CN111810173A - Construction method for synchronizing shield tunneling and segment splicing - Google Patents
Construction method for synchronizing shield tunneling and segment splicing Download PDFInfo
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- CN111810173A CN111810173A CN202010720574.1A CN202010720574A CN111810173A CN 111810173 A CN111810173 A CN 111810173A CN 202010720574 A CN202010720574 A CN 202010720574A CN 111810173 A CN111810173 A CN 111810173A
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- 238000010276 construction Methods 0.000 title claims abstract description 40
- 230000005641 tunneling Effects 0.000 title claims abstract description 33
- 230000006837 decompression Effects 0.000 claims description 38
- 230000001360 synchronised effect Effects 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 8
- 230000008569 process Effects 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 9
- 238000004364 calculation method Methods 0.000 description 3
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- NMFHJNAPXOMSRX-PUPDPRJKSA-N [(1r)-3-(3,4-dimethoxyphenyl)-1-[3-(2-morpholin-4-ylethoxy)phenyl]propyl] (2s)-1-[(2s)-2-(3,4,5-trimethoxyphenyl)butanoyl]piperidine-2-carboxylate Chemical compound C([C@@H](OC(=O)[C@@H]1CCCCN1C(=O)[C@@H](CC)C=1C=C(OC)C(OC)=C(OC)C=1)C=1C=C(OCCN2CCOCC2)C=CC=1)CC1=CC=C(OC)C(OC)=C1 NMFHJNAPXOMSRX-PUPDPRJKSA-N 0.000 description 1
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- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21D—SHAFTS; TUNNELS; GALLERIES; LARGE UNDERGROUND CHAMBERS
- E21D9/00—Tunnels or galleries, with or without linings; Methods or apparatus for making thereof; Layout of tunnels or galleries
- E21D9/06—Making by using a driving shield, i.e. advanced by pushing means bearing against the already placed lining
- E21D9/0621—Shield advancing devices
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21D—SHAFTS; TUNNELS; GALLERIES; LARGE UNDERGROUND CHAMBERS
- E21D11/00—Lining tunnels, galleries or other underground cavities, e.g. large underground chambers; Linings therefor; Making such linings in situ, e.g. by assembling
- E21D11/04—Lining with building materials
- E21D11/08—Lining with building materials with preformed concrete slabs
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- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21D—SHAFTS; TUNNELS; GALLERIES; LARGE UNDERGROUND CHAMBERS
- E21D11/00—Lining tunnels, galleries or other underground cavities, e.g. large underground chambers; Linings therefor; Making such linings in situ, e.g. by assembling
- E21D11/40—Devices or apparatus specially adapted for handling or placing units of linings or supporting units for tunnels or galleries
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- E—FIXED CONSTRUCTIONS
- E21—EARTH OR ROCK DRILLING; MINING
- E21D—SHAFTS; TUNNELS; GALLERIES; LARGE UNDERGROUND CHAMBERS
- E21D9/00—Tunnels or galleries, with or without linings; Methods or apparatus for making thereof; Layout of tunnels or galleries
- E21D9/06—Making by using a driving shield, i.e. advanced by pushing means bearing against the already placed lining
- E21D9/0607—Making by using a driving shield, i.e. advanced by pushing means bearing against the already placed lining the shield being provided with devices for lining the tunnel, e.g. shuttering
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Abstract
The construction method for synchronizing the shield tunneling and the segment splicing can improve the construction efficiency in a crossing manner, integrate the segment splicing time into the shield propulsion, shorten the tunnel construction period by half to the maximum extent and improve the shield construction efficiency. Meanwhile, the construction method for synchronizing shield tunneling and segment splicing is simple and easy to understand, has strong operability, and is suitable for propelling a straight segment and a curved segment of the shield and rectifying the posture of the shield. The invention solves the problem that shield construction period is long as shield propulsion and segment assembly are alternately carried out in the traditional shield construction.
Description
Technical Field
The invention relates to the technical field of shield construction, in particular to a construction method for synchronizing shield tunneling and segment splicing.
Background
In the development of the shield tunnel technology, in the course of 200 years, the shield machine has become an underground high-end device which integrates multiple disciplines such as machinery, hydraulic pressure, electricity, computers, measurement and the like, is called king of engineering machinery, and is an important mark for measuring the research and development level of national underground engineering mechanical equipment. With the continuous improvement of the construction technology, a large number of successful cases of the classical shield tunnel emerge at home and abroad, and the shield construction improves the construction efficiency by optimizing the capability of the shield equipment on the premise of ensuring safety and reliability, but the effect is not obvious. Because the traditional shield construction shield propulsion and segment assembly are carried out alternately, in the process of forming the shield tunnel, the construction period mainly depends on the two parts of time of the shield propulsion and the segment assembly, and the two parts are close to each other in time consumption.
Disclosure of Invention
In order to overcome the defects in the prior art, a construction method for synchronizing shield tunneling and segment splicing is provided so as to solve the problem that shield tunneling construction is long in construction period because shield tunneling propulsion and segment splicing are alternately carried out in the traditional shield construction.
In order to achieve the purpose, the shield tunneling and segment splicing synchronous construction method is provided, the shield tunneling machine comprises a plurality of propelling jacks arranged at intervals along the circumferential direction of a middle shield and a segment splicing machine arranged on the middle shield, and the construction method is characterized by comprising the following steps of:
a. the multi-ring duct piece assembly is alternately carried out by the propelling of a plurality of propelling jacks and the duct piece assembly of the duct piece assembly machine, and the conventional propelling force of the propelling jacks is obtained in the propelling process of the plurality of propelling jacks;
b. after the conventional thrust is obtained, dividing a plurality of propelling jacks into a retraction section, a decompression propelling section and two pressurization propelling sections, wherein the retraction section corresponds to the position of a segment to be assembled of the next ring segment, the decompression propelling section is arranged opposite to the retraction section, the two pressurization propelling sections are symmetrically arranged between the retraction section and the left side and the right side of the decompression propelling section, the thrust of the propelling jacks of the decompression propelling section is smaller than the conventional thrust, the thrust of the propelling jacks of the pressurization propelling sections is larger than the conventional thrust, and the sum of the real-time thrusts of the decompression propelling sections and the propelling jacks of the two pressurization propelling sections and the generated resultant moment are respectively equal to the sum of the conventional thrusts of all the propelling jacks and the generated resultant moment;
c. the advancing jacks of the retraction section retract, the decompression advancing section and the advancing jacks of the plurality of the pressurization advancing sections advance;
d. after the pushing jack of the retraction section retracts, the duct piece to be assembled is assembled by the duct piece flush mounting machine;
e. and d, repeating the steps b to d, and sequentially finishing the installation of the whole ring of pipe pieces.
Further, the retraction section corresponds to the segment to be assembled, the range of the decompression advancing section is larger than or equal to that of the retraction section, and the range of the decompression advancing section is smaller than the semicircular range of the middle shield.
Further, each of the pressurized propulsion sections comprises a plurality of gradient pressurized propulsion sections, and the thrust of the gradient pressurized propulsion sections is gradually increased from the decompression propulsion section to the retraction section.
Further, the thrust of a plurality of gradient pressurization propelling sections is gradually increased from the decompression propelling section to the retraction section by a certain value increment.
The construction method has the advantages that the construction efficiency is improved in a crossing mode, the segment assembling time is integrated into the shield propulsion, the tunnel construction period can be shortened by half to the maximum extent, and the shield construction efficiency is improved subversively. Meanwhile, the construction method for synchronizing shield tunneling and segment splicing is simple and easy to understand, has strong operability, and is suitable for propelling a straight segment and a curved segment of the shield and rectifying the posture of the shield.
Drawings
Fig. 1 is a schematic structural diagram of a middle shield of a shield tunneling machine according to an embodiment of the present invention.
Fig. 2 is a schematic structural diagram of a tail end of a middle shield of the shield tunneling machine according to the embodiment of the present invention.
Fig. 3 is an exploded structural diagram of a middle shield of the shield tunneling machine according to the embodiment of the present invention.
Fig. 4 is a first sectional view of a propulsion jack on a middle shield of the shield tunneling machine according to the embodiment of the present invention.
Fig. 5 is a second sectional view of a propulsion jack on a middle shield of the shield tunneling machine according to the embodiment of the present invention.
Detailed Description
The embodiments of the present invention are described below with reference to specific embodiments, and other advantages and effects of the present invention will be easily understood by those skilled in the art from the disclosure of the present specification. The invention is capable of other and different embodiments and of being practiced or of being carried out in various ways, and its several details are capable of modification in various respects, all without departing from the spirit and scope of the present invention.
Fig. 1 is a schematic structural diagram of a middle shield of a shield tunneling machine according to an embodiment of the present invention, fig. 2 is a schematic structural diagram of a tail end of the middle shield of the shield tunneling machine according to the embodiment of the present invention, fig. 3 is a schematic exploded structural diagram of the middle shield of the shield tunneling machine according to the embodiment of the present invention, fig. 4 is a schematic sectional diagram of a jack on the middle shield of the shield tunneling machine according to the embodiment of the present invention, and fig. 5 is a schematic sectional diagram of a jack on the middle shield of the shield tunneling machine according to the embodiment of the present invention.
Referring to fig. 1 to 5, the shield tunneling machine includes a plurality of jack jacks 2 arranged at intervals in a circumferential direction of a middle shield 1, and a segment erector 3 mounted to the middle shield.
In the invention, the shield propulsion has a normal propulsion mode and a splicing propulsion synchronous mode.
The conventional propulsion mode refers to a mode that all the propulsion jacks simultaneously propel and then stop, and then segment assembly of the segment erector is performed alternately with the propulsion.
And in the splicing and pushing synchronous mode, after the shield machine starts to splice a multi-ring duct piece with a section of mileage in a conventional mode, a part of the pushing jacks are pushed to push, and a part of the pushing jacks are retracted. A space with at least one segment width is formed between the retracted propelling jack and the assembled segments, and then the segments in the space are assembled by the segment assembling machine, so that the segments can be assembled in the propelling process of the shield tunneling machine.
In this example, the total number of full-circle segments is 9, which are segment F, segment L1, segment L2, segment B1, segment B2, segment B3, segment B4, segment B5, and segment B6.
The pushing jack retracted each time corresponds to one segment. The assembling sequence of the segments of one ring can be carried out in sequence by installing the traditional segment assembling sequence.
With continuing reference to fig. 1 to 5, the invention provides a construction method for synchronizing shield tunneling and duct piece splicing, which comprises the following steps:
a. the multi-ring duct piece 4 is assembled by alternately pushing the plurality of pushing jacks 2 and assembling the duct pieces of the duct piece assembling machine, and the conventional pushing force of all the pushing jacks 2 is obtained in the pushing process of all the pushing jacks 2.
b. After obtaining the conventional thrust, the plurality of the propulsion jacks 2 are divided into a retraction section G0, a decompression propulsion section G1 and two pressurization propulsion sections, wherein the retraction section G0 corresponds to the position of a segment B3 to be spliced of the next ring segment, the decompression propulsion section G1 is arranged opposite to the retraction section G0, and the two pressurization propulsion sections are symmetrically arranged between the left side and the right side of the retraction section G0 and the decompression propulsion section G1. The thrust of the thrust jacks 2 of the decompression thrust section G1 is less than their normal thrust. The thrust of the propulsion jacks 2 of the supercharged propulsion sections is greater than their conventional thrust.
The sum of the real-time thrusts of the decompression propulsion section G1 and the two supercharged propulsion sections of the propulsion jacks 2 is equal to the sum of the conventional thrusts of all the propulsion jacks 2, and the resultant moment of the real-time thrusts of the decompression propulsion section G1 and the two supercharged propulsion sections of the propulsion jacks 2 is equal to the resultant moment of the conventional thrusts of all the propulsion jacks 2.
c. The advancing jacks 2 of the retracting section G0 retract, the decompression advancing section G1 and the advancing jacks 2 of the plurality of the pressurization advancing sections advance.
d. And after the pushing jack 2 of the retraction section G0 retracts, the segment erector assembles the segment B3 to be assembled.
e. And d, repeating the steps b to d, and sequentially finishing the installation of the whole ring of pipe pieces.
And the segment assembly of the whole tunnel is completed by the construction synchronously performed by pushing and assembling.
The construction method for synchronously tunneling the shield and splicing the duct pieces improves the construction efficiency in a crossing manner, integrates the duct piece splicing time into the shield propulsion, and can shorten the tunnel construction period by half to the maximum extent, thereby improving the shield construction efficiency subversively. Meanwhile, the construction method for synchronizing shield tunneling and segment splicing is simple and easy to understand, has strong operability, and is suitable for propelling a straight segment and a curved segment of the shield and rectifying the posture of the shield.
In a preferred embodiment, step b is performed by further dividing the pressurized propulsion section. Each of the booster propulsion sections includes a plurality of gradient booster propulsion sections. The thrust of the multiple gradient pressurization propelling sections is gradually increased from the decompression propelling section to the retraction section into a small pressurization propelling section and a large pressurization propelling section.
The thrust of the gradient pressurization propelling section is gradually increased from the decompression propelling section to the retraction section by a certain value increment.
Referring to fig. 4, in the present embodiment, fig. 4 shows a first division method, when a segment B3 is a segment to be spliced, a segment division diagram of a plurality of pushing jacks in the range of a whole ring segment is shown.
Segment B3 of the segment to be assembled corresponds to the retracted segment G0. A reduced pressure advancing section G1 opposite the position of retraction section G0, reduced pressure advancing section G1 comprising segment F and segment L2. The retraction section and the decompression propulsion section are respectively positioned at two ends of the same diameter line. The decompression advancing section G1 and the retracting section G0 are arranged symmetrically about a central axis a passing through the axial center of the middle shield.
The remaining sections on the left and right sides of the centering axis a are supercharging propulsion sections. Specifically, each of the boosted propulsion sections is divided into two gradient boosted propulsion sections.
As shown in fig. 4, the supercharged propulsion section to the left of the central axis a is divided into a gradient supercharged propulsion section G2 and a gradient supercharged propulsion section G4. The pressurized propulsion section to the right of axis a is divided into a gradient pressurized propulsion section G3 and a gradient pressurized propulsion section G5.
The gradient pressurizing propulsion sections on the left side and the right side of the central axis A are respectively and symmetrically arranged. Thus, the gradient boosting propelling section G2 and the gradient boosting propelling section G3 are symmetrically arranged, and the gradient boosting propelling section G4 and the gradient boosting propelling section G5 are symmetrically arranged. The gradient boosting propelling section G2 and the gradient boosting propelling section G3 are respectively adjacent to the decompression propelling section G1. The gradient pressurization propelling section G4 and the gradient pressurization propelling section G5 are respectively adjacent to the retraction section G0.
The thrust of the gradient boost propulsion section G2 is less than the thrust of the gradient boost propulsion section G4, and the difference in thrust of the gradient boost propulsion section G2 and the gradient boost propulsion section G4 is the fixed increment. The thrust of the gradient boosting propelling section G3 is smaller than that of the gradient boosting propelling section G4, and the difference between the thrust of the gradient boosting propelling section G3 and the thrust of the gradient boosting propelling section G5 is the fixed value increment.
In some embodiments, each of the boosted propulsion sections is divided into a number of gradient boosted propulsion segments greater than three.
At this point, a plurality of propelling jacks of the middle shield are numbered from No.1 to No.34 in the clockwise direction. Wherein, the number of the propelling jacks in the segment B3 range of the segment to be assembled is No. 15-No. 18.
The rest of the propelling jacks are divided into 5 sections (G1-G5), wherein the decompression propelling section G1 comprises 6 propelling jacks in total, namely No.1, No.2, No.31, No.32, No.33 and No. 34; the gradient pressurizing propelling section G2 is provided with 4 propelling jacks from No.27 to No. 30; the G3 group of the gradient pressurizing propelling section has 4 propelling jacks of No. 3-No. 6; the G4 group of the gradient pressurizing propelling section has 8 propelling jacks from No.19 to No. 26; the G5 group of the gradient pressurizing propelling section has 8 propelling jacks from No.7 to No. 14.
The normal thrust (f) of each thrust jack is collected in the normal mode1、f2…f34)。
According to the division of the sections, in order to advance the jack to the shield, under the synchronous pushing and splicing state, the distribution calculation of the jacking force is carried out, so as to ensure that the total jacking force of the shield and the acting point (resultant moment) are kept unchanged, then:
thrust f of the propulsion jack in the range of the retraction section G015+f16+f17+f18＝FG1+FG2+FG3+FG4+FG5，
Wherein, FG1An increment of thrust for the decompression boost section G1;
FG2an increment of thrust for the gradient boost propulsion section G2;
FG3an increment of thrust for the gradient boost propulsion section G3;
FG4an increment of thrust for the gradient boost propulsion section G4;
FG5an increment of thrust for the gradient boost propulsion section G5;
FG2-FG1＝Δf1，FG4-FG2＝Δf1，FG3-FG1＝Δf2，FG5-FG3＝Δf2，Δf1and Δ f2Positive values.
In the invention, the decompression propulsion section opposite to the retraction section is used for realizing decompression propulsion of the propulsion jack of the section during propulsion, and the boosting mode of the propulsion jacks of the rest sections can realize accurate control of the force of the propulsion system based on a certain calculation method; if the decompression propulsion section adopts a mode that the propulsion jacks retract simultaneously and the propulsion jacks in the rest sections are stressed passively, the jacking force of a propulsion (jack) system of the shield machine is insufficient due to insufficient oil pressure redundancy of part of the propulsion jacks, and the shield attitude and the propulsion speed are not controlled; moreover, excessive loss of the jack (oil cylinder) causes difficulty increase in the aspect of posture control during shield deviation correction and turning.
In this embodiment, fig. 5 shows a second division method, in which when a segment F is a segment to be assembled, a segment of a plurality of pushing jacks in the range of a whole ring segment is divided into segments.
And the segment F of the segment to be assembled corresponds to the retraction segment G0. The reduced pressure advancing section G1, opposite the position of the retracting section G0, the reduced pressure advancing section G1 includes tube sheet B3 and tube sheet B4. The retraction section and the decompression propulsion section are respectively positioned at two ends of the same diameter line. The decompression advancing section G1 and the retracting section G0 are arranged symmetrically about a central axis a passing through the axial center of the middle shield.
The remaining sections on the left and right sides of the centering axis a are supercharging propulsion sections. Specifically, each of the boosted propulsion sections is divided into a plurality of gradient boosted propulsion sections.
As shown in fig. 5, the supercharged propulsion section to the left of the central axis a is divided into a gradient supercharged propulsion section G2 and a gradient supercharged propulsion section G4. The pressurized propulsion section to the right of axis a is divided into a gradient pressurized propulsion section G3 and a gradient pressurized propulsion section G5.
The gradient pressurizing propulsion sections on the left side and the right side of the central axis A are respectively and symmetrically arranged.
At this point, a plurality of propelling jacks of the middle shield are numbered from No.1 to No.34 in the clockwise direction. Wherein, the numbers of the propelling jacks in the range of the segment B3 of the segment to be spliced are No.31 and No. 32.
The rest of the propelling jacks are divided into 5 sections (G1-G5), wherein the decompression propelling section G1 comprises 8 propelling jacks from No.11 to No. 18; the gradient pressurizing propelling section G2 is provided with 4 propelling jacks from No.7 to No. 10; the G3 group of the gradient pressurizing propelling section has 4 propelling jacks from No.19 to No. 22; the G4 group of the gradient pressurization propelling section comprises 8 propelling jacks, namely No.1, No.2, No.3, No.4, No.5, No.6, No.33 and No. 34; the G5 group of the gradient pressurizing propelling section has 8 propelling jacks from No.23 to No. 30.
The normal thrust (f) of each thrust jack is collected in the normal mode1、f2…f34)。
According to the division of the sections, in order to push the jack to the shield, the distribution calculation of the jacking force is carried out under the synchronous pushing and splicing state, so that the total jacking force of the shield and the acting point are ensured to be unchanged.
Based on the above detailed description, all the segment division methods are not exhaustive here.
The construction method for synchronizing shield tunneling and segment splicing can also divide a plurality of propelling jacks 4 into regions or 6 into regions, and perform tunneling and deviation rectification according to the conventional operation experience of a shield driver.
When the shield machine is normally propelled, the oil pressure opening value of each subarea and the subarea jacking force converted from the rodless cavity pressure of each subarea jack acquired by the PLC are displayed on the operation interface of the shield machine, so that preparation is made for shield deviation correction in a subsequent pushing and splicing synchronization mode.
Before the propulsion jacks are separated from the duct pieces in the range of the duct pieces to be assembled, linear pressure relief is firstly carried out, and the other propulsion jacks carry out linear pressurization, so that the stable posture of the shield tunneling machine is ensured.
The oil pressure opening setting function of the conventional propelling interface of the shield machine is locked, and the shield machine can be corrected or turned by modifying the total jacking force of the propelling jacks in the section.
And distributing the increment value obtained by the pushing jack of each section to each pushing jack of the section, thereby obtaining the redistribution original value of the jacking force after entering the pushing and splicing synchronous mode of the next ring segment again.
It should be noted that the structures, ratios, sizes, and the like shown in the drawings attached to the present specification are only used for matching the disclosure of the present specification, so as to be understood and read by those skilled in the art, and are not used to limit the conditions of the present invention, so that the present invention has no technical essence, and any structural modification, ratio relationship change, or size adjustment should still fall within the scope of the present invention without affecting the efficacy and the achievable purpose of the present invention. In addition, the terms "upper", "lower", "left", "right", "middle" and "one" used in the present specification are for clarity of description, and are not intended to limit the scope of the present invention, and the relative relationship between the terms and the terms is not to be construed as a scope of the present invention.
While the present invention has been described in detail and with reference to the embodiments thereof as illustrated in the accompanying drawings, it will be apparent to one skilled in the art that various changes and modifications can be made therein. Therefore, certain details of the embodiments are not to be interpreted as limiting, and the invention is to be defined by the scope of the appended claims.
Claims (4)
1. A shield tunneling and segment splicing synchronous construction method is characterized in that the construction method comprises the following steps:
a. the multi-ring duct piece assembly is alternately carried out by the propelling of a plurality of propelling jacks and the duct piece assembly of the duct piece assembly machine, and the conventional propelling force of the propelling jacks is obtained in the propelling process of the plurality of propelling jacks;
b. after the conventional thrust is obtained, dividing a plurality of propelling jacks into a retraction section, a decompression propelling section and two pressurization propelling sections, wherein the retraction section corresponds to the position of a segment to be assembled of the next ring segment, the decompression propelling section is arranged opposite to the retraction section, the two pressurization propelling sections are symmetrically arranged between the retraction section and the left side and the right side of the decompression propelling section, the thrust of the propelling jacks of the decompression propelling section is smaller than the conventional thrust, the thrust of the propelling jacks of the pressurization propelling sections is larger than the conventional thrust, and the sum of the real-time thrusts of the decompression propelling sections and the propelling jacks of the two pressurization propelling sections and the generated resultant moment are respectively equal to the sum of the conventional thrusts of all the propelling jacks and the generated resultant moment;
c. the advancing jacks of the retraction section retract, the decompression advancing section and the advancing jacks of the plurality of the pressurization advancing sections advance;
d. after the pushing jack of the retraction section retracts, the duct piece to be assembled is assembled by the duct piece flush mounting machine;
e. and d, repeating the steps b to d, and sequentially finishing the installation of the whole ring of pipe pieces.
2. The synchronous shield tunneling and segment splicing construction method according to claim 1, wherein the retraction section corresponds to a segment to be spliced, the range of the decompression propulsion section is greater than or equal to that of the retraction section, and the range of the decompression propulsion section is smaller than the semicircular range of the middle shield.
3. The synchronous shield tunneling and segment splicing construction method according to claim 1, wherein each of the pressurizing and propelling sections comprises a plurality of gradient pressurizing and propelling sections, and the thrust of the gradient pressurizing and propelling sections is gradually increased from the pressure reducing and propelling section to the retraction section.
4. The synchronous shield tunneling and segment splicing construction method according to claim 3, wherein the thrust of the plurality of gradient pressurizing propulsion segments is gradually increased from the pressure reducing propulsion segment to the retraction segment by a certain value increment.
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112627835A (en) * | 2021-01-15 | 2021-04-09 | 刁志刚 | Feed-through continuous jacking device and shield launching method |
| CN112832787A (en) * | 2021-03-09 | 2021-05-25 | 上海隧道工程有限公司 | Uniform-speed propulsion valve control method and system for shield tunneling machine in pushing and splicing synchronization state |
| CN112832790A (en) * | 2021-03-09 | 2021-05-25 | 上海隧道工程有限公司 | Method and system for controlling uniform-speed propulsion pump in shield tunneling machine push-splicing synchronous state |
| CN114135300A (en) * | 2021-11-22 | 2022-03-04 | 中铁工程装备集团有限公司 | Method, device, equipment and medium for distributing thrust of synchronous pushing and splicing system of shield tunneling machine |
| WO2023130972A1 (en) * | 2022-01-07 | 2023-07-13 | 中建三局集团有限公司 | Control system and control method for tunneling-erecting synchronous construction by tunnel boring machine |
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| CN112627835A (en) * | 2021-01-15 | 2021-04-09 | 刁志刚 | Feed-through continuous jacking device and shield launching method |
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| CN112832790A (en) * | 2021-03-09 | 2021-05-25 | 上海隧道工程有限公司 | Method and system for controlling uniform-speed propulsion pump in shield tunneling machine push-splicing synchronous state |
| CN112832790B (en) * | 2021-03-09 | 2023-12-26 | 上海隧道工程有限公司 | Constant-speed propulsion pump control method and system in pushing and splicing synchronous state of shield machine |
| CN114135300A (en) * | 2021-11-22 | 2022-03-04 | 中铁工程装备集团有限公司 | Method, device, equipment and medium for distributing thrust of synchronous pushing and splicing system of shield tunneling machine |
| CN114135300B (en) * | 2021-11-22 | 2024-04-12 | 中铁工程装备集团有限公司 | Method, device, equipment and medium for distributing propelling force of synchronous pushing and splicing system of shield machine |
| WO2023130972A1 (en) * | 2022-01-07 | 2023-07-13 | 中建三局集团有限公司 | Control system and control method for tunneling-erecting synchronous construction by tunnel boring machine |
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Effective date of registration: 20211223 Address after: No. 1099, No. 5, Wan Ping Nan Road, Xuhui District, Shanghai Patentee after: SHANGHAI TUNNEL ENGINEERING Co.,Ltd. Patentee after: Shanghai Waigaoqiao tunnel machinery Co.,Ltd. Address before: No. 1099, No. 5, Wan Ping Nan Road, Xuhui District, Shanghai Patentee before: SHANGHAI TUNNEL ENGINEERING Co.,Ltd. |
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Address after: No. 1099, No. 5, Wan Ping Nan Road, Xuhui District, Shanghai Patentee after: SHANGHAI TUNNEL ENGINEERING Co.,Ltd. Patentee after: Shanghai urban construction tunnel equipment Co., Ltd Address before: No. 1099, No. 5, Wan Ping Nan Road, Xuhui District, Shanghai Patentee before: SHANGHAI TUNNEL ENGINEERING Co.,Ltd. Patentee before: Shanghai Waigaoqiao tunnel machinery Co., Ltd |
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