CN203451853U - Lint shaver - Google Patents
Lint shaver Download PDFInfo
- Publication number
- CN203451853U CN203451853U CN201320547740.8U CN201320547740U CN203451853U CN 203451853 U CN203451853 U CN 203451853U CN 201320547740 U CN201320547740 U CN 201320547740U CN 203451853 U CN203451853 U CN 203451853U
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- CN
- China
- Prior art keywords
- fuselage
- conducting strip
- battery
- hair bulb
- folding shape
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- 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
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- 239000002184 metal Substances 0.000 claims description 39
- 229910052751 metal Inorganic materials 0.000 claims description 39
- 210000004209 hair Anatomy 0.000 claims description 18
- 210000003660 reticulum Anatomy 0.000 claims description 17
- 239000002537 cosmetic Substances 0.000 claims description 6
- 238000005034 decoration Methods 0.000 claims description 6
- 150000002739 metals Chemical class 0.000 claims description 6
- 238000003032 molecular docking Methods 0.000 claims description 3
- 238000005457 optimization Methods 0.000 abstract description 3
- 230000010354 integration Effects 0.000 abstract description 2
- 238000005520 cutting process Methods 0.000 description 7
- 230000005611 electricity Effects 0.000 description 3
- 230000007613 environmental effect Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000013138 pruning Methods 0.000 description 1
- 210000002268 wool Anatomy 0.000 description 1
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Abstract
The utility model discloses a lint shaver. The present lint shavers are supplied with power by dry batteries, rechargeable batteries or direct-plug type power supplies; the direct-plug type power supplies are very inconvenient to use, while the batteries are neither economical nor environment-friendly. The lint shaver disclosed by the utility model is characterized in that a working circuit is composed of a motor, a fuse switch, a battery and a detachable DC (Direct Current) socket, wherein the fuse switch can be disconnected or connected through the operation of a switch push button; the fuse switch, the battery and the detachable DC socket are arranged inside a shaver body, and the switch push button is arranged on the shaver body. By optimization and integration of the battery and a power supply direct-plug structure, the lint shaver disclosed by the utility model not only can be used in urban areas with enough electric power in a direct-plug manner through an adapter to achieve an economical and environment-friendly effect, but also can be used in areas with unstable electric power or without electric power.
Description
Technical field
The utility model relates to small household appliances, specifically a kind of hair bulb clipping machine.
Background technology
Hair bulb clipping machine is applied to wool, sportswear, skirt, scarf, woollen blanket etc., for shaving off rapidly ball top, and can not destroy sweater itself, shaves the fluffy sense that Mao Houke keeps fabric.Hair bulb clipping machine, as a kind of simple and practical small household appliances, is being played the part of more and more important role in life, and the product of selling in market is also multifarious, very different.Power supply to hair bulb clipping machine power supply is dry cell, rechargeable battery or straight cutting power supply at present; Straight cutting power supply is very inconvenient in the use, and particularly in the unsettled area of power supply, straight cutting power supply can allow again you often without the available and troublesome of electricity; Use not only uneconomical but also not environmental protection of battery.
Utility model content
Technical problem to be solved in the utility model is to overcome the defect that above-mentioned prior art exists, provide a kind of by the hair bulb clipping machine of battery and power supply straight cutting structure optimization integration, make its both can be in city many electricity area adopt adapter straight cuttings to use and reach economy, environmental protection, again can be at power supply unstable or use without electric area.
For this reason, the utility model adopts following technical scheme: a kind of hair bulb clipping machine, comprise plastic fuselage and for the head of blade is installed, one motor is housed in described fuselage, it is characterized in that, described motor and a discharge cock, a battery and a separate type DC socket form an operating circuit, described discharge cock is realized its disconnection or closure by the operation of a switch push button, described discharge cock, battery and separate type DC socket are positioned at fuselage, and described switch push button is arranged on fuselage;
When separate type DC socket is not inserted DC power plug, the battery-powered machine operation of giving; When separate type DC socket inserts DC power plug, the power supply circuits of battery disconnect, by DC power supply to machine operation.
Described battery is dry cell or rechargeable battery.Adopt separate type DC socket, during insertion, battery circuit disconnects, and prevents because using adapter to produce the potential safety hazard of conflicting for direct current with powered battery.
As the further of technique scheme improved and supplemented, the utility model is taked following technical measures:
Described separate type DC socket is by plastic casing, being arranged on the metal clips that three conducting strips on plastic casing and can deformation forms, on plastic casing, have a jack, on fuselage, there is a through hole communicating with jack, the first conducting strip is connected with discharge cock, the second conducting strip is connected with the negative pole of battery, the 3rd conducting strip is connected with the positive pole of battery, the positive pole of battery is connected with one end of motor, the other end of motor is connected with discharge cock, described metal clips is located between the first conducting strip and the second conducting strip throws off or contacts for controlling both, on the 3rd conducting strip, connect a perpendicular transverse conductance post, transverse conductance post is placed in jack, when jack is not inserted DC power plug, metal clips is connected the first conducting strip with the second conducting strip, and powered battery is to machine operation, when jack inserts DC power plug, the negative pole that is positioned at DC power plug sidepiece is thrown off metal clips generation deformation and the second conducting strip, only contact with the first conducting strip, the positive pole that is positioned at DC power plug head is enclosed within on transverse conductance post and is connected with the 3rd conducting strip, by DC power supply to machine operation.
Described metal clips and the first conducting strip are connected as a single entity, and convenient processing, reduces costs.
On described fuselage, form the handle of a handled easily, operate comfortable.
Described fuselage is formed by left fuselage and the docking of right fuselage, on described left fuselage and right fuselage, respectively forms half handles, assembles simple and efficient, easy to maintenance.
Described head comprise be arranged on underbelly case ring, adopt the cutter reticulum be threaded and be arranged on the cutter net on cutter reticulum with case ring, described discharge cock consists of two folding shape sheet metals, on the inwall of described left fuselage or right fuselage, form one for placing the mount pad of discharge cock, mount pad is provided with two locating slots; One end of two folding shape sheet metals is separately positioned in corresponding locating slot, and the other end is free end; Be positioned at folding shape sheet metal free end and be provided with a location-plate, between described head and location-plate, be provided with one the Arming Assembly that cutter reticulum cannot be worked is not installed.
Described Arming Assembly comprises bumper bar and relief spring, has a breach on the inwall of case ring; When cutter reticulum is threaded with case ring, on bumper bar, move, relief spring is compressed, the lower end of bumper bar is arranged in breach and bottom is against on the upper end of case ring, the upper end of bumper bar is used in conjunction with the folding shape sheet metal that is positioned at inner side, upwards the folding shape sheet metal of inner side, top outwards moves, and can make two folding shape sheet metal contact conductions in the opereating specification of switch push button;
While not connecting cutter reticulum on case ring, relief spring makes the upper end of bumper bar and have an insurance distance between the folding shape sheet metal of inner side, cannot make two folding shape sheet metal contact conductions in the opereating specification of switch push button.
On described bumper bar, form a platform, the lower end of relief spring is against on platform, and upper end is against on the inwall of a positioning sleeve, and described positioning sleeve is enclosed within outside relief spring.
Described grip is provided with leader's cosmetic sheet, the front portion of described fuselage is provided with a front decoration sheet, by front decoration sheet, with the screw in handle cosmetic sheet, left and right fuselage is fixedly connected with, on the inwall of fuselage, be formed for the centring ring that dog screw is used in conjunction with, the centre of screw has an opening that can make its diameter change.By said structure, make the sound construction of the utility model fuselage reliable, and assemble simple and efficient.
The bottom of described fuselage is equipped with one for storing the large capacity disposable box of detachable of ball top, and the large capacity disposable box of this detachable communicates with head inner chamber.The large capacity disposable box of detachable had both increased the continuous pruning working time, clean convenient again.
The utlity model has following beneficial effect: battery and the structure optimization of power supply straight cutting are integrated, make its both can be in city many electricity area adopt adapter straight cuttings to use to reach economy, environmental protection, again can be at power supply unstable or use without electric area; Sound construction is reliable, assembles simple and efficient, easy to maintenance; Prune continuously longevity of service, clean convenient again.
Below in conjunction with specification drawings and specific embodiments, the utility model is further described.
Accompanying drawing explanation
Fig. 1 is STRUCTURE DECOMPOSITION figure of the present utility model.
Fig. 2-3 are local structural graph of the present utility model (removing after right fuselage).
Fig. 4 is the structural representation (removing after right fuselage) that the utility model is not installed cutter reticulum.
Fig. 5 is the structural representation of the utility model cutter reticulum and case ring.
Fig. 6 is the structure chart of the utility model separate type DC socket.
Fig. 7 is that the utility model separate type DC socket inserts the structure chart after DC power plug.
Fig. 8 is circuit theory diagrams of the present utility model.
The specific embodiment
Hair bulb clipping machine as shown in the figure, motor 1 is housed in plastic fuselage, described motor 1 forms operating circuit with discharge cock 2, battery 3 and separate type DC socket 4, described discharge cock 2 is realized its disconnection or closure by the operation of switch push button 5, described discharge cock 2, battery 3 and separate type DC socket 4 are positioned at fuselage, and described switch push button 5 is arranged on fuselage.
Described separate type DC socket 4 is by plastic casing 41, being arranged on three conducting strips on plastic casing 41 and metal clips 42 that can deformation forms, on plastic casing 41, have jack, on fuselage, have the through hole 6 communicating with jack, the first conducting strip 43 is connected with discharge cock 2, the second conducting strip 44 is connected with the negative pole of battery 3, the 3rd conducting strip 45 is connected with the positive pole of battery 3, the positive pole of battery 3 is connected with one end of motor 1, the other end of motor 1 is connected with discharge cock 2, described metal clips 42 and the first conducting strip 43 are connected as a single entity, metal clips is located between the first conducting strip 43 and the second conducting strip 44 throws off or contacts for controlling both.On the 3rd conducting strip 45, connect a perpendicular transverse conductance post 46, transverse conductance post 46 is placed in jack.When jack is not inserted DC power plug, metal clips is connected the first conducting strip with the second conducting strip, and powered battery is to machine operation; When jack inserts DC power plug, the negative pole that is positioned at DC power plug sidepiece is thrown off metal clips generation deformation and the second conducting strip, only contact with the first conducting strip, the positive pole that is positioned at DC power plug head is enclosed within on transverse conductance post and is connected with the 3rd conducting strip, by DC power supply to machine operation.
On described fuselage, form the handle 7 of handled easily, described fuselage is formed by left fuselage 8 and 9 docking of right fuselage, on described left fuselage 8 and right fuselage 9, respectively forms half handles.Described head comprise be arranged on underbelly case ring 12, adopt the cutter reticulum 13 be threaded and be arranged on the cutter net 14 on cutter reticulum with case ring, described discharge cock 2 consists of two folding shape sheet metals 21,22, on the inwall of described left fuselage or right fuselage, form one for placing the mount pad 10 of discharge cock, mount pad 10 is provided with two locating slots; One end of two folding shape sheet metals is separately positioned in corresponding locating slot, and the other end is free end.Be positioned at folding shape sheet metal free end and be provided with location-plate 11, between described head and location-plate, be provided with the Arming Assembly that cutter reticulum cannot be worked is not installed, described Arming Assembly is comprised of bumper bar 15 and relief spring 16, has breach 17 on the inwall of case ring 12.On described bumper bar 15, form platform 18, the lower end of relief spring 16 is against on platform 18, and upper end is against on the inwall of positioning sleeve 19, and described positioning sleeve 19 is enclosed within outside relief spring 16.
When cutter reticulum is threaded with case ring, on bumper bar, move, relief spring is compressed, the lower end of bumper bar is arranged in breach and bottom is against on the upper end of case ring, the upper end of bumper bar is used in conjunction with the folding shape sheet metal 22 that is positioned at inner side, upwards the folding shape sheet metal 22 of inner side, top outwards moves, and can make two folding shape sheet metal contact conductions in the opereating specification of switch push button.
While not connecting cutter reticulum on case ring, relief spring makes the upper end of bumper bar and have an insurance distance between the folding shape sheet metal of inner side, cannot make two folding shape sheet metal contact conductions in the opereating specification of switch push button.
Described grip is provided with handle cosmetic sheet 20, the front portion of described fuselage is provided with front decoration sheet 23, by front decoration sheet 23, with the dog screw 24 in handle cosmetic sheet 20, left and right fuselage is fixedly connected with, on the inwall of fuselage, be formed for the centring ring 25 that dog screw is used in conjunction with, the centre of dog screw 24 has an opening that can make its diameter change.
The bottom of described fuselage is equipped with one for storing the large capacity disposable box 26 of detachable of ball top, and the large capacity disposable box 26 of this detachable communicates with head inner chamber.
The above, be only preferred embodiment of the present utility model, not structure of the present utility model done to any pro forma restriction.Any simple modification, equivalent variations and modification that every foundation technical spirit of the present utility model is done above embodiment, all fall in protection domain of the present utility model.
Claims (10)
1. a hair bulb clipping machine, comprise plastic fuselage and for the head of blade is installed, one motor (1) is housed in described fuselage, it is characterized in that, described motor (1) forms an operating circuit with a discharge cock (2), a battery (3) and a separate type DC socket (4), described discharge cock (2) is realized its disconnection or closure by the operation of a switch push button (5), described discharge cock (2), battery (3) and separate type DC socket (4) are positioned at fuselage, and described switch push button (5) is arranged on fuselage;
When separate type DC socket is not inserted DC power plug, the battery-powered machine operation of giving; When separate type DC socket inserts DC power plug, the power supply circuits of battery disconnect, by DC power supply to machine operation.
2. hair bulb clipping machine according to claim 1, it is characterized in that, described separate type DC socket (4) is by plastic casing (41), being arranged on the metal clips (42) that three conducting strips on plastic casing (41) and can deformation forms, plastic casing has a jack on (41), on fuselage, there is a through hole communicating with jack (6), the first conducting strip (43) is connected with discharge cock (2), the second conducting strip (44) is connected with the negative pole of battery (3), the 3rd conducting strip (45) is connected with the positive pole of battery (3), the positive pole of battery (3) is connected with one end of motor (1), the other end of motor (1) is connected with discharge cock (2), described metal clips is located between the first conducting strip (43) and the second conducting strip (44) throws off or contacts for controlling both, the upper perpendicular transverse conductance post (46) that connects of the 3rd conducting strip (45), transverse conductance post (46) is placed in jack, when jack is not inserted DC power plug, metal clips is connected the first conducting strip with the second conducting strip, and powered battery is to machine operation, when jack inserts DC power plug, the negative pole that is positioned at DC power plug sidepiece is thrown off metal clips generation deformation and the second conducting strip, only contact with the first conducting strip, the positive pole that is positioned at DC power plug head is enclosed within on transverse conductance post and is connected with the 3rd conducting strip, by DC power supply to machine operation.
3. hair bulb clipping machine according to claim 2, is characterized in that, described metal clips (42) is connected as a single entity with the first conducting strip (43).
4. hair bulb clipping machine according to claim 1 and 2, is characterized in that, forms the handle (7) of a handled easily on described fuselage.
5. hair bulb clipping machine according to claim 4, is characterized in that, described fuselage is formed by left fuselage (8) and right fuselage (9) docking, on described left fuselage (8) and right fuselage (9), respectively forms half handles.
6. hair bulb clipping machine according to claim 5, it is characterized in that, described head comprise be arranged on underbelly case ring (12), adopt the cutter reticulum (13) be threaded and be arranged on the cutter net (14) on cutter reticulum with case ring, described discharge cock (2) consists of two folding shape sheet metals (21,22), on the inwall of described left fuselage or right fuselage, form one for placing the mount pad (10) of discharge cock, mount pad (10) is provided with two locating slots; One end of two folding shape sheet metals is separately positioned in corresponding locating slot, and the other end is free end;
Be positioned at folding shape sheet metal free end and be provided with a location-plate (11), between described head and location-plate, be provided with one the Arming Assembly that cutter reticulum cannot be worked is not installed.
7. hair bulb clipping machine according to claim 6, is characterized in that, described Arming Assembly comprises bumper bar (15) and relief spring (16), has a breach (17) on the inwall of case ring (12);
When cutter reticulum is threaded with case ring, on bumper bar, move, relief spring is compressed, the lower end of bumper bar is arranged in breach and bottom is against on the upper end of case ring, the upper end of bumper bar is used in conjunction with the folding shape sheet metal (22) that is positioned at inner side, upwards the folding shape sheet metal (22) of inner side, top outwards moves, and can make two folding shape sheet metal contact conductions in the opereating specification of switch push button;
While not connecting cutter reticulum on case ring, relief spring makes the upper end of bumper bar and have an insurance distance between the folding shape sheet metal of inner side, cannot make two folding shape sheet metal contact conductions in the opereating specification of switch push button.
8. hair bulb clipping machine according to claim 7, it is characterized in that, the upper platform (18) that forms of described bumper bar (15), the lower end of relief spring (16) is against on platform (18), upper end is against on the inwall of a positioning sleeve (19), and described positioning sleeve (19) is enclosed within outside relief spring (16).
9. hair bulb clipping machine according to claim 5, it is characterized in that, described grip is provided with leader's cosmetic sheet (20), the front portion of described fuselage is provided with a front decoration sheet (23), by front decoration sheet (23), with the dog screw (24) in handle cosmetic sheet (20), left and right fuselage is fixedly connected with, on the inwall of fuselage, be formed for the centring ring (25) that dog screw is used in conjunction with, the centre of dog screw (24) has an opening that can make its diameter change.
10. hair bulb clipping machine according to claim 1 and 2, is characterized in that, the bottom of described fuselage is equipped with one for storing the large capacity disposable box of detachable (26) of ball top, and the large capacity disposable box of this detachable (26) communicates with head inner chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320547740.8U CN203451853U (en) | 2013-09-04 | 2013-09-04 | Lint shaver |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320547740.8U CN203451853U (en) | 2013-09-04 | 2013-09-04 | Lint shaver |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203451853U true CN203451853U (en) | 2014-02-26 |
Family
ID=50131746
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320547740.8U Expired - Fee Related CN203451853U (en) | 2013-09-04 | 2013-09-04 | Lint shaver |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203451853U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105821615A (en) * | 2016-04-15 | 2016-08-03 | 崔维群 | Hair ball trimming and collecting integrated equipment |
| CN108742473A (en) * | 2018-08-31 | 2018-11-06 | 佛山市顺德区德尔玛电器有限公司 | A kind of defeathering ball machine with extension handle function |
-
2013
- 2013-09-04 CN CN201320547740.8U patent/CN203451853U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105821615A (en) * | 2016-04-15 | 2016-08-03 | 崔维群 | Hair ball trimming and collecting integrated equipment |
| CN108742473A (en) * | 2018-08-31 | 2018-11-06 | 佛山市顺德区德尔玛电器有限公司 | A kind of defeathering ball machine with extension handle function |
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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: 20140226 |