CN108000276A - A kind of efficient letter box arrangement - Google Patents
A kind of efficient letter box arrangement Download PDFInfo
- Publication number
- CN108000276A CN108000276A CN201711297874.8A CN201711297874A CN108000276A CN 108000276 A CN108000276 A CN 108000276A CN 201711297874 A CN201711297874 A CN 201711297874A CN 108000276 A CN108000276 A CN 108000276A
- Authority
- CN
- China
- Prior art keywords
- wall
- tail end
- chamber
- spiral shell
- cone pulley
- 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.)
- Withdrawn
Links
- 238000004140 cleaning Methods 0.000 claims abstract description 32
- 238000005498 polishing Methods 0.000 claims abstract description 18
- 238000012423 maintenance Methods 0.000 claims description 9
- 238000009413 insulation Methods 0.000 claims description 8
- 239000006096 absorbing agent Substances 0.000 claims description 7
- 238000013016 damping Methods 0.000 claims description 6
- 230000013011 mating Effects 0.000 claims description 2
- 239000007787 solid Substances 0.000 claims 1
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000010626 work up procedure Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B9/00—Machines or devices designed for grinding edges or bevels on work or for removing burrs; Accessories therefor
- B24B9/02—Machines or devices designed for grinding edges or bevels on work or for removing burrs; Accessories therefor characterised by a special design with respect to properties of materials specific to articles to be ground
- B24B9/04—Machines or devices designed for grinding edges or bevels on work or for removing burrs; Accessories therefor characterised by a special design with respect to properties of materials specific to articles to be ground of metal, e.g. skate blades
-
- B08B1/12—
-
- B08B1/32—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B13/00—Accessories or details of general applicability for machines or apparatus for cleaning
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B47/00—Drives or gearings; Equipment therefor
- B24B47/10—Drives or gearings; Equipment therefor for rotating or reciprocating working-spindles carrying grinding wheels or workpieces
- B24B47/12—Drives or gearings; Equipment therefor for rotating or reciprocating working-spindles carrying grinding wheels or workpieces by mechanical gearing or electric power
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B55/00—Safety devices for grinding or polishing machines; Accessories fitted to grinding or polishing machines for keeping tools or parts of the machine in good working condition
- B24B55/06—Dust extraction equipment on grinding or polishing machines
Abstract
The invention discloses a kind of efficient letter box arrangement, including arm and the fuselage for being fixedly mounted on the arm bottom end face, it is characterised in that：Slide slot and the left conduction chamber being arranged at left and right sides of the slide slot and right conduction chamber are provided with the fuselage inner wall, cooperation is slided in the slide slot, and skid is installed, spiral shell type line, which coordinates, in the skid is provided with spiral shell type line rotation axis, tail end is connected with the slide slot inner left wall rotatable engagement on the left of the spiral shell type line rotation axis, and tail end and the first motor power are connected on the right side of the spiral shell type line rotation axis；The configuration of the present invention is simple, easy to operate, polishing and cleaning are all completed by a machine, efficient without artificial nuisance operation, time saving and energy saving.
Description
Technical field
The present invention relates to mailbox technical field, is specifically a kind of efficient letter box arrangement.
Background technology
General mailbox is welded by several pieces of metallic plates, and weld seam needs to polish, and traditional manual grinding is time-consuming to be taken
Power, needs to brush the metal fragment on mailbox surface with brush after polishing, and polishing operation is substantially by machine on modernization assembly line
Device is completed, but is still needed the mailbox surface manually finished to polishing and cleared up, relatively complicated.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of efficient letter box arrangement, it can solve above-mentioned present skill
The problem of in art.
The present invention is achieved through the following technical solutions：A kind of efficient letter box arrangement of the present invention, including arm
And the fuselage of the arm bottom end face is fixedly mounted on, slide slot is provided with the fuselage inner wall and is arranged on institute
The left conduction chamber at left and right sides of slide slot and right conduction chamber are stated, sliding cooperation in the slide slot is provided with skid, the cunning
Spiral shell type line, which coordinates, in row frame is provided with spiral shell type line rotation axis, on the left of the spiral shell type line rotation axis in tail end and slide slot left side
Wall rotatable engagement connects, and tail end and the first motor power are connected on the right side of the spiral shell type line rotation axis, outside first motor
Surface is installed in the fuselage inner wall, is installed with the skid inner wall on the upside of the spiral shell type line rotation axis
Second motor, the second motor left and right sides penetrate through wall body at left and right sides of the skid, the second motor left side tail end
Power, which coordinates, is provided with the first engagement shaft, and right side tail end power, which coordinates, is provided with the second engagement shaft, the left conduction chamber with it is described
Rotatable engagement is provided with the first column spinner in the fuselage inner wall between slide slot, in the first column spinner its right end face
The first engaging chamber to be connected with the first engagement shaft snap fit is provided with, tail end is put on the left of first column spinner
In the left conduction chamber and tail end is installed with the first taper cone pulley, and the first taper cone pulley rotatable engagement connects cleaning plant,
Rotatable engagement is provided with the second column spinner in the fuselage inner wall between the slide slot and the right conduction chamber, and described the
It is provided with the second slot to be connected with the second engagement shaft snap fit in two column spinner left end faces, described second
Tail end is put in the right conduction chamber on the right side of column spinner and tail end is installed with the second taper cone pulley, the second taper cone pulley rotation
Mating connection sanding apparatus, the fuselage surface lower part coordinate the cleaning plant and the sanding apparatus to be respectively arranged with conveniently
The left window and right window of observation, the fuselage surface top are provided with maintenance notch, coordinate in the maintenance notch and set
Access panel is equipped with, the access panel is connected by hinge with the maintenance notch outer wall rotatable engagement, on the right side of the access panel
Drawing handle is fixedly installed, the access panel lower right corner is provided with sash lock, sound insulation vibration absorber is provided with first motor.
Preferably technical solution, the cleaning plant include the fuselage for being arranged on the left conduction chamber lower side
Lower conduction chamber in inner wall and the cleaning chamber for being arranged on the lower conduction chamber right-hand end, are provided with phase in the lower conduction chamber
Mutually ratcheting triconic wheel and the 4th taper cone pulley, the triconic wheel top end surface are installed with the 3rd column spinner, institute
State the 3rd column spinner be connected with the fuselage inner wall rotatable engagement and top tail end put in it is described it is left conduction chamber in and tail end consolidate
Dingan County is equipped with the 5th taper cone pulley, and the 5th taper cone pulley and first taper cone pulley are mutually ratcheting, on the right side of the 4th taper cone pulley
End face is installed with rotating arm, and the rotating arm passes through to the right the fuselage inner wall and rotatable engagement is connected and put in described
Cleaning chamber is connected with end wall rotatable engagement on the right side of the cleaning chamber, and the rotating arm outer surface in the cleaning chamber is circumferentially fixed
There is brush head.
Preferably technical solution, the sanding apparatus include being arranged in the fuselage bottom end face being located at the right side
The polishing chamber at chamber lower position is conducted, is slided in the polishing chamber and is connected with casing, rotated in described sleeve pipe inner wall
Cooperation is provided with rotating cylinder, the 3rd slot is provided with the rotating cylinder, snap fit is provided with the 3rd in the 3rd slot
Engagement shaft, the 3rd engagement shaft top is connected through the fuselage inner wall and rotatable engagement, at the top of the 3rd engagement shaft
Tail end is put in the right conduction chamber and tail end is installed with the 6th taper cone pulley, the 6th taper cone pulley and second taper
Wheel is mutually ratcheting, and inner wall is arranged with cavity at left and right sides of the polishing chamber, and cooperation is slided in the cavity and is provided with even block, often
A even block inner side end is fixedly connected with described sleeve pipe left and right sides and the cooperation of spiral shell type line is provided with spiral shell type bar, the spiral shell
Type bar bottom tail end is connected with the cavity base end wall rotatable engagement, and tail end and the 3rd motor power coordinate at the top of the spiral shell type bar
Connection, the 3rd outer surface of motor are fixedly installed in the cavity top end wall, and the cylinder bottom end face is installed with
Grinding head.
Preferably technical solution, the sound insulation vibration absorber include being fixed at first motor both sides up and down
The sound insulating pad in face and the damping block for being fixed at the first motor right flank, the sound insulating pad and the damping block respectively with
The fuselage inner wall is connected.
The beneficial effects of the invention are as follows：The configuration of the present invention is simple, it is easy to operate, by being provided with cunning in fuselage inner wall
Row groove and the left conduction chamber being arranged at left and right sides of slide slot and right conduction chamber, slide cooperation in slide slot and are provided with and slide
Frame, spiral shell type line, which coordinates, in skid is provided with spiral shell type line rotation axis, tail end and slide slot inner left wall on the left of spiral shell type line rotation axis
Rotatable engagement connects, and tail end and the first motor power are connected on the right side of spiral shell type line rotation axis, and the first outer surface of motor is installed on
In fuselage inner wall, the second motor, the second motor or so are installed with the skid inner wall on the upside of spiral shell type line rotation axis
Wall body at left and right sides of both sides perforation skid, the second motor left side tail end power, which coordinates, is provided with the first engagement shaft, right side tail end
Power, which coordinates, is provided with the second engagement shaft, and rotatable engagement is provided with first in the fuselage inner wall between left conduction chamber and slide slot
Column spinner, the first engaging chamber to be connected with the first engagement shaft snap fit is provided with the first column spinner its right end face, the
Tail end is put in left conduction chamber on the left of one column spinner and tail end is installed with the first taper cone pulley, and the first taper cone pulley rotatable engagement connects
Cleaning plant is connect, rotatable engagement is provided with the second column spinner, the second rotation in the fuselage inner wall between slide slot and right conduction chamber
The second slot to be connected with the second engagement shaft snap fit, the second column spinner right side tail are provided with rotary column left end face
End is put in right conduction chamber and tail end is installed with the second taper cone pulley, and the second taper cone pulley rotatable engagement connects sanding apparatus, from
And realize and the work of mailbox weld grinding or chip cleaning work, polishing and cleaning are all completed by a machine automatically, without
Artificial nuisance operation, it is efficient, it is time saving and energy saving.
Brief description of the drawings
For ease of explanation, the present invention is described in detail by following specific embodiment and attached drawing.
Fig. 1 is overall structure diagram inside a kind of efficient letter box arrangement of the present invention；
Fig. 2 is the partial enlargement structural representation in Fig. 1 of the present invention；
Fig. 3 is a kind of efficient letter box arrangement external structure schematic diagram of the present invention.
Embodiment
As shown in Figure 1-Figure 3, a kind of efficient letter box arrangement of the invention, including arm 7 and be fixedly mounted on described
The fuselage 8 of 7 bottom end face of arm, is provided with slide slot 808 in 8 inner wall of fuselage and is arranged on the slide slot 808
The left conduction chamber 812 of the left and right sides and right conduction chamber 802, slide cooperation in the slide slot 808 and are provided with skid 827, institute
State spiral shell type line cooperation in skid 827 and spiral shell type line rotation axis 822, the 822 left side tail end of spiral shell type line rotation axis and institute are installed
State the connection of 808 inner left wall rotatable engagement of slide slot, the 822 right side tail end of spiral shell type line rotation axis and 824 power of the first motor
It is connected, 824 outer surface of the first motor is installed in 8 inner wall of fuselage, the upside of spiral shell type line rotation axis 822
827 inner wall of the skid in be installed with the second motor 806, described in the perforation of the left and right sides of the second motor 806
827 left and right sides wall body of skid, the 806 left side tail end power of the second motor, which coordinates, is provided with the first engagement shaft 807, right side
Tail end power, which coordinates, is provided with the second engagement shaft 823, the fuselage 8 between the left conduction chamber 812 and the slide slot 808
Rotatable engagement is provided with the first column spinner 810 in inner wall, be provided with 810 its right end face of the first column spinner to institute
The first engaging chamber 809 of 807 snap fit of the first engagement shaft connection is stated, the 810 left side tail end of the first column spinner puts in described
In left conduction chamber 812 and tail end is installed with the first taper cone pulley 811,811 rotatable engagement of the first taper cone pulley connection cleaning
Rotatable engagement is provided with second in device, the slide slot 808 and right 8 inner wall of the fuselage conducted between chamber 802
Column spinner 804, is provided with 804 left end face of the second column spinner to connect with 823 snap fit of the second engagement shaft
The second slot 805 connect, the 804 right side tail end of the second column spinner is put in the right conduction chamber 802 and tail end fixes peace
Equipped with the second taper cone pulley 803,803 rotatable engagement of the second taper cone pulley connects sanding apparatus, and 8 surface lower portions of fuselage coordinate
The cleaning plant and the sanding apparatus are respectively arranged with the left window 851 and right window 852 of convenient observation, the machine
8 surface top of body is provided with maintenance notch 86, and access panel 861, the access panel 861 are equipped with the maintenance notch 86
It is connected by hinge 862 with the maintenance 86 outer wall rotatable engagement of notch, the right side of access panel 861 is fixedly installed drawing handle
863,861 lower right corner of access panel is provided with sash lock 864, and sound insulation vibration absorber is provided with first motor 824.
Valuably, the cleaning plant includes being arranged in 8 inner wall of the fuselage of 812 lower side of the left conduction chamber
Lower conduction chamber 815 and be arranged on it is described it is lower conduction 815 right-hand end of chamber cleaning chamber 821, it is described it is lower conduction chamber 815 in set
There is mutually ratcheting 818 and the 4th taper cone pulley 816 of triconic wheel, 818 top end surface of triconic wheel is installed with
3rd column spinner 814, the 3rd column spinner 814 is connected with the 8 inner wall rotatable engagement of fuselage and top tail end puts in institute
State in left conduction chamber 812 and tail end is installed with the 5th taper cone pulley 813, the 5th taper cone pulley 813 and first taper
Wheel 811 is mutually ratcheting, and 816 its right end face of the 4th taper cone pulley is installed with rotating arm 817, and the rotating arm 817 is to the right
Connect through 8 inner wall of fuselage and rotatable engagement and put in the cleaning chamber 821 and revolved with the 821 right side end wall of cleaning chamber
Turn to be connected, 817 outer surface of the rotating arm in the cleaning chamber 821 is circumferentially installed with brush head 820, so as to fulfill hair
Brush head 820 rotates cleaning work automatically, improves cleaning efficiency.
Valuably, the sanding apparatus is included being arranged in 8 bottom end face of fuselage under the right conduction chamber 802
Polishing chamber 826 at side position, slides and is connected with casing 833 in the polishing chamber 826, in 833 inner wall of described sleeve pipe
Rotatable engagement is provided with rotating cylinder 845, and the 3rd slot 830 is provided with the rotating cylinder 845, is blocked in the 3rd slot 830
Close cooperation and the 3rd engagement shaft 844 is installed, the top of the 3rd engagement shaft 844 passes through 8 inner wall of fuselage and rotatable engagement
Connection, the 844 top tail end of the 3rd engagement shaft is put in the right conduction chamber 802 and tail end is installed with the 6th taper cone pulley
801, the 6th taper cone pulley 801 and second taper cone pulley 803 are mutually ratcheting, polishing 806 left and right sides inner wall pair of chamber
Title is equipped with cavity 847, and cooperation is slided in the cavity 847 and is provided with even block 848, each even 848 inner side end of block and the institute
State 833 left and right sides of casing be fixedly connected and spiral shell type line coordinate spiral shell type bar 831, the 831 bottom tail end of spiral shell type bar are installed
It is connected with the 847 base end wall rotatable engagement of cavity, the 831 top tail end of spiral shell type bar and 846 power of the 3rd motor, which coordinate, to be connected
Connect, 846 outer surface of the 3rd motor is fixedly installed in 847 top end wall of cavity, and 845 bottom end face of rotating cylinder is fixed
Grinding head 825 is installed, so as to fulfill automatic flexible and rotary-grinding work up and down, manpower is effectively reduced and uses, increase polishing
Efficiency.
Valuably, the sound insulation vibration absorber includes being fixed at the sound insulation of the first motor two sides about 824
Pad 8241 and the damping block 8242 for being fixed at 824 right flank of the first motor, the sound insulating pad 8241 and the vibration damping
Plate 8242 is connected with 8 inner wall of fuselage respectively, by setting the sound insulation vibration absorber effectively to reduce first electricity
The noise and vibrations that the operating of machine 824 produces.
During original state, skid 827 is located at 808 middle position of slide slot, and at this time, the first engagement shaft 807 is not
Contacted with the first engaging chamber 809, the second engagement shaft 823 is not contacted with the second engaging chamber 805.
When needing polishing work, fuselage 8 is moved to by the mailbox weld seam upper side position for needing to polish by arm 7, is led to
Cross the first motor 824 driving rotation spiral shell type line rotation axis 822 to rotate, the rotation of spiral shell type line rotation axis 822 drives skid 827 to the right
Side is moved, until the second engagement shaft 824 is put in the second engaging chamber 805 completely, at this time, driving the second motor 806 rotation drives
Second column spinner 804 and the second taper cone pulley 803 rotate, and rotate the grinding head driven in cleaning plant by the second taper cone pulley 803
825 rotary works, meanwhile, driving the 3rd motor 846 rotation drives spiral shell type bar 831 to rotate, and the rotation of spiral shell type bar 831 drives even block
848 glide downwards, so that grinding head 825 is bonded downwards mailbox weld seam, so as to complete polishing work.
When needing cleaning work, fuselage 8 is moved to by the mailbox weld seam upper side position for needing to clear up by arm 7, is led to
Cross the first motor 824 driving rotation spiral shell type line rotation axis 822 to rotate, the rotation of spiral shell type line rotation axis 822 drives skid 827 to the left
Side is moved, until the first engagement shaft 807 is put in the first engaging chamber 809 completely, at this time, driving the second motor 806 rotation drives
First column spinner 810 and the first taper cone pulley 811 rotate, and the first taper cone pulley 811 drives the 5th taper cone pulley 813 to rotate, the 5th taper
The rotation of wheel 813 drives the 3rd column spinner 814 to rotate, and the rotation of the 3rd column spinner 814 drives triconic wheel 818 to rotate, third hand tap
The rotation of shape wheel 818 drives the 4th taper cone pulley 816 to rotate, and the 4th taper cone pulley 816 rotation rotating arm 817 rotates, and rotating arm 817 rotates
Brush head 820 is set to rotate into cleaning state, so as to carry out cleaning work to mailbox surface debris.
The beneficial effects of the invention are as follows：The configuration of the present invention is simple, it is easy to operate, by being provided with slide slot in fuselage inner wall
And the left conduction chamber at left and right sides of slide slot and right conduction chamber are arranged on, sliding cooperation in slide slot is provided with skid, sliding
Spiral shell type line, which coordinates, in row frame is provided with spiral shell type line rotation axis, and tail end is matched somebody with somebody with the rotation of slide slot inner left wall on the left of spiral shell type line rotation axis
Connection is closed, spiral shell type line rotation axis right side tail end and the first motor power are connected, and the first outer surface of motor is installed in fuselage
In wall body, the second motor is installed with the skid inner wall on the upside of spiral shell type line rotation axis, is passed through at left and right sides of the second motor
Wall body at left and right sides of logical skid, the second motor left side tail end power, which coordinates, is provided with the first engagement shaft, and right side tail end power is matched somebody with somebody
Conjunction is provided with the second engagement shaft, and rotatable engagement is provided with the first rotation in the fuselage inner wall between left conduction chamber and slide slot
Column, the first engaging chamber to be connected with the first engagement shaft snap fit, the first rotation are provided with the first column spinner its right end face
Tail end is put in left conduction chamber on the left of rotary column and tail end is installed with the first taper cone pulley, and the connection of the first taper cone pulley rotatable engagement is clear
Device is managed, rotatable engagement is provided with the second column spinner, the second column spinner in the fuselage inner wall between slide slot and right conduction chamber
The second slot to be connected with the second engagement shaft snap fit is provided with left end face, tail end is stretched on the right side of the second column spinner
Into in right conduction chamber and tail end is installed with the second taper cone pulley, the second taper cone pulley rotatable engagement connection sanding apparatus, so that real
Now the work of mailbox weld grinding or chip cleaning work, polishing and cleaning are all completed by a machine automatically, without artificial
Nuisance operation, it is efficient, it is time saving and energy saving.
The above description is merely a specific embodiment, but protection scope of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, it is of the invention
Protection domain should be determined by the scope of protection defined in the claims.
Claims (4)
1. a kind of efficient letter box arrangement, including arm and the fuselage for being fixedly mounted on the arm bottom end face, its feature
It is：Slide slot and the left conduction chamber and the right biography that are arranged at left and right sides of the slide slot are provided with the fuselage inner wall
Guide cavity, cooperation is slided in the slide slot and is provided with skid, and spiral shell type line, which coordinates, in the skid is provided with the rotation of spiral shell type line
Axis, spiral shell type line rotation axis left side tail end are connected with the slide slot inner left wall rotatable engagement, the spiral shell type line rotation axis
Right side tail end and the first motor power are connected, and first outer surface of motor is installed in the fuselage inner wall, described
The second motor is installed with the skid inner wall on the upside of spiral shell type line rotation axis, is passed through at left and right sides of second motor
Wall body at left and right sides of the logical skid, the second motor left side tail end power, which coordinates, is provided with the first engagement shaft, right side tail
End power, which coordinates, is provided with the second engagement shaft, rotation in the fuselage inner wall between the left conduction chamber and the slide slot
Cooperation is provided with the first column spinner, is provided with the first column spinner its right end face and matches somebody with somebody to engage with first engagement shaft
Close the first engaging chamber of connection, tail end is put in the left conduction chamber on the left of first column spinner and tail end is installed with the
One taper cone pulley, the first taper cone pulley rotatable engagement connect cleaning plant, the institute between the slide slot and the right conduction chamber
State rotatable engagement in fuselage inner wall and the second column spinner be installed, be provided with the second column spinner left end face to institute
The second slot of the second engagement shaft snap fit connection is stated, tail end is put in the right conduction chamber on the right side of second column spinner
And tail end is installed with the second taper cone pulley, the second taper cone pulley rotatable engagement connects sanding apparatus, under the fuselage surface
Portion coordinates the cleaning plant and the sanding apparatus to be respectively arranged with the left window of convenient observation and right window, the machine
Body surface top is provided with maintenance notch, is equipped with access panel in the maintenance notch, the access panel by hinge with
The maintenance notch outer wall rotatable engagement connection, the access panel right side are fixedly installed drawing handle, the access panel lower right corner
Sash lock is provided with, sound insulation vibration absorber is provided with first motor.
A kind of 2. efficient letter box arrangement according to claim 1, it is characterised in that：The cleaning plant includes being arranged on
Lower conduction chamber in the fuselage inner wall of the left conduction chamber lower side and it is arranged on the lower conduction chamber right-hand end
Chamber is cleared up, mutually ratcheting triconic wheel and the 4th taper cone pulley, the triconic wheel top are provided with the lower conduction chamber
End surface is installed with the 3rd column spinner, and the 3rd column spinner is connected with the fuselage inner wall rotatable engagement and top tail
End is put in the left conduction chamber and tail end is installed with the 5th taper cone pulley, the 5th taper cone pulley and first taper cone pulley
Mutually ratcheting, the 4th taper cone pulley its right end face is installed with rotating arm, and the rotating arm is passed through in the fuselage to the right
Wall body and rotatable engagement connect and put in the cleaning chamber and be connected with end wall rotatable engagement on the right side of the cleaning chamber, the cleaning chamber
In the rotating arm outer surface be circumferentially installed with brush head.
A kind of 3. efficient letter box arrangement according to claim 1, it is characterised in that：The sanding apparatus includes being arranged on
In the fuselage bottom end face mating connection is slided in the right polishing chamber conducted at chamber lower position, the polishing chamber
There is a casing, rotatable engagement is provided with rotating cylinder in described sleeve pipe inner wall, is provided with the 3rd slot in the rotating cylinder, and the described 3rd
Snap fit is provided with the 3rd engagement shaft in slot, matches somebody with somebody at the top of the 3rd engagement shaft through the fuselage inner wall and rotation
Connection is closed, the 3rd engagement shaft top tail end is put in the right conduction chamber and tail end is installed with the 6th taper cone pulley, institute
State the 6th taper cone pulley and second taper cone pulley is mutually ratcheting, inner wall is arranged with cavity at left and right sides of the polishing chamber, described
Cooperation is slided in cavity even block is installed, each even block inner side end is fixedly connected with described sleeve pipe left and right sides and spiral shell
Type line, which coordinates, is provided with spiral shell type bar, and the spiral shell type bar bottom tail end is connected with the cavity base end wall rotatable engagement, the spiral shell type
Tail end and the 3rd motor power are connected at the top of bar, and the 3rd outer surface of motor is fixedly installed in the cavity top end wall
Interior, the cylinder bottom end face is installed with grinding head.
A kind of 4. efficient letter box arrangement according to claim 1, it is characterised in that：The sound insulation vibration absorber includes solid
Surely first motor sound insulating pad of two sides and the damping block for being fixed at the first motor right flank up and down are arranged on,
The sound insulating pad is connected with the fuselage inner wall respectively with the damping block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711297874.8A CN108000276A (en) | 2017-12-08 | 2017-12-08 | A kind of efficient letter box arrangement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711297874.8A CN108000276A (en) | 2017-12-08 | 2017-12-08 | A kind of efficient letter box arrangement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108000276A true CN108000276A (en) | 2018-05-08 |
Family
ID=62057927
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711297874.8A Withdrawn CN108000276A (en) | 2017-12-08 | 2017-12-08 | A kind of efficient letter box arrangement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108000276A (en) |
-
2017
- 2017-12-08 CN CN201711297874.8A patent/CN108000276A/en not_active Withdrawn
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