CN2856101Y - Slope positioning device of slope industrial washing machine - Google Patents
Slope positioning device of slope industrial washing machine Download PDFInfo
- Publication number
- CN2856101Y CN2856101Y CN 200520077120 CN200520077120U CN2856101Y CN 2856101 Y CN2856101 Y CN 2856101Y CN 200520077120 CN200520077120 CN 200520077120 CN 200520077120 U CN200520077120 U CN 200520077120U CN 2856101 Y CN2856101 Y CN 2856101Y
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- base
- fuselage
- pin shaft
- hinged
- hinging pin
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Abstract
The utility model discloses an inclination positioning device for inclined industrial washing machine having machine body with both forward inclination and backward inclination functions. The inclination positioning device mainly comprises base; machine body disposed on the base; hoisting device disposed between the base and bottom plate of the machine body; positioning protruded block disposed on lower side of the bottom plate; hinge blocks respectively disposed on lower front and back ends of the bottom plate; positioning seat disposed on the base and corresponding to the positioning protruded block; hinge seat disposed on the base and corresponding to the hinge blocks; and hinge pin disposed between the hinge block and hinge seat. The utility model is characterized by disposing drive device on the base for driving movement of the hinge pin. The drive device consists essentially of air cylinder, and link rod respectively connected with piston rod of the air cylinder and the hinge pin. By using the above inclination positioning device on large-scale industrial washing machine, the washing machine can possess automatic feeding and discharging functions and convenient operation.
Description
Technical field
The utility model relates to the large scale industry washing machine that the fuselage tiltable is rotated, and refers more particularly to the sloped position device that can control the fuselage incline direction in this kind washing machine.
Background technology
In the hotel, place such as restaurant, hospital, washing service centre, usually use the large scale industry washing machine of drying washing capacity at over 80 kg.Because the washing capacity of this washing machine is big especially; it is just very inconvenient to only depend on operator's manual operations to carry out charging or discharging; therefore, in this washing machine, also be provided with the sloped position device that can make fuselage inclination certain angle usually, realize automatic feed or discharging to cooperate.The structure of traditional sloped position device mainly comprises: base, fuselage is arranged on the upside of base, between base and fuselage base plate, being provided with and rising ejection device---the ejection device that rises commonly used can be cylinder, oil cylinder or air bag, downside at the fuselage base plate is provided with locating convex block, front end or rear end at fuselage base plate downside are provided with hinged block, on base, be respectively arranged with the corresponding positioning seat of locating convex block, with the corresponding hinged seat of hinged block, between hinged block and hinged seat, be set with hinging pin shaft.The principle that its fuselage tilts is: when hinged block is arranged on the front end of fuselage base plate, under the effect that rises ejection device, fuselage just can be around the hinged place between its base plate front end and the base---the hinging pin shaft rotation, fuselage certain angle that just can lean forward, make gate downward, at this moment, open gate, just can realize the function of self-emptying; When hinged block is arranged on the rear end of fuselage base plate, under the effect that rises ejection device, fuselage just can be around the hinged place between its base plate rear end and the base---the hinging pin shaft rotation, but fuselage is the certain angle of hypsokinesis just, make gate upwards, at this moment, open gate, under the cooperation of the hanging device that disposes in addition, just can realize automatically feed function.The shortcoming of above-mentioned sloped position device is: because hinged block only is arranged on the front end of fuselage base plate usually or only is arranged on the rear end of fuselage base plate, and fixedly connected by hinging pin shaft between hinged block and the hinged seat, therefore, can only realize single leaning forward or the function of hypsokinesis, washing machine can only be realized automatic feed or can only realize self-emptying, and can not both take into account; In addition, when fuselage is placed when steady, a part of weight of fuselage can rely on hinging pin shaft to bear and transmit, like this, when washing, when especially dewatering, hinging pin shaft can bear the bigger dynamic load that fuselage produces for a long time, and hinging pin shaft is worn and torn and modification too much, influence the normal use of machine, also can produce bigger noise.
Summary of the invention
At the problems referred to above, the utility model will provide a kind of fuselage that can make industry washer to realize simultaneously leaning forward and the sloped position device of hypsokinesis function.
For achieving the above object, the technical solution adopted in the utility model is: the sloped position device in the described fuselage tilting industry washer, mainly comprise: base, fuselage is arranged on the upside of base, between base and fuselage base plate, be provided with and rise ejection device, downside at the fuselage base plate is provided with locating convex block, rear and front end at fuselage base plate downside is respectively arranged with hinged block, on base, be respectively arranged with the corresponding positioning seat of locating convex block, with the corresponding hinged seat of hinged block, between hinged block and hinged seat, be provided with hinging pin shaft; Be characterized in: on base, also be provided with and drive the drive unit that hinging pin shaft moves.
The structure of above-mentioned drive unit is: cylinder is installed on the base, and the piston rod of cylinder is connected with hinging pin shaft by bindiny mechanism.A kind of structure of described bindiny mechanism is: the piston rod of cylinder is connected with a rotary body, and rotary body is movably arranged on the base, and rotary body is connected with hinging pin shaft by connecting rod again.
In addition, work more reliably for making hinging pin shaft, also hinging pin shaft can be movably arranged in the guide holder, guide holder is fixed on the base.
Equally, also can be set to dovetail shaped by described locating convex block, described positioning seat also is set to dovetail shaped.
The utility model has the advantages that: in fuselage tilting industry washer, use described sloped position device, the fuselage of washing machine can be realized leaning forward and can realize the function of hypsokinesis, that is to say, washing machine can realize can automatic feed again can self-emptying function, use convenient; And the weight of fuselage can pass to base effectively by locating convex block and positioning seat, and reaches the earth, and hinging pin shaft does not bear the weight of fuselage, more stable work, and work noise is lower.
Description of drawings
Fig. 1 is the main TV structure schematic diagram of the sloped position device in the fuselage tilting industry washer described in the utility model;
Fig. 2 be base shown in Fig. 1 and drive unit mounted thereto overlook the direction schematic diagram;
Fig. 3 is the cross-sectional view of the left apparent direction of the drive unit shown in the branch of right side among Fig. 2.
Embodiment
Below in conjunction with the drawings and specific embodiments technical scheme described in the utility model and operation principle thereof and advantage are further described.
As shown in Figure 1, in the present embodiment, fuselage 7 is arranged on the upside of base 1, be provided with gate 8 in the front side of fuselage 7, between base 1 and fuselage base plate 5, be provided with and rise ejection device 11---in the present embodiment, use air bag 11 as rising ejection device, be provided with some locating convex blocks 6 at the downside of fuselage base plate 5, locating protruding fast 6 quantity can determine according to actual needs, generally four locating convex blocks 6 can evenly be set at the downside of base plate 5; Rear and front end at fuselage base plate 5 downsides is respectively arranged with hinged block---in the present embodiment,---be right-hand member among Fig. 1 be respectively arranged with two hinged blocks 9, in the rear end---is that left end among Fig. 1 also is respectively arranged with two hinged blocks 4 at front end, certainly, the quantity of hinged block also can be determined according to actual needs; As shown in Figure 2, on base 1, be respectively arranged with and locating convex block 6 corresponding four positioning seats 3, with hinged block 9 and 4 corresponding hinged seats 10,21 and 2,23, between hinged block and hinged seat, be provided with hinging pin shaft, on base 1, also be provided with and drive the drive unit that hinging pin shaft moves, as shown in Figure 2, in the present embodiment, because base 1 upper left side is identical with the structure of the drive unit shown in the right side, so be that example illustrates syndeton and the operating principle thereof between hinging pin shaft and the drive unit with the drive unit shown in the right side below, as Fig. 2, shown in Figure 3, the structure of drive unit is: cylinder 17 is installed on the base 1, the piston rod of cylinder 17 is connected with a rotary body 16, rotary body 16 is movably arranged on the installation shaft 22 on the base 1, rotary body 16 is connected with hinging pin shaft 12 by connecting rod 14 respectively again, be connected with hinging pin shaft 20 by connecting rod 18, hinging pin shaft 12 and 20 is movably arranged on respectively in guide holder 13 and 19, guide holder 13 and 19 is separately fixed on the base 1, and the effect that guide holder 13 and 19 are set is to have better directionality when hinging pin shaft 12 and 20 is moved.In addition, in the present embodiment, described locating convex block 6 is the dovetail shaped locating convex block, and described positioning seat 3 is the dovetail shaped positioning seat; Certainly, in actual applications, the shape that locating convex block 6 and positioning seat 3 also can select for use taper, sphere etc. to be convenient to mutually combine.
The operation principle of the sloped position device of said structure is: (one), when fuselage 7 is in the duty of horizontal on base 1, this moment, air bag 11 was in shrivelled state, two hinged blocks 9 of fuselage base plate 5 front sides lay respectively in the hinged groove 101 and 211 on hinged seat 10 and 21, at this moment, hinging pin shaft 12 extend in the hole of a hinged block 9 and hinged seat 10 and with they bolt jails, 20 of hinging pin shafts extend in the hole of another hinged block 9 and hinged seat 21 and with they bolt jails---as shown in Figure 3, among Fig. 3 for expressing hinged groove 101 and 211, so in hinged groove 101 and 211, do not express hinged block 9 respectively.Equally, two hinged blocks 4 of fuselage base plate 5 rear sides also lay respectively in the hinged groove on hinged seat 2 and 23, and equally by corresponding hinging pin shaft bolt jail.At this moment, locating convex block 6 also drops in the positioning seat 3 all, and locating convex block 6 is bearing the fuselage weight of the overwhelming majority with positioning seat 3, hinging pin shaft between fuselage base plate 5 and the base 1 then is in the gap state that freely becomes flexible, bearing load hardly, like this, the bigger load that produces during machine works all passes to base 1 by locating convex block 6 and positioning seat 3, and reaching the earth, hinging pin shaft just can not produce wearing and tearing and distortion.(2), when fuselage 7 being receded when the needs charging, as Fig. 2, shown in Figure 3, control cylinder 17, its piston rod is withdrawn inwards, 16 rotations of piston rod pulling rotary body, rotary body 16 is pulled out hinging pin shaft 12 by connecting rod 14 respectively, by connecting rod 18 hinging pin shaft 20 is pulled out, the hinged block 4 and the hinged seat 2 and 23 of fuselage base plate 5 rear sides then still is in bolt jail state, in air bag 11, charge into gases at high pressure then, rising under the effect of top of air bag 11, the hinged block 9 of fuselage base plate 5 front sides will be separated with hinged seat 10 and 21 respectively, and fuselage base plate 5 can be around the hinged block 4 and the rotation of the hinging pin shaft between hinged seat 2 and 23 of its rear side, like this, fuselage 7 certain angle that will recede after reaching required angle, can be opened gate 8, under the cooperation of the hanging device that disposes in addition, just can realize automatically feed function.After the feeder finishes, gas in the air bag 11 is bled off, under the effect of gravity, fuselage 7 can be got back to the horizontal state again lentamente, two hinged blocks 9 of fuselage base plate 5 front sides just can drop into respectively again in the hinged groove 101 and 211 on hinged seat 10 and 21, then, control cylinder 11 counteragents again, order about that hinging pin shaft 12 extend in the hole of a hinged block 9 and hinged seat 10 and with their bolt jails, order about hinging pin shaft 20 and extend in the hole of another hinged block 9 and hinged seat 21 and they bolt jails, like this, washing machine just can begin to have washed work normally.(3), when fuselage 7 being turned forward when the needs discharging, then opposite with the action of above-mentioned charging---promptly: draw back the hinged block 4 of fuselage base plate 5 rear sides and the hinging pin shaft between hinged seat 2 and 23, hinging pin shaft 12 and 20 then still is in bolt jail state between the hinged block 9 of fuselage base plate 5 front sides and hinged seat 10 and 21, in air bag 11, charge into gases at high pressure then, rising under the effect of top of air bag 11, the hinged block 4 of fuselage base plate 5 rear sides will be separated with hinged seat 2 and 23 respectively, and fuselage base plate 5 can be around the hinged block 9 and the rotation of the hinging pin shaft between hinged seat 10 and 21 of its front side, like this, fuselage 7 certain angle that will turn forward, after reaching required angle, open gate 8, just can realize the function of self-emptying.
As seen, use sloped position device described in the utility model in the large scale industry washing machine, the fuselage of washing machine can be realized leaning forward and can realize that is to say the function of hypsokinesis, washing machine can realize can automatic feed again can self-emptying function, use convenient.
Claims (5)
1, the sloped position device in the fuselage tilting industry washer, mainly comprise: base, fuselage is arranged on the upside of base, between base and fuselage base plate, be provided with and rise ejection device, downside at the fuselage base plate is provided with locating convex block, rear and front end at fuselage base plate downside is respectively arranged with hinged block, on base, be respectively arranged with the corresponding positioning seat of locating convex block, with the corresponding hinged seat of hinged block, between hinged block and hinged seat, be provided with hinging pin shaft; It is characterized in that: on base, also be provided with and drive the drive unit that hinging pin shaft moves.
2, sloped position device according to claim 1, it is characterized in that: the structure of described drive unit is: cylinder is installed on the base, and the piston rod of cylinder is connected with hinging pin shaft by bindiny mechanism.
3, sloped position device according to claim 2, it is characterized in that: the structure of described bindiny mechanism is: the piston rod of cylinder is connected with a rotary body, rotary body is movably arranged on the base, and rotary body is connected with hinging pin shaft by connecting rod again.
4, according to claim 1 or 2 or 3 described sloped position devices, it is characterized in that: hinging pin shaft is movably arranged in the guide holder, and guide holder is fixed on the base.
5, sloped position device according to claim 1 and 2 is characterized in that: described locating convex block is the dovetail shaped locating convex block, and described positioning seat is the dovetail shaped positioning seat.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN 200520077120 CN2856101Y (en) | 2005-11-04 | 2005-11-04 | Slope positioning device of slope industrial washing machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200520077120 CN2856101Y (en) | 2005-11-04 | 2005-11-04 | Slope positioning device of slope industrial washing machine |
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CN2856101Y true CN2856101Y (en) | 2007-01-10 |
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CN 200520077120 Expired - Fee Related CN2856101Y (en) | 2005-11-04 | 2005-11-04 | Slope positioning device of slope industrial washing machine |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102330317A (en) * | 2011-01-05 | 2012-01-25 | 袁廷荣 | Automatic discharging process in washing and dehydrating |
CN103046301A (en) * | 2013-01-21 | 2013-04-17 | 上海航星机械(集团)有限公司 | Control device and control method of integrated automatic washing system |
CN104032537A (en) * | 2014-06-17 | 2014-09-10 | 冯晋 | Preliminary cleaning machine for spinning |
CN105019187A (en) * | 2015-07-27 | 2015-11-04 | 江苏海狮机械集团有限公司 | Blanking device in liner of water washing and extracting device |
CN105780403A (en) * | 2016-05-19 | 2016-07-20 | 蓬莱市大成洗涤机械有限公司 | Industrial clothes washing dehydration machine |
CN110894666A (en) * | 2019-11-22 | 2020-03-20 | 江苏汇布洗涤机械制造有限公司 | Sanitary isolation type washing machine convenient for pouring out washings |
-
2005
- 2005-11-04 CN CN 200520077120 patent/CN2856101Y/en not_active Expired - Fee Related
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102330317A (en) * | 2011-01-05 | 2012-01-25 | 袁廷荣 | Automatic discharging process in washing and dehydrating |
CN103046301A (en) * | 2013-01-21 | 2013-04-17 | 上海航星机械(集团)有限公司 | Control device and control method of integrated automatic washing system |
CN104032537A (en) * | 2014-06-17 | 2014-09-10 | 冯晋 | Preliminary cleaning machine for spinning |
CN105019187A (en) * | 2015-07-27 | 2015-11-04 | 江苏海狮机械集团有限公司 | Blanking device in liner of water washing and extracting device |
CN105019187B (en) * | 2015-07-27 | 2017-03-01 | 江苏海狮机械集团有限公司 | Doffer in eluting machine liner |
CN105780403A (en) * | 2016-05-19 | 2016-07-20 | 蓬莱市大成洗涤机械有限公司 | Industrial clothes washing dehydration machine |
CN110894666A (en) * | 2019-11-22 | 2020-03-20 | 江苏汇布洗涤机械制造有限公司 | Sanitary isolation type washing machine convenient for pouring out washings |
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Legal Events
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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: 20070110 Termination date: 20141104 |
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EXPY | Termination of patent right or utility model |