CN207882081U - Shield duct piece mechanical simulation test device - Google Patents
Shield duct piece mechanical simulation test device Download PDFInfo
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- CN207882081U CN207882081U CN201820026238.5U CN201820026238U CN207882081U CN 207882081 U CN207882081 U CN 207882081U CN 201820026238 U CN201820026238 U CN 201820026238U CN 207882081 U CN207882081 U CN 207882081U
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- 238000009434 installation Methods 0.000 claims abstract description 12
- 230000008901 benefit Effects 0.000 claims description 3
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Abstract
The utility model provides a kind of shield duct piece mechanical simulation test device, including main body reaction frame, radial loaded mechanism and expansion carrier beam, the radial loaded mechanism includes installation end and elongated end, the radial loaded mechanism can carry out angle offset fine tuning to the adjustable inner wall for being installed on the main body reaction frame of the installation end in same sagittal plane relative to a certain radial direction in turn, the elongated end adjustably stretches or extends to the center of the main body reaction frame relative to the installation end, it is described to expand carrier beam along the axial setting of shield duct piece and be removably mounted to the elongated end, radial load is transferred to by the radial loaded mechanism applies radial load to the expansion carrier beam by the expansion carrier beam outer wall of shield duct piece.The utility model it is multidirectional load be accurately oriented to by way of the mechanical behavior of shield duct piece is simulated, to improve the quality and efficiency of shield tunnel full scale test.
Description
Technical field
The utility model belongs to Tunnel Engineering technical field, is related to a kind of shield duct piece mechanical simulation test device.
Background technology
With the development of urban track traffic, Shield-bored tunnels are asked in construction with all kinds of safety encountered during one's term of military service
Topic also receives more and more extensive concern.
For Shield-bored tunnels because of the periphery construction disturbance that encounters or because structure itself carries in Different Strata condition
Performance change and the lotus that occurs becomes phenomenon, need the lotus that accurate simulation goes out shield tunnel to become process, and to the synthesis of tunnel segment structure
Mechanical property situation carries out the research of regularity, to preferably safeguard the structure safety of shield tunnel, extends shield tunnel
Service life.
For this purpose, being mainly engaged in correlative study using the methods of numerical simulation, scale (model) test and full scale test both at home and abroad.
Then, exist between the model and actual object of numerical simulation and hand over big difference, when structure generates large deformation and has destruction trend, number
The result that value calculates is difficult to reflect truth；Scale (model) test has relatively flexible feature, but by cast material
Can limitation, also tend to that there are larger differences between test structure and truth.Thus, full scale test has been increasingly becoming research shield
The important directions of structure section of jurisdiction mechanical property.
For full scale test, the structural behaviour of counterforce device and the reasonability of load mode are that can experiment preferably mould
The key of quasi- tunnel actual loading situation.Due to shield structure can be made to generate enough deformations so that load when destroying compared with
Greatly, it is therefore desirable to there is the counterforce device of sufficient intensity and rigidity to be supported.
Currently, the counterforce device of Tunnel Engineering technical field shield tunnel full scale test generally comprises counter force wall, horizontal right
Anchor cable, bar is drawn to add center drum and vertical loading frame etc..However, counter-force wall loading device occupied space is big, underaction,
It does not simply fail to adapt to the different shield duct piece of radius, and wall damage can be generated when load is larger；Level is to drawing anchor cable formula
Counterforce device generates pressure by anchor cable to being pulled in shield duct piece surface, but this pressure is smaller and can not flexibly change；Bar adds
Bar is passed through shield duct piece by center circle cartridge type counterforce device, generates the pressure to shield duct piece by the pulling force of bar, while in circle
Self-balancing is realized at cylinder, but such device can generate shield duct piece destruction, the load-carrying properties of the section of jurisdiction of reduction cause experiment to be tied
Fruit is inaccurate；Vertical loading frame considers the gravity of shield duct piece itself, but structure can not be in stable equilibrium state, add
It will produce impact force action during carrying, increase the extent of the destruction to section of jurisdiction, cause test result inaccurate.In addition, testing
In, when shield duct piece load is larger, big radial deformation and the existing shield tunnel foot of tangential deformation can occur for structure
Ruler experimental rig can not keep the stability in load direction and the accuracy of load in this condition.
Therefore, it is necessary to research and develop a kind of new with the polycyclic shield mechanical simulation test device of combined type being accurately oriented to.
Utility model content
To overcome the defects of present in the prior art, a kind of shield duct piece mechanical simulation test device is now provided, by more
The mechanical behavior of shield duct piece is simulated with the mode being accurately oriented to load, to improve the matter of shield tunnel full scale test
Amount and efficiency.
To achieve the above object, the solution of the utility model is：A kind of shield duct piece mechanical simulation test dress is provided
It sets, including main body reaction frame, radial loaded mechanism and expansion carrier beam, the radial loaded mechanism includes installation end and extension
End, the radial loaded mechanism can be in same radial direction in turn for the adjustable inner wall for being installed on the main body reaction frame of the installation end
Carry out angle offset fine tuning relative to a certain radial direction in plane, the elongated end relative to the installation end adjustably to
The center of the main body reaction frame is flexible or extends, described to expand carrier beam along the axial setting of shield duct piece and be removably mounted to institute
Elongated end is stated, it will be radial by the expansion carrier beam by radial loaded mechanism applies radial load to the expansion carrier beam
Load is transferred to the outer wall of shield duct piece.
Preferably, the main body reaction frame includes upper and lower spaced multilayer counter-force ring element, the adjacent counter-force ring
It is connected by more spaced columns between unit, oblique rib is equipped between two columns and is supportted, multiple radial loadeds
Mechanism is uniformly distributed in the inner wall of each layer counter-force ring element.
Preferably, the counter-force ring element includes outer wall edge of a wing ring, inner wall edge of a wing ring and web connection ring, the web
Connection ring is fixed between outer wall edge of a wing ring and inner wall edge of a wing ring, and the web connection ring includes combinable multistage
Web semi-ring, adjacent two sections of web semi-rings coordinate high-strength bolt seamless spliced by arc pressuring plate.
Preferably, each radial loaded mechanism includes jack base, radial jack, cantilever and adjusts support
Arm, the radial direction jack are pivotably installed on the inner wall of the counter-force ring element, two institutes by the jack base
It states cantilever and is fixed on the jack base and respectively along the both sides of the radial jack and extend outwardly, the length of the cantilever
Degree offers sliding slot on direction, and the adjusting support arm includes fixed part and extension, and the fixed part is arranged in the cunning
In slot and then telescopic slide is adjusted along the cantilever in the adjusting support arm, and the expansion carrier beam is installed and connected in the extension
Portion.
Preferably, the jack base includes bottom plate, support ear, shaft, sleeve and connecting piece for lengthening, the bottom plate
It is fastened by bolts in the inner wall of the counter-force ring element, the support ear is fixedly arranged on the bottom plate, and the shaft is arranged in
On the support ear, the sleeve is movably set in the shaft, and one end of the connecting piece for lengthening is fixed in the sleeve
Outer surface, the flange in the bottom of the other end of the connecting piece for lengthening and the radial jack is fastenedly connected, and then the diameter
To jack shaft rotation is finely adjusted around the shaft.
Preferably, the radial jack is connected with hydraulic-pressure control apparatus control, and the hydraulic-pressure control apparatus includes pressure
Control pump, oil pipe, oil path distributor, hand control valve and pressure retaining valve, the pressure control pump by the oil pipe respectively with
The hand control valve, the pressure retaining valve and oil path distributor control connection, each radial jack pass through institute
It states oil pipe to connect with oil path distributor control, oil is provided to the entire hydraulic-pressure control apparatus by the pressure control pump
It presses and simultaneously provides pressure control in the initial oil transportation stage, by the hand control valve to the oil pipe hierarchical loading and benefit/unload
Pressure.
Preferably, the expansion carrier beam is I-beam, is located between the flange plate for expanding carrier beam described in different height equipped with multiple
Deep floor is installed with support shaft under the deep floor, card slot mouth is offered on the extension for adjusting support arm,
The support shaft fixing card is set to the card slot mouth and then the expansion carrier beam is installed on described in both sides and adjusts on support arm and with institute
It states and adjusts support arm adjusting radial position.
Being preferably located between the flange plate for expanding carrier beam described in different height uniformly distributed has rubber sheet gasket for uniformly passing
Pass the load force suffered by the flange plate of outside in the expansion carrier beam.
Preferably, including multiple axially loaded mechanisms, each axially loaded mechanism are held on the shield duct piece axis
Upward upper edge and lower edge applies xial feed in turn, has uniform intervals between the two neighboring axially loaded mechanism；Institute
It includes upper load plate and lower load plate to state axially loaded mechanism, is rigidly connected between the upper load plate and the lower load plate
And form grasping part for being clamped two edge up and down of the shield duct piece, the upper load plate be equipped with vertical jack for
The upper edge of shield duct piece described in top pressure, the lower load board clamping contact at the lower edge of the shield duct piece.
Preferably, include the multiple section of jurisdiction slide carriage mechanisms for supplying to be supported under the shield duct piece, the section of jurisdiction slide carriage mechanism
Including bearing seat, sliding rail and slide plate, the sliding rail is fixedly arranged on along its length on the bearing seat, and the slide plate is slidedly arranged on institute
It states on the sliding rail of bearing seat, the slide plate is held on the bottom of the shield duct piece and then the radial direction along shield duct piece
Sliding.
The advantageous effect of the utility model shield duct piece mechanical simulation test device includes：
1) experimental rig is composed of a variety of duplicate components, on the one hand can carry out more ring shield pipes by assembling
On the other hand the full scale test of piece can be repaired and be renewed to experimental rig by dismounting, the spirit of experimental rig is kept with this
Activity and durability；
2) monocycle main body counter-force annulus unit has sufficiently large intensity and rigidity, and structure size is according to monocycle shield pipe
Worst load of piece under the conditions of limiting damage is designed, by the deformation and the stress that control main body counter-force annulus unit
State ensures that structure has 2.5 times or more of safety coefficient, maximum distortion is no more than 10mm, it can be achieved that right in safe range
The shield lining structure of domestic and international common-size carries out overall process load up to limiting damage, and is in self-balancing during the test
State；
3) hydraulic jack is installed on by flange on main body counter-force annulus unit every 15 °, can arbitrarily be dismantled, be maintained
Test the flexibility of load mode；And by way of directly being loaded on the outside of shield duct piece, it ensure that the initial of section of jurisdiction
Non-destructive；
4) finder charge reaches slidingtype expansion carrier beam by hydraulic jack, then uniform in the mode of flexible contact by rubber pad
Ground is transmitted on shield duct piece, and developmental tube piece load can be made to be closer to true stratum load；
5) allow thousand when tangential deformation occurs for section of jurisdiction by the rotating mechanism being arranged in each hydraulic jack top/bottom part
The rotation of jin top to ensure equipment safety, while may make jack top to eliminate the tangential force effect that section of jurisdiction tangential deformation is brought
Force direction is always perpendicular to section of jurisdiction surface.
6) by using hydraulic pump control pressure under lower pressure and using manual fine control valve tune under condition of high voltage
The combination control method for saving hydraulic pressure, realize stablize under lower pressure, quick accurately controlling under load and condition of high voltage
It is required that improving the control ability to finder charge.
Description of the drawings
Fig. 1 is the overall structure diagram of the utility model shield duct piece mechanical simulation test device；
Fig. 2 is the structural schematic diagram corresponding to counter-force ring element in Fig. 1；
Fig. 3 is the side structure schematic diagram corresponding to Fig. 1；
Fig. 4 is the enlarged structure schematic diagram corresponding to radial load maintainer in Fig. 1；
Fig. 5 shows the enlarged structure schematic diagram of a-quadrant to be enclosed corresponding to dotted line in Fig. 1；
The structural schematic diagram for the hydraulic loaded equipment that Fig. 6 is connected by the utility model jack；
Fig. 7 is to expand the structural schematic diagram that carrier beam is connect with radial loaded mechanism corresponding to slidingtype in Fig. 1；
Fig. 8 shows the side enlarged structure schematic diagram of B area to be enclosed corresponding to dotted line in Fig. 7；
Fig. 9 is corresponding to the overlooking structure diagram under Fig. 1 practical application trystates；
Figure 10 is the application structure signal of axial load maintainer in the utility model shield duct piece mechanical simulation test device
Figure；
Figure 11 is the structural schematic diagram of section of jurisdiction slide carriage mechanism in the utility model shield duct piece mechanical simulation test device；
Figure 12 is the use state diagram corresponding to Figure 11.
Specific implementation mode
The utility model is further illustrated below in conjunction with the embodiment shown in that figure.
As shown in Figure 1, the utility model provides firstly a kind of shield duct piece mechanical simulation test device, as shown in Figure 1,
Utility model device includes main body reaction frame 99, attached connecting component, radial loaded mechanism 98, hydraulic loaded equipment, sliding
Formula expands carrier beam 19 and axial (vertical) load maintainer.Specifically：
As shown in Fig. 2, the main body reaction frame 99 includes upper and lower spaced multilayer counter-force ring element 1, as undertaking
The agent structure of finder charge and the basis for connecting other component are connected by column between the adjacent counter-force ring element 1,
Multiple radial loaded mechanisms 98 are uniformly distributed in the inner wall of each layer counter-force ring element 1.Each main body counter-force annulus list
Member 1 is by vertical 3 blocking steel-casting of edge of a wing portion annulus (the two edges of a wing portion annulus of a horizontal web portion annulus 2 and two
3 respectively as main body counter-force annulus unit 1 inner and outer wall), then by playing bolt on steel-casting and main ring connecting plate 4
Eight block casting steel parts are spliced by hole by high-strength bolt 5, and cross section is in " I-shaped " type, and this section structure is when being pressurized
It is the most advantageous.Main body counter-force annulus unit 1 is the agent structure for undertaking finder charge, and monocycle main body counter-force annulus unit 1 undertakes
The finder charge of monocycle shield duct piece, worst lotus of the structure size according to monocycle shield duct piece under the conditions of limiting damage
Load is designed, and the load under the conditions of limiting damage is carried out according to domestic and international full scale test result combination numerical simulation calculation result
Value.By testing main body counter-force annulus unit 1, the deformation of control main body counter-force annulus unit 1 exists with stress
In safe range, ensure that structure has 2.5 times or more of safety coefficient, maximum distortion is no more than 10mm, it can be achieved that domestic and international
The shield lining structure of common-size carries out overall process load up to limiting damage, and is in self-balancing state during the test.
Meanwhile main body counter-force annulus unit 1 also as connection other component and undertakes the foundation structure of its weight.
As shown in figure 3, for tricyclic main body counter-force annulus unit 1 to be connected into the reaction frame 99 of an entirety, and realize each
It is organically combined between component, plays respective specific function, the present apparatus devises numerous attached connecting components：Vertical upright column 6
Assume responsibility for main body counter-force annulus unit 1 and dead weight that is being connected to other component on annulus, oblique rib support 7 strengthen multiple circles
Multiple main body counter-force annulus units 1 are connected into an entirety, and ensure to finish by the bonding strength of interannular, the two collective effect
The globality of structure, wherein being set between two main body counter-force annulus units 1 every 15 °, there are one vertical upright columns 6, and there are two connecting
Oblique rib supports 7, and 24 vertical upright columns 6 and 48 oblique ribs supports 7 are equipped between arbitrary two rings main body counter-force annulus unit 1.
In conjunction with shown in Fig. 2 and Fig. 4, each radial loaded mechanism 98 include jack base 8, hydraulic jack 10,
Cantilever 11 and adjusting support arm 13, in vertical edge of a wing portion, the madial wall of annulus 3 is uniformly distributed several jack bases 8, very heavy
The installation site of pedestal 8 is pushed up in the surface or underface of vertical force column, 15 ° is spaced, passes through among each jack base
There are one hydraulic jacks 10 for the connection of flange 9, and are welded with a pair of of connecting cantilever 11 in the both sides of jack base, each outstanding
Sliding slot 12 is provided with by fluting on arm 11, each sliding slot 12 is interior, and there are one support arm 13, slidingtypes by bolt fastening installation
Expand carrier beam 19 to be installed at the outermost end card slot mouth 130 of support arm 13, it can by adjusting depth of the support arm 13 in sliding slot 12
To change the initial position that slidingtype expands carrier beam 19.
As shown in figure 5, the pedestal 8 in each hydraulic jack 10 is the rotating mechanism that shaft rotation fine tuning can be achieved, the rotation
Mechanism includes jack extension element 24, shaft 25, sleeve 32 and support ear 26, to form jack base 8.Jack lengthens
Part 24 is connect with jack flange 9, and various sizes of section of jurisdiction experiment can be matched by changing its length, such as can be by subtracting
The size of small jack extension element 24 matches the section of jurisdiction of outer diameter bigger, is matched by increasing the size of jack extension element 24
The smaller section of jurisdiction of outer diameter is to meet experiment demand；Support ear 26 is installed on by bolt on main body counter-force annulus unit 1；Sleeve
32 are welded on jack extension element 24, by support ear 26 and sleeve 32 it is embedded turn to take out 25 with realize rotating mechanism with
The connection of main body counter-force annulus unit 1.50 tons of shear load can be carried by turning pumping 25, allowed jack 10 to rotate, worked as pipe
When tangential deformation occurs for piece, the tangential force effect eliminated section of jurisdiction tangential deformation and brought can be rotated by jack 10, is set with ensureing
Standby safety, while may make jack top force direction always perpendicular to section of jurisdiction surface.
As shown in fig. 6, to accurately control the pressure of hydraulic jack 10, utility model device further includes that hydraulic loaded is set
Standby 97, the hydraulic loaded equipment 97 include pressure control pump 14, oil pipe 15, oil path distributor 16, precise manual control valve 17,
Pressure retaining valve 18.According to structural load model, actual formation is divided into multigroup lotuses such as vertical load, side load and shoulder load
It carries, multigroup load is taken compared with being close in actual formation as principle with internal force with the deformation of Control experiment load lower structure
Value, while it is different groups to divide hydraulic jack 10 according to load grouping, every group of jack 10 passes through oil path distributor 16 and oil
Pipe 15 is connected to pressure control pump 14, and same group 10 pressure change process of hydraulic jack is completely the same during ensure that experiment.
According to the difference to stratum Load Simulation fineness, hydraulic jack 10 lay interval can from 15 ° to 180 ° between arbitrarily adjust, adjust
It is 15 ° to save scale division value.Pressure control pump 14 is responsible for providing oil pressure to a whole set of hydraulic test, and provides pressure in the initial oil transportation stage
Control.Pressure retaining valve 18 has the function of ensureing that existing oil pressure does not decline, realizes and test the steady of graded loading test pressure process
It is fixed.After oil pressure is gradually increased, controlling oil pressure by pressure control pump 14 can become difficult, and be changed to through precise manual control valve
17 realize high-precision, the hierarchical loading of small magnitude and benefit/release, realize the Precise control of complete test process.
In conjunction with shown in Fig. 4, Fig. 7 and 8, slidingtype expand carrier beam 19 by standard system I-beam, I-beam reinforcing plate 20 and
Rubber sheet gasket 21 forms.When experiment, the piston top of hydraulic jack 10 acts on slidingtype along the radial direction of shield duct piece
Expand on the anchor tip 101 of carrier beam 19, the corresponding contact of piston top and anchor tip 101 can preferably accurate jack
Active position between 10 and expansion carrier beam 19 expands carrier beam 19 by slidingtype and converts the load of hydraulic jack 10 to
Load is evenly applied to 22 outside of experiment section of jurisdiction by cloth load, then the rubber pad 21 by closely testing the end installation of section of jurisdiction 22, is protected
Demonstrate,proved slidingtype expand between carrier beam 19 and experiment shield duct piece uniform flexible contact, to more truly simulating shield duct piece
Stressing conditions in actual formation.Meanwhile when hydraulic jack 10 applies pressure, the elongation of piston top, slidingtype, which expands, to be carried
Beam 19 realizes sliding by supporting slide-bar 23 to be mounted in the card slot mouth 130 of support arm 13, to which slidingtype expands carrier beam
19 is common mobile with the piston top of jack 10, ensure that finder charge continues, steadily acts on shield duct piece.
As shown in figure 9, when being tested, this experimental rig need to be located to the outside of subjects, i.e., will test shield
Section of jurisdiction 22 surrounds.Before experiment, need to assemble entire experimental rig, a whole set of experimental rig is kept flat on the ground.Experiment
When, mainly load counter-force is provided by counter-force ring element 1.
As shown in Figure 10, it is more fully to be further applied load to shield duct piece 22, the experimental rig of the utility model further includes
Axially loaded mechanism 27, for simulating the longitudinal restraint force effect between section of jurisdiction, which includes vertical jack
28, connection screw thread bar 29, top load plate 30 and lower part load plate 31.Altogether experiment is distributed in equipped with 6 axially loaded mechanisms 27
Section of jurisdiction 22, experiment section of jurisdiction 22 is between top load plate 30 and lower part load plate 31, when vertical jack 28 provides pressure,
29 tension of connection screw thread bar, to be converted into the vertical pressure to testing section of jurisdiction 22 of top load plate 30 and lower part load plate 31
Power, for simulating longitudinal restraint force effect between section of jurisdiction.
As is illustrated by figs. 11 and 12, for the utility model above-mentioned purpose, the experimental rig of the utility model is better achieved
Further include for being uniformly distributed and being supported in multiple section of jurisdiction slide carriage mechanisms 50 under the shield duct piece 22, the section of jurisdiction slide carriage mechanism
50 include bearing seat 52, sliding rail 54 and slide plate 56, and the sliding rail 54 is fixedly arranged on along its length on the bearing seat 52, described
Slide plate 56 is slidedly arranged on the sliding rail 54 of the bearing seat 52, the slide plate 56 be held on the bottom of the shield duct piece 22 into
And it is slided along the radial direction of shield duct piece 22.When in use, first experiment section of jurisdiction is positioned on slide plate 56, and bearing seat 52
Lie against ground, slide plate 56 and sliding rail 54 are steel material, and between contact surface coating butter to reduce frictional force, sliding rail 54
It for steel rail material and pours in the bearing seat 52 of concrete material, by 12 uniformly distributed support carriers bearing test sections of jurisdiction
Weight.With this, when shield duct piece 22 receives load and is deformed or when displacement, shield duct piece 22 every sky in ground without with
Ground generates friction, and then horizontal friction force when effectively reducing section of jurisdiction stress deformation, makes section of jurisdiction stress closer to true
Layer on the spot.
After completing above-mentioned implementation process, the utility model following characteristics should be able to be embodied：
Utility model device can be simulated accurately logical for the full scale test of the shield duct piece of domestic and international common-size
The real processes of complicated mechanical change occur under the conditions of Different Strata for the shield duct piece of the difference assembly form such as seam, fissure of displacement, and
Being precisely controlled for finder charge can be realized in the case where experiment section of jurisdiction tends to the trystate destroyed, ensure that the safety of experimental rig
Property, it obtains more accurate data for experiment and provides sufficient guarantee.
This reality can be understood and applied the above description of the embodiments is intended to facilitate those skilled in the art
With novel.Person skilled in the art obviously easily can make various modifications to these embodiments, and saying herein
Bright General Principle is applied in other embodiment without having to go through creative labor.Therefore, the utility model is not limited to
Embodiment is stated, those skilled in the art's announcement according to the present utility model does not depart from the improvement that the utility model scope is made
It should be all within the protection scope of the utility model with modification.
Claims (10)
1. a kind of shield duct piece mechanical simulation test device, it is characterised in that：Including main body reaction frame, radial loaded mechanism and
Expand carrier beam, the radial loaded mechanism includes installation end and elongated end, and the installation end is adjustable, and to be installed on the main body anti-
The radial loaded mechanism can be inclined relative to a certain radial direction progress angle in same sagittal plane in turn for the inner wall of power frame
Fine tuning is moved, the elongated end adjustably stretches to the center of the main body reaction frame or extends, institute relative to the installation end
It states and expands carrier beam along the axial setting of shield duct piece and be removably mounted to the elongated end, by the radial loaded mechanism to institute
It states and expands the outer wall that carrier beam applies radial load and then radial load is transferred to shield duct piece by the expansion carrier beam.
2. shield duct piece mechanical simulation test device according to claim 1, it is characterised in that：The main body reaction frame packet
Spaced multilayer counter-force ring element up and down is included, is connected by more spaced columns between the adjacent counter-force ring element
It connects, oblique rib is equipped between two columns and is supportted, multiple radial loaded mechanisms are uniformly distributed in each layer counter-force ring element
Inner wall.
3. shield duct piece mechanical simulation test device according to claim 2, it is characterised in that：The counter-force ring element packet
Outer wall edge of a wing ring, inner wall edge of a wing ring and web connection ring are included, the web connection ring is fixed in outer wall edge of a wing ring and institute
Between stating inner wall edge of a wing ring, the web connection ring includes combinable multistage web semi-ring, adjacent two sections of web semi-rings
Coordinate high-strength bolt seamless spliced by arc pressuring plate.
4. shield duct piece mechanical simulation test device according to claim 3, it is characterised in that：Each radial loaded
Mechanism includes jack base, radial jack, cantilever and adjusts support arm, and the radial direction jack passes through the jack
Pedestal is pivotably installed on the inner wall of the counter-force ring element, and two cantilevers are fixed on the jack base and divide
Do not extend outwardly along the both sides of the radial jack, sliding slot, the adjusting support are offered on the length direction of the cantilever
Arm includes fixed part and extension, and the fixed part is arranged in the sliding slot and then the adjusting support arm is along the cantilever
Adjustable telescopic slide, the expansion carrier beam are installed and connected in the extension.
5. shield duct piece mechanical simulation test device according to claim 4, it is characterised in that：The jack base packet
Bottom plate, support ear, shaft, sleeve and connecting piece for lengthening are included, the bottom plate is fastened by bolts in the counter-force ring element
Inner wall, the support ear are fixedly arranged on the bottom plate, and the shaft is arranged on the support ear, and the sleeve is movably set in
In the shaft, one end of the connecting piece for lengthening is fixed in the outer surface of the sleeve, the other end of the connecting piece for lengthening
It is fastenedly connected with the flange in the bottom of the radial jack, and then the radial jack is finely adjusted shaft rotation around the shaft.
6. shield duct piece mechanical simulation test device according to claim 4, it is characterised in that：It is described radial direction jack with
Hydraulic-pressure control apparatus control connection, the hydraulic-pressure control apparatus include pressure control pump, oil pipe, oil path distributor, manually control
Valve and pressure retaining valve, the pressure control pump by the oil pipe respectively with the hand control valve, the pressure retaining valve and institute
Oil path distributor control connection is stated, each radial jack is connected by the oil pipe and oil path distributor control,
Oil pressure is provided to the entire hydraulic-pressure control apparatus and provide pressure control in the initial oil transportation stage by the pressure control pump,
By the hand control valve to the oil pipe hierarchical loading and benefit/release.
7. shield duct piece mechanical simulation test device according to claim 4, it is characterised in that：The expansion carrier beam is I-shaped
Beam is equipped with multiple deep floors between the flange plate for expanding carrier beam described in different height, branch is installed under the deep floor
Axis is supportted, card slot mouth is offered on the extension for adjusting support arm, the support shaft fixing card is set to the card slot mouth
And then the expansion carrier beam is installed on described in both sides and adjusts on support arm and adjust radial position with the adjusting support arm.
8. shield duct piece mechanical simulation test device according to claim 7, it is characterised in that：Described in different height
It is uniformly distributed between the flange plate of expansion carrier beam to have rubber sheet gasket for uniformly transferring the outside flange plate institute in the expansion carrier beam
The load force being subject to.
9. shield duct piece mechanical simulation test device according to any one of claims 1 to 8, it is characterised in that：Including multiple
Axially loaded mechanism, the upper edge and lower edge that each axially loaded mechanism is held in the shield duct piece axial direction apply in turn
Xial feed has uniform intervals between the two neighboring axially loaded mechanism；The axially loaded mechanism includes upper load
Plate and lower load plate are rigidly connected between the upper load plate and the lower load plate and form grasping part for institute is clamped
State two edge up and down of shield duct piece, the upper load plate is equipped with vertical jack for the upper edge of shield duct piece described in top pressure,
The lower load board clamping contacts at the lower edge of the shield duct piece.
10. shield duct piece mechanical simulation test device according to any one of claims 1 to 8, it is characterised in that：Including for branch
Supportting multiple section of jurisdiction slide carriage mechanisms under the shield duct piece, the section of jurisdiction slide carriage mechanism includes bearing seat, sliding rail and slide plate,
The sliding rail is fixedly arranged on along its length on the bearing seat, and the slide plate is slidedly arranged on the sliding rail of the bearing seat, institute
Slide plate is stated to be held on the bottom of the shield duct piece and then slide along the radial direction of the shield duct piece.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820026238.5U CN207882081U (en) | 2018-01-08 | 2018-01-08 | Shield duct piece mechanical simulation test device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820026238.5U CN207882081U (en) | 2018-01-08 | 2018-01-08 | Shield duct piece mechanical simulation test device |
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| CN207882081U true CN207882081U (en) | 2018-09-18 |
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| CN201820026238.5U Expired - Fee Related CN207882081U (en) | 2018-01-08 | 2018-01-08 | Shield duct piece mechanical simulation test device |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108344637A (en) * | 2018-01-08 | 2018-07-31 | 同济大学 | Shield duct piece mechanical simulation test device |
| CN109459311A (en) * | 2018-12-19 | 2019-03-12 | 中国地质大学（武汉） | A kind of experimental provision for simulating pipe ring stress deformation in tunnel under different stress conditions |
| CN110645015A (en) * | 2019-09-28 | 2020-01-03 | 同济大学 | Shield tunnel segment joint test model with different rigidity under positive and negative bending moment |
| CN113008685A (en) * | 2021-02-25 | 2021-06-22 | 中国矿业大学 | Multipoint loading self-balancing counter force system with adjustable loading position and implementation method |
| CN117907109A (en) * | 2023-12-27 | 2024-04-19 | 山东大学 | Self-adaptive circumferential mechanical loading system |
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2018
- 2018-01-08 CN CN201820026238.5U patent/CN207882081U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108344637A (en) * | 2018-01-08 | 2018-07-31 | 同济大学 | Shield duct piece mechanical simulation test device |
| CN108344637B (en) * | 2018-01-08 | 2024-04-26 | 同济大学 | Shield segment mechanics simulation test device |
| CN109459311A (en) * | 2018-12-19 | 2019-03-12 | 中国地质大学（武汉） | A kind of experimental provision for simulating pipe ring stress deformation in tunnel under different stress conditions |
| CN109459311B (en) * | 2018-12-19 | 2024-02-27 | 中国地质大学（武汉） | Experimental device for tunnel pipe ring atress warp under simulation different atress conditions |
| CN110645015A (en) * | 2019-09-28 | 2020-01-03 | 同济大学 | Shield tunnel segment joint test model with different rigidity under positive and negative bending moment |
| CN113008685A (en) * | 2021-02-25 | 2021-06-22 | 中国矿业大学 | Multipoint loading self-balancing counter force system with adjustable loading position and implementation method |
| CN113008685B (en) * | 2021-02-25 | 2022-05-17 | 中国矿业大学 | Multipoint loading self-balancing counter force system with adjustable loading position |
| CN117907109A (en) * | 2023-12-27 | 2024-04-19 | 山东大学 | Self-adaptive circumferential mechanical loading system |
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