CN203330989U - Staple-shooting-type stapler - Google Patents

Staple-shooting-type stapler Download PDF

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Publication number
CN203330989U
CN203330989U CN2013201357248U CN201320135724U CN203330989U CN 203330989 U CN203330989 U CN 203330989U CN 2013201357248 U CN2013201357248 U CN 2013201357248U CN 201320135724 U CN201320135724 U CN 201320135724U CN 203330989 U CN203330989 U CN 203330989U
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CN
China
Prior art keywords
fuselage
staple
energy
assembly
nail
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Expired - Lifetime
Application number
CN2013201357248U
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Chinese (zh)
Inventor
杨小荣
段忠民
代长海
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Guangzhou Eagle Technology Development Co ltd
Original Assignee
GUANGZHOU PANYU TONGYONG STATIONERY FACTORY CO Ltd
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Priority to CN2013201357248U priority Critical patent/CN203330989U/en
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Publication of CN203330989U publication Critical patent/CN203330989U/en
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Abstract

The embodiment of the utility model discloses a staple-shooting-type stapler. The energy of an energy-storing and energy-releasing assembly can be stored by utilizing the lever principle; then a staple pressing sheet is driven by the elastic force generated by the elastic potential energy released by the energy-storing and energy-releasing assembly so as to promote a staple to penetrate through paper; the feet of the staple are bent under the action of a bead position plate, so that the paper can be conveniently stapled in a labor-saving manner. The staple-shooting-type stapler comprises a top plate (01), a stapler body and a base, wherein the stapler body comprises the energy-storing and energy-releasing assembly, a staple containing assembly and a staple pusher assembly, wherein the energy-storing and energy-releasing assembly is positioned in the stapler body and connected with the top plate as well as used for storing and releasing the elastic potential energy; the staple containing assembly is used for containing the staple; the staple pusher assembly is used for pushing the staple; the base comprises a base plate (13) and the bead position plate (14); the bead position plate (14) is fixed on the base plate (13) and opposite to a staple outlet.

Description

A kind of nailing formula stapler
Technical field
The utility model relates to the stapler technical field, relates in particular to a kind of nailing formula stapler.
Background technology
Stapler is a kind of stationery of bound document paper, is widely used among office now.
Existing stapler generally is comprised of the parts such as at the bottom of machine side, nail pressing sheet, movement, nail pushing device, looper platform and machine.During use, by exerting pressure to machine side, then through machine side, pressure is passed to the nail pressing sheet, then by the nail pressing sheet, promote the book pin, make the book pin puncture paper, and make the stitch bending of book pin under the effect of pearl position plate, realize the function of stapler bookbinding paper.
Yet, because existing stapler is directly to make the book pin wear paper, clubfoot by manpower by the nail pressing sheet, therefore common stapler needs manually to impose severe pressure in forwarding, causes very large use inconvenience.
The utility model content
The utility model embodiment provides a kind of nailing formula stapler, can utilize lever principle to release and can carry out accumulation of energy by assembly accumulation of energy, then utilize accumulation of energy to release the elastic band dynamic pressure produced when the energy assembly discharges elastic potential energy and follow closely sheet, the nail pressing sheet promotes staple and makes staple wear paper, the nail pin of staple is crooked under the effect of pearl position plate, thereby can realize binding the function of paper convenient and strength-savingly.
The nailing formula stapler that the utility model embodiment provides comprises:
Top board 01, be flexibly connected by rotating shaft with fuselage, for to fuselage, providing pressure;
Fuselage, the two ends of described fuselage are respectively by rotating shaft and described top board 01 and base flexible connection;
Base, for supporting described fuselage, and the nail pin of crooked staple;
Described fuselage comprises that accumulation of energy is released can assembly, put screw assembly and nail pushing device assembly, described accumulation of energy is released and can be placed in fuselage and be connected with described top board by assembly, for savings and release elastic potential energy, the described screw assembly of putting is for placing staple, and described nail pushing device assembly is for promoting described staple;
Described base comprises: base plate 13 and pearl position plate 14, described pearl position plate 14 is fixed on described base plate 13 and exports relative with staple.
Alternatively,
Described accumulation of energy is released and can be comprised by assembly:
Nail pressing sheet 04, driving lever 05, reduction torsion spring 06, shell fragment 07;
Described nail pressing sheet 04 is placed in described fuselage and on the guide groove vertical with described fuselage, and described nail pressing sheet 04 top offers the aperture that the end with described driving lever 05 is used in conjunction with, and the middle part of described nail pressing sheet 04 offers the aperture be used in conjunction with described shell fragment 07;
Described driving lever 05 is movably connected on described fuselage interior by rotating shaft, on described driving lever 05, offers with described rotating shaft, to be used in conjunction with and area is greater than the aperture of the sectional area of described rotating shaft;
One end of described reduction torsion spring 06 is connected with an end of described driving lever 05 and described top board 01, and the other end of described reduction torsion spring 06 is connected with described fuselage;
One end of described shell fragment is connected with described nail pressing sheet, and the other end of described shell fragment 07 is fixed on described fuselage.
Alternatively,
The described screw assembly of putting comprises the left plate 02 of fuselage, fuselage right panel 03 and guide nail slot 08;
Offer the inclined-plane be used in conjunction with described driving lever 05 on the left plate 02 of described fuselage and described fuselage right panel 03;
Described guide nail slot 08 is fixed in described fuselage interior.
Alternatively,
Described nail pushing device assembly comprises pusher 09, spring 10, machine mandrel 11 and by system 12;
One end of described spring 10 connects described pusher 09, and the other end of described spring 10 connects described by system 12;
Described machine mandrel is fixedly connected with by system 12 with described;
Described pusher 09 is slidably connected with described machine mandrel 11.
Alternatively,
Described base also comprises elastic component 15;
Described elastic component 15 1 ends are connected with described base plate 13, and the other end is connected with described fuselage, for, guaranteeing to maintain a certain distance between fuselage and base during in off working state when nailing formula stapler.
Alternatively,
Aperture on described driving lever 05 is oval aperture.
Alternatively,
Take the plane at body bottom surface place is horizontal plane, and the inclination angle on described inclined-plane is 43 ° to 47 °.
Alternatively,
Described elastic component 15 is spring.
Alternatively,
Described elastic component 15 is shell fragment.
As can be seen from the above technical solutions, the utility model embodiment has the following advantages: compared to the prior art, the nailing formula stapler that the utility model provides, be provided with accumulation of energy in fuselage interior and release the energy device, in use, with hand top board 01, give top board 01 downward pressure, accumulation of energy release can assembly because the effect of top board 01 pressure starts elasticity of saving potential energy, when top board 01 moves downward certain position, the elastic potential energy that the savings of energy assembly are released in accumulation of energy reaches maximum, when top board 01 continues to move downward, the elastic potential energy that the energy assembly starts the release savings due to the effect of fuselage is released in accumulation of energy, and drive nail pressing sheet 04 moves downward, nail pressing sheet 04 promotes staple, make staple wear paper and crooked nail pin under the effect of pearl position plate 14, and then complete whole forwarding.Because hand utilizes lever principle to release and can carry out accumulation of energy by assembly accumulation of energy by top board 01, thereby do not need very large pressure just can complete easily binding work.
The accompanying drawing explanation
The decomposition chart that Fig. 1 is nailing formula stapler in the utility model embodiment;
Fig. 2 is the structure chart of nailing formula stapler when off working state in the utility model embodiment;
Fig. 3 is structure chart when in the utility model embodiment, nailing formula stapler is in running order;
The left plate of fuselage that Fig. 4 is nailing formula stapler in the utility model embodiment and the structure chart of fuselage right panel;
In above-mentioned figure:
Top board 01, the left plate 02 of fuselage, fuselage right panel 03, nail pressing sheet 04, driving lever 05, reduction torsion spring 06, shell fragment 07, guide nail slot 08, pusher 09, spring 10, machine mandrel 11, by system 12, base plate 13, pearl position plate 14 and elastic component 15.
The specific embodiment
The utility model embodiment discloses a kind of nailing formula stapler, can utilize easily lever principle to carry out accumulation of energy to shell fragment, the press belt dynamic pressure nail sheet produced while then utilizing shell fragment to discharge elastic potential energy, the nail pressing sheet promotes staple and makes staple wear paper, the nail pin of staple is crooked under the effect of pearl position plate, thereby can realize binding the function of paper convenient and strength-savingly.
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is known and detailed description, obviously, described embodiment is only a part of embodiment of the present utility model, rather than whole embodiment.Embodiment based in the utility model, those of ordinary skills are not making all other embodiment that obtain under the creative work prerequisite, all belong to the scope of the utility model protection.Refer to Fig. 1, in the utility model embodiment, nailing formula stapler embodiment comprises:
Top board 01, be flexibly connected by rotating shaft with fuselage, for to fuselage, providing pressure;
Fuselage, the two ends of fuselage are respectively by rotating shaft and top board 01 and base flexible connection;
Base, for supporting fuselage, and the nail pin of crooked staple;
Fuselage comprises that accumulation of energy is released can assembly, put screw assembly and nail pushing device assembly, and accumulation of energy is released and can be placed in fuselage and be connected with top board by assembly, for savings with discharge elastic potential energy, puts screw assembly for placing staple, and the nail pushing device assembly is used for promoting staple;
Base comprises: base plate 13 and pearl position plate 14, pearl position plate 14 is fixed on base plate 13 and exports relative with staple.
Alternatively,
Accumulation of energy is released and can be comprised by assembly:
Nail pressing sheet 04, driving lever 05, reduction torsion spring 06, shell fragment 07;
Nail pressing sheet 04 is placed in fuselage and on the guide groove vertical with fuselage, and nail pressing sheet 04 top offers the aperture that the end with driving lever 05 is used in conjunction with, and the middle part of nail pressing sheet 04 offers the aperture be used in conjunction with shell fragment 07;
Driving lever 05 is movably connected on fuselage interior by rotating shaft, on driving lever 05, offers with rotating shaft, to be used in conjunction with and area is greater than the aperture of the sectional area of rotating shaft;
One end of reduction torsion spring 06 is connected with an end of driving lever 05 and top board 01, and the other end of reduction torsion spring 06 is connected with fuselage;
One end of shell fragment is connected with the nail pressing sheet, and the other end of shell fragment 07 is fixed on fuselage.
Alternatively,
Put screw assembly and comprise the left plate 02 of fuselage, fuselage right panel 03 and guide nail slot 08;
Offer the inclined-plane be used in conjunction with driving lever 05 on the left plate 02 of fuselage and fuselage right panel 03;
Guide nail slot 08 is fixed in fuselage interior.
Alternatively,
The nail pushing device assembly comprises pusher 09, spring 10, machine mandrel 11 and by system 12;
One end of spring 10 connects pusher 09, and the other end of spring 10 connects by system 12;
Machine mandrel with by system, 12 be fixedly connected with;
Pusher 09 is slidably connected with machine mandrel 11.For ease of understanding, below the course of work of the nailing formula stapler of the utility model embodiment is described in detail:
The nailing formula stapler of the utility model embodiment, be provided with in fuselage interior the accumulation of energy formed by shell fragment 07, driving lever 05, nail pressing sheet 04 and reduction torsion spring and release the energy device, refer to Fig. 2, when nailing formula stapler during in off working state, shell fragment is according to the design needs, can be in natural straight configuration, also can be in case of bending, that is there is certain initial elasticity potential energy, shell fragment in the utility model embodiment possesses certain initial elasticity potential energy, and the nail pressing sheet is due to the lower end of effect in the fuselage guide groove of shell fragment.
Refer to Fig. 3, when nailing formula stapler is started working, with hand top board 01, give top board 01 downward pressure, top board 01 utilizes lever principle to give reduction torsion spring 06 downward pressure, make it to move downward and drive driving lever 05 rotation, the nail pressing sheet 04 that driving lever 05 drives an other end in the process of rotating moves upward along guide groove, when arriving beveled top end, the link of driving lever 05 and nail pressing sheet 04 completes the process of shell fragment 07 accumulation of energy, when top board 01 continues to move downward, with nail pressing sheet 04, the extruding due to beveled top end separates driving lever 05, now, shell fragment 07 discharges the elastic potential energy of accumulating, and drive nail pressing sheet 04 moves downward, nail pressing sheet 04 promotes staple, make staple wear paper and crooked nail pin under the effect of pearl position plate 14, and then complete whole forwarding.
Base also comprises elastic component 15;
Elastic component 15 1 ends are connected with base plate 13, and the other end is connected with fuselage, for, guaranteeing to maintain a certain distance between fuselage and base during in off working state when nailing formula stapler.
Alternatively,
Take the plane at body bottom surface place is horizontal plane, and the inclination angle on inclined-plane is 43 ° to 47 °, preferably can be 45 °.
Alternatively,
Aperture on driving lever 05 is oval aperture.
Alternatively, elastic component 15 is spring.
Alternatively, elastic component 15 is shell fragment.
Refer to Fig. 4, above-mentioned inclined-plane and the effect of oval aperture are: when the elastic potential energy of shell fragment reaches maximum, driving lever 05 is separated with nail pressing sheet 04, thereby shell fragment 07 can discharge elastic potential energy smoothly, and then complete whole forwarding, aperture on above-mentioned driving lever 05 is not limited to the oval aperture in the utility model embodiment, but can be the aperture of other shape, but need to meet the requirement that driving lever 05 can move forward and backward along rotating shaft, above-mentioned moving forward and backward be take nail pressing sheet position as front, after by position processed being.
The effect of above-mentioned elastic component is: guarantee that nailing formula stapler is when off working state, between fuselage and base, maintain a certain distance, above-mentioned elastic component is not limited to the spring in the utility model legend, also is not limited to shell fragment, can be that other possesses ejusdem generis material.
As can be seen from the above technical solutions, the utility model embodiment has the following advantages: compared to the prior art, the nailing formula stapler that the utility model provides, in fuselage interior, be provided with by shell fragment 07, driving lever 05, the energy device is released in the accumulation of energy that nail pressing sheet 04 and reduction torsion spring form, in use, with hand top board 01, give top board 01 downward pressure, top board 01 utilizes lever principle to give reduction torsion spring 06 downward pressure, make it to move downward and drive driving lever 05 rotation, the nail pressing sheet 04 that driving lever 05 drives an other end in the process of rotating moves upward along guide groove, when arriving beveled top end, the link of driving lever 05 and nail pressing sheet 04 completes the process of shell fragment 07 accumulation of energy, when top board 01 continues to move downward, with nail pressing sheet 04, the extruding due to beveled top end separates driving lever 05, now, shell fragment 07 discharges the elastic potential energy of accumulating, and drive nail pressing sheet 04 moves downward, nail pressing sheet 04 promotes staple, make staple wear paper and crooked nail pin under the effect of pearl position plate 14, and then complete whole forwarding.Because hand utilizes lever principle to carry out accumulation of energy to shell fragment 07 by top board 01, thereby do not need very large pressure just can complete easily binding work.
Above nailing formula stapler provided by the utility model is described in detail, for one of ordinary skill in the art, thought according to the utility model embodiment, all will change in specific embodiments and applications, in sum, this description should not be construed as restriction of the present utility model.

Claims (9)

1. a nailing formula stapler, is characterized in that, comprising:
Top board (01), be flexibly connected by rotating shaft with fuselage, for to fuselage, providing pressure;
Fuselage, the two ends of described fuselage are respectively by rotating shaft and described top board (01) and base flexible connection;
Base, for supporting described fuselage, and the nail pin of crooked staple;
Described fuselage comprises that accumulation of energy is released can assembly, put screw assembly and nail pushing device assembly, described accumulation of energy is released and can be placed in fuselage and be connected with described top board by assembly, for savings and release elastic potential energy, the described screw assembly of putting is for placing staple, and described nail pushing device assembly is for promoting described staple;
Described base comprises: base plate (13) and pearl position plate (14), it is upper and relative with the staple outlet that described pearl position plate (14) is fixed on described base plate (13).
2. nailing formula stapler according to claim 1, is characterized in that, described accumulation of energy is released and can be comprised by assembly:
Nail pressing sheet (04), driving lever (05), reduction torsion spring (06), shell fragment (07);
Described nail pressing sheet (04) is placed on the guide groove that described fuselage is interior and vertical with described fuselage, described nail pressing sheet (04) top offers the aperture that the end with described driving lever (05) is used in conjunction with, and the middle part of described nail pressing sheet (04) offers the aperture be used in conjunction with described shell fragment (07);
Described driving lever (05) is movably connected on described fuselage interior by rotating shaft, on described driving lever (05), offers with described rotating shaft, to be used in conjunction with and area is greater than the aperture of the sectional area of described rotating shaft;
One end of described reduction torsion spring (06) is connected with an end and the described top board (01) of described driving lever (05), and the other end of described reduction torsion spring (06) is connected with described fuselage;
One end of described shell fragment is connected with described nail pressing sheet, and the other end of described shell fragment (07) is fixed on described fuselage.
3. nailing formula stapler according to claim 1, is characterized in that, the described screw assembly of putting comprises the left plate of fuselage (02), fuselage right panel (03) and guide nail slot (08);
Offer the inclined-plane be used in conjunction with described driving lever (05) on the left plate of described fuselage (02) and described fuselage right panel (03);
Described guide nail slot (08) is fixed in described fuselage interior.
4. nailing formula stapler according to claim 1, is characterized in that, described nail pushing device assembly comprises pusher (09), spring (10), machine mandrel (11) and presses system (12);
One end of described spring (10) connects described pusher (09), and the other end of described spring (10) connects described by system (12);
Described machine mandrel is fixedly connected with by system (12) with described;
Described pusher (09) is slidably connected with described machine mandrel (11).
5. according to the described nailing formula of any one in claim 1 to 4 stapler, it is characterized in that, described base also comprises elastic component (15);
Described elastic component (15) one ends are connected with described base plate (13), and the other end is connected with described fuselage, for, guaranteeing to maintain a certain distance between fuselage and base during in off working state when nailing formula stapler.
6. nailing formula stapler according to claim 2, is characterized in that,
Aperture on described driving lever (05) is oval aperture.
7. nailing formula stapler according to claim 3, is characterized in that,
Take the plane at body bottom surface place is horizontal plane, and the inclination angle on described inclined-plane is 43 ° to 47 °.
8. nailing formula stapler according to claim 5, is characterized in that, described elastic component (15) is spring.
9. nailing formula stapler according to claim 5, is characterized in that, described elastic component (15) is shell fragment.
CN2013201357248U 2013-03-22 2013-03-22 Staple-shooting-type stapler Expired - Lifetime CN203330989U (en)

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CN2013201357248U CN203330989U (en) 2013-03-22 2013-03-22 Staple-shooting-type stapler

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Application Number Priority Date Filing Date Title
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103128709A (en) * 2013-03-22 2013-06-05 广州番禺通用文具制品厂有限公司 Nail shooting type stapler
US9446508B2 (en) 2013-12-06 2016-09-20 ACCO Brands Corporation Stored energy stapler
US9687976B2 (en) 2013-12-06 2017-06-27 ACCO Brands Corporation Stored energy stapler
CN107717874A (en) * 2017-11-02 2018-02-23 佛山市金钜伦五金文具有限公司 A kind of multifunctional force saving stapler
US11267117B2 (en) 2018-09-14 2022-03-08 ACCO Brands Corporation Staple pusher assembly and method of installing same

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103128709A (en) * 2013-03-22 2013-06-05 广州番禺通用文具制品厂有限公司 Nail shooting type stapler
US9446508B2 (en) 2013-12-06 2016-09-20 ACCO Brands Corporation Stored energy stapler
US9687976B2 (en) 2013-12-06 2017-06-27 ACCO Brands Corporation Stored energy stapler
CN107717874A (en) * 2017-11-02 2018-02-23 佛山市金钜伦五金文具有限公司 A kind of multifunctional force saving stapler
CN107717874B (en) * 2017-11-02 2024-04-02 佛山市金钜伦五金文具有限公司 Multifunctional labor-saving stapler
US11267117B2 (en) 2018-09-14 2022-03-08 ACCO Brands Corporation Staple pusher assembly and method of installing same

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C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20180207

Address after: 510000 the first floor, three to six floors, one to five floors of building B1, B3 building C5, one floor of A1, DLONG Road, DLONG Road, Dlong street, Panyu District, Guangzhou.

Patentee after: GUANGZHOU EAGLE TECHNOLOGY DEVELOPMENT CO.,LTD.

Address before: 511442 General Industrial City No. 238, NANDA Road, South Village, Panyu District, Guangzhou, Guangdong

Patentee before: GUANGZHOU PANYU TUNG YUNG STATIONERY MFY., Ltd.

CX01 Expiry of patent term
CX01 Expiry of patent term

Granted publication date: 20131211