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CN104163329B - A kind of cyclic conveying device - Google Patents

A kind of cyclic conveying device Download PDF

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Publication number
CN104163329B
CN104163329B CN201410320372.2A CN201410320372A CN104163329B CN 104163329 B CN104163329 B CN 104163329B CN 201410320372 A CN201410320372 A CN 201410320372A CN 104163329 B CN104163329 B CN 104163329B
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China
Prior art keywords
fuselage
cross bar
connecting rod
conveying device
column
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CN201410320372.2A
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Chinese (zh)
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CN104163329A (en
Inventor
刘航东
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Suzhou qiongpairuite Technology Co.,Ltd.
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Suzhou Transparent Electronic Technology Co Ltd
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Priority to CN201410320372.2A priority Critical patent/CN104163329B/en
Publication of CN104163329A publication Critical patent/CN104163329A/en
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Abstract

One cyclic conveying device of the present invention, cyclic conveying device includes being arranged on fuselage: workbench group, Power Component and body feed tank;Workbench group includes multiple transmission platform;The two ends of workbench group are additionally provided with independent lifting saddle;Power Component is responsible for pushing on each transmission platform the article on lifting saddle;Fuselage includes some frame components;Frame component is linked in sequence and forms fuselage main body;Frame component includes unit support and connecting rod, is connected by connecting rod between relative unit support;Unit support includes the cross bar between column, column and fuselage plaque;The upper end of column connects radian board member;Cross bar is positioned at the lower section of described radian board member;Cross bar is equipped with board slot in the opposite of radian board member;Fuselage plaque is installed in board slot.By invention, it is provided that a kind of cyclic conveying device, its fuselage is the most quick detachable, and prepares aspect at fuselage, and the consumption of its aluminium section bar lowers significantly, has saved entreprise cost greatly.

Description

A kind of cyclic conveying device
Technical field
The present invention relates to production run equipment technical field, particularly relate to a kind of cyclic conveying device.
Background technology
In production in light industry field, various large-size pipelines produce and have trended towards scale and automatization.For the production process of clothing, comprising: blanking, cut out, sew, flatiron etc..In order to quantify to produce, often set operation is all that special messenger has been responsible for.Material is thus formed the process of a Transmission, after last process completes, semi-finished product will be transported to and at next procedure, go processing;If transmitted by manpower, nature can affect production efficiency.Therefore a kind of circulation conveying arrangement of new line, such as Chinese invention patent " a kind of circulation conveying arrangement ", its Application No. 201120179504.6, disclose a kind of cyclic conveying device, use the mode that dividing plate is set on conveyer belt, realize the Separate transport of unit material, mechanical construction and control system is the simplest, cost is relatively low, safe and reliable, and achieves streamline automated job.But, the structure of its fuselage ring be connected underaction, the fastening of connected mode many employings screw between plaque and the frame member on its fuselage, which complexity is loaded down with trivial details, and from the point of view of cost-effective, its cost prepared is relatively big, is unfavorable for expanding production.
Summary of the invention
The technical problem that present invention mainly solves is to provide a kind of cyclic conveying device, and it is reasonable in design, simple in construction, also improves the structure problem of fuselage while solving to lack protection structure.
For solving above-mentioned technical problem, the technical scheme that the present invention uses is to provide a kind of cyclic conveying device, and described cyclic conveying device includes being arranged on fuselage: workbench group, Power Component and body feed tank;Described workbench group includes multiple transmission platform;The two ends of described workbench group are additionally provided with independent lifting saddle;Described Power Component is responsible for pushing on each transmission platform the article on lifting saddle;Described fuselage includes some frame components;Described frame component is linked in sequence and forms fuselage main body;Described frame component includes unit support and connecting rod, is connected by connecting rod between relative unit support;Described unit support includes the cross bar between column, column and fuselage plaque;The upper end of described column connects radian board member;Described cross bar is positioned at the lower section of described radian board member;Described cross bar is equipped with board slot in the opposite of described radian board member;Described fuselage plaque is installed in described board slot.
Preferably, described radian board member is one-body molded by mould;Described radian board member includes X-type attachment structure, H type board face structure and radian plate;Two support ends on described its top of X-type attachment structure the most vertically extend and form H type board face structure;The upper end of described board face structure is then by radian disc seal;Described board slot is set at least one connection end in two connection ends of described X-type attachment structure bottom.
Preferably, described cross bar is the hollow aluminum section of cross section I-shaped;Described cross bar includes: upper pressure-bearing unit, support unit and lower pressure-bearing unit;Dividing plate it is provided with in support unit;Described dividing plate will be divided into upper and lower two die cavities inside cross bar;The both sides of described support unit are all set to seal groove;The sidewall of described lower pressure-bearing unit is provided with described board slot.
Preferably, the cross section of described connecting rod is rectangular frame structure;Described connecting rod includes: is in the center brace panel of diagonal positions, and lays respectively at the support side plate of center brace panel both sides;All it is connected by arc between described support side plate with described center brace panel;The cavity of pressure-bearing is formed between described support side plate and described center brace panel;The end of described center brace panel, end and the arc of support side plate surround seal groove.
Preferably, the opening part of described seal groove is provided with prominent hook formation.
The invention has the beneficial effects as follows: providing a kind of cyclic conveying device, its main body mechanism of circulation conveying arrangement using this support mechanism is light, the most quick detachable, and prepares aspect at fuselage, and the consumption of its aluminium section bar lowers significantly, has saved entreprise cost greatly.
Accompanying drawing explanation
Fig. 1 It it is the structural representation of a kind of cyclic conveying device of the present invention;
Fig. 2 is the structural representation of frame component;
Fig. 3 is the structural representation of unit pedestal;
Fig. 4 is the structural representation of radian board member;
Fig. 5 is the structural representation of cross bar;
Fig. 6 is the structural representation of connecting rod;
In accompanying drawing, the labelling of each parts is as follows: 1, fuselage;2, workbench group;3, Power Component;4, body feed tank;5, lifting saddle;6, unit support;7, cross bar;8, column;9, connecting rod;10, radian board member;11, X-type attachment structure;12, H type board face structure;13, radian plate;14, board slot;15, fuselage plaque;16, dividing plate;17, seal groove;18, center brace panel;19, the first support side plate;20, the second support side plate;21, arc;22, hook formation.
Detailed description of the invention
Below in conjunction with the accompanying drawings presently preferred embodiments of the present invention is described in detail, so that advantages and features of the invention can be easier to be readily appreciated by one skilled in the art, thus protection scope of the present invention is made apparent clear and definite defining.
Referring to accompanying drawing 1 to 6, the embodiment of the present invention includes:
A kind of cyclic conveying device, such as Fig. 1, it includes arranging on the fuselage 1: workbench group 2, Power Component 3 and body feed tank 4;Workbench group 2 is divided into upper and lower transmission platform, workbench group all to select cylinder transmission means, is additionally provided with independent lifting saddle 5 at the two ends of workbench group 2;Described Power Component 3 is responsible for pushing on each transmission platform the article on lifting saddle 5.
Such as Fig. 1 and 2, fuselage 1 includes some frame components;Frame component is linked in sequence and forms fuselage 1 main body;Frame component also includes: unit support 6 and connecting rod 9, is connected by connecting rod 9 between relative unit support 6;Described unit support 6 then includes: the cross bar 7 between column 8 and column;Such as Fig. 3 and 4, support a radian board member 10 in the upper end of two columns, this radian board member is extruded one-body molded by mould, and it is based on an X-type attachment structure 11;The most vertically extended by two support ends on its top of X-type attachment structure and form H type board face structure 12, wherein side plate face is slightly lower, the upper end of H type board face structure 12 is then sealed by radian plate 13, so formation one is to the cambered surface declined, and can not only increase aesthetics and can improve service behaviour;At least one in two connection ends of X-type attachment structure 11 its underpart connects the board slot 14 being provided with plaque on end, and in the present embodiment, the connection end in left side is provided with board slot 14, and right side connects the cavity that end is then rectangle.It is equipped with seal groove on three scope of freedoms in X-type attachment structure 11.Cross bar 7 on support is positioned at the lower section of X-type attachment structure 11, and between cross bar and X-type attachment structure and equipped with fuselage plaque 15, the top edge of this fuselage plaque is flush-mounted in the board slot 14 of X-type attachment structure 11, the most just so that handling become simpler.This structure can conveniently install various fuselage plaque, it is not necessary to is fixing fuselage plaque by modes such as punching, screws;The connected mode making fuselage plaque is more flexible, also saves substantial amounts of manpower and materials simultaneously.
Such as Fig. 5, cross bar 7 is the hollow aluminum section of cross section I-shaped, includes the most successively: upper pressure-bearing unit, support unit and lower pressure-bearing unit;Being provided with dividing plate 16 in support unit, this dividing plate 16 is divided into upper and lower two die cavities by internal for cross bar 7;The both sides of support unit are all set to seal groove;The board slot 14 for fitting machine body structure it is additionally provided with on the sidewall of described lower pressure-bearing unit.The cross bar of this kind of structure is difficult to dust stratification, easily clears up;More it is advantageous that, the cross bar of this interfacial structure can save substantial amounts of material of preparing, and saves great amount of cost.
Such as figure 6, the connecting rod 9 connected between unit support, its cross section is rectangular frame structure, comprising: be in the center brace panel 18 of diagonal positions, and laying respectively at the support side plate of center brace panel 18 both sides, they are the first support side plate 19 and the second support side plate 20.All it is connected by arc 21 between support side plate with center brace panel so that between support side plate and center brace panel, form the cavity of pressure-bearing;The end of described center brace panel, end and the arc of support side plate surround seal groove.The opening part of described seal groove is provided with prominent hook formation 22.This kind of its closed area of connecting rod quantitatively decreases, and region expands as far as possible, thus can be difficult to dust stratification with easy cleaning.Furthermore compare area of section, reduced.Show according to experimental data, the consumption aspect preparing material of this connecting rod: improvement pre-structure, in its every meter, the usage amount of aluminium section bar saves More than 300 gram, at cost-effective aspect, the structure in the present invention has the biggest advantage, can save the cost of enterprise greatly.
Analyzing in terms of the material consumption of support, the support of this kind of structure is light, can be connected by connecting rod, and this support saves closely than existing support between adjacent support The consumption of 3.8%, the most this design can bring considerable cost savings to garment making equipment enterprise.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every equivalent structure utilizing description of the invention content to be made or equivalence flow process conversion; or directly or indirectly it is used in other relevant technical fields, the most in like manner it is included in the scope of patent protection of the present invention.

Claims (1)

1. a cyclic conveying device, it is characterised in that: described cyclic conveying device includes being arranged on fuselage: workbench group, Power Component and body feed tank;Described workbench group includes multiple transmission platform;The two ends of described workbench group are additionally provided with independent lifting saddle;Described Power Component is responsible for pushing on each transmission platform the article on lifting saddle;Described fuselage includes some frame components;Described frame component is linked in sequence and forms fuselage main body;Described frame component includes unit support and connecting rod, is connected by connecting rod between relative unit support;Described unit support includes the cross bar between column, column and fuselage plaque;The upper end of described column connects radian board member;Described cross bar is positioned at the lower section of described radian board member;Described cross bar is equipped with board slot in the opposite of described radian board member;Described fuselage plaque is installed in described board slot;The cross section of described connecting rod is rectangular frame structure;Described connecting rod includes: is in the center brace panel of diagonal positions, and lays respectively at the support side plate of center brace panel both sides;All it is connected by arc between described support side plate with described center brace panel;The cavity of pressure-bearing is formed between described support side plate and described center brace panel;The end of described center brace panel, end and the arc of support side plate surround seal groove.
CN201410320372.2A 2014-07-04 2014-07-04 A kind of cyclic conveying device Active CN104163329B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410320372.2A CN104163329B (en) 2014-07-04 2014-07-04 A kind of cyclic conveying device

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Application Number Priority Date Filing Date Title
CN201410320372.2A CN104163329B (en) 2014-07-04 2014-07-04 A kind of cyclic conveying device

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CN104163329A CN104163329A (en) 2014-11-26
CN104163329B true CN104163329B (en) 2016-08-17

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102320456A (en) * 2011-06-10 2012-01-18 无锡杰思物流设备有限公司 Sectional material structure for belt conveying machine framework
CN202445197U (en) * 2012-03-06 2012-09-26 苏州琼派瑞特电子科技有限公司 Baffle
CN102785904A (en) * 2012-07-14 2012-11-21 苏州琼派瑞特电子科技有限公司 Cyclic transmission device
CN202953510U (en) * 2012-11-29 2013-05-29 金仙惠 Rack of candy conveyor

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB531912A (en) * 1939-07-12 1941-01-14 Angus Wellesley Duncan Improvements relating to conveyors
DE3012275A1 (en) * 1980-03-29 1981-10-15 Robert Bosch Gmbh, 7000 Stuttgart CARRIER PROFILE FOR CONVEYOR BELTS
FR2621022B2 (en) * 1986-04-08 1992-07-31 Mach Speciales Manutention SELF-SUPPORTING MODULAR SIDE
US5082108A (en) * 1989-07-20 1992-01-21 Simplimatic Engineering Company Modular conveyor beam and method of assembly therefor
CN202115961U (en) * 2011-05-31 2012-01-18 苏州琼派瑞特电子科技有限公司 Cyclic transmission device
CN204057084U (en) * 2014-07-04 2014-12-31 苏州琼派瑞特电子科技有限公司 A kind of cyclic conveying device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102320456A (en) * 2011-06-10 2012-01-18 无锡杰思物流设备有限公司 Sectional material structure for belt conveying machine framework
CN202445197U (en) * 2012-03-06 2012-09-26 苏州琼派瑞特电子科技有限公司 Baffle
CN102785904A (en) * 2012-07-14 2012-11-21 苏州琼派瑞特电子科技有限公司 Cyclic transmission device
CN202953510U (en) * 2012-11-29 2013-05-29 金仙惠 Rack of candy conveyor

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Address after: 215000 No. 555, Jiangxing East Road, Wujiang Economic and Technological Development Zone, Suzhou City, Jiangsu Province

Patentee after: Suzhou qiongpairuite Technology Co.,Ltd.

Address before: 215104 Suzhou qiongpairuite Electronic Technology Co., Ltd., floor 1, building 1, No. 165, Dongwu South Road, Wuzhong Economic Development Zone, Suzhou, Jiangsu

Patentee before: SUZHOU TRANSPARENT ELECTRONIC TECHNOLOGY Co.,Ltd.