CN204854702U - Big batch detection device of bearing ring - Google Patents

Big batch detection device of bearing ring Download PDF

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Publication number
CN204854702U
CN204854702U CN201520416115.9U CN201520416115U CN204854702U CN 204854702 U CN204854702 U CN 204854702U CN 201520416115 U CN201520416115 U CN 201520416115U CN 204854702 U CN204854702 U CN 204854702U
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CN
China
Prior art keywords
fuselage
bearing ring
cylinder
check
detection device
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Withdrawn - After Issue
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CN201520416115.9U
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Chinese (zh)
Inventor
余天明
梅开红
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Anhui Baiji Electromechanical Technology Co Ltd
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Anhui Baiji Electromechanical Technology Co Ltd
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Priority to CN201520416115.9U priority Critical patent/CN204854702U/en
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Abstract

The utility model relates to a bearing detection device, specific big batch detection device of bearing ring that says so, including fuselage, detection device, material feeding unit and pusher, detection device be located the fuselage right side, just detection device be located the waist, material feeding unit be located fuselage left side, detection device include turning device, pick -up plate, expect the cylinder, the poor device of perpendicular volume, parallel tolerance device and signal collecting box, the poor device of perpendicular volume include vertical support plate and the poor table of perpendicular volume, parallel tolerance device include rodless cylinder, seat and parallel tolerance table slide, signal collecting box fixed mounting bottom surface under the fuselage, material feeding unit include feeding funnel, (mixing) shaft, stirring vane, agitator motor and transfer passage, pusher include propelling movement cylinder and push plate. The utility model discloses very big improvement detection efficiency, and satisfied current bearing ring's detection demand.

Description

A kind of bearing ring mass detection device
Technical field
The utility model relates to a kind of bearing detecting device, specifically a kind of bearing ring mass detection device.
Background technology
Bearing ring plane and external diameter are the benchmark of later process mill raceway groove and mill endoporus, and technological requirement, by after flat surface grinding, mill external diameter, guarantees the depth of parallelism of lasso two plane, the verticality of external diameter circularity and plane and end face.But when flat surface grinding, because the improper or equipment feed lead rail of emery wheel adjustment, discharge guide adjustment are improper, plane and external diameter out of plumb will be made, namely occur that vertical difference (Sd2) is overproof.The H902 height-gauge used when flat surface grinding at present can only check the depth of parallelism (VBs), cannot control vertical difference (Sd2) simultaneously, be unfavorable for the subsequent processing operations of bearing ring.
The notification number that Chinese patent is announced is a kind of bearing ring pick-up unit of CN104406503A, detects, but cannot adapt to the detection of bearing ring in enormous quantities, have impact on work efficiency while it can realize bearing ring vertical difference and the depth of parallelism.
Utility model content
In order to make up the deficiencies in the prior art, the utility model which provides a kind of device that simultaneously can carry out vertical difference and Parallel testing to bearing ring in enormous quantities.
The utility model solves the technical scheme that its technical matters adopts: a kind of bearing ring mass detection device, comprise fuselage, pick-up unit, pay-off and pusher, described pick-up unit is positioned on the right side of fuselage, and described pick-up unit is positioned at waist, described pay-off is positioned on the left of fuselage.
Described pick-up unit comprises turning device, check-out console, batch turning cylinder, vertical amount difference device, parallel measurement apparatus and signal collection case, described turning device is made up of ten to two ten roll-over units, described roll-over unit comprises returning face plate and upset cylinder, the cross section of described returning face plate is " L " shape structure, and the vertical edge of returning face plate is outward-dipping, the effect that the vertical edge of returning face plate is outward-dipping makes the bearing ring entering turning device from pay-off not easily drop into check-out console from returning face plate, the base upper surface of returning face plate along fuselage from after be tilted to lower layout gradually, base upper surface along fuselage from after be tilted to lower layout gradually effect be the vertical edge making bearing ring can be close to returning face plate, be hinged on front side of described upset cylinder bottom and body bottom surface, the side of upset cylinder head and turning device is hinged, contact with each other between each roll-over unit, and each roll-over unit is connected by a rotating shaft, a rotating shaft runs through the base of each roll-over unit, and a rotating shaft is arranged on above fuselage bottom surface by a pair supporting seat, and the distance of each returning face plate left and right side is equal with bearing ring external diameter, thus a corresponding bearing ring on each returning face plate, during work, bearing ring enters the returning face plate of pick-up unit from pay-off with vertical state, after bearing ring enters returning face plate, due to the inclined design of returning face plate upper plate, the inclination vertical edge that bearing ring is close to returning face plate rolls, until bearing ring is covered with whole turning device, then, upset cylinder stretches out, the returning face plate of each roll-over unit rotates backward around a rotating shaft, thus the bearing ring on each returning face plate falls into check-out console from returning face plate, after bearing ring on device to be flipped all falls into check-out console, bearing ring on pay-off is again rolled into and is covered with whole turning device.
The string configuration of described check-out console to be cross section be " ┘ " shape, and check-out console is positioned on rear side of turning device, check-out console is several detection zones by vertical baffle even partition, the number of described detection zone equals the number of roll-over unit, and positive front end, each detection zone correspond to a roll-over unit, thus returning face plate on each roll-over unit is when rotating, bearing ring on returning face plate falls into corresponding detection zone, bottom, each detection zone is provided with a pair bottom support and a side bearing, bottom support is used for spring bearing lasso bottom surface, collateral support is used for spring bearing lasso side, the rear lower portion of described check-out console runs through No. two rotating shafts, No. two described rotating shafts are arranged on above fuselage bottom surface by a pair supporting seat, described batch turning cylinder top is hinged on lower surface in the middle part of check-out console, batch turning cylinder end is hinged on rear side of body bottom surface, under original state, batch turning cylinder stretches out and makes check-out console be in horizontality, during work, after returning face plate rotation makes bearing ring fall into detection zone, batch turning cylinder continues to protract, check-out console is rotated clockwise around No. two rotating shafts, bearing ring is slided backward thus is close to side bearing, then batch turning cylinder shrinks and makes check-out console again keep horizontality, and after bearing ring has detected, batch turning cylinder shrinks, check-out console is rotated counterclockwise around No. two rotating shafts, check-out console is tilted to down on front side of fuselage, bearing ring from detection zone landing to turning device and check-out console below fuselage.
Described vertical amount difference device comprises vertical back up pad and vertical amount difference table, described vertical back up pad is flat string configuration, described vertical amount difference table is horizontally fixed in vertical back up pad, and vertically back up pad two ends are connected on check-out console by a pair web joint, rear, each detection zone is all provided with a vertically amount difference table, thus each vertical amount difference table can the bearing ring of each detection zone of independent detection, and the side bearing front end face of vertical amount difference table tip and detection zone is in the same plane, during work, first mix up vertically measuring poor table, after bearing ring enters each detection zone and maintenance is stable, the tip contacts bearing ring sidewall of each vertical amount difference table is to carry out the detection of vertical difference to bearing ring.
Described parallel measurement apparatus comprises Rodless cylinder, slip base and parallel meter, described Rodless cylinder has two, vertically be arranged in the two ends, left and right of check-out console, Rodless cylinder is provided with the slip base of a flat strip, thus slip base can slide up and down on Rodless cylinder, described depth of parallelism scale is vertically fixed on sliding seat lower surface, and correspondence is furnished with a depth of parallelism scale above each detection zone, thus each depth of parallelism scale can the bearing ring of each detection zone of independent detection, during work, when detection zone is covered with bearing ring, and after bearing ring is stable, slip base drives each depth of parallelism scale to move downward above detection zone, to carry out Parallel testing to the bearing ring in each detection zone.
Described signal collection case is fixedly mounted on fuselage bottom surface, and signal collection case is connected with pick-up unit by signal wire, and vertical difference and the depth of parallelism of each detection zone inner bearing lasso all feed back in signal collection case.
Described pay-off comprises feeding funnel, shaft, stirring vane, stirring motor and transfer passage, described feeding funnel upper opening is larger than lower openings, in inverted boss type structure, rectangular through-hole is provided with in the middle part of feeding funnel bottom surface, bearing ring enters transfer passage from rectangular through-hole, described shaft is arranged symmetrically with along feeding funnel and runs through feeding funnel, the stirring vane of five flat strips is evenly provided with in the middle part of shaft, and stirring vane is in directly over rectangular through-hole, shaft both sides are fixed on fuselage by pair of supporting, described stirring motor is fixedly mounted on fuselage bottom surface, and be connected by belt between stirring motor with shaft, during work, stirring motor rotates and drives shaft to rotate, thus drive stirring vane to rotate above rectangular through-hole, thus make bearing ring not easily accumulated plugging rectangular through-hole, described transfer passage cross section is " Qian " shape structure, transfer passage is downward-sloping gradually from left to right along fuselage, transfer passage left end is connected with feeding funnel bottom surface, and the delivery port of transfer passage is positioned at immediately below rectangular through-hole, transfer passage right-hand member is positioned on the left of pick-up unit, and port contacts with the returning face plate of the turning device leftmost side on the right side of transfer passage, during work, the bearing ring fallen from rectangular through-hole enters transfer passage, be rolled into the returning face plate of turning device from transfer passage again, more than the height of bearing ring five millimeters of distance between the biside plate of transfer passage, thus bearing ring rolls downwards with erectility after entering transfer passage, and distance between the biside plate of transfer passage is equal with the width on returning face plate base, thus after bearing ring is rolled into turning device, bearing ring is on returning face plate completely.
Described pusher comprises propelling movement cylinder and pushing plate, described propelling movement cylinder is horizontally disposed above the bottom surface of fuselage, and propelling movement cylinder bottom is connected mutually with fuselage, push cylinder head to be connected mutually with pushing plate, described pushing plate is flat string configuration, pushing plate is vertically arranged in fuselage upper surface, and pushing plate is positioned at below pick-up unit, during work, when bearing ring detected and from landing check-out console to turning device and check-out console below fuselage on after, pusher works, propelling movement cylinder stretches out, pushing plate is driven to move right and push away below check-out console by bearing ring, thus be convenient to the collection of the bearing ring after being detected.
The bearing ring pick-up unit that the utility model provides, check-out console is divided into multiple region by it, thus the multiple bearing rings entering turning device are detected simultaneously, greatly improve detection efficiency, and vertical difference scale and depth of parallelism scale are used simultaneously, can the simultaneously vertical difference of detection axis bearing ring and the depth of parallelism, meet the detection demand of existing bearing ring.
Accompanying drawing explanation
Below in conjunction with drawings and embodiments, the utility model is further illustrated.
Fig. 1 is one-piece construction schematic diagram of the present utility model;
Fig. 2 is the structural representation of pay-off of the present utility model;
Fig. 3 is the partial schematic diagram after the utility model removing pay-off;
Fig. 4 is the one-piece construction schematic diagram of pick-up unit of the present utility model;
Fig. 5 is the structural representation of turning device of the present utility model;
Fig. 6 is the structural representation after pick-up unit of the present utility model removing turning device;
Fig. 7 is the A-A cut-open view of Fig. 4;
Fig. 8 is the partial structurtes schematic diagram at pusher place of the present utility model;
In figure: fuselage 1, pick-up unit 2, pay-off 3, pusher 4, turning device 21, check-out console 22, batch turning cylinder 23, vertical amount difference device 24, parallel measurement apparatus 25, signal collection case 26, roll-over unit 21a, returning face plate 211, upset cylinder 212, a rotating shaft 213, detection zone 221, bottom support 2211, side bearing 2212, No. two rotating shafts 222, vertical back up pad 241, vertical amount difference table 242, Rodless cylinder 251, slip base 252, depth of parallelism scale 253, feeding funnel 31, shaft 32, stirring vane 33, stirring motor 34, transfer passage 35, rectangular through-hole 311, push cylinder 41, pushing plate 42.
Embodiment
The technological means realized to make the utility model, creation characteristic, reaching object and effect is easy to understand, below in conjunction with concrete diagram, setting forth the utility model further.
As shown in Figure 1, Figure 2, shown in Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 7 and Fig. 8, a kind of bearing ring mass detection device described in the utility model, comprise fuselage 1, pick-up unit 2, pay-off 3 and pusher 4, described pick-up unit 2 is positioned on the right side of fuselage 1, and described pick-up unit 2 is positioned in the middle part of fuselage 1, described pay-off 3 is positioned on the left of fuselage 1.
As Fig. 1, Fig. 4, shown in Fig. 5 and Fig. 7, a kind of bearing ring mass detection device described in the utility model, described pick-up unit 2 comprises turning device 21, check-out console 22, batch turning cylinder 23, vertical amount difference device 24, parallel measurement apparatus 25 and signal collection case 26, described turning device 21 is made up of ten to two ten roll-over unit 21a, described roll-over unit 21a comprises returning face plate 211 and upset cylinder 212, the cross section of described returning face plate 211 is " L " shape structure, and the vertical edge of returning face plate 211 is outward-dipping, the effect that the vertical edge of returning face plate 211 is outward-dipping makes the bearing ring entering turning device 21 from pay-off 3 not easily drop into check-out console 22 from returning face plate 211, the base upper surface of returning face plate 211 along fuselage 1 from after be tilted to lower layout gradually, base upper surface along fuselage 1 from after be tilted to lower layout gradually effect be the vertical edge making bearing ring can be close to returning face plate 211, be hinged bottom described upset cylinder 212 with on front side of fuselage 1 bottom surface, the side of upset cylinder 212 top and turning device 21 is hinged, contact with each other between each roll-over unit 21a, and each roll-over unit 21a is connected by a rotating shaft 213, a rotating shaft 213 runs through the base of each roll-over unit 21a, and a rotating shaft 213 is arranged on above fuselage 1 bottom surface by a pair supporting seat, and the distance of each returning face plate about 211 side is equal with bearing ring external diameter, thus a corresponding bearing ring on each returning face plate 211, during work, bearing ring enters the returning face plate 211 of pick-up unit 2 from pay-off 3 with vertical state, after bearing ring enters returning face plate 211, due to the inclined design of returning face plate 211 upper plate, the inclination vertical edge that bearing ring is close to returning face plate 211 rolls, until bearing ring is covered with whole turning device 21, then, upset cylinder 212 stretches out, the returning face plate 211 of each roll-over unit 21a rotates backward around a rotating shaft 213, thus the bearing ring on each returning face plate 211 falls into check-out console 22 from returning face plate 211, after bearing ring on device 21 to be flipped all falls into check-out console 22, bearing ring on pay-off 3 is again rolled into and is covered with whole turning device 21.
As Fig. 1, Fig. 4, shown in Fig. 6 and Fig. 7, a kind of bearing ring mass detection device described in the utility model, described check-out console 22 is the string configuration of cross section in " ┘ " shape, and check-out console 22 is positioned on rear side of turning device 21, check-out console 22 is several detection zones 221 by vertical baffle even partition, the number of described detection zone 221 equals the number of roll-over unit 21a, and positive front end, each detection zone 221 correspond to a roll-over unit 21a, thus the returning face plate 211 on each roll-over unit 21a is when rotating, bearing ring on returning face plate 211 falls into corresponding detection zone 221, bottom, each detection zone 221 is provided with a pair bottom support 2211 and a side bearing 2212, bottom support 2211 is for spring bearing lasso bottom surface, collateral support 2212 is for spring bearing lasso side, the rear lower portion of described check-out console 22 runs through No. two rotating shafts 222, No. two described rotating shafts 222 are arranged on above fuselage 1 bottom surface by a pair supporting seat, described batch turning cylinder 23 top is hinged on lower surface in the middle part of check-out console 22, batch turning cylinder 23 bottom is hinged on fuselage 1 bottom surface back, under original state, batch turning cylinder 23 stretches out and makes check-out console 22 be in horizontality, during work, after returning face plate 211 rotation makes bearing ring fall into detection zone 221, batch turning cylinder 23 continues to protract, check-out console 22 is rotated clockwise around No. two rotating shafts 222, bearing ring is slided backward thus is close to side bearing 2212, then batch turning cylinder 23 shrinks and makes check-out console 22 again keep horizontality, and after bearing ring has detected, batch turning cylinder 23 shrinks, check-out console 22 is rotated counterclockwise around No. two rotating shafts 222, check-out console 222 is tilted to down on front side of fuselage 1, bearing ring from detection zone 221 landing to turning device 21 with check-out console 22 below fuselage 1.
As Fig. 1, Fig. 4, shown in Fig. 6 and Fig. 7, a kind of bearing ring mass detection device described in the utility model, described vertical amount difference device 24 comprises vertical back up pad 241 and vertical amount difference table 242, described vertical back up pad 241 is flat string configuration, described vertical amount difference table 242 is horizontally fixed in vertical back up pad 241, and vertically back up pad 241 two ends are connected on check-out console 22 by a pair web joint, rear, each detection zone 221 is all provided with a vertically amount difference table 242, thus each vertical amount difference table 242 can the bearing ring of each detection zone 221 of independent detection, and side bearing 2212 front end face of vertical amount difference table 242 tip and detection zone 221 is in the same plane, during work, first mix up vertically measuring poor table 242, after bearing ring enters each detection zone 221 and maintenance is stable, the tip contacts bearing ring sidewall of each vertical amount difference table 242 is to carry out the detection of vertical difference to bearing ring.
As Fig. 1, Fig. 4, shown in Fig. 6 and Fig. 7, a kind of bearing ring mass detection device described in the utility model, described parallel measurement apparatus 25 comprises Rodless cylinder 251, slip base 252 and parallel meter 253, described Rodless cylinder 251 has two, vertically be arranged in the two ends, left and right of check-out console 22, Rodless cylinder 251 is provided with the slip base 252 of a flat strip, thus slip base 252 can slide up and down on Rodless cylinder 251, described depth of parallelism scale 253 is vertically fixed on sliding seat 252 lower surface, and correspondence is furnished with a depth of parallelism scale 253 above each detection zone 221, thus each depth of parallelism scale 253 can the bearing ring of each detection zone 221 of independent detection, during work, when detection zone 221 is covered with bearing ring, and after bearing ring is stable, slip base 252 drives each depth of parallelism scale 253 to move downward above detection zone 221, to carry out Parallel testing to the bearing ring in each detection zone 221.
As shown in Fig. 1, Fig. 4 and Fig. 7, a kind of bearing ring mass detection device described in the utility model, described signal collection case 26 is fixedly mounted on fuselage 1 bottom surface, and signal collection case 26 is connected with pick-up unit 2 by signal wire, vertical difference and the depth of parallelism of each detection zone 221 inner bearing lasso all feed back in signal collection case 26.
As depicted in figs. 1 and 2, a kind of bearing ring mass detection device described in the utility model, described pay-off 3 comprises feeding funnel 31, shaft 32, stirring vane 33, stirring motor 34 and transfer passage 35, described feeding funnel 31 upper opening is larger than lower openings, in inverted boss type structure, rectangular through-hole 311 is provided with in the middle part of feeding funnel 31 bottom surface, bearing ring enters transfer passage 35 from rectangular through-hole 311, described shaft 32 is arranged symmetrically with along feeding funnel 31 and runs through feeding funnel 31, the stirring vane 33 of five flat strips is evenly provided with in the middle part of shaft 32, and stirring vane 33 is in directly over rectangular through-hole 311, shaft 32 both sides are fixing on the fuselage 1 by pair of supporting, described stirring motor 34 is fixedly mounted on fuselage 1 bottom surface, and be connected by belt between stirring motor 34 with shaft 32, during work, stirring motor 34 rotates and drives shaft 32 to rotate, thus drive stirring vane 33 to rotate above rectangular through-hole 311, thus make bearing ring not easily accumulated plugging rectangular through-hole 311, described transfer passage 35 cross section is " Qian " shape structure, transfer passage 35 is downward-sloping gradually from left to right along fuselage 1, transfer passage 35 left end is connected with feeding funnel 31 bottom surface, and the delivery port of transfer passage 35 is positioned at immediately below rectangular through-hole 311, transfer passage 35 right-hand member is positioned on the left of pick-up unit 2, and port contacts with the returning face plate 211 of turning device 21 leftmost side on the right side of transfer passage 35, during work, the bearing ring fallen from rectangular through-hole 311 enters transfer passage 35, be rolled into the returning face plate 211 of turning device 21 from transfer passage 35 again, more than the height of bearing ring five millimeters of distance between the biside plate of transfer passage 35, thus bearing ring rolls downwards with erectility after entering transfer passage 35, and distance between the biside plate of transfer passage 35 is equal with the width on returning face plate 211 base, thus after bearing ring is rolled into turning device 21, bearing ring is on returning face plate 211 completely.
As Fig. 1, Fig. 2, shown in Fig. 3 and Fig. 8, a kind of bearing ring mass detection device described in the utility model, described pusher 4 comprises propelling movement cylinder 41 and pushing plate 42, described propelling movement cylinder 41 is horizontally disposed above the bottom surface of fuselage 1, and be connected mutually with fuselage 1 bottom propelling movement cylinder 41, push cylinder 41 top to be connected mutually with pushing plate 42, described pushing plate 42 is flat string configuration, pushing plate 42 is vertically arranged in fuselage 1 upper surface, and pushing plate 42 is positioned at below pick-up unit 2, during work, when bearing ring detected and from landing check-out console 22 to turning device 21 with check-out console 22 below fuselage 1 on after, pusher 4 works, push cylinder 41 to stretch out, pushing plate 42 is driven to move right and pushed away by bearing ring below check-out console 22, thus be convenient to the collection of the bearing ring after being detected.
During work, bearing ring in hopper 11 enters transfer passage 35 from rectangular through-hole 311, and stirring motor 34 rotation drives shaft 32 to rotate, thus drive stirring vane 33 to rotate above rectangular through-hole 311, thus make bearing ring not easily accumulated plugging rectangular through-hole 311, after the bearing ring fallen from rectangular through-hole 311 enters transfer passage 35, be rolled into the returning face plate 211 of turning device 21 from transfer passage 35, after bearing ring enters returning face plate 211, due to the inclined design of returning face plate 211 upper plate, the inclination vertical edge that bearing ring is close to returning face plate 211 rolls, until bearing ring is covered with whole turning device 21, then, upset cylinder 212 stretches out, the returning face plate 211 of each roll-over unit 21a rotates backward around a rotating shaft 213, thus the bearing ring on each returning face plate 211 falls into check-out console 22 from returning face plate 211, after bearing ring on device 21 to be flipped all falls into check-out console 22, bearing ring on pay-off 3 is again rolled into and is covered with whole turning device 21.
Under original state, batch turning cylinder 23 stretches out and makes check-out console 22 be in horizontality, during work, after returning face plate 211 rotation makes bearing ring fall into detection zone 221, batch turning cylinder 23 continues to protract, check-out console 22 is rotated clockwise around No. two rotating shafts 222, bearing ring is slided backward thus is close to side bearing 2212, then batch turning cylinder 23 shrinks and makes check-out console 22 again keep horizontality, then mix up vertically measuring poor table 242, after bearing ring enters each detection zone 221 and maintenance is stable, the tip contacts bearing ring sidewall of each vertical amount difference table 242 is to carry out the detection of vertical difference to bearing ring, slip base 252 drives each depth of parallelism scale 253 to move downward above detection zone 221 simultaneously, to carry out Parallel testing to the bearing ring in each detection zone 221, vertical difference and the depth of parallelism of each detection zone 221 inner bearing lasso feed back in signal collection case 26 again.
After bearing ring has detected, batch turning cylinder 23 shrinks, check-out console 22 is rotated counterclockwise around No. two rotating shafts 222, check-out console 222 is tilted to down on front side of fuselage 1, bearing ring from detection zone 221 landing to turning device 21 with check-out console 22 below fuselage 1, then pusher 4 works, and pushes cylinder 41 and stretches out, drive pushing plate 42 move right and pushed away by bearing ring below check-out console 22, thus be convenient to the collection of the bearing ring after being detected.
More than show and describe ultimate principle of the present utility model, principal character and advantage.The technician of the industry should understand; the utility model is not restricted to the described embodiments; description in above-described embodiment and instructions principle of the present utility model is just described; under the prerequisite not departing from the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall within the scope of claimed the utility model.The claimed scope of the utility model is defined by appending claims and equivalent thereof.

Claims (7)

1. a bearing ring mass detection device, comprise fuselage (1), pick-up unit (2), pay-off (3) and pusher (4), it is characterized in that: described pick-up unit (2) is positioned at fuselage (1) right side, and described pick-up unit (2) is positioned at fuselage (1) middle part, described pay-off (3) is positioned at fuselage (1) left side, wherein:
Described pick-up unit (2) comprises turning device (21), check-out console (22), batch turning cylinder (23), vertical amount difference device (24), parallel measurement apparatus (25) and signal collection case (26), described turning device (21) is made up of ten to two ten roll-over units (21a), described roll-over unit (21a) comprises returning face plate (211) and upset cylinder (212), the cross section of described returning face plate (211) is " L " shape structure, and the vertical edge of returning face plate (211) is outward-dipping, the base upper surface of returning face plate (211) along fuselage (1) from after be tilted to lower layout gradually, be hinged on front side of described upset cylinder (212) bottom and fuselage (1) bottom surface, the side of upset cylinder (212) top and turning device (21) is hinged, contact with each other between each roll-over unit (21a), and each roll-over unit (21a) is connected by a rotating shaft (213), a rotating shaft (213) runs through the base of each roll-over unit (21a), and a rotating shaft (213) is arranged on above fuselage (1) bottom surface by a pair supporting seat, and the distance of each returning face plate (211) left and right side is equal with bearing ring external diameter.
2. a kind of bearing ring mass detection device according to claim 1, it is characterized in that: described check-out console (22) is the string configuration of cross section in " ┘ " shape, and check-out console (22) is positioned at turning device (21) rear side, check-out console (22) is several detection zones (221) by vertical baffle even partition, the number of described detection zone (221) equals the number of roll-over unit (21a), and each detection zone (221) positive front end correspond to a roll-over unit (21a), each detection zone (221) bottom is provided with a pair bottom support (2211) and a side bearing (2212), the rear lower portion of described check-out console (22) runs through No. two rotating shafts (222), No. two described rotating shafts (222) are arranged on above fuselage (1) bottom surface by a pair supporting seat, described batch turning cylinder (23) top is hinged on lower surface, check-out console (22) middle part, batch turning cylinder (23) bottom is hinged on fuselage (1) bottom surface back.
3. a kind of bearing ring mass detection device according to claim 1, it is characterized in that: described vertical amount difference device (24) comprises vertical back up pad (241) and vertical amount difference table (242), described vertical back up pad (241) is flat string configuration, described vertical amount difference table (242) is horizontally fixed in vertical back up pad (241), and vertically back up pad (241) two ends are connected on check-out console (22) by a pair web joint, each detection zone (221) rear is all provided with vertically amount difference table (242), and side bearing (2212) front end face of vertical amount difference table (242) tip and detection zone (221) is in the same plane.
4. a kind of bearing ring mass detection device according to claim 1, it is characterized in that: described parallel measurement apparatus (25) comprises Rodless cylinder (251), slip base (252) and parallel meter (253), described Rodless cylinder (251) has two, vertically be arranged in the two ends, left and right of check-out console (22), Rodless cylinder (251) is provided with the slip base (252) of a flat strip, described depth of parallelism scale (253) is vertically fixed on sliding seat (252) lower surface, and each detection zone (221) top correspondence is furnished with a depth of parallelism scale (253).
5. a kind of bearing ring mass detection device according to claim 1, it is characterized in that: described signal collection case (26) is fixedly mounted on fuselage (1) bottom surface, and signal collection case (26) is connected with pick-up unit (2) by signal wire.
6. a kind of bearing ring mass detection device according to claim 1, it is characterized in that: described pay-off (3) comprises feeding funnel (31), shaft (32), stirring vane (33), stirring motor (34) and transfer passage (35), described feeding funnel (31) upper opening is larger than lower openings, in inverted boss type structure, rectangular through-hole (311) is provided with in the middle part of feeding funnel (31) bottom surface, described shaft (32) is arranged symmetrically with along feeding funnel (31) and runs through feeding funnel (31), shaft (32) middle part is evenly provided with the stirring vane (33) of five flat strips, and stirring vane (33) is in directly over rectangular through-hole (311), shaft (32) both sides are fixed on fuselage (1) by pair of supporting, described stirring motor (34) is fixedly mounted on fuselage (1) bottom surface, and be connected by belt between stirring motor (34) with shaft (32), described transfer passage (35) cross section is " Qian " shape structure, transfer passage (35) is downward-sloping gradually from left to right along fuselage (1), transfer passage (35) left end is connected with feeding funnel (31) bottom surface, and the delivery port of transfer passage (35) is positioned at immediately below rectangular through-hole (311), transfer passage (35) right-hand member is positioned at pick-up unit (2) left side, and transfer passage (35) right side port contacts with the returning face plate (211) of turning device (21) leftmost side, more than the height of bearing ring five millimeters of distance between the biside plate of transfer passage (35), and distance between the biside plate of transfer passage (35) is equal with the width on returning face plate (211) base.
7. a kind of bearing ring mass detection device according to claim 1, it is characterized in that: described pusher (4) comprises propelling movement cylinder (41) and pushing plate (42), described propelling movement cylinder (41) is horizontally disposed above the bottom surface of fuselage (1), and propelling movement cylinder (41) bottom is connected mutually with fuselage (1), push cylinder (41) top to be connected mutually with pushing plate (42), described pushing plate (42) is flat string configuration, pushing plate (42) is vertically arranged in fuselage (1) upper surface, and pushing plate (42) is positioned at pick-up unit (2) below.
CN201520416115.9U 2015-06-16 2015-06-16 Big batch detection device of bearing ring Withdrawn - After Issue CN204854702U (en)

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CN201520416115.9U Withdrawn - After Issue CN204854702U (en) 2015-06-16 2015-06-16 Big batch detection device of bearing ring

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104913758A (en) * 2015-06-16 2015-09-16 安徽省百基机电科技有限公司 Bearing ring mass detection device
CN106091979A (en) * 2016-06-03 2016-11-09 人本集团有限公司 A kind of sealing bearing seal structure and sealing ring method for detecting shape thereof

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104913758A (en) * 2015-06-16 2015-09-16 安徽省百基机电科技有限公司 Bearing ring mass detection device
CN104913758B (en) * 2015-06-16 2017-05-10 安徽省百基机电科技有限公司 Bearing ring mass detection device
CN106091979A (en) * 2016-06-03 2016-11-09 人本集团有限公司 A kind of sealing bearing seal structure and sealing ring method for detecting shape thereof

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AV01 Patent right actively abandoned

Granted publication date: 20151209

Effective date of abandoning: 20170510

AV01 Patent right actively abandoned