CN109174495A - A kind of building scaffold outer surface of steel tube later period prosthetic device - Google Patents

A kind of building scaffold outer surface of steel tube later period prosthetic device Download PDF

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Publication number
CN109174495A
CN109174495A CN201811292568.XA CN201811292568A CN109174495A CN 109174495 A CN109174495 A CN 109174495A CN 201811292568 A CN201811292568 A CN 201811292568A CN 109174495 A CN109174495 A CN 109174495A
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CN
China
Prior art keywords
fixed
fuselage
paint
prosthetic
steel tube
Prior art date
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.)
Pending
Application number
CN201811292568.XA
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Chinese (zh)
Inventor
方标
许萌
柯军梁
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shangyu Research Institute of ZJUT
Original Assignee
Shangyu Research Institute of ZJUT
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shangyu Research Institute of ZJUT filed Critical Shangyu Research Institute of ZJUT
Priority to CN201811292568.XA priority Critical patent/CN109174495A/en
Publication of CN109174495A publication Critical patent/CN109174495A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B9/00Spraying apparatus for discharge of liquids or other fluent material, without essentially mixing with gas or vapour
    • B05B9/03Spraying apparatus for discharge of liquids or other fluent material, without essentially mixing with gas or vapour characterised by means for supplying liquid or other fluent material
    • B05B9/04Spraying apparatus for discharge of liquids or other fluent material, without essentially mixing with gas or vapour characterised by means for supplying liquid or other fluent material with pressurised or compressible container; with pump
    • B05B9/0403Spraying apparatus for discharge of liquids or other fluent material, without essentially mixing with gas or vapour characterised by means for supplying liquid or other fluent material with pressurised or compressible container; with pump with pumps for liquids or other fluent material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B13/00Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
    • B05B13/02Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work
    • B05B13/0221Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work characterised by the means for moving or conveying the objects or other work, e.g. conveyor belts
    • B05B13/0228Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work characterised by the means for moving or conveying the objects or other work, e.g. conveyor belts the movement of the objects being rotative
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B13/00Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
    • B05B13/02Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work
    • B05B13/0278Arrangement or mounting of spray heads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B13/00Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
    • B05B13/02Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work
    • B05B13/0285Stands for supporting individual articles to be sprayed, e.g. doors, vehicle body parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B14/00Arrangements for collecting, re-using or eliminating excess spraying material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05DPROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D3/00Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
    • B05D3/04Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases
    • B05D3/0406Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases the gas being air
    • B05D3/0413Heating with air

Abstract

The present invention relates to technical field of buildings, and disclose a kind of building scaffold outer surface of steel tube later period prosthetic device, mechanism, mobile Pai Qi mechanism, clout collecting mechanism and heat blocking mechanism are brushed including rack, fuselage, position restriction mechanism, rotation driving mechanism, barrier plate, heating, the fuselage is fixed on the top of rack, and the middle part on the left of fuselage is arranged in the position restriction mechanism.The rotation for making its circumference is fixed in scaffolding steel pipe by the present invention, five spray heads moved left and right carry out uniform spray painting operation to steel pipe, the paint sprayed downwards and the paint dripped from steel pipe can fall in the top of collecting board, it prevents paint from flying upward everywhere and causes environmental pollution, paint can be to gathering in the middle part of collecting board, it is fallen into from funnel to the inside of collecting box, facilitate the Collection utilization of paint, the heat that heater strip energization generates brushes downwards, the skin of paint of outer surface of steel tube is heated, the dry efficiency of skin of paint is improved.

Description

A kind of building scaffold outer surface of steel tube later period prosthetic device
Technical field
It is repaired and is filled with the outer surface of steel tube later period the present invention relates to technical field of buildings more particularly to a kind of building scaffold It sets.
Background technique
In construction, in order to which construction personnel works or perimeter security net is gone along with sb. to guard him and high-altitude installation component up and down, need Scaffold is set up on construction site, scaffold making material is usually steel pipe, for the recycling of resource, a construction site Steel pipe after use, which needs to transport to next building site, to be continued to use, however is destroyed using the outer surface rust-proof coating of rear steel pipe , reuse and be easy to cause security risk, in order to which next construction site can continue to use, in the rust for removing outer surface of steel tube After spot, need again spray anti-rust oil paint carry out surface reconditioning, now on-site, scaffolding steel pipe is generally used paint pump into Row spray painting, steel pipe is placed in support device, and worker, which holds paint pump and overturns one by one to steel pipe, to paint, efficiency of painting It is low, while painting to be easy to spread everywhere in painting process and causing environmental pollution.
Summary of the invention
Goal of the invention of the invention is to provide a kind of building scaffold outer surface of steel tube later period prosthetic device, the building Steel pipe for scaffold outer surface later period prosthetic device is easy to use, and spray painting uniformly, is painted high-efficient, while being reduced paint and flown upward and making At environmental pollution.
To achieve the goals above, the present invention is to realize by the following technical solutions: a kind of building scaffold steel Tube outer surface later period prosthetic device, including rack, fuselage, position restriction mechanism, rotation driving mechanism, barrier plate, heating are brushed Mechanism, mobile Pai Qi mechanism, clout collecting mechanism and heat blocking mechanism, the fuselage are fixed on the top of rack, institute's rheme It sets and limits the middle part that mechanism is arranged on the left of fuselage, the left side of fuselage inner bottom wall, the resistance is arranged in the rotation driving mechanism Baffle is fixed on the right side of fuselage interior, and perforative through-hole is offered in the middle part of the barrier plate side, and machine is brushed in the heating The right side of fuselage inner roof wall is arranged in structure, and the left side of fuselage inner roof wall is arranged in the mobile Pai Qi mechanism, and the clout is collected The middle part of fuselage inner bottom wall is arranged in mechanism, and the middle part on the right side of fuselage is arranged in the heat blocking mechanism.
Further, the position restriction mechanism includes bearing, rotation pipe, four struts and clamping mechanism, the axis The middle part being embedded on the left of fuselage is held, the rotation pipe is fixedly plugged in the inside of bearing, and four struts are equidistantly fixed on The left side of rotation pipe, the clamping mechanism are fixedly connected with four struts.
Further, the clamping mechanism includes annulus, four connecting rods and scroll chuck, four connecting rod circles Ring is equidistantly welded on the inner wall of annulus, and four struts are fixed on the middle part of four connecting rods, and the scroll chuck is fixed on Between four struts.
Further, the rotation driving mechanism includes decelerating motor, driving wheel, driven wheel and transmission belt, described to subtract Speed motor is fixed on the left side of fuselage inner bottom wall, and the driving wheel is fixedly attached on the output end of decelerating motor, described driven Wheel is fixedly attached to the outer surface of rotation pipe, and driven wheel is connect by transmission belt with capstan drive.
Further, it includes positive and negative motor, flabellum, heater strip and first bevel gear that mechanism is brushed in the heating, described Positive and negative motor is fixed on the right side of fuselage inner roof wall, and the output shaft of the positive and negative motor is fixedly connected with rotation by shaft coupling Axis, the flabellum are fixedly attached to the outer surface of rotation axis bottom, and the first bevel gear is fixedly attached to rotation axis outer surface Middle part, between the heater strip is fixed on the right side of barrier plate and fuselage inner wall, the underface of heater strip is arranged in the flabellum.
Further, the mobile Pai Qi mechanism includes threaded rod, second bevel gear, thread bush, sliding block, sliding rail, oil Paint case, fluid hose, paint pump, fixed ring, connecting tube and five spray heads, the threaded rod are movably connected in the left side of fuselage inner wall The right end at the top between barrier plate, the threaded rod runs through and extends the right side of barrier plate, and the second bevel gear is fixed It is socketed in the right end of threaded rod, second bevel gear is engaged with first bevel gear, and the thread bush screw thread is socketed in threaded rod appearance The left side in face, the sliding block are fixed on the top of thread bush, and the sliding rail is fixed on the inner roof wall of fuselage, and the sliding block sliding connects It connects in the inside of sliding rail, the painting case is fixed on the top of fuselage, and the paint pump is fixed on the bottom of thread bush, the oil Paint pump is connected to between painting case by fluid hose, and the fixed ring is fixed on the bottom of paint pump, and the fixed ring is two points One of annular shape, and the inside of fixed ring offers circular cavity, and the paint pump is connected to by connecting tube with cavity, five A spray head is equidistantly fixed on the inner wall of fixed ring, and spray head is connected to cavity.
Further, the clout collecting mechanism includes that there are four upright bar, collecting board, funnel and collecting boxs, described in four Upright bar is fixed on the inner bottom wall of fuselage, and the collecting board is fixed on the top of four upright bars, and the shape of the collecting board is circular arc Shape, and the height in the middle part of collecting board is lower than the height of collecting board surrounding, the fixed connection of the funnel are described at the middle part of collecting board Collecting box is fixed on collecting box, and collecting box is located at the underface of funnel.
Further, the heat blocking mechanism includes circle set, four the first gaskets and four the second gaskets, institute It states circle set and is embedded in middle part on the right side of fuselage, four first gaskets are equidistantly fixed on the inner wall of circle set, and four described the Two gaskets are equidistantly fixed on the inner wall of circle set, and the first gasket is staggered with the second gasket.
Compared with prior art:
1, building scaffold outer surface of steel tube later period prosthetic device, by the setting of position restriction mechanism, by steel pipe from three It is penetrated in the middle part of dog chuck to the inside of fuselage, rotating ring counterclockwise drives the external disk of scroll chuck to turn by connecting rod It is dynamic, the outer surface of steel pipe is squeezed so that three latches move inward, and then steel pipe is fixed, guarantees carrying out The stability of steel pipe when spray painting.
2, building scaffold outer surface of steel tube later period prosthetic device, by the setting of rotation driving mechanism, slow down electricity Machine work operation drives driving wheel rotation, and driving wheel drives driven wheel to rotate by transmission belt, and driven wheel is fixedly attached to rotation The outer surface of pipe drives rotation pipe in the inner rotation of bearing, and then drives the rotation for the steel pipe circumference fixed by scroll chuck, It ensure that the continuity and uniformity of spray painting.
3, building scaffold outer surface of steel tube later period prosthetic device passes through the setting of mobile Pai Qi mechanism, positive and negative electricity Machine work operation drives rotation axis rotation, drives the first bevel gear rotation being socketed in the middle part of rotation axis, first bevel gear and the The engagement of two bevel gears, so that threaded rod rotates, the restriction by sliding block and sliding rail to thread bush, so that thread bush is in threaded rod The rotation of outer surface or so, paint pump are extracted the paint inside painting case by fluid hose, enter to cavity by connecting tube Inside, then sprayed from five spray heads, ensure that steel pipe spray painting uniformity, while ensure that spray painting after steel pipe surface The thickness of face skin of paint, preventing the outer surface skin of paint of steel pipe to be destroyed causes steel pipe to corrode, and improves safety.
4, building scaffold outer surface of steel tube later period prosthetic device brushes the setting of mechanism, positive and negative electricity by heating Machine work operation drives rotation axis rotation, drives the flabellum of rotation axis outer surface bottom quickly to rotate, heater strip is powered and is produced Raw heat brushes downwards, heats to the skin of paint of outer surface of steel tube, improves the dry efficiency of skin of paint.
5, building scaffold outer surface of steel tube later period prosthetic device, passes through the setting of clout collecting mechanism, collecting board Positioned at the lower section of steel pipe, when painting to steel pipe, the paint sprayed downwards and the paint dripped from steel pipe can fall in collecting board Top prevents paint from flying upward cause environmental pollution everywhere, and dropping down onto the paint at the top of collecting board can be to gathering in the middle part of collecting board, so The Collection utilization for facilitating paint to the inside of collecting box is fallen into from funnel afterwards, reduces the waste of paint.
6, building scaffold outer surface of steel tube later period prosthetic device, by the setting of heat blocking mechanism, in steel pipe When passing through from circle set, the first gasket and the second gasket can play the effect of sealing, reduce heat and reveal from circle set, The temperature that ensure that chamber between on the right side of barrier plate and on the left of fuselage inner wall, further improves dry to outer surface of steel tube skin of paint Dry efficiency.
Detailed description of the invention
Fig. 1 is schematic structural view of the invention;
Fig. 2 is clamping mechanism structural side view of the present invention;
Fig. 3 is paint pump of the present invention and fixed ring structural side view;
Fig. 4 is heat blocking mechanism structural side view of the present invention;
Fig. 5 is collecting board structural side view of the present invention.
In figure: 1 rack, 2 fuselages, 3 position restriction mechanisms, 301 bearings, 302 rotation pipes, 303 struts, 304 clamping mechanisms, It is 3041 annulus, 3042 connecting rods, 3043 scroll chucks, 4 rotation driving mechanisms, 401 decelerating motors, 402 driving wheels, 403 driven Wheel, 404 transmission belts, 5 barrier plates, 6 through-holes, 7 heating brush mechanism, 701 positive and negative motors, 702 rotation axis, 703 flabellums, 704 plus Heated filament, 705 first bevel gears, 8 mobile Pai Qi mechanisms, 801 threaded rods, 802 second bevel gears, 803 thread bush, 804 sliding blocks, 805 sliding rails, 806 painting cases, 807 fluid hoses, 808 paint pumps, 809 fixed rings, 810 cavitys, 811 connecting tubes, 812 spray heads, more than 9 Expect collecting mechanism, 901 upright bars, 902 collecting boards, 903 funnels, 904 collecting boxs, 10 heat blocking mechanisms, 1001 circle sets, 1,002 the One gasket, 1,003 second gaskets.
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below with reference to Specific embodiment, the present invention is further explained.
Please refer to Fig. 1-5, a kind of building scaffold outer surface of steel tube later period prosthetic device, including rack 1, fuselage 2, position It sets and limits mechanism 3, rotation driving mechanism 4, barrier plate 5, heats and brush mechanism 7, mobile Pai Qi mechanism 8,9 and of clout collecting mechanism Heat blocking mechanism 10, fuselage 2 are fixed on the top of rack 1, and the middle part in 2 left side of fuselage, position is arranged in position restriction mechanism 3 Limiting mechanism 3 includes that bearing 301,302, four struts 303 of rotation pipe and clamping mechanism 304, bearing 301 are embedded in fuselage 2 The middle part in left side, rotation pipe 302 are fixedly plugged in the inside of bearing 301, and four struts 303 are equidistantly fixed on rotation pipe 302 Left side, clamping mechanism 304 are fixedly connected with four struts 303, and clamping mechanism 304 includes 3041, four connecting rods of annulus 3042 and scroll chuck 3043, four 3042 annulus 3041 of connecting rod be equidistantly welded on the inner wall of annulus 3041, four struts 303 It is fixed on the middle part of four connecting rods 3042, scroll chuck 3043 is fixed between four struts 303, passes through position restriction mechanism 3 setting penetrates steel pipe to the inside of fuselage 2 from the middle part of scroll chuck 3043, and rotating ring 3041 counterclockwise passes through Connecting rod 3042 drives the external disk rotation of scroll chuck 3043, so that three latches move inward the outer surface progress to steel pipe It squeezes, and then steel pipe is fixed, guarantee the stability of the steel pipe when being painted.
Rotation driving mechanism 4 is arranged in the left side of 2 inner bottom wall of fuselage, rotation driving mechanism 4 include decelerating motor 401, Driving wheel 402, driven wheel 403 and transmission belt 404, decelerating motor 401 are fixed on the left side of 2 inner bottom wall of fuselage, and driving wheel 402 is solid Surely it is socketed on the output end of decelerating motor 401, driven wheel 403 is fixedly attached to the outer surface of rotation pipe 302, and driven wheel 403 are sequentially connected by transmission belt 404 and driving wheel 402, pass through the setting of rotation driving mechanism 4, the work fortune of decelerating motor 401 Row drives driving wheel 402 to rotate, and driving wheel 402 drives driven wheel 403 to rotate by transmission belt 404, and driven wheel 403 is fixedly attached It in the outer surface of rotation pipe 302, drives rotation pipe 302 in the inner rotation of bearing 301, and then drives and consolidated by scroll chuck 3043 The rotation of fixed steel pipe circumference ensure that the continuity and uniformity of spray painting.
Barrier plate 5 is fixed on the right side inside fuselage 2, and perforative through-hole 6 is offered in the middle part of 5 side of barrier plate, heating The right side that 2 inner roof wall of fuselage is arranged in mechanism 7 is brushed, it includes positive and negative motor 701, flabellum 703, heating that mechanism 7 is brushed in heating Silk 704 and first bevel gear 705, positive and negative motor 701 are fixed on the right side of 2 inner roof wall of fuselage, and the output shaft of positive and negative motor 701 is logical It crosses shaft coupling and is fixedly connected with rotation axis 702, flabellum 703 is fixedly attached to the outer surface of 702 bottom of rotation axis, first bevel gear 705 are fixedly attached to the middle part of 702 outer surface of rotation axis, and heater strip 704 is fixed between barrier plate 5 and 2 inner wall of fuselage right side, The underface of heater strip 704 is arranged in flabellum 703, and the setting of mechanism 7, the positive and negative work of motor 701 operation band are brushed by heating Turn moving axis 702 rotates, and drives the flabellum 703 of 702 outer surface bottom of rotation axis quickly to rotate, heater strip 704 is powered and is produced Raw heat brushes downwards, heats to the skin of paint of outer surface of steel tube, improves the dry efficiency of skin of paint.
Mobile Pai Qi mechanism 8 is arranged in the left side of 2 inner roof wall of fuselage, and mobile Pai Qi mechanism 8 includes threaded rod 801, the Two bevel gears 802, thread bush 803, sliding block 804, sliding rail 805, painting case 806, fluid hose 807, paint pump 808, fixed ring 809, connecting tube 811 and five spray heads 812, threaded rod 801 are movably connected between the left side and barrier plate 5 of 2 inner wall of fuselage The right end at top, threaded rod 801 runs through and extends the right side of barrier plate 5, and second bevel gear 802 is fixedly attached to threaded rod 801 Right end, second bevel gear 802 engages with first bevel gear 705, and 803 screw thread of thread bush is socketed in 801 outer surface of threaded rod Left side, sliding block 804 are fixed on the top of thread bush 803, and sliding rail 805 is fixed on the inner roof wall of fuselage 2, and sliding block 804 is slidably connected In the inside of sliding rail 805, painting case 806 is fixed on the top of fuselage 2, and paint pump 808 is fixed on the bottom of thread bush 803, oil It is connected between paint pump 808 and painting case 806 by fluid hose 807, fixed ring 809 is fixed on the bottom of paint pump 808, fixed ring 809 is circular for half, and the inside of fixed ring 809 offers circular cavity 810, and paint pump 808 passes through connection Pipe 811 is connected to cavity 810, and five spray heads 812 are equidistantly fixed on the inner wall of fixed ring 809, and spray head 812 and cavity 810 connect Logical, by the setting of mobile Pai Qi mechanism 8, the positive and negative work of motor 701 operation drives rotation axis 702 to rotate, and drive, which is socketed in, to be turned The first bevel gear 705 at 702 middle part of moving axis rotates, and first bevel gear 705 is engaged with second bevel gear 802, so that threaded rod 801 Rotation, the restriction by sliding block 804 and sliding rail 805 to thread bush 803, so that thread bush 803 is left in the outer surface of threaded rod 801 Paint inside painting case 806 is extracted by fluid hose 807, is entered to by connecting tube 811 by right rotation, paint pump 808 Then the inside of cavity 810 is sprayed from five spray heads 812, ensure that the uniformity to steel pipe spray painting, while ensure that spray painting The thickness of outer surface of steel tube skin of paint afterwards, preventing the outer surface skin of paint of steel pipe to be destroyed causes steel pipe to corrode, and improves safety Property.
Clout collecting mechanism 9 is arranged in the middle part of 2 inner bottom wall of fuselage, clout collecting mechanism 9 include there are four upright bar 901, Collecting board 902, funnel 903 and collecting box 904, four upright bars 901 are fixed on the inner bottom wall of fuselage 2, and collecting board 902 is fixed on four The top of a upright bar 901, the shape of collecting board 902 is arc-shaped, and the height at 902 middle part of collecting board is lower than collecting board 902 4 The height in week, for the fixed connection of funnel 903 at the middle part of collecting board 902, collecting box 904 is fixed on collecting box 904, and collecting box 904 are located at the underface of funnel 903, and by the setting of clout collecting mechanism 9, collecting board 902 is located at the lower section of steel pipe, to steel pipe When spray painting, the paint sprayed downwards and the paint dripped from steel pipe can fall in the top of collecting board 902, prevent paint from flying everywhere It raises and causes environmental pollution, the paint for dropping down onto 902 top of collecting board can be gathered to the middle part of collecting board 902, then from funnel 903 The Collection utilization for facilitating paint to the inside of collecting box 904 is fallen into, the waste of paint is reduced.
The middle part on 2 right side of fuselage is arranged in heat blocking mechanism 10, and heat blocking mechanism 10 includes 1001, four, circle set First gasket 1002 and four the second gaskets 1003, circle set 1001 are embedded in the middle part on 2 right side of fuselage, four first sealings Pad 1002 is equidistantly fixed on the inner wall of circle set 1001, and four the second gaskets 1003 are equidistantly fixed on the inner wall of circle set 1001, and First gasket 1002 is staggered with the second gasket 1003, by the setting of heat blocking mechanism 10, covers in steel pipe from circle When passing through in 1001, the first gasket 1002 and the second gasket 1003 can play the effect of sealing, reduce heat and cover from circle It is revealed in 1001, ensure that the temperature of chamber between on the left of 5 right side of barrier plate and 2 inner wall of fuselage, further improve to steel pipe The dry efficiency of outer surface skin of paint.
When in use, one end of steel pipe is penetrated from the middle part of scroll chuck 3043 to the inside of fuselage 2, rotation counterclockwise Turn the external disk rotation that annulus 3041 drives scroll chuck 3043 by connecting rod 3042, so that three latches move inward to steel The outer surface of pipe is squeezed, and then steel pipe is fixed, and the work operation of decelerating motor 401 drives driving wheel 402 to rotate, main Driving wheel 402 drives driven wheel 403 to rotate by transmission belt 404, and driven wheel 403 is fixedly attached to the outer surface of rotation pipe 302, band Rotation pipe 302 is moved in the inner rotation of bearing 301, and then drives the rotation for the steel pipe circumference fixed by scroll chuck 3043, just The anti-work of motor 701 operation drives rotation axis 702 to rotate, and drives 705 turns of first bevel gear for being socketed in 702 middle part of rotation axis Dynamic, first bevel gear 705 is engaged with second bevel gear 802, so that threaded rod 801 rotates, it is right by sliding block 804 and sliding rail 805 The restriction of thread bush 803, so that rotation of the thread bush 803 in the outer surface of threaded rod 801 or so, paint pump 808 pass through paint Pipe 807 extracts the paint inside painting case 806, and the inside of cavity 810 is entered to by connecting tube 811, then sprays from five It sprays in first 812, paints to the outer surface of steel pipe, collecting board 902 is located at the lower section of steel pipe, when painting to steel pipe, downwards The paint of sprinkling and the paint dripped from steel pipe can fall in the top of collecting board 902, and collecting board 902 is located at the lower section of steel pipe, The paint sprayed downwards and the paint dripped from steel pipe can fall in the top of collecting board 902, drop down onto the oil at 902 top of collecting board Paint can be gathered to the middle part of collecting board 902, and the receipts that paint is facilitated to the inside of collecting box 904 are then fallen into from funnel 903 Collection utilizes, and after the completion of steel pipe wherein one section of spray painting, makes steel pipe mobile to the inside of fuselage 2 by unclamping clamping mechanism 304, So that steel pipe is penetrated from through-hole 6 on barrier plate 5 to the lower section of heater strip 704, the positive and negative work of motor 701 operation band turn slowly Moving axis 702 rotates, and the flabellum 703 of 702 outer surface bottom of rotation axis is driven quickly to rotate, and the energization of heater strip 704 is generated Heat brushes downwards, heats to the skin of paint of outer surface of steel tube, after the completion of the skin of paint of outer surface of steel tube is dry, so that Steel pipe is pierced by from circle set 1001, to complete the steel pipe spray painting operation to scaffold.

Claims (8)

1. a kind of building scaffold outer surface of steel tube later period prosthetic device, including rack (1), fuselage (2), position restriction mechanism (3), mechanism (7), mobile Pai Qi mechanism (8), clout collecting mechanism (9) are brushed in rotation driving mechanism (4), barrier plate (5), heating With heat blocking mechanism (10), it is characterised in that: the fuselage (2) is fixed on the top of rack (1), the position restriction mechanism (3) middle part on the left of fuselage (2) is set, and rotation driving mechanism (4) setting is described in the left side of fuselage (2) inner bottom wall Barrier plate (5) is fixed on the internal right side of fuselage (2), offers perforative through-hole (6) in the middle part of barrier plate (5) side, The heating brushes mechanism (7) setting on the right side of fuselage (2) inner roof wall, and the mobile Pai Qi mechanism (8) is arranged in fuselage (2) The left side of inner roof wall, the clout collecting mechanism (9) are arranged in the middle part of fuselage (2) inner bottom wall, the heat blocking mechanism (10) middle part being arranged on the right side of fuselage (2).
2. a kind of building scaffold outer surface of steel tube later period prosthetic device according to claim 1, it is characterised in that: institute Stating position restriction mechanism (3) includes bearing (301), rotation pipe (302), four struts (303) and clamping mechanism (304), institute The middle part that bearing (301) is embedded on the left of fuselage (2) is stated, the rotation pipe (302) is fixedly plugged in the inside of bearing (301), Four struts (303) are equidistantly fixed on the left side of rotation pipe (302), the clamping mechanism (304) and four struts (303) It is fixedly connected.
3. a kind of building scaffold outer surface of steel tube later period prosthetic device according to claim 2, it is characterised in that: institute Stating clamping mechanism (304) includes annulus (3041), four connecting rods (3042) and scroll chuck (3043), four connections Bar (3042) annulus (3041) is equidistantly welded on the inner wall of annulus (3041), and four struts (303) are fixed on four connections The middle part of bar (3042), the scroll chuck (3043) are fixed between four struts (303).
4. a kind of building scaffold outer surface of steel tube later period prosthetic device according to claim 3, it is characterised in that: institute Stating rotation driving mechanism (4) includes decelerating motor (401), driving wheel (402), driven wheel (403) and transmission belt (404), institute The left side that decelerating motor (401) is fixed on fuselage (2) inner bottom wall is stated, the driving wheel (402) is fixedly attached to decelerating motor (401) on output end, the driven wheel (403) is fixedly attached to the outer surface of rotation pipe (302), and driven wheel (403) is logical Transmission belt (404) and driving wheel (402) are crossed to be sequentially connected.
5. a kind of building scaffold outer surface of steel tube later period prosthetic device according to claim 4, it is characterised in that: institute Stating heating to brush mechanism (7) includes positive and negative motor (701), flabellum (703), heater strip (704) and first bevel gear (705), The positive and negative motor (701) is fixed on the right side of fuselage (2) inner roof wall, and the output shaft of the positive and negative motor (701) passes through shaft coupling Device is fixedly connected with rotation axis (702), and the flabellum (703) is fixedly attached to the outer surface of rotation axis (702) bottom, and described One bevel gear (705) is fixedly attached to the middle part of rotation axis (702) outer surface, and the heater strip (704) is fixed on barrier plate (5) Between on the right side of fuselage (2) inner wall, underface of flabellum (703) setting in heater strip (704).
6. a kind of building scaffold outer surface of steel tube later period prosthetic device according to claim 5, it is characterised in that: institute Stating mobile Pai Qi mechanism (8) includes threaded rod (801), second bevel gear (802), thread bush (803), sliding block (804), sliding rail (805), painting case (806), fluid hose (807), paint pump (808), fixed ring (809), connecting tube (811) and five spray heads (812), the threaded rod (801) is movably connected in the top between the left side and barrier plate (5) of fuselage (2) inner wall, the spiral shell The right end of rasp bar (801) runs through and extends the right side of barrier plate (5), and the second bevel gear (802) is fixedly attached to threaded rod (801) right end, second bevel gear (802) are engaged with first bevel gear (705), and thread bush (803) screw thread is socketed in spiral shell The left side of rasp bar (801) outer surface, the sliding block (804) are fixed on the top of thread bush (803), and the sliding rail (805) is fixed Inner roof wall in fuselage (2), the sliding block (804) are slidably connected at the inside of sliding rail (805), and the painting case (806) is fixed At the top of fuselage (2), the paint pump (808) is fixed on the bottom of thread bush (803), the paint pump (808) and paint It is connected between case (806) by fluid hose (807), the fixed ring (809) is fixed on the bottom of paint pump (808), described solid Determining ring (809) is that half is circular, and the inside of fixed ring (809) offers circular cavity (810), the paint Pump (808) is connected to by connecting tube (811) with cavity (810), and five spray heads (812) are equidistantly fixed on fixed ring (809) Inner wall, and spray head (812) is connected to cavity (810).
7. a kind of building scaffold outer surface of steel tube later period prosthetic device according to claim 6, it is characterised in that: institute Stating clout collecting mechanism (9) includes four there are four upright bar (901), collecting board (902), funnel (903) and collecting box (904) The upright bar (901) is fixed on the inner bottom wall of fuselage (2), and the collecting board (902) is fixed on the top of four upright bars (901), The shape of the collecting board (902) is arc-shaped, and the height in the middle part of collecting board (902) is lower than the height of collecting board (902) surrounding Degree, for the fixed connection of the funnel (903) at the middle part of collecting board (902), the collecting box (904) is fixed on collecting box (904), And collecting box (904) is located at the underface of funnel (903).
8. a kind of building scaffold outer surface of steel tube later period prosthetic device according to claim 7, it is characterised in that: institute Stating heat blocking mechanism (10) includes circle set (1001), four the first gaskets (1002) and four the second gaskets (1003), the circle set (1001) is embedded in the middle part on the right side of fuselage (2), and four first gaskets (1002) are equidistantly fixed In the inner wall of circle set (1001), four second gaskets (1003) are equidistantly fixed on the inner wall of circle set (1001), and first Gasket (1002) is staggered with the second gasket (1003).
CN201811292568.XA 2018-11-01 2018-11-01 A kind of building scaffold outer surface of steel tube later period prosthetic device Pending CN109174495A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110280429A (en) * 2019-06-21 2019-09-27 南京亚页防护设备制造有限公司 A kind of numerically-controlled machine tool processing spray equipment having air-drying function
CN112958341A (en) * 2021-03-19 2021-06-15 杭州湘泰环境科技有限公司 Spraying device for pipeline repair and using method thereof

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN206652652U (en) * 2017-04-08 2017-11-21 黄忠南 A kind of tubular member spray-painting plant for building
CN207823288U (en) * 2017-12-29 2018-09-07 天津华冠木器有限公司 A kind of timber processing spray drying all-in-one machine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN206652652U (en) * 2017-04-08 2017-11-21 黄忠南 A kind of tubular member spray-painting plant for building
CN207823288U (en) * 2017-12-29 2018-09-07 天津华冠木器有限公司 A kind of timber processing spray drying all-in-one machine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110280429A (en) * 2019-06-21 2019-09-27 南京亚页防护设备制造有限公司 A kind of numerically-controlled machine tool processing spray equipment having air-drying function
CN112958341A (en) * 2021-03-19 2021-06-15 杭州湘泰环境科技有限公司 Spraying device for pipeline repair and using method thereof
CN112958341B (en) * 2021-03-19 2022-01-18 杭州湘泰环境科技有限公司 Spraying device for pipeline repair and using method thereof

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