CN105403366A - Anti-permeability performance test system for shield tunnel segment circumferential seams - Google Patents
Anti-permeability performance test system for shield tunnel segment circumferential seams Download PDFInfo
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- CN105403366A CN105403366A CN201510610858.4A CN201510610858A CN105403366A CN 105403366 A CN105403366 A CN 105403366A CN 201510610858 A CN201510610858 A CN 201510610858A CN 105403366 A CN105403366 A CN 105403366A
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Abstract
The invention relates to an anti-permeability performance test system for shield tunnel segment circumferential seams. The system comprises a segment test piece positioned in a frame and used for an anti-permeability performance test of the circumferential seams, a water pressure loading assembly including a water supply tank, a hydraulic press, and a water storage tank with a scale connected in sequence via a water pipe, and an observation record sub-assembly including a laser displacement sensor and digital close-range photogrammetric equipment. According to the system, a conventional segment joint mechanical performance test system is employed for loading, a water-resistant performance test of the shield tunnel lining segment circumferential seams is accomplished, the stress and deformation states of the shield tunnel circumferential seams in the practical condition are accurately simulated, the waterproof capability of the shield tunnel circumferential seams in conditions of different opening amounts, dislocation amounts, and opening angles is tested, quantitative reference basis is provided for the seam waterproof fine design of tunnel engineering, the consistency of the manufacturing precision of test segment members and actual tunnel segments and the accuracy of test data are guaranteed, the machining cost of a steel die of the test piece is reduced, and the test time is reduced.
Description
Technical field
The present invention relates to a kind of test unit, especially relate to a kind of duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system.
Background technology
Along with moving forward steadily of China's new round Development of China's Urbanization, urban track traffic has become expansion city physical space, facilitates the important way that the people goes on a journey.And the running tunnel of the system core is handed over as city rail, adopt shield method in a large number.Current shield tunnel lining structure mostly is prefabricated reinforced concrete section of jurisdiction and is spliced by coupling bolt, due to the structural property of segment joint, seam rigidity and bearing capacity are far below the rigidity of section of jurisdiction itself and bearing capacity, it is the stressed weak link in tunnel, especially be in the stratum that this kind of lateral pressure coefficient of muddy soft soil is little, larger seam corner distortion very easily occurs under the impact of periphery engineering activity, seam opens distortion and seam dislocation distortion.
For shield tunnel, percolating water is an outstanding difficult problem for puzzlement structure of the subway safety and normal operation always.Investigation finds, most percolating water all betides segment joint position, and the waterproof sealing of seam generally adopts the elastic sealing gasket be pasted onto near section of jurisdiction extrados to realize.As can be seen here, the anti-permeability performance of tunnel seam is most important for the reliable military service of shield tunnel.The seam of shield tunnel can be divided into longitudinal seam (section of jurisdiction-section of jurisdiction) and hoop seam (Lining Ring-Lining Ring).Therefore, for ensureing the waterproof sealing of shield tunnel in horizontal and vertical two dimensions, need to carry out impervious study mechanism for longitudinal seam and hoop seam respectively.
Make a general survey of domestic and international shield tunnel seam waterproof correlation test device, patent of invention as published in Tongji University---elastic sealing gasket of shield tunnel " yi word pattern " watertightness verifying attachment (CN201010145789), the published utility model patent of Central South University---shield duct piece joint anti-permeability performance test unit (CN104075854A), propose and open rectangular channel separately on upper and lower two pieces of steel cover plates, adopt after elastic sealing gasket being closed into frame-type and be gluingly connected in groove, with bolt, sealing gasket is compressed, pad is utilized to simulate the different joint open of section of jurisdiction, simultaneously at device sidewall mounting limit plate, to simulate the faulting of slab ends situation of section of jurisdiction.Above-mentioned patent is all indoor model tests of small scale, and itself just exists following problems:
1) front duct pieces of shield tunnel is based on prefabricated reinforced concrete section of jurisdiction pattern, adopts steel groove can not reflect the actual contact condition of elastic sealing gasket elastomeric material and concrete groove, thus test findings and the larger discrepancy of engineering physical presence;
2) a large amount of Engineering Projects shows, due to the construction deviation of construction stage duct piece assembling machine, and operation stage soft soil layer the superposition of the multiple factors such as relative settlement, very easily there is the faulting of slab ends amount of 15mm in circumferential weld and circumferential weld, and be limited to the size of cover plate, seam big shearing working condition tests cannot be carried out;
3) adopt bolt presses simulation seam joint open, pad spacing simulation seam faulting of slab ends amount, need manual setting to measure, test accuracy is lower;
4) this patent of invention is positioned the subway tunnel of diameter about the 6m adopting single track elastic sealing gasket waterproof, corresponding cover plate size is less, cannot adopt the waterproof ability of the major diameter cross-river tunnel of more than the diameter 10m of two pass elastic sealing gasket waterproof by scientific evaluation;
5) have ignored the connection of shield tunnel circumferential weld and circumferential weld and the otherness of structure, broadly the impervious condition of two kinds of different seams is lumped together;
6) waterproof ability of actual reinforced concrete segment seam under different open-angle can not be simulated.
7) based on the waterproof test of punching block fixture, cannot the mechanical behavior of simulating reinforced concrete segment joint reality and contact condition.
In addition, by the investigation to domestic and international Patents and document, the test unit that can carry out assay for tunnel circumferential weld waterproof sealing ability is not found.
In sum, in view of duct pieces of shield tunnel seam complexity stress with contact condition; the indoor model test of small scale is difficult to the waterproof sealing mechanism accurately reflecting that it is true and reliable; therefore research and develop duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system, most important for the deep development promoting shield tunnel waterproof technique field.
Summary of the invention
Object of the present invention is exactly provide a kind of duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system of warranty test data accuracy to overcome defect that above-mentioned prior art exists.
Object of the present invention can be achieved through the following technical solutions:
Duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system, comprising:
For the duct piece specimen of circumferential weld anti-permeability performance test, be positioned at framework,
Water hydraulic static pressure loading assembly, comprises the aqua storage tank of supply tank, water pressure engine and the chi with a scale connected successively through water pipe,
Observational record sub-component, comprises laser displacement sensor and Digital Close-range Photogrammetry equipment.
Described duct piece specimen is combined by A type section of jurisdiction and Type B section of jurisdiction and forms,
Described A type section of jurisdiction forms by by the curved bolted two panels section of jurisdiction of hoop, and form longitudinal joint between the interface of two panels section of jurisdiction, section of jurisdiction has longitudinal groove on corresponding contact face, is provided with a circle elastic sealing gasket in longitudinal joint,
Described Type B section of jurisdiction is the section of jurisdiction that two panels passes through longitudinally tiltedly bolt connection A type section of jurisdiction, and form circumferential weld between interface, section of jurisdiction has hoop groove on corresponding surface of contact, is provided with a circle elastic sealing gasket in circumferential weld; The inner ring of this elastic sealing gasket surrounds a hydraulic pressure chamber.
Described Type B section of jurisdiction is provided with the water filling duct with Water hydraulic static pressure loading assembly UNICOM.
It is inner that described water filling duct is embedded in Type B section of jurisdiction, and section of jurisdiction extrados is that water pipe is connected as press water water inlet by bolt hole and Water hydraulic static pressure loading assembly.
Described duct piece specimen arranges hoop groove and longitudinal groove respectively and pastes elastic sealing gasket on circumferential weld and longitudinal joint surface of contact, forms airtight pressure water action space.
Water pipe between the aqua storage tank of described water pressure engine and chi with a scale is provided with valve, and water pipe, being reserved with bolt hole near duct piece specimen side, is connected with water pressure gauge by this bolt hole.
Described laser displacement sensor is connected to the lower surface of framework back timber, the signal output part of this laser displacement sensor is connected with the displacement signal input end loading actuator, the control output end of described loading actuator respectively with X to loading the control input end of actuator, control input end that Y-direction loads actuator and Z-direction load that the control input end of actuator is corresponding to be connected.
Described X loads actuator control duct piece specimen move in three directions to loading actuator, Y-direction loading actuator, Z-direction.
Described Digital Close-range Photogrammetry equipment is made up of two high pixel digital single-lens reflex cameras, tripod and four photograph lamp boxes.
Compared with prior art, the present invention has the following advantages:
1) conventional duct piece connector mechanical property testing system can be utilized to load, complete the water resistance test of shield tunnel lining segment circumferential weld, fully excavate the potentiality of existing testing equipment;
2) the existing punching block of shield tunnel is adopted to carry out the making of developmental tube sheet element, warranty test section of jurisdiction component and actual tunnel section of jurisdiction can not only make the consistance of precision, ensure that the accuracy of test figure, and decrease the punching block processing cost of test specimen, shorten test period;
3) overcome indoor small scale model test and the actual shortcomings such as shield tunnel circumferential weld contact condition is misfitted, precision is low, error is large, test findings is more true and reliable.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is the main TV structure schematic diagram of section of jurisdiction charging assembly;
Fig. 3 is the side-looking structural representation of section of jurisdiction charging assembly;
Fig. 4 is the plan structure schematic diagram of section of jurisdiction charging assembly;
Fig. 5 is the structural representation of duct piece specimen;
Fig. 6 is duct piece specimen A-1 circumferential weld surface of contact schematic diagram (by duct piece specimen B-1 side);
Fig. 7 is duct piece specimen A-1 circumferential weld surface of contact schematic diagram (by duct piece specimen B-2 side);
Fig. 8 is duct piece specimen A-1 longitudinal joint surface of contact schematic diagram;
Fig. 9 is duct piece specimen A-1 intrados schematic diagram;
Figure 10 is duct piece specimen A-2 circumferential weld surface of contact schematic diagram (by duct piece specimen B-1 side);
Figure 11 is duct piece specimen A-2 circumferential weld surface of contact schematic diagram (by duct piece specimen B-2 side);
Figure 12 is duct piece specimen A-2 longitudinal joint surface of contact schematic diagram;
Figure 13 is duct piece specimen A-2 intrados schematic diagram;
Figure 14 is duct piece specimen B-1 circumferential weld surface of contact schematic diagram;
Figure 15 is duct piece specimen B-1 intrados schematic diagram;
Figure 16 is duct piece specimen B-1 side view;
Figure 17 is duct piece specimen B-2 circumferential weld surface of contact schematic diagram;
Figure 18 is duct piece specimen B-2 intrados schematic diagram;
Figure 19 is duct piece specimen B-2 side view.
In figure, the aqua storage tank of 1-duct piece specimen, 101-duct piece specimen A-1,102-duct piece specimen A-2,103-duct piece specimen B-1,104-duct piece specimen B-2,2-supply tank, 3-water pressure engine, 4-valve, 5-chi with a scale, 6-water pressure gauge, 7-framework, 8-X are to loading actuator, 9-Y to loading actuator, 10-Z to loading actuator, 11-digital single-lens reflex camera, 12-photograph lamp box.
Embodiment
Below in conjunction with the drawings and specific embodiments, the present invention is described in detail.
Embodiment
Duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system, its structure as shown in Figure 1, mainly comprise the duct piece specimen 1 for the test of circumferential weld anti-permeability performance, Water hydraulic static pressure loading assembly, mainly comprise the aqua storage tank 5 of supply tank 2, water pressure engine 3, water pressure gauge 6, valve 4 and chi with a scale, Water hydraulic static pressure loading assembly and framework 7 constitute section of jurisdiction charging assembly jointly, as in Figure 2-4.Observational record assembly, mainly comprises laser displacement sensor and Digital Close-range Photogrammetry equipment.Next, above-mentioned each assembly is described in further detail again.
The concrete structure of duct piece specimen 1 as shown in figs. 5-19, duct piece specimen 1 is primarily of the large class composition in A type section of jurisdiction and two, Type B section of jurisdiction, wherein, A type section of jurisdiction is made up of duct piece specimen A-1101, duct piece specimen A-2102, and Type B section of jurisdiction is made up of duct piece specimen B-1103, duct piece specimen B-2104.
Duct piece specimen A-1101, duct piece specimen A-2102 are bolted together by hoop is curved, and form longitudinal joint between the interface of two test sections of jurisdiction, section of jurisdiction has longitudinal groove on corresponding contact face, is provided with a circle elastic sealing gasket in longitudinal joint; Duct piece specimen B-1103, duct piece specimen B-2104 and A type section of jurisdiction are tiltedly bolted together by longitudinal, and and form circumferential weld between the interface of A type section of jurisdiction, section of jurisdiction has hoop groove on corresponding surface of contact, is provided with a circle elastic sealing gasket in circumferential weld; The inner ring of described elastic sealing gasket surrounds a hydraulic pressure chamber, and duct piece specimen B-1103, duct piece specimen B-2104 are provided with water filling duct and are connected with hydraulic pressure chamber, and water filling duct is connected with Water hydraulic static pressure loading assembly.
In Water hydraulic static pressure loading assembly, supply tank 2 is connected with water pressure engine 3 by water pipe, for water pressure engine 3 provides input water; Valve 4 side is connected with water pressure engine 3, and opposite side is connected with the aqua storage tank 5 of chi with a scale; The aqua storage tank 5 of chi with a scale is connected with section of jurisdiction assembly by water pipe; Wherein water pipe is being reserved with bolt hole near assembly side, section of jurisdiction, is connected with water pressure gauge 6 by this bolt hole.
The lower surface of the back timber of framework 7 is provided with the laser displacement sensor of displacement, joint open and open-angle for monitoring section of jurisdiction, the signal output part of laser displacement sensor is connected with the displacement signal input end of data acquisition system (DAS), the control output end of loading control respectively with X to loading the control input end of actuator 8, control input end that Y-direction loads actuator 9 and Z-direction load that the control input end of actuator 10 is corresponding to be connected.Laser displacement sensor adopts triangulation to measure displacement, and precision is high.Digital Close-range Photogrammetry equipment is made up of two high pixel digital single-lens reflex cameras 11, tripod and four photograph lamp boxes 12, adopt high-speed digital camera technique record infiltration phenomenon and infiltration orientation, high-speed digital photograph gathers the overall process that can not only capture percolating water and occur, also observe by comparative analysis the details that naked eyes can not observe, accurate recording Longitudinal Joint between Segments stress deformation opens the destructive process of seepage flow.
The present invention in use, after shield tunnel circumferential weld anti-permeability performance test unit is installed, upper connecting rod is loaded by two Z-directions, two Z-directions load lower link, 1 Z-direction loads actuator and forms the longitudinal axis direction load application of self-balancing reaction frame along lining segment, simulate the longitudinal load that actual shield tunnel lining segment is subject to, top actuator is loaded by 1 Y-direction, vertical force is equally assigned into two vertical uniform load q in middle section of jurisdiction (A type section of jurisdiction) by Y-direction load distribution beam, section of jurisdiction (A type section of jurisdiction) and section of jurisdiction, both sides (duct piece specimen B-1103 in the middle of promoting, duct piece specimen B-2104) there is the changing of the relative positions of certain value, make to produce a known controlled shearing force at circumferential weld place, and to loading actuator, pressure is applied to longitudinal joint by 4 X, seam is made to be in impaction state, and pressurizeed to section of jurisdiction circumferential weld water filling by hydraulic pressure applying subsystem, thus formed with airtight pressure water space in circumferential weld surface of contact, in conjunction with the seam displacement that laser displacement sensor is measured, the changing value of joint open and open-angle, the dynamic realtime state of application digital single-lens reflex camera record loading procedure, the different joint open of shield tunnel circumferential weld is determined with this, waterproof ability under the operating mode such as magnitude of misalignment and open-angle.
Claims (9)
1. duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system, is characterized in that, this pilot system comprises:
For the duct piece specimen of circumferential weld anti-permeability performance test, be positioned at framework,
Water hydraulic static pressure loading assembly, comprises the aqua storage tank of supply tank, water pressure engine and the chi with a scale connected successively through water pipe,
Observational record sub-component, comprises laser displacement sensor and Digital Close-range Photogrammetry equipment.
2. duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system according to claim 1, is characterized in that, described duct piece specimen is combined by A type section of jurisdiction and Type B section of jurisdiction and forms,
Described A type section of jurisdiction forms by by the curved bolted two panels section of jurisdiction of hoop, and form longitudinal joint between the interface of two panels section of jurisdiction, section of jurisdiction has longitudinal groove on corresponding contact face, is provided with a circle elastic sealing gasket in longitudinal joint,
Described Type B section of jurisdiction is that two panels is connected to the section of jurisdiction of both sides, A type section of jurisdiction by longitudinal tiltedly bolt, and form circumferential weld between interface, section of jurisdiction has hoop groove on corresponding surface of contact, is provided with a circle elastic sealing gasket in circumferential weld; The inner ring of this elastic sealing gasket surrounds a hydraulic pressure chamber.
3. duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system according to claim 2, it is characterized in that, described Type B section of jurisdiction is provided with the water filling duct with Water hydraulic static pressure loading assembly UNICOM.
4. duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system according to claim 3, it is characterized in that, it is inner that described water filling duct is embedded in Type B section of jurisdiction, and section of jurisdiction extrados is that water pipe is connected as press water water inlet by bolt hole and Water hydraulic static pressure loading assembly.
5. duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system according to claim 2, it is characterized in that, described duct piece specimen arranges hoop groove and longitudinal groove respectively and pastes elastic sealing gasket on circumferential weld and longitudinal joint surface of contact, forms airtight pressure water action space.
6. duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system according to claim 1, it is characterized in that, water pipe between the aqua storage tank of described water pressure engine and chi with a scale is provided with valve, and water pipe, being reserved with bolt hole near duct piece specimen side, is connected with water pressure gauge by this bolt hole.
7. duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system according to claim 1, it is characterized in that, described laser displacement sensor is connected to the lower surface of framework back timber, the signal output part of this laser displacement sensor is connected with the displacement signal input end loading actuator, the control output end of described loading actuator respectively with X to loading the control input end of actuator, control input end that Y-direction loads actuator and Z-direction load that the control input end of actuator is corresponding to be connected.
8. duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system according to claim 7, is characterized in that, described X loads actuator control duct piece specimen move in three directions to loading actuator, Y-direction loading actuator, Z-direction.
9. duct pieces of shield tunnel circumferential weld anti-permeability performance pilot system according to claim 1, is characterized in that, described Digital Close-range Photogrammetry equipment is made up of two high pixel digital single-lens reflex cameras, tripod and four photograph lamp boxes.
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