CN108086160A - A kind of novel bridge constructing device - Google Patents
A kind of novel bridge constructing device Download PDFInfo
- Publication number
- CN108086160A CN108086160A CN201710553260.5A CN201710553260A CN108086160A CN 108086160 A CN108086160 A CN 108086160A CN 201710553260 A CN201710553260 A CN 201710553260A CN 108086160 A CN108086160 A CN 108086160A
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- chamber
- fuselage
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- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01D—CONSTRUCTION OF BRIDGES, ELEVATED ROADWAYS OR VIADUCTS; ASSEMBLY OF BRIDGES
- E01D21/00—Methods or apparatus specially adapted for erecting or assembling bridges
Abstract
The invention discloses a kind of novel bridge constructing devices, including the fuselage being made of upper fuselage and lower fuselage, lower fuselage interior is equipped with stir chamber, the agitating shaft for extending set up and down is equipped in stir chamber, equity is equipped with insertion part at left and right sides of lower fuselage top surface, the first motor is equipped in upper fuselage, first electronic motor spindle is connected with rotating speed control machine, rotating speed control motor spindle is connected with the first rotation axis of the upper body bottom surface of perforation and rotatable engagement connection, it is equipped in upper fuselage top surface at left and right sides of first rotation axis and plugs together slot with what insertion part was oppositely arranged, sealed slide slot is equipped in two groups of side walls for plugging together the opposite side of slot, each sealed slide slot, which leaves to plug together the perforation of slot one side and be equipped with to extend backward, the first of setting slides chamber；The configuration of the present invention is simple, maintenance easy to disassemble can realize that automatic uniform speed stirs work, improve blanking efficiency.
Description
Technical field
The present invention relates to bridge fields, are specifically a kind of novel bridge constructing device.
Background technology
, it is necessary to largely use concrete in bridge construction process, generally all carry out at the construction field (site) to sand, stone, water etc. by
Ratio cooperation stirring generation concrete, existing concrete mixer is bulky, and because construction needs, it is often necessary to few
The concrete of amount is stirred, and can consume unnecessary energy using large-scale concrete mixer at this time, increases construction cost,
Some pony mixers for occurring on the market are there are the problem of mixing effect is bad, blanking is difficult at present, and these small-sized stirrings
Machine is an integral structure, and transport is inconvenient for use, and motor, which is arranged in stir chamber, easily increases loss.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of novel bridge constructing device, can solve above-mentioned present
The problem of in technology.
The present invention is achieved through the following technical solutions：The present invention a kind of novel bridge constructing device, including by
The fuselage of upper fuselage and lower fuselage composition, the lower fuselage interior are equipped with stir chamber, are equipped in the stir chamber and extend up and down
The agitating shaft of setting, the lower fuselage top surface left and right sides equity are equipped with insertion part, the first motor are equipped in the upper fuselage,
The first electronic motor spindle is connected with rotating speed control machine, and the rotating speed control motor spindle, which is connected with, to be penetrated through on described
Body bottom surface and the first rotation axis of rotatable engagement connection, in the upper fuselage top surface at left and right sides of first rotation axis
Equipped with slot is plugged together with what the insertion part was oppositely arranged, plugged together described in two groups and sealed slide is equipped in the side wall of the opposite side of slot
Slot, each sealed slide slot leave it is described plug together the perforation of slot one side and be equipped with to extend backward the first of setting slide chamber, two groups
Described first slides in the upper fuselage between chamber and slides chamber equipped with second, and first slides chamber and the described second cunning described in two groups
It is connected between an actor's rendering of an operatic tune sides adjacent equipped with via, locking block is equipped in each sealed slide slot, each described first
It slides intracavitary and slides and be connected with the first sliding block, slided in each via and be connected with both sides to the left and right and prolong
The push rod set is opened up, the opposite side of push rod described in two groups reaches described first and slides intracavitary and the institute for sliding intracavitary with described first
The first sliding block to be stated to be fixedly connected, push rod opposite side described in two groups reaches the described second top for sliding intracavitary, and described second
It slides and the first squint face is equipped on each push rod of intracavitary, described second slides below intracavitary equipped with front and rear setting of extending
Spiral shell type bar, spiral shell type line is connected with conflict sliding block on the spiral shell type bar, and the conflict sliding block front end both sides are set respectively
Have to contradict the conflict squint face for sliding cooperation with the first squint face on push rod described in two groups, on front side of the lower fuselage
Face sets fenestrate chamber, and observation window is provided on the window chamber, is hinged on the right side of the observation window by hinge and the lower fuselage, institute
It states and capacity monitoring device is provided in stir chamber.
Preferably technical solution, the first rotation axis bottom are fixed with the card reached outside the upper body bottom surface
Sympodium.
Preferably technical solution, the agitating shaft top penetrates through the lower fuselage top surface and rotatable engagement connects, institute
It states shaft bottom tail end to be connected with the stir chamber inner bottom wall rotatable engagement, is equipped with and uses in tail end side at the top of the agitating shaft
With the slot being connected with the engagement shaft, equity is equipped with downward in the stir chamber inner bottom wall of the agitating shaft both sides
Extend the discharge channel set, and electrically-controlled valve is equipped in each discharge channel, and the agitating shaft outer surface is equipped with paddle.
Preferably technical solution, the lower fuselage bottom both sides equity is equipped with leg, between leg described in two groups
The lower fuselage bottom is equipped with blanking device, and compression pump, each discharge channel bottom extension section are equipped in the blanking device
It is connected with the compression pump, the compression pump bottom is equipped with the blanking groove for penetrating through the blanking device bottom surface and being fixedly connected,
The blanking trench bottom tail end reaches outside the blanking device bottom surface and tail end is connected with notch.
Preferably technical solution, the insertion part is interior to be equipped with locking holes, and opposite side is equal at the top of insertion part described in two groups
Equipped with the second squint face.
Preferably technical solution, the spiral shell type bar rear side end are connected with the second motor, and described second is electronic
Machine outer surface is arranged at described second and slides in chamber rear side inner wall and be fixedly connected, and the spiral shell type bar front side end is slided with described second
An actor's rendering of an operatic tune front inner wall rotatable engagement connects.
Preferably technical solution, each locking block, which leaves, described to be plugged together slot tail end and is equipped with compression spring, Mei Gesuo
It states the first sliding block front end and is fixed with the first guiding block, being connected with leading flank in each first guiding block stretches
The second guiding block being fixedly connected in the sealed slide slot and with the locking block, locking block described in two groups are all provided with to offside
Have respectively contradicting the 3rd squint face of mating connection of sliding with the second squint face in the insertion part of the left and right sides.
Preferably technical solution, the capacity monitoring device include being fixed at the stir chamber right part medial surface
On capacity monitoring device, the capacity monitoring device and flashing lamp are electrically connected, and the flashing lamp is fixed at the upper fuselage
Leading flank bottom.
The beneficial effects of the invention are as follows：
1. being all provided with sealed slide slot in the side wall for plugging together the opposite side of slot by two groups, each sealed slide slot, which leaves, plugs together slot one side
Perforation sets the first of setting of extending backward and slides chamber, and second is set in two group of first upper fuselage slided between chamber and slides chamber, two groups
First, which slides chamber and second, slides to connect between chamber sides adjacent and sets via, is all provided with locking block in each sealed slide slot, often
A first, which slides intracavitary, slides first sliding block that is connected, and mating connection is slided in each via, and both sides are extended to the left and right
The push rod of setting, the opposite side of two groups of push rods, which reaches the first the first sliding block for sliding intracavitary and sliding intracavitary with first and fixes, to be connected
It connects, two groups of push rod opposite sides reach the second top for sliding intracavitary, and second slides first is all provided on each push rod of intracavitary tiltedly
Incline face, second slides the front and rear spiral shell type bar for extending and setting is set below intracavitary, and spiral shell type line, which is connected, on spiral shell type bar contradicts sliding block,
Sliding block front end both sides are contradicted to be set respectively to contradict the conflict squint face for sliding cooperation with the first squint face on two groups of push rods,
So as to fulfill automatic locking installment work, easy disassembly speed improves the whole work efficiency of concrete discharging, dimension easy to disassemble
Shield.
2. it is connected by the lower fuselage top surface of perforation at the top of agitating shaft and rotatable engagement, shaft bottom tail end and stir chamber
Inner bottom wall rotatable engagement connects, and the slot to be connected with engagement shaft, agitating shaft are set in the tail end side of agitating shaft top
Equity sets the discharge channel for extending set downwards in the stir chamber inner bottom wall of both sides, and electrically-controlled valve, agitating shaft are all provided in each discharge channel
Outer surface sets paddle, and so as to automatically control agitating shaft rotation, realization is automatically performed stirring work.
3. setting leg by lower fuselage bottom both sides equity, the lower fuselage bottom between two groups of legs sets blanking device, under
Compression pump is set in material device, each discharge channel bottom extension Duan Junyu compression pumps connection, compression pump bottom sets perforation blanking device
Bottom surface and the blanking groove being fixedly connected, blanking trench bottom tail end reaches outside blanking device bottom surface and tail end mouth of connecting trough, so as to real
Now high speed blanking work improves work efficiency.
4. the configuration of the present invention is simple, easy to operate, automatic locking installation and automatic unlocking dismantlement work can be realized, it is convenient
Demolition and maintenance can realize that automatic uniform speed stirs work, prevent that concrete mixing is uneven, so as to improve blanking efficiency.
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 outside a kind of novel bridge constructing device of the present invention；
Fig. 2 is overall structure diagram inside a kind of novel bridge constructing device of the present invention；
Fig. 3 is the upper fuselage interior top view of the present invention；
Fig. 4 is the conflict sliding block overall structure diagram of the present invention；
Fig. 5 is a kind of structure diagram of the novel bridge constructing device of present invention when installation is complete.
Specific embodiment
As Figure 1-Figure 5, a kind of novel bridge constructing device of the invention, including by 6 groups of upper fuselage 5 and lower fuselage
Into fuselage, the lower fuselage 6 is internally provided with stir chamber 64, the agitating shaft for extending set up and down is equipped in the stir chamber 64
641, lower 6 top surface of the fuselage left and right sides equity is equipped with insertion part 63, and the first motor 52, institute are equipped in the upper fuselage 5
It states 52 bottom of the first motor and is connected with rotating speed control machine 53,53 bottom of rotating speed control machine is connected with perforation institute
State the first rotation axis 54 of 5 bottom surface of fuselage and rotatable engagement connection, the upper machine of 54 left and right sides of the first rotation axis
The side wall for plugging together slot 55,55 opposite side of slot being plugged together described in two groups being oppositely arranged with the insertion part 63 is equipped in 5 top surface of body
Inside be equipped with sealed slide slot 56, each sealed slide slot 56 leave it is described plug together the perforation of 55 one side of slot and be equipped with extend backward
What is set first slides chamber 57, and first slides in the upper fuselage 5 between chamber 57 and slide chamber 58 equipped with second described in two groups, and two
Group described first slides chamber 57 and described second and slides and connect between 58 sides adjacent of chamber equipped with via 59, each described sealed
Locking block 561 is equipped in slide slot 56, each described first slides to slide in chamber 57 and be connected with the first sliding block
571, it is each slided in the via 59 and is connected with the push rod 591 that both sides extension to the left and right is set, push rod described in two groups
It is solid that 591 opposite sides reach the described first first sliding block 571 for sliding in chamber 57 and being slided with described first in chamber 57
Fixed connection, 591 opposite side of push rod described in two groups reach described second and slide top in chamber 58, and described second slides in chamber 58
Each push rod 591 on be equipped with the first squint face 5910, described second, which slides lower section in chamber 58, is equipped with front and rear extension and sets
The spiral shell type bar 581 put, spiral shell type line, which is connected with, on the spiral shell type bar 581 contradicts sliding block 582, the conflict sliding block 582
Front end both sides are respectively equipped with to contradict the conflict for sliding cooperation with the first squint face 5910 on push rod 591 described in two groups
Squint face 5821, lower 6 leading flank of fuselage set fenestrate chamber 601, observation window 602, the sight are provided on the window chamber 601
It is hinged by hinge and the lower fuselage 6 to examine 602 right side of window, capacity monitoring device is provided in the stir chamber 64.
Wherein, 54 bottom of the first rotation axis is fixed with the engagement shaft 541 reached outside 5 bottom surface of upper fuselage.
Wherein, 641 top of agitating shaft penetrates through lower 6 top surface of fuselage and rotatable engagement connects, the agitating shaft 641
Bottom tail end is connected with the 64 inner bottom wall rotatable engagement of stir chamber, in the 641 top tail end side of agitating shaft be equipped with to
The slot 642 being connected with the engagement shaft 541, it is right in 64 inner bottom wall of the stir chamber of 641 both sides of agitating shaft
Deng the discharge channel 644 equipped with setting of extending downwards, electrically-controlled valve 6441, the agitating shaft are equipped in each discharge channel 644
641 outer surfaces are equipped with paddle 643, are rotated so as to automatically control agitating shaft 641, and realization is automatically performed stirring work.
Wherein, 6 two bottom sides of the lower fuselage equity is equipped with leg 61, the lower fuselage between leg 61 described in two groups
6 bottoms are equipped with blanking device 62, and compression pump 622, each 644 bottom extension section of discharge channel are equipped in the blanking device 62
It is connected with the compression pump 622,622 bottom of compression pump is equipped with what is penetrated through 62 bottom surface of blanking device and be fixedly connected
Blanking groove 623, the 623 bottom tail end of blanking groove reaches outside 62 bottom surface of blanking device and tail end is connected with notch 621, from
And realize high speed blanking work, improve work efficiency.
Wherein, locking holes 631 are equipped in the insertion part 63, the opposite side in 63 top of insertion part is equipped with second described in two groups
Sealed, raising installation speed is installed in squint face 632 automatically so as to convenient.
Wherein, 581 rear side end of spiral shell type bar is connected with the second motor 583,583 appearance of the second motor
Face is arranged at described second and slides in 58 rear side inner wall of chamber and be fixedly connected, and 581 front side end of spiral shell type bar is slided with described second
58 front inner wall rotatable engagement of an actor's rendering of an operatic tune connects, so as to fulfill unlock work, maintenance work easy to disassemble is automatically controlled.
Wherein, each locking block 561 leave it is described plug together 55 tail end of slot and be equipped with compression spring 5611, each described first
571 front end of sliding block is fixed with the first guiding block 572, and front side is connected in each first guiding block 572
Face reaches the second guiding block 5612 being fixedly connected in the sealed slide slot 56 and with the locking block 561, lock described in two groups
Block 561 is closed to be equipped with respectively to the second squint face 632 conflict cunning in insertion part 63 described with the left and right sides to offside
The 3rd squint face 5610 that row is connected so as to fulfill automatic locking and resets work.
Wherein, the capacity monitoring device includes the capacity monitoring being fixed on the 64 right part medial surface of stir chamber
Device 640, the capacity monitoring device 640 and flashing lamp 65 are electrically connected, before the flashing lamp 65 is fixed at the upper fuselage 5
Side bottom, when the 64 inner concrete height of stir chamber is less than 640 preset value of capacity monitoring device, the capacity monitoring
Device 640 controls the flashing lamp 65 to light.
During original state, contradict sliding block 582 and be located at second and slide last side position in chamber 58, at this point, locking block 561
It is subject to the conflict power of compression spring 5611, the locking block 561 of 5610 one side of the 3rd squint face is made utmostly to contact at and is plugged together in slot 55,
Meanwhile locking block 561 drives the first guiding block 572 and the first guiding block 572 of the mating connection on the second guiding block 5612
First sliding block 571 of rear side is moved to first and slides 57 inside of chamber, at this point, the first sliding block 571 drives the first squint face
The push rod 591 of 5910 one sides utmostly reaches second and slides in chamber 58, makes 5910 backside segments of the first squint face with contradicting squint
Face 5821, which contradicts, to be connected.
When needing ready-mixed concrete, lower fuselage 6 is moved to the lower position of upper fuselage 5 first, makes lower 6 top left of fuselage
The insertion part 63 of right both sides is in relative status with the slot 55 that plugs together at left and right sides of upper 5 bottom of fuselage, meanwhile, make engagement shaft
541 are in relative status with slot 642, and mobile lower fuselage 6, is gradually inserted the insertion part 63 on lower fuselage 6 then up
It plugs together in slot 55, until the second squint face 632 in insertion part 63 as shown in Figure 5 is with plugging together the 3rd squint face 5610 in slot 55
It abuts against, at this point, continuing to move up lower fuselage 6, the second squint face 632 and the 3rd squint face 5610 is made to contradict and slide cooperation,
At this point, the locking block 561 of both sides respectively overcomes the conflict power of the compression spring 5611 in the sealed slide slot 56 in both sides, make locking block 561
It gradually contradicts and slips into sealed slide slot 56, until when 63 top surface of insertion part as shown in Figure 5 is abutted against with plugging together 55 inner roof wall of slot,
At this point, locking block 561 is contradicted completely in sealed slide slot 56, meanwhile, locking block 561 drives the second guiding block 5612 and the
The first guiding block 572 and the first sliding block 571 on two guiding blocks 5612 are moved to first and slide outermost position in chamber 57
It puts, at this point, 6 top surface of lower fuselage is abutted against with upper 5 bottom surface of fuselage, meanwhile, engagement shaft 541 is made to be fully inserted into slot 642, this
When, by the first sliding block 571 push rod 591 of 5910 one side of the first squint face is driven utmostly to leave second and slided in chamber 58,
Meanwhile the locking block 561 of 5610 one side of locking holes 631 and the 3rd squint face in insertion part 63 is made to be in relative position, at this point,
Since locking block 561 is subject to the conflict power of compression spring 5611, the locking block 561 of 5610 one side of the 3rd squint face is made to contradict into locking holes
In 631, meanwhile, locking block 561 drives the first guiding block 572 and the first leading of the mating connection on the second guiding block 5612
First sliding block 571 of 572 rear side of block is moved to first and slides 57 inside of chamber, at this point, the first sliding block 571 drives the first squint
The push rod 591 of 5910 one side of face utmostly reaches second and slides in chamber 58, makes 5910 backside segments of the first squint face oblique with contradicting
The conflict of face 5821 of inclining is connected, meanwhile, by the first motor 52 the first rotation axis is driven after 53 speed change of rotating speed control machine
54 low speed rotations drive 641 low speed rotation of agitating shaft, so as to fulfill at the uniform velocity stirring by the engagement shaft 541 of 54 bottom of the first rotation axis
Work is mixed, control electrically-controlled valve 6441 and compression pump 622 are opened after the completion of stirring, so as to fulfill concrete automatic blanking work
Make；
When blanking completion needs dismounting, by the second motor 583 spiral shell type bar 581 is driven to rotate first, by 581 band of spiral shell type bar
Dynamic conflict sliding block 582 slides 58 front side direction of chamber along second and moves, at this point, by the conflict squint face in conflict sliding block 582
5821 slide cooperation with the first squint face 5910 conflict on left and right sides push rod 591, at this point, being driven by conflict sliding block 582
Left and right sides push rod 591 is slided in chamber 57 towards first and moved, meanwhile, by push rod 591 the first sliding block 571 and first is driven to slide
The first guiding block 572 on row block 571 slides 57 outside movement of chamber towards first, at this point, the first guiding block 572 drives the second leading
Locking block 561 on 5612 and second guiding block 5612 of block overcomes the conflict power of compression spring 5611, makes the 3rd squint face 5,610 1
The locking block 561 of side gradually slips away and plugs together slot 55, and most front side position in chamber 58 is slided until contradicting sliding block 582 and being moved to second
When putting, at this point, the push rod 591 of 5910 one side of the first squint face is slid completely into via 59, meanwhile, 5610 one side of the 3rd squint face
Locking block 561 completion reach in sealed slide slot 56, move down lower fuselage 6 at this time and dismantlement work can be completed, so as to side
Just later maintenance.
The beneficial effects of the invention are as follows：
1. being all provided with sealed slide slot in the side wall for plugging together the opposite side of slot by two groups, each sealed slide slot, which leaves, plugs together slot one side
Perforation sets the first of setting of extending backward and slides chamber, and second is set in two group of first upper fuselage slided between chamber and slides chamber, two groups
First, which slides chamber and second, slides to connect between chamber sides adjacent and sets via, is all provided with locking block in each sealed slide slot, often
A first, which slides intracavitary, slides first sliding block that is connected, and mating connection is slided in each via, and both sides are extended to the left and right
The push rod of setting, the opposite side of two groups of push rods, which reaches the first the first sliding block for sliding intracavitary and sliding intracavitary with first and fixes, to be connected
It connects, two groups of push rod opposite sides reach the second top for sliding intracavitary, and second slides first is all provided on each push rod of intracavitary tiltedly
Incline face, second slides the front and rear spiral shell type bar for extending and setting is set below intracavitary, and spiral shell type line, which is connected, on spiral shell type bar contradicts sliding block,
Sliding block front end both sides are contradicted to be set respectively to contradict the conflict squint face for sliding cooperation with the first squint face on two groups of push rods,
So as to fulfill automatic locking installment work, easy disassembly speed improves the whole work efficiency of concrete discharging, dimension easy to disassemble
Shield.
2. it is connected by the lower fuselage top surface of perforation at the top of agitating shaft and rotatable engagement, shaft bottom tail end and stir chamber
Inner bottom wall rotatable engagement connects, and the slot to be connected with engagement shaft, agitating shaft are set in the tail end side of agitating shaft top
Equity sets the discharge channel for extending set downwards in the stir chamber inner bottom wall of both sides, and electrically-controlled valve, agitating shaft are all provided in each discharge channel
Outer surface sets paddle, and so as to automatically control agitating shaft rotation, realization is automatically performed stirring work.
3. setting leg by lower fuselage bottom both sides equity, the lower fuselage bottom between two groups of legs sets blanking device, under
Compression pump is set in material device, each discharge channel bottom extension Duan Junyu compression pumps connection, compression pump bottom sets perforation blanking device
Bottom surface and the blanking groove being fixedly connected, blanking trench bottom tail end reaches outside blanking device bottom surface and tail end mouth of connecting trough, so as to real
Now high speed blanking work improves work efficiency.
4. the configuration of the present invention is simple, easy to operate, automatic locking installation and automatic unlocking dismantlement work can be realized, it is convenient
Demolition and maintenance can realize that automatic uniform speed stirs work, prevent that concrete mixing is uneven, so as to improve blanking efficiency.
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 (8)
1. a kind of novel bridge constructing device, including the fuselage being made of upper fuselage and lower fuselage, it is characterised in that：Lower fuselage
Stir chamber is internally provided with, the agitating shaft that upper and lower extension is set is equipped in stir chamber, equity is equipped with slotting at left and right sides of lower fuselage top surface
Component, upper fuselage is interior to be equipped with the first motor, and the first electronic motor spindle is connected with rotating speed control machine, rotating speed control motor spindle
It is connected with and penetrates through the first rotation axis that upper body bottom surface and rotatable engagement connect, the upper fuselage at left and right sides of the first rotation axis
It is equipped in top surface and plugs together slot with what insertion part was oppositely arranged, sealed slide is equipped in two groups of side walls for plugging together the opposite side of slot
Slot, each sealed slide slot, which leaves to plug together the perforation of slot one side and be equipped with to extend backward, the first of setting slides chamber, and two group first is slided
Chamber is slided equipped with second, two group first is slided chamber and second and slide to connect between chamber sides adjacent and set in upper fuselage between chamber
There is via, be equipped with locking block in each sealed slide slot, each first, which slides intracavitary, slides and be connected with first and slide
Block slides in each via and is connected with both sides to the left and right and extends the push rod set, and the opposite side of two groups of push rods reaches the
One slides intracavitary and the first sliding block of intracavitary is slided with first and is fixedly connected, and two groups of push rod opposite sides reach second and slide chamber
Interior top, second slides the first squint face is equipped on each push rod of intracavitary, and second slides front and rear prolongs is equipped with below intracavitary
The spiral shell type bar set is opened up, spiral shell type line is connected with conflict sliding block on spiral shell type bar, contradicts sliding block front end both sides and is respectively equipped with
To contradict the conflict squint face for sliding cooperation with the first squint face on two groups of push rods, lower fuselage leading flank sets fenestrate chamber,
Observation window is provided on window chamber, is hinged on the right side of observation window by hinge and lower fuselage, capacity monitoring device is provided in stir chamber.
2. a kind of novel bridge constructing device according to claim 1, it is characterised in that：The first rotation axis bottom is consolidated
It is fixed to be equipped with the engagement shaft reached outside the upper body bottom surface.
3. a kind of novel bridge constructing device according to claim 2, it is characterised in that：Perforation institute at the top of the agitating shaft
It states lower fuselage top surface and rotatable engagement connects, the shaft bottom tail end is connected with the stir chamber inner bottom wall rotatable engagement,
The slot being connected with the engagement shaft is equipped at the top of the agitating shaft in tail end side, the agitating shaft both sides
Equity is equipped with the discharge channel for extending set downwards in the stir chamber inner bottom wall, and electrically-controlled valve is equipped in each discharge channel,
The agitating shaft outer surface is equipped with paddle.
4. a kind of novel bridge constructing device according to claim 3, it is characterised in that：The lower fuselage bottom both sides pair
Deng equipped with leg, the lower fuselage bottom between leg described in two groups is equipped with blanking device, and pressure is equipped in the blanking device
Power pumps, compression pump connection described in each discharge channel bottom extension Duan Junyu, the compression pump bottom be equipped with penetrate through it is described under
Material device bottom surface and the blanking groove being fixedly connected, the blanking trench bottom tail end is reached outside the blanking device bottom surface and tail end connects
It is connected to notch.
5. a kind of novel bridge constructing device according to claim 1, it is characterised in that：It is equipped in the insertion part sealed
Hole, the opposite side in insertion part top is equipped with the second squint face described in two groups.
6. a kind of novel bridge constructing device according to claim 1, it is characterised in that：The spiral shell type bar rear side end and the
Two motor are connected, and the second motor outer surface is arranged at described second and slides on rear side of chamber in inner wall and fixed connect
It connects, the spiral shell type bar front side end slides chamber front inner wall rotatable engagement with described second and is connected.
7. a kind of novel bridge constructing device according to claim 5, it is characterised in that：Each locking block leaves institute
It states and plugs together slot tail end and be equipped with compression spring, each first sliding block front end is fixed with the first guiding block, and each described the
Leading flank is connected in one guiding block and reaches second be fixedly connected in the sealed slide slot and with the locking block
Guiding block, locking block described in two groups to offside be equipped with respectively to second squint in the insertion part of the left and right sides
Face contradicts the 3rd squint face for sliding mating connection.
8. a kind of novel bridge constructing device according to claim 1, it is characterised in that：The capacity monitoring device includes
The capacity monitoring device being fixed on the stir chamber right part medial surface, the capacity monitoring device and flashing lamp are electrically connected,
The flashing lamp is fixed at the upper fuselage leading flank bottom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710553260.5A CN108086160A (en) | 2017-07-07 | 2017-07-07 | A kind of novel bridge constructing device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710553260.5A CN108086160A (en) | 2017-07-07 | 2017-07-07 | A kind of novel bridge constructing device |
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| CN108086160A true CN108086160A (en) | 2018-05-29 |
Family
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|---|---|---|---|
| CN201710553260.5A Pending CN108086160A (en) | 2017-07-07 | 2017-07-07 | A kind of novel bridge constructing device |
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Application publication date: 20180529 |