CN206752225U - Suspension type erecting machine - Google Patents
Suspension type erecting machine Download PDFInfo
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- CN206752225U CN206752225U CN201720791740.0U CN201720791740U CN206752225U CN 206752225 U CN206752225 U CN 206752225U CN 201720791740 U CN201720791740 U CN 201720791740U CN 206752225 U CN206752225 U CN 206752225U
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- suspension type
- fuselage
- erecting machine
- type erecting
- support frame
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Abstract
The utility model belongs to facilities for transport and communication field, specifically provides a kind of suspension type erecting machine.The utility model is aimed to solve the problem that the problem of causing the environmental disruption and environmental pollution of large area because laying interim transport routes, accumulation material and poured in place concrete when existing suspension type monorail traffic system is built.Suspension type erecting machine of the present utility model includes fuselage, running gear, the first conveying device and the second conveying device.Wherein, running gear sets the top to fuselage, and the length direction walking of the box track girder that can be fixed along having installed of running gear.First conveying device sets the inner bottom part of fuselage in which can walk, for carrying and transporting box track girder to be installed.Second conveying device sets the outer bottom of fuselage in which can walk, for carrying and transporting column to be installed.Therefore, suspension type erecting machine of the present utility model is capable of the transport and installation of the box track girder of complete independently and column, protects the environment in construction area.
Description
Technical field
The utility model belongs to facilities for transport and communication field, specifically provides a kind of suspension type erecting machine.
Background technology
Suspension type monorail traffic system mainly includes box track girder, overhead rail train and the bogie of car.Vehicle turns
The inside of box track girder is arranged on to frame, for driving length direction walking of the overhead rail train along box track girder.Case
Formula track girder is supported in the air by column (steel stake or concrete stake), and the bottom plate of box track girder is provided with groove along its length
Mouthful, the bottom of the bogie of car passes through the notch with being connected at the top of overhead rail train.
Suspension type monorail traffic system is during construction, it is necessary to which supporting equipment column and box track girder are carried out
Transport and lifting.Because suspension type monorail traffic system will generally pass through tourist district, greenery patches, the woods, lawn, farmland, waters etc.
Area will certainly cause the environmental disruption of large area, it is necessary to lay interim transport routes, accumulation material and poured in place concrete
And environmental pollution.
Therefore, this area needs a kind of new spanning equipment for suspension type monorail traffic system to solve above-mentioned ask
Topic.
Utility model content
In order to solve above mentioned problem of the prior art, when being that the existing suspension type monorail traffic system of solution is built
Cause because laying interim transport routes, accumulation material and poured in place concrete the environmental disruption and environmental pollution of large area
Problem, the utility model provide a kind of suspension type erecting machine, and the suspension type erecting machine includes fuselage, is arranged at the fuselage
The running gear at top；The fuselage includes loading the fuselage body of first object object, conveyed along the fuselage length direction
First conveying device of the first object object；First conveying device is arranged at the fuselage body inner bottom part；It is described
Running gear includes road wheel, the drive device for driving road wheel, attachment means；The road wheel can be placed at box
In track girder；The drive device can drive rail of the road wheel along the box track girder in the box track girder
Walk in road direction；The running gear is connected by the attachment means with the fuselage.
In the optimal technical scheme of above-mentioned suspension type erecting machine, the suspension type erecting machine also includes telescopic nose girder；
The telescopic nose girder is installed in the bottom of the fuselage body, can be stretched along the fuselage length direction；It is described telescopic
When nose girder is in extended configuration, one end of its length direction is connected with one end of the fuselage body length direction, and described
The road wheel of one conveying device can walk on the telescopic nose girder.
In the optimal technical scheme of above-mentioned suspension type erecting machine, the telescopic nose girder is additionally provided with support frame；The branch
Support provides support force when the telescopic nose girder is in extended configuration for the telescopic nose girder.
In the optimal technical scheme of above-mentioned suspension type erecting machine, one end of support frame as described above is filled by being pivotally connected mode
Located at the telescopic nose girder.
In the optimal technical scheme of above-mentioned suspension type erecting machine, set between support frame as described above and the telescopic nose girder
There is closing device, for controlling support frame as described above to open or withdrawing.
In the optimal technical scheme of above-mentioned suspension type erecting machine, the closing device is motor, hydraulic motor or hydraulic pressure
Cylinder.
In the optimal technical scheme of above-mentioned suspension type erecting machine, support frame as described above is one, and the support frame is stretched with described
The pivot section of contracting formula nose girder is arranged on one end away from the fuselage under the telescopic nose girder extended configuration.
In the optimal technical scheme of above-mentioned suspension type erecting machine, support frame as described above is multiple, and the support frame is stretched with described
The pivot section of contracting formula nose girder is disposed on the telescopic nose girder bottom.
In the optimal technical scheme of above-mentioned suspension type erecting machine, support frame as described above includes support frame body, height is adjusted
Device；The arrangement for adjusting height is used for the height for adjusting support frame as described above.
In the optimal technical scheme of above-mentioned suspension type erecting machine, the telescopic nose girder top dress is additionally provided with lifting dress
Put, for lifting the first object object to object height.
In the optimal technical scheme of above-mentioned suspension type erecting machine, the lifting device at least two.
In the optimal technical scheme of above-mentioned suspension type erecting machine, the suspension type erecting machine also includes being arranged at the machine
Second conveying device of body body outer bottom；Second conveying device is used to hang the second target object, and by described second
Target object conveys along the fuselage length direction.
In the optimal technical scheme of above-mentioned suspension type erecting machine, balance weight mechanism is additionally provided with the fuselage, described
When telescopic nose girder stretches out the fuselage body, the center of gravity that the balance weight mechanism is used to make the suspension type erecting machine is in the machine
In the length range of body body.
It will be appreciated to those of skill in the art that in optimal technical scheme of the present utility model, by fuselage sheet
The top of body sets running gear, the rail that the road wheel of the running gear can be placed in the box track girder that installation fixes
On road so that running gear can drive fuselage body along the length direction walking for having installed the box track girder fixed.Enter
One step, the inner bottom part of fuselage body is provided with the first conveying device, first conveying device can carry and along fuselage body
Length direction conveying first object object.First object object is preferably box track girder to be installed, therefore, this practicality
New suspension type erecting machine can receive box track girder to be installed by the first conveying device, can by running gear
Box track girder to be installed is transported along the length direction for having installed the box track girder fixed, faced so as to avoid
When transport routes construction, saved construction cost, protected the environment in construction area.
Further, by setting the second conveying device in the outer bottom of fuselage body, second conveying device is used to hang
And convey the second target object along the length direction of fuselage body.Second target object is preferably column to be installed, therefore
Suspension type erecting machine of the present utility model can receive column to be installed by the second conveying device, can by running gear
Column to be installed is transported along the length direction for having installed the box track girder fixed, so as to avoid interim transport
The construction of road, has saved construction cost, protects the environment in construction area.
Further, when telescopic nose girder is in extended configuration, one end and the fuselage body length direction of its length direction
One end connection so that the road wheel of the first conveying device can walk on telescopic nose girder.By on telescopic nose girder
Box track girder to be installed can be lifted to the position being aligned with having installed the box track girder fixed by lifting device, from
And box track girder to be installed is subjected to installation fixation.Support force is provided for telescopic nose girder by support frame, prevents from stretching
Formula nose girder is bent over deforming.Therefore, being capable of the box track girder of complete independently and vertical by suspension type erecting machine of the present utility model
The transport of post, and the installation of complete independently box track girder to be installed are fixed.
Scheme 1, a kind of suspension type erecting machine, it is characterised in that the suspension type erecting machine include fuselage, be arranged at it is described
The running gear of fuselage roof；
The fuselage includes loading the fuselage body of first object object, conveys described first along the fuselage length direction
First conveying device of target object；First conveying device is arranged at the fuselage body inner bottom part；
The running gear includes road wheel, the drive device for driving road wheel, attachment means；The road wheel energy
Enough it is placed in box track girder；The drive device can drive the road wheel in the box track girder along the case
The orbital direction walking of formula track girder；The running gear is connected by the attachment means with the fuselage.
Scheme 2, the suspension type erecting machine according to scheme 1, it is characterised in that the suspension type erecting machine also includes stretching
Contracting formula nose girder；The telescopic nose girder is installed in the bottom of the fuselage body, can be stretched along the fuselage length direction；
When the telescopic nose girder is in extended configuration, one end of its length direction and the fuselage body length direction
One end connects, and the road wheel of first conveying device can walk on the telescopic nose girder.
Scheme 3, the suspension type erecting machine according to scheme 2, it is characterised in that the telescopic nose girder is additionally provided with support
Frame；Support frame as described above provides support force when the telescopic nose girder is in extended configuration for the telescopic nose girder.
Scheme 4, the suspension type erecting machine according to scheme 3, it is characterised in that one end of support frame as described above passes through pivot
Connected mode is installed in the telescopic nose girder.
Scheme 5, the suspension type erecting machine according to scheme 4, it is characterised in that support frame as described above telescopic is led with described
Closing device is provided between beam, for controlling support frame as described above to open or withdrawing.
Scheme 6, the suspension type erecting machine according to scheme 4, it is characterised in that the closing device is motor, hydraulic pressure
Motor or hydraulic cylinder.
Scheme 7, the suspension type erecting machine according to any one of scheme 4-6, it is characterised in that support frame as described above one
Individual, the pivot section of the support frame and the telescopic nose girder is arranged under the telescopic nose girder extended configuration away from described
One end of fuselage.
Scheme 8, the suspension type erecting machine according to any one of scheme 4-6, it is characterised in that support frame as described above is more
Individual, the pivot section of the support frame and the telescopic nose girder is disposed on the telescopic nose girder bottom.
Scheme 9, the suspension type erecting machine according to any one of scheme 3-6, it is characterised in that support frame as described above includes
Support frame body, arrangement for adjusting height；The arrangement for adjusting height is used for the height for adjusting support frame as described above.
Scheme 10, the suspension type erecting machine according to any one of scheme 2-6, it is characterised in that described telescopic to lead
Beam top dress is additionally provided with lifting device, for lifting the first object object to object height.
Scheme 11, the suspension type erecting machine according to scheme 2, it is characterised in that the lifting device at least two.
Scheme 12, the suspension type erecting machine according to any one of scheme 1-6, it is characterised in that the suspension type frame
Beam machine also includes the second conveying device for being arranged at the fuselage body outer bottom；Second conveying device is used to hang second
Target object, and second target object is conveyed along the fuselage length direction.
Scheme 13, the suspension type erecting machine according to any one of scheme 1-6, it is characterised in that on the fuselage also
Balance weight mechanism is provided with, when the telescopic nose girder stretches out the fuselage body, the balance weight mechanism is used to make the suspension
The center of gravity of formula erecting machine is in the length range of the fuselage body.
Brief description of the drawings
Preferred embodiment of the present utility model described with reference to the accompanying drawings, in accompanying drawing：
Fig. 1 is the first isometric side view of suspension type erecting machine of the present utility model；
Fig. 2 is the second isometric side view of suspension type erecting machine of the present utility model；
Fig. 3 is effect diagram when suspension type erecting machine of the present utility model transports box track girder；
Fig. 4 is effect diagram of the box track girder when being moved on suspension type erecting machine；
Isometric view when Fig. 5 is suspension type erecting machine transport Y type columns of the present utility model；
Fig. 6 is the rearview of the suspension type erecting machine in Fig. 5；
Fig. 7 is sectional view of the suspension type erecting machine along A-A directions in Fig. 6.
Reference numerals list：
1st, fuselage；11st, inner orbit；12nd, outside track；2nd, running gear；21st, road wheel；22nd, directive wheel；3rd, it is telescopic to lead
Beam；31st, extension rail；32nd, governor motion；4th, support frame；41st, hydraulic cylinder；51st, the first box track girder；52nd, the second box rail
Road beam；6th, the second conveying device；61st, the second road wheel；7th, Y types column.
Embodiment
It will be apparent to a skilled person that these embodiments are used only for explaining that technology of the present utility model is former
Reason, is not intended to limit the scope of protection of the utility model.Although for example, it is to close by a certain percentage between each part in accompanying drawing
What system drew, but this proportionate relationship is not unalterable, those skilled in the art can make adjustment to it as needed,
To adapt to specific application scenario, the technical scheme after adjustment will fall into the scope of protection of the utility model.
It should be noted that in description of the present utility model, term " " center ", " on ", " under ", it is "left", "right", " perpendicular
Directly ", the direction of instruction such as " level ", " interior ", " outer " or the term of position relationship are closed based on direction shown in the drawings or position
System, this is intended merely to facilitate description, rather than instruction or hint described device or element must have specific orientation, Yi Te
Fixed azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.In addition, term " first ", " second ",
" the 3rd " is only used for describing purpose, and it is not intended that instruction or hint relative importance.
In addition it is also necessary to explanation, in description of the present utility model, unless otherwise clearly defined and limited, art
Language " installation ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or
It is integrally connected；Can be joined directly together, can also be indirectly connected by intermediary, can be the company of two element internals
It is logical.To those skilled in the art, concrete meaning of the above-mentioned term in the utility model can be understood as the case may be.
As depicted in figs. 1 and 2, suspension type erecting machine of the present utility model mainly includes fuselage (not indicated in figure) and set
In the running gear 2 of fuselage roof.Wherein, fuselage mainly includes the conveying device (not shown) of fuselage body 1 and first again.
The top of fuselage body 1 is fixedly connected with running gear 2, and the running gear 2 is used to drive fuselage body 1 to walk.Fuselage body 1
Inner bottom part be provided with two it is parallel or be similar to parallel inner orbit 11, the first conveying device is arranged at two inner orbits
On 11.It should be noted that fixed to the running gear 2 on fuselage body 1 and the first conveying device set to inner orbit 11
Can be any amount, for example, one, two, four etc..It will be apparent to a skilled person that the knot of fuselage body 1
Configuration shape is not limited only to a kind of form shown in Fig. 1, and it can also be made as other any feasible planforms, example
Such as, external circumferential is welded with the square tubular structure of floor.
As shown in figure 1, running gear 2 mainly includes bogie (not indicated in figure), road wheel 21, directive wheel 22, driving
Device (not shown) and attachment means (not shown).Wherein, bogie is fixed by attachment means and fuselage body 1
Connection, it will be apparent to a skilled person that attachment means can any can be fixed bogie and fuselage body 1
The structure connected together, such as be provided with the steel construction of multiple mounting holes, make attachment means respectively with bogie and fuselage sheet
Body 1 is bolted.It will be appreciated to those of skill in the art that it can also be used between bogie and fuselage body 1
He is secured together any feasible connected mode, such as bolt connection, welds, is integrally formed.Road wheel 21 and bogie
It is pivotally connected, and road wheel 21 being capable of driven device driving rotation.Directive wheel 22 is pivotally connected with bogie, for row
The direction of travel of walking apparatus 2 guides.In a kind of feasible embodiment, the road wheel of running gear 2 of the present utility model
21 and directive wheel 22 be placed in the box track girder of suspension type monorail traffic system.Specifically, the walking of the both sides of running gear 2
21 bottom plate respectively with box track girder of wheel is in rolling contact, the directive wheels 22 of the both sides of running gear 2 respectively with box track girder
Two side plates are in rolling contact.In the presence of drive device (such as motor and hydraulic motor), road wheel 21 can be along box rail
The length direction of road beam rolls, and then drives running gear 2 to walk.
Although not showed that in figure, the first conveying device includes the first carrying platform, the first road wheel and first is led
To wheel.Wherein, the first road wheel and the first directive wheel are pivotally connected with the first carrying platform respectively, the first carrying platform both sides
First road wheel is in rolling contact with two inner orbits 11 respectively, the first directive wheel of the first carrying platform both sides respectively with fuselage sheet
Two side plates of body 1 are in rolling contact.In the presence of the drive motor of the first conveying device, the first road wheel can be along inner orbit
11 length direction rolls, and then drives the walking of the first conveying device.In addition, those skilled in the art can also be as needed,
Appropriate adjustment is carried out to the planform of the first conveying device, for example, the first road wheel is arranged to rail wheel, and correspondingly
The track that inner orbit 11 is arranged to match with the rail wheel.In a kind of feasible embodiment, the first conveying device is used to hold
Carry and transport the box track girder as first object object.
Further, although not showed that in figure, suspension type erecting machine of the present utility model also includes lifting device, should
Lifting device is used to the box track girder of above-mentioned first conveying device conveying giving rise to default height.In addition, the lifting fills
Put and be also similarly set on two inner orbits 11 with the first conveying device.Specifically, the lifting device include lifting mechanism,
Road wheel and directive wheel.Wherein, the road wheel and the directive wheel are pivotally connected with lifting mechanism respectively, the row of lifting mechanism both sides
Walk wheel to be in rolling contact with two inner orbits 11 respectively, the directive wheels of lifting mechanism both sides two side plates with fuselage body 1 respectively
It is in rolling contact.In the presence of the drive motor of lifting device, road wheel can roll along the length direction of inner orbit 11, and then
Drive lifting device walking.In addition, those skilled in the art can also be as needed, the planform of lifting device is fitted
When adjustment, for example, the road wheel of lifting device is arranged into rail wheel, and correspondingly inner orbit 11 is arranged to and the track
Take turns the track of matching.
In addition to the said structure of lifting device, those skilled in the art can also be as needed, by lifting device and
One conveying device is arranged to an entirety.Exemplarily, lifting mechanism is set on the architecture basics of the first conveying device, be used for
Lift box track girder.Further, the lifting mechanism can be any mechanism that can realize lifting function, such as scissor-type is lifted
The machine of liter.
With continued reference to Fig. 1 and Fig. 2, suspension type erecting machine of the present utility model also includes telescopic nose girder 3.This is telescopic to lead
Beam 3 is slidably connected with fuselage body 1, it will be apparent to a skilled person that between telescopic nose girder 3 and fuselage body 1
It can be slidably connected to together using any connected mode, for example, being fixedly installed slide rail on fuselage body 1, make to stretch
Formula nose girder 3 is slidably connected with the slide rail.Further, telescopic nose girder 3 is in the presence of itself drive mechanism (such as motor), energy
Enough length directions along fuselage body 1 slide, until skidding off fuselage body 1.Further, in order to prevent telescopic nose girder 3 from
Slipped on fuselage body 1, limited position mechanism (not shown) is set between telescopic nose girder 3 and fuselage body 1, for limiting
Telescopic nose girder 3 relative to fuselage body 1 sliding length.
Fig. 1 and Fig. 2 are further regarded to, telescopic nose girder 3 includes two parallel extension rails 31 and governor motion 32.Adjust
Mechanism 32 is saved to be used to adjust the distance between two extension rails 31.In a kind of feasible embodiment, governor motion 32 includes
Motor and by motor-driven two screw rods, wherein one end of a screw rod is connected with an extension rail 31, wherein another
One end of screw rod is connected with another extension rail 31.The rotation of screw rod is driven by the rotation of motor, and then changes two and prolongs
Stretch the distance between track 31.After telescopic nose girder 3 stretches out fuselage body 1, motor drives two screw rod synchronous axial systems, makes two
Individual extension rail 31 is aligned with two inner orbits 11 respectively.When telescopic nose girder 3 needs retraction fuselage body 1, motor driving
Two screw rods in opposite direction, synchronously rotate, and two extension rails 31 is offseted each other.In addition those skilled in the art go back
Can be as needed, appropriate adjustment is carried out to the structure of above-mentioned governor motion 32, to be applicable specific application scenario, adjustment
Technical scheme afterwards will fall into the scope of protection of the utility model without deviating from technical principle of the present utility model.
Referring again to Fig. 1 and Fig. 2, one end of telescopic nose girder 3 is provided with support frame 4.Fuselage is stretched out in telescopic nose girder 3
Afterwards, the support frame 4 is used for support telescopic formula nose girder 3.Preferably, support frame 4 is pivotally connected with telescopic nose girder 3, specifically, branch
Rotating shaft (not indicated in figure) between support 4 and telescopic nose girder 3 by being used as pivot section is pivotally attached to together.Or
Those skilled in the art can also be as needed, and support frame 4 and telescopic nose girder 3 are connected into one using other connected modes
Rise, for example, make support frame 4 perpendicular to or be similar to vertically be fixedly attached together with telescopic nose girder 3.Need what is illustrated
It is that the quantity of support frame 4 is not limited only to one shown in Fig. 1 and Fig. 2, those skilled in the art can be according to being actually needed and will prop up
Support 4 is arranged to any number of, and the plurality of support frame 4 is arranged equally spaced to the bottom of telescopic nose girder 3.
Fig. 1 and Fig. 2 are further regarded to, support frame 4 mainly includes support frame body (not indicated in figure) and height regulation dress
Put and (do not indicated in figure).One end of support frame body is pivotally connected with telescopic nose girder 3, the other end and the height of support frame body
Adjusting means is fixedly connected, and the arrangement for adjusting height is used for the height for adjusting support frame 4.In optimization technique side of the present utility model
In case, arrangement for adjusting height is hydraulic cylinder 41, and the length of cylinder barrel is stretched out by changing the upper piston rod of hydraulic cylinder 41, can change liquid
The entire length of cylinder pressure 41.And then the in the vertical direction of support frame 4 can be adjusted by changing the entire length of hydraulic cylinder 41
Highly, so as to adjusting the levelness of telescopic nose girder 3.It will be apparent to a skilled person that support frame 4 is with stretching
Any feasible closing device driving support frame 4 can be used to rotate around the shaft between formula nose girder 3 makes support frame 4 be opened or receive
Return, for example, making rotating shaft be fixedly connected with support frame 4, rotating shaft is pivotally connected with telescopic nose girder 3, pass through motor or hydraulic pressure horse
Rotated up to drive shaft, and then drive support frame 4 to rotate；Or the bottom of the cylinder barrel of hydraulic cylinder and telescopic nose girder 3 are pivoted
Connection, the top of the piston rod of hydraulic cylinder and the support frame body of support frame 4 are pivotally connected, and stretch out cylinder by changing piston rod
The length of cylinder drives the support frame 4 to rotate around the axis.
The operation principle of suspension type erecting machine of the present utility model is described in detail with reference to Fig. 3 and Fig. 4.
It should be noted that the box track girder at the top of Fig. 3 and Fig. 4 middle fuselages body 1 is to have installed the first case fixed before this
The box track girder of formula track girder 51, the inside of Fig. 3 and Fig. 4 middle fuselages body 1 or the top of telescopic nose girder 3 is to be installed second
Box track girder 52.
As shown in figure 3, before suspension type erecting machine transports the second box track girder 52, can by the first conveying device and
The outside conveying arrangement (such as crane) being engaged with the first conveying device transports the second box track girder 52 to fuselage sheet
The inside of body 1.Then, running gear 2 drives length direction walking of the suspension type erecting machine along the first box track girder 51, until
Untill the end (front end of the first box track girder 51 in such as Fig. 3) for running to the first box track girder 51.
As shown in figure 4, when suspension type erecting machine is moved to the end of the first box track girder 51, telescopic nose girder 3 exists
In the presence of itself drive mechanism, fuselage body 1 is skidded off along the length direction of the first box track girder 51.When telescopic nose girder 3
After skidding off fuselage body 1, adjustment structure 32 drive two extension rails 31 be located remotely from each other, until two extension rails 31 respectively with
Untill two inner orbits 11 alignment of the bottom of fuselage body 1.During telescopic nose girder 3 skids off fuselage body 1, Huo Zhe
During two extension rails 31 are located remotely from each other, or after extension rail 32 and inner orbit 31 are aligned, support frame 4 rotates
Axle rotates, until support frame 4 is vertical with horizontal direction or close to vertical.Now, the piston rod of hydraulic cylinder 41 stretches out cylinder barrel, makes
The bottom of hydraulic cylinder 41 contacts with ground, and adjusts telescopic nose girder 3, makes extension rail 32 and the keep level of inner orbit 31 or connects
It is bordering on level.Then, the first conveying device drives length side of the second box track girder 52 along inner orbit 31 and extension rail 32
To walking.When the second box track girder 52 is transferred to predetermined position, the lifting mechanism of the first conveying device is by the second case
Formula track girder 52 lifts, and makes the left end pair of the first box track girder 51 in the right-hand member and Fig. 4 of the second box track girder 52 in Fig. 4
Standard, the left end of the second box track girder 52 in Fig. 4 is set to be aligned with column, and then by bolt by the two of the second box track girder 52
End is fixedly connected with the first box track girder 51 and column respectively.It should be noted that in the lifting mechanism of the first conveying device
During being lifted to the second box track girder 52, and ensure the second box track girder 52 both ends respectively with the first box rail
In the case that road beam 51 and column are respectively aligned to, the second box track girder 52 can be made horizontal or there is a clamp with horizontal direction
Angle, such as when laying box track girder on inclined ramp.
In addition, in order to ensure the smooth installation of the second box track girder 52, the support frame 4 under working condition is located at the first case
Between formula track girder 51 and column, i.e., the second box track girder 52 is in vacant state close to one end of column.
Further, in order to ensure the stability of suspension type erecting machine of the present utility model, suspension type frame of the present utility model
Beam machine also includes balance weight mechanism, and the counter weight construction is arranged in fuselage body 1.When telescopic nose girder 3 stretches out fuselage body 1,
The center of gravity that balance weight mechanism is used to make suspension type erecting machine is in the length range of fuselage body 1.
It will be appreciated to those of skill in the art that suspension type erecting machine of the present utility model can not only complete box rail
The transport of road beam, moreover it is possible to which box track girder to be installed is completed by telescopic nose girder 3, the conveying device of support frame 4 and first
Installation.Therefore, in the process of construction of box track girder, laying can be avoided to face by suspension type erecting machine of the present utility model
When transport routes, accumulation material, and then avoid the destruction and pollution of environment in construction area.
Further, those skilled in the art can also be as needed, and the second conveying device 6 is set on fuselage body 1, is used for
The second target object is conveyed, in preferred embodiment of the present utility model, the second target object is that transport suspension formula single track is handed over
The column of way system.In a kind of feasible embodiment, as shown in Figures 5 to 7, the bottom outside of fuselage body 1 is provided with outside
Track 12.The top of second conveying device 6 is provided with the second road wheel 61, and the second road wheel 61 is in rolling contact with outside track 12.
In other words, the second conveying device 6 be arranged on fuselage body 1 lower section and can be along the length direction row of fuselage body 1
Walk.Further, brake gear is additionally provided with the second conveying device 6, the brake gear is used to fill the second conveying under normality
6 are put to be relatively fixed with fuselage body 1.Further, the bottom of the second conveying device 6 is provided with fixing device and (not marked in figure
Show), the fixing device is used to column (Y types column 7 as shown in Figure 5) being fixed to the second conveying device 6, and then makes this
The suspension type erecting machine of utility model can transport to Y types column 7.It is similar with the first conveying device, extension rail 31
It by governor motion 32, can be aligned with outside track 12, enable the second conveying device 6 along extension rail 31 that Y types column 7 is defeated
Deliver to and position is fixedly mounted.The Y types column 7 for being transported to fixed installation position can be fixed by auxiliary equipment (such as crane)
It is installed on ground.
In another feasible embodiment, those skilled in the art can also suitably adjust the structure of support frame 4, make Y types
Column 7 can pass through among support frame 4.Specifically, second conveying in left side in the left end and Fig. 5 of Y types column 7 in Fig. 5 is made
Device 6 is pivotally connected, and second conveying device 6 on right side in the right-hand member and Fig. 5 of Y types column 7 in Fig. 5 is connected by wire harness, should
One end of wire harness is fixedly connected with the right-hand member of Y types column 7, and the other end of the wire harness is wound into Wire harness box, the Wire harness box with
Second conveying device 6 on right side is fixedly connected in Fig. 5.When Y types column 7 is delivered to, and position is fixedly mounted, the other end of wire harness
It is slowly released from Wire harness box, the right-hand member of Y types column 7 can turn around the hub switch side in the left side of Y types column 7 under gravity
It is dynamic, untill the right-hand member of Y types column 7 contacts with the fixed position on ground.Now Y types column 7 is fixed on ground.This
Art personnel are, it is understood that because Y types column 7 can pass through among support frame 4, so being consolidated in Y types column 7
During determining to ground, support frame 4 will not hinder Y types column 7.Further, by adjusting the second conveying device 6 in outside track
Position on 12, the relative distance of fixed position on Y types column 7 and ground can also be adjusted, to ensure that Y types column 7 can be by
It is installed on fixed position predetermined on ground.It should be noted that although the work of the utility model suspension type erecting machine is former
Reason is illustrated with Y types column 7, but the utility model suspension type erecting machine can also be applied to other structures type
Column, such as inverted L shape column.
Therefore, suspension type erecting machine of the present utility model can not only complete the transport and erection of box track girder, moreover it is possible to
The transport and erection of column are enough completed, the interim transport routes of laying, accumulation material is avoided relative to prior art, protects and apply
Environment in the domain of work area.
It should be noted that running gear 2, the first conveying device and the second conveying device 6 are preferably both provided with braking
Device, in order to make suspension type erecting machine of the present utility model rest in any position installed in the box track girder fixed
Put, the optional position for making the first conveying device and the second conveying device 6 rest on the length direction of fuselage body 1.The brake fills
It can be any form of brake to put, such as hypervelocity brake and power interruption braking device.
So far, combined preferred embodiment shown in the drawings describes the technical solution of the utility model, still, this
Art personnel are it is easily understood that the scope of protection of the utility model is expressly not limited to these embodiments.
On the premise of principle of the present utility model, those skilled in the art can make equivalent change to correlation technique feature
Or replace, the technical scheme after these are changed or replaced it is fallen within the scope of protection of the utility model.
Claims (13)
1. a kind of suspension type erecting machine, it is characterised in that the suspension type erecting machine includes fuselage, is arranged at the fuselage roof
Running gear；
The fuselage includes loading the fuselage body of first object object, conveys the first object along the fuselage length direction
First conveying device of object；First conveying device is arranged at the fuselage body inner bottom part；
The running gear includes road wheel, the drive device for driving road wheel, attachment means；The road wheel can be by
It is placed in box track girder；The drive device can drive the road wheel in the box track girder along the box rail
The orbital direction walking of road beam；The running gear is connected by the attachment means with the fuselage.
2. suspension type erecting machine according to claim 1, it is characterised in that the suspension type erecting machine also includes telescopic
Nose girder；The telescopic nose girder is installed in the bottom of the fuselage body, can be stretched along the fuselage length direction；
When the telescopic nose girder is in extended configuration, one end of its length direction and one end of the fuselage body length direction
Connection, and the road wheel of first conveying device can walk on the telescopic nose girder.
3. suspension type erecting machine according to claim 2, it is characterised in that the telescopic nose girder is additionally provided with support frame；
Support frame as described above provides support force when the telescopic nose girder is in extended configuration for the telescopic nose girder.
4. suspension type erecting machine according to claim 3, it is characterised in that one end of support frame as described above is by being pivotally connected
Mode is installed in the telescopic nose girder.
5. suspension type erecting machine according to claim 4, it is characterised in that support frame as described above and the telescopic nose girder it
Between be provided with closing device, for control support frame as described above open or withdraw.
6. suspension type erecting machine according to claim 5, it is characterised in that the closing device is motor, hydraulic motor
Or hydraulic cylinder.
7. the suspension type erecting machine according to any one of claim 4-6, it is characterised in that support frame as described above is one,
The pivot section of the support frame and the telescopic nose girder is arranged under the telescopic nose girder extended configuration away from the machine
One end of body.
8. the suspension type erecting machine according to any one of claim 4-6, it is characterised in that support frame as described above to be multiple,
The pivot section of the support frame and the telescopic nose girder is disposed on the telescopic nose girder bottom.
9. the suspension type erecting machine according to any one of claim 3-6, it is characterised in that support frame as described above includes support
Frame body, arrangement for adjusting height；The arrangement for adjusting height is used for the height for adjusting support frame as described above.
10. the suspension type erecting machine according to any one of claim 2-6, it is characterised in that on the telescopic nose girder
Portion's dress is additionally provided with lifting device, for lifting the first object object to object height.
11. suspension type erecting machine according to claim 10, it is characterised in that the lifting device at least two.
12. the suspension type erecting machine according to any one of claim 1-6, it is characterised in that the suspension type erecting machine
Also include the second conveying device for being arranged at the fuselage body outer bottom；Second conveying device is used to hang the second target
Object, and second target object is conveyed along the fuselage length direction.
13. the suspension type erecting machine according to any one of claim 1-6, it is characterised in that also set up on the fuselage
There is balance weight mechanism, when the telescopic nose girder stretches out the fuselage body, the balance weight mechanism is used to make the suspension type frame
The center of gravity of beam machine is in the length range of the fuselage body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720791740.0U CN206752225U (en) | 2017-07-02 | 2017-07-02 | Suspension type erecting machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720791740.0U CN206752225U (en) | 2017-07-02 | 2017-07-02 | Suspension type erecting machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206752225U true CN206752225U (en) | 2017-12-15 |
Family
ID=60622581
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720791740.0U Withdrawn - After Issue CN206752225U (en) | 2017-07-02 | 2017-07-02 | Suspension type erecting machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206752225U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107254815A (en) * | 2017-07-02 | 2017-10-17 | 中建空列（北京）科技有限公司 | Suspension type erecting machine |
| CN109677860A (en) * | 2019-02-23 | 2019-04-26 | 谢力 | Overhead rail train rail docking facilities |
-
2017
- 2017-07-02 CN CN201720791740.0U patent/CN206752225U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107254815A (en) * | 2017-07-02 | 2017-10-17 | 中建空列（北京）科技有限公司 | Suspension type erecting machine |
| CN107254815B (en) * | 2017-07-02 | 2018-05-22 | 中建空列（北京）科技有限公司 | Suspension type erecting machine |
| CN109677860A (en) * | 2019-02-23 | 2019-04-26 | 谢力 | Overhead rail train rail docking facilities |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20171215 Effective date of abandoning: 20180522 |