm 17 one end can be rotated and is installed on fixed head 16, first drive unit drives rocking arm 17 reciprocally swinging, rocking arm 17 other end is provided with clamping device 18, clamping device 18 can clamp standard component, second drive unit drives clamping device 18 clamp and unclamp, standard component can be sent into locating device place and position by the clamping device 18 of rocking arm 17 other end, controller controls first, two drive units 19, 20 actions, bearing outer ring 9 standard component is clamped by clamping device, swung by rocking arm 17, bearing outer ring 9 standard component is extend into and locating device positions and measures, and then realize the check and correction of measuring equipment, the rear clamping device 18 that detection completes picks up bearing outer ring 9 standard component again, get out of the way transfer passage 7, wait for and proofreading next time.
Described first drive unit is upset cylinder.
Described second drive unit is gripper cylinder, clamping device 18 be two can relative sliding arrange handgrip, two handgrips are fixedly connected with the tache motorice of gripper cylinder respectively.
Claims (10)
1. a deep groove ball bearing outer ring standard component automatic Proofreading mechanism, it is characterized in that: comprise base plate (1), measure installing plate (2), translation driving device (3), activity test aircraft (4), test aircraft drive unit (5), fixing side frame (6), transfer passage (7), survey pen (8), standard component pay-off and controller, transfer passage is positioned on base plate, transfer passage is for carrying bearing outer ring (9) to be detected, in transfer passage, setting position is provided with locating device, this locating device can make the bearing outer ring of this position of arrival keep stationary state, measuring installing plate can be located on base plate along the horizontal slip of vertical transport passage throughput direction, translation driving device drives measures installing plate motion, fixing test aircraft is fixedly installed in be measured on installing plate, movable side frame one end longitudinally can motion positions on measurement installing plate, fixing side frame and movable side frame one end are equipped with ditch position gauge head, and the ditch position gauge head on movable side frame and the ditch position gauge head on fixing side frame can be tight against the bearing outer ring channel surface on locating device just respectively, survey pen can carry out survey measurements to activity test aircraft one end uper side surface height and be messaging in controller, one end lengthwise movement of test aircraft drive unit driving activity test aircraft, the locating device that outer ring standard component can be sent to transfer passage by standard component pay-off is located, and the outer ring 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, translation driving device, survey pen and the action of standard component pay-off.
2. deep groove ball bearing outer 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 outer ring, and the feed end height of this ramp way is higher than discharge end height.
3. deep groove ball bearing outer ring standard component automatic Proofreading mechanism according to claim 2, it is characterized in that: described locating device comprises the first limited block (10) and the first limit driving device (11), first limited block can extend into transfer passage and be positioned at the side of measuring position towards conveying front, first limited block sidewall be able to stop that the bearing outer ring 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 outer ring standard component automatic Proofreading mechanism according to claim 3, it is characterized in that: be also provided with pan feeding inductor (12), second limited block (13) and the second spacing driving (14), described pan feeding inductor can sense that transfer passage inflow point needs detection axis bearing outer-ring and enters and be 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 that pan feeding inductor senses, second limit driving device drives the second limited block motion, controller controls the second limit driving device action.
5. deep groove ball bearing outer ring standard component automatic Proofreading mechanism according to claim 1, it is characterized in that: the described activity test aircraft other end is articulated with to be measured on installing plate, also be provided with an elastic component, this elastic component provides the confining force longitudinally moved downward can to test aircraft one end.
6. deep groove ball bearing outer 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 (15), measure installing plate and be provided with inverted v-shaped hinged seat, the activity 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 outer ring standard component automatic Proofreading mechanism according to claim 1, is characterized in that: described fixing side frame is two, is symmetrically distributed in movable side frame both sides.
8. deep groove ball bearing outer ring standard component automatic Proofreading mechanism according to claim 1, it is characterized in that: described standard component pay-off comprises fixed head (16), rocking arm (17), clamping device (18) and first, two drive units (19, 20), described fixed head is fixedly installed on transfer passage sidewall, one end can rotate and be installed on fixed head, first drive unit drives rocking arm reciprocally swinging, the rocking arm other end is provided with clamping device, clamping device can clamp standard component, second drive unit drives clamping device clamping and unclamps, standard component can be sent into locating device place and position by the clamping device of the rocking arm other end, controller controls first, two drive unit actions.
9. deep groove ball bearing outer ring standard component automatic Proofreading mechanism according to claim 8, is characterized in that: described first drive unit is upset cylinder.
10. deep groove ball bearing outer ring standard component automatic Proofreading mechanism according to claim 8, it is characterized in that: described second drive unit is gripper cylinder, clamping device be two can relative sliding arrange handgrip, two handgrips are fixedly connected with the tache motorice of gripper cylinder respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520770045.7U CN205002753U (en) | 2015-09-30 | 2015-09-30 | Automatic mechanism of proofreading of deep groove ball bearing outer lane standard component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520770045.7U CN205002753U (en) | 2015-09-30 | 2015-09-30 | Automatic mechanism of proofreading of deep groove ball bearing outer lane standard component |
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| Publication Number | Publication Date |
|---|---|
| CN205002753U true CN205002753U (en) | 2016-01-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520770045.7U Expired - Fee Related CN205002753U (en) | 2015-09-30 | 2015-09-30 | Automatic mechanism of proofreading of deep groove ball bearing outer lane standard component |
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| CN (1) | CN205002753U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107626602A (en) * | 2017-09-27 | 2018-01-26 | 常熟理工学院 | Bearing automatic measurement sorting equipment based on micro-displacement sensor |
| CN108444415A (en) * | 2018-05-14 | 2018-08-24 | 电子科技大学中山学院 | Motor end cover automatic detection mechanism and motor end cover production line using same |
| 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 |
| CN112683201A (en) * | 2020-12-30 | 2021-04-20 | 新昌县环富机械科技有限公司 | Double-channel ball bearing outer ring detection device and control system |
| CN112902809A (en) * | 2021-01-26 | 2021-06-04 | 新昌沛斯轴承配件有限公司 | Detection apparatus for bearing inner race axiality |
| CN113503845A (en) * | 2021-05-24 | 2021-10-15 | 黄山明明德集团有限公司 | Automatic calibration device of bearing outer ring outer diameter detection machine |
-
2015
- 2015-09-30 CN CN201520770045.7U patent/CN205002753U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107626602A (en) * | 2017-09-27 | 2018-01-26 | 常熟理工学院 | Bearing automatic measurement sorting equipment based on micro-displacement sensor |
| 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 |
| CN108444415A (en) * | 2018-05-14 | 2018-08-24 | 电子科技大学中山学院 | Motor end cover automatic detection mechanism and motor end cover production line using same |
| CN112683201A (en) * | 2020-12-30 | 2021-04-20 | 新昌县环富机械科技有限公司 | Double-channel ball bearing outer ring detection device and control system |
| CN112902809A (en) * | 2021-01-26 | 2021-06-04 | 新昌沛斯轴承配件有限公司 | Detection apparatus for bearing inner race axiality |
| CN113503845A (en) * | 2021-05-24 | 2021-10-15 | 黄山明明德集团有限公司 | Automatic calibration device of bearing outer ring outer diameter detection machine |
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| Date | Code | Title | Description |
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| 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: 20200930 |
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| CF01 | Termination of patent right due to non-payment of annual fee |