JPS6078096A - Positional detection of shield drilling machine - Google Patents

Positional detection of shield drilling machine

Info

Publication number
JPS6078096A
JPS6078096A JP18489083A JP18489083A JPS6078096A JP S6078096 A JPS6078096 A JP S6078096A JP 18489083 A JP18489083 A JP 18489083A JP 18489083 A JP18489083 A JP 18489083A JP S6078096 A JPS6078096 A JP S6078096A
Authority
JP
Japan
Prior art keywords
propulsion
shield
tube
pipe
gap
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP18489083A
Other languages
Japanese (ja)
Inventor
滝川 篁
田口 武雄
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zenitaka Corp
Mitsui Engineering and Shipbuilding Co Ltd
Mitsui Zosen KK
Original Assignee
Zenitaka Corp
Mitsui Engineering and Shipbuilding Co Ltd
Mitsui Zosen KK
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zenitaka Corp, Mitsui Engineering and Shipbuilding Co Ltd, Mitsui Zosen KK filed Critical Zenitaka Corp
Priority to JP18489083A priority Critical patent/JPS6078096A/en
Publication of JPS6078096A publication Critical patent/JPS6078096A/en
Pending legal-status Critical Current

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  • Excavating Of Shafts Or Tunnels (AREA)
  • Geophysics And Detection Of Objects (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 □ 〔発明の技術分野〕 ン−a)yzpp++l−4−k −/ −) n−m
Mrm +rr +−Jr七 7− 、・i ++、t
’利…進様の位置を検出するシールド掘進機の位置検出
方法に関するものである。
[Detailed description of the invention] □ [Technical field of the invention] n-a)yzpp++l-4-k -/-) nm
Mrm +rr +-Jr7 7-,・i++,t
This invention relates to a method for detecting the position of a shield excavator that detects the position of a pilot.

〔従来技術〕[Prior art]

近年、下水道の普及にともない各地で下水道管を埋設す
るためのトンネル工事が行なわれている。
In recent years, with the spread of sewage systems, tunnel construction for burying sewage pipes has been carried out in various places.

都市部ではこの工事によって道路交通じ影響を与えない
ように、「もぐら工法」と呼ばれるシールド掘進機を使
用したシールド工法や、推進工法を行なうことが多い。
In urban areas, in order to avoid the impact of this construction on road traffic, a shield construction method using a shield excavator known as the ``mole method'' or a propulsion method is often used.

この場合、1−ンネルを正しく目標地点まで掘進めるに
はシールド掘進機の位置を正確に検出する必要がある。
In this case, it is necessary to accurately detect the position of the shield excavator in order to correctly excavate the tunnel to the target point.

シールド掘進機の位置検出は通常、トランシフトまたは
レーザ光によって行なわれていたが、近年はと「業員の
入れないような小口径のトンネルを掘削することが多く
、このよう外小口径のトンネルで曲線施工部があると従
来の方法は使用できない。このため例えばジャイロスコ
ープを用いるなど、各種の提案がなされているが精度、
経済性に問題があり、実用的でなかった。
The position detection of shield tunneling machines was normally carried out using transshift or laser beams, but in recent years, tunnels with small diameters that cannot be accessed by workers are often excavated. If there is a curved construction part, conventional methods cannot be used.For this reason, various proposals have been made, such as using a gyroscope, but accuracy and
There were economic problems and it was not practical.

〔発明の目的および構成〕[Object and structure of the invention]

したがってこの発明の目的は、精度および経済性が良く
、し、かも実用的な位置検出が行なえる、シールド掘進
機の位置検出方法を提供することにある。
SUMMARY OF THE INVENTION Accordingly, an object of the present invention is to provide a method for detecting the position of a shield excavator, which is highly accurate and economical, and also enables practical position detection.

このような目的を達成するだめにこの発明は、隣接する
W、進管接続部の隙間データおよび元押しジヤツキ側推
進管のデータから進行側推進管の位置をめ、この操作を
順次進行側推進管に適用して推進管最先端部のシールド
掘進機の位置を検出するようにしたものである。以下、
実施例を示す図面を用いてこの発明の詳細な説明する。
In order to achieve such an object, the present invention determines the position of the advancing side propulsion tube from the adjacent W, gap data of the advancing tube connection part, and data of the main push jack side propulsion tube, and sequentially performs this operation to advance the advancing side propulsion tube. This method is applied to a pipe to detect the position of a shield tunneling machine at the leading edge of a propulsion pipe. below,
The present invention will be described in detail using drawings showing embodiments.

〔実施例〕〔Example〕

第1図はこの発明の方法を適用した装置でトンネルを構
築する時の一実施例を示す水平面断面図である。同図に
おいて1はシールド掘進機、21〜2nは推進管、3は
立坑、41.42は元押しジヤツキ、”+152はシー
ルド掘進機1の方向を修正する方向修正ジヤツキである
。各推進管接続部であって対向する管壁部分に、隣接す
る推進管の隙間を検出する隙間検出器61〜6 (2n
−2)が設けられており、推進管2nとシールド掘進機
1との接続部は同様の方法で隙間検出器”2n、6(2
n−1)が設けられている。
FIG. 1 is a horizontal sectional view showing an embodiment of constructing a tunnel using an apparatus to which the method of the present invention is applied. In the figure, 1 is a shield tunneling machine, 21 to 2n are propulsion pipes, 3 is a vertical shaft, 41.42 is a main push jack, and +152 is a direction correction jack that corrects the direction of the shield tunneling machine 1. Each propulsion pipe connection Gap detectors 61 to 6 (2n
-2) is provided, and the connection between the propulsion pipe 2n and the shield excavator 1 is connected to the gap detector "2n, 6 (2)" in the same way.
n-1) is provided.

第2図は位置検出装置のブロック図であシ、h〜Inは
隙間検出器61〜6nで検出した信号を信号伝送に適す
る形式に変換する信号変換器、8はこれらの信号変換器
からの信号を切換える信号切換器、9は8/D変換器、
104,10□はデータ送受信器、11は演算部、12
はデータ設定部、13は表示部である。とこで、信号切
換器8と一変換器9はデータ送受信機101,102を
介して行なわれる演算部11からの指示により動作ル し1隙間検出61〜6nの検出信号が順次ディジクル信
号に変換され、演算部11に送出されるようになってい
る。データ設定部12は立坑3に隣接する推進管2Iの
位置、方位、長さ、隙間検出器の管径方向の取付間隔デ
ータを設定するようになっている。寸た、データ送受信
器102、演算部11、データ設定部12、表示部13
は坑外の建屋14または立坑3の適当な位置に設置され
る。なお、第2図に示す隙間検出器は61 + 62 
+ 63 +”(n I)+6+1Lか示していないが
、隙間検出器62.64+66168、・・・62n 
も同様な方法で接続されている。
FIG. 2 is a block diagram of the position detection device, where h to In are signal converters that convert the signals detected by the gap detectors 61 to 6n into a format suitable for signal transmission, and 8 is the signal converter from these signal converters. A signal switcher that switches signals, 9 is an 8/D converter,
104, 10□ is a data transmitter/receiver, 11 is a calculation unit, 12
1 is a data setting section, and 13 is a display section. The signal switch 8 and the converter 9 are operated in response to instructions from the arithmetic unit 11 via the data transmitter/receiver 101 and 102, and the detection signals of the first gap detections 61 to 6n are sequentially converted into digital signals. , are sent to the calculation unit 11. The data setting unit 12 is configured to set the position, orientation, and length of the propulsion pipe 2I adjacent to the shaft 3, and the installation interval data of the gap detector in the pipe radial direction. data transmitter/receiver 102, calculation section 11, data setting section 12, display section 13
is installed at an appropriate position in the building 14 outside the mine or in the shaft 3. Note that the gap detector shown in Fig. 2 is 61 + 62
+63 +”(n I)+6+1L is not shown, but the gap detector 62.64+66168,...62n
are also connected in the same way.

このように構成された装置の動作は次の通シである。シ
ールド掘進機1は元押しジヤツキ41 。
The operation of the device configured as described above is as follows. Shield tunneling machine 1 is Motoshi Jatsuki 41.

42の押圧力を受け推進管21〜2nと共に推進し、そ
の推進方向は方向修正ジヤツキ”I+52や、推進管端
部に取付けられる図上省略した開口調整材によって制御
される。
It is propelled together with the propulsion tubes 21 to 2n under the pressure of 42, and its propulsion direction is controlled by a direction correction jack "I+52" and an aperture adjusting member (not shown in the figure) attached to the end of the propulsion tube.

各推進管が直線状に連らなっている時は管径方向に相対
する隙間検出器からの信号は等しり、また各推進管の配
列が直線から外れた時は隙間検出器からの信号は異なる
When the propulsion tubes are arranged in a straight line, the signals from the gap detectors facing each other in the tube diameter direction are equal, and when the propulsion tubes are arranged out of a straight line, the signals from the gap detectors are equal. different.

第1図において紙面の左右方向をX座標、上下方向をX
座標とし、第3図に示すように推進管21の中心部の座
標を(”+ + 、’/1) + 進行方位を01、推
進管22の中心部の座標を(”2 ’ 312) + 
その進行方位をθ2とする。但し、進行方位はy軸を基
準とし、右廻りの角をプラスとする。また、各推進管の
長さを61管径方向の隙間検出器取付間隙をD1隙間検
出器61.62の隙間データをd、1d2 とすると推
進管22のX座標x2、y座標y2、方位θ2は次式で
表わされる。
In Figure 1, the horizontal direction of the paper is the X coordinate, and the vertical direction is the X coordinate.
As shown in Fig. 3, the coordinates of the center of the propulsion tube 21 are (''+ +, '/1) + the traveling direction is 01, and the coordinates of the center of the propulsion tube 22 are (''2 ' 312) +
Let the traveling direction be θ2. However, the direction of travel is based on the y-axis, and the clockwise angle is taken as a plus. In addition, if the length of each propulsion tube is 61, the installation gap of the gap detector in the pipe radial direction is D1, and the gap data of the gap detector 61.62 is d, 1d2, then the X coordinate of the propulsion tube 22 is x2, the y coordinate is y2, and the orientation θ2. is expressed by the following equation.

r2 ”” rl + 0.5 t(s石θ トsin
 θ )y2= ’14 + 0−51 (cosθI
 ” oθ2 )すなわち、推進管21の中心座標(x
I + 、Vl )と進行方向が決まれば、この点をも
とに推進管22の座標がまる。この演算を縁り返し順次
進行側推進管の位置をめ5ことによってシールド掘進機
1の位置をめることができる。
r2 ”” rl + 0.5 t(s stone θ tosin
θ )y2='14 + 0-51 (cosθI
” oθ2 ), that is, the center coordinates of the propulsion tube 21 (x
I + , Vl ) and the direction of travel are determined, the coordinates of the propulsion tube 22 are determined based on this point. The position of the shield tunneling machine 1 can be determined by repeating this calculation and sequentially determining the position of the advancing side propulsion pipe.

第1図は隙間検出器を水平面に配置し、シールド掘進機
の水平面内の位置を検出した例であるが、第4図に示す
ように隙間検出器6を推進管2の上下、左右に増刊けた
り、第5図に示すように推進管2の円周方向に45度、
135度、225度、315度の角度に配置することも
できる。
Fig. 1 shows an example in which gap detectors are placed on a horizontal plane to detect the position of a shield tunneling machine in the horizontal plane. 45 degrees in the circumferential direction of the propulsion tube 2 as shown in FIG.
It can also be arranged at an angle of 135 degrees, 225 degrees, or 315 degrees.

この時はシールド掘進機1の水平面内の位置ばかりでな
く、垂直面内の位置についても知ることができる。
At this time, it is possible to know not only the position of the shield tunneling machine 1 in the horizontal plane but also the position in the vertical plane.

また第1図では立坑3よりシールド掘進機1丑での全推
進管に隙間検出器を取付けたが、シールド掘進機1に続
く一部の推進管だけに隙間検出器を増刊けて、掘削開始
時からのシールド掘進器1の位置の変化分を常時検出し
、これを積算する事によってもシールド掘進機10位置
を検出することができる。
In addition, in Figure 1, gap detectors were installed on all propulsion pipes from shaft 3 to shield excavator 1, but clearance detectors were added to only some propulsion pipes following shield excavator 1, and excavation was started. The position of the shield excavator 10 can also be detected by constantly detecting changes in the position of the shield excavator 1 from time to time and integrating the changes.

隙間検出器は隙間間隔に比例して電気抵抗値が変る直綜
摺動形ポテンショメータ、光学式や磁気式のリニアスケ
ール等を使用すると良い。
As the gap detector, it is preferable to use a straight sliding type potentiometer whose electrical resistance value changes in proportion to the gap interval, an optical type or a magnetic type linear scale, or the like.

なお、推進管に傾斜計を取付け、推進管のピッチ角、ロ
ール角信号を検出し、隙間検出器の信号を補正すること
によって位置検出精度を高めることもできる。
Note that the position detection accuracy can also be improved by attaching an inclinometer to the propulsion tube, detecting the pitch angle and roll angle signals of the propulsion tube, and correcting the signal of the gap detector.

〔発明の効果〕〔Effect of the invention〕

以上説明したようにこの発り」に係るシールド掘進機の
位置検出方法は、隣接する推進管の間にできる隙間を検
出してシールド掘進機の位置を検出しているので、作業
員の入れないような小口径でしかも曲線施工部のおるト
ンネルであっても高精度で経済性の良い位置検出が行な
えるという効果を有する。
As explained above, the method for detecting the position of the shield tunneling machine related to "This Origin" detects the position of the shield tunneling machine by detecting the gap created between adjacent propulsion pipes, so it is difficult for workers to enter. The present invention has the effect that position detection can be performed with high precision and good economic efficiency even in tunnels with small diameters such as those with curved construction parts.

【図面の簡単な説明】[Brief explanation of drawings]

第1図はこの発明を適用してトンネル掘削を行なってい
る部分の水平面断面図、第2図は位置検出装置のブロッ
ク図、第3図は各諸元の関係を説明するだめの図、第4
図および第5図は隙間検出器の取付状態を示す図である
。 1・・・・シールド掘進機、2.21〜2n・・・・推
進管、3・・・・立坑、41.42・・・・元押しジヤ
ツキ、51+52・・・・方向作置ジヤツキ、6+6z
〜62n・・・・隙間検出器、71〜7n・・・・信号
変換器、8・・・・信号切換器、9・・・φ/変換器、
、10..10□ ・・・・デ−タ送受信器、11・・
・・演算部、12・・・データ設定部、13・・・・表
示部。 特許出願人 三井造船株式会社 株式会社銭 高 組 代理人 山川政樹(ほか1名) 2A1図 vA2図 笥3図 第4図 第5図
Fig. 1 is a horizontal sectional view of the part where tunnel excavation is being carried out by applying the present invention, Fig. 2 is a block diagram of the position detection device, Fig. 3 is a diagram for explaining the relationship between each specification, and Fig. 4
FIG. 5 and FIG. 5 are diagrams showing the mounting state of the gap detector. 1... Shield excavator, 2.21~2n... Propulsion pipe, 3... Vertical shaft, 41.42... Main push jack, 51+52... Direction setting jack, 6+6z
~62n...Gap detector, 71~7n...Signal converter, 8...Signal switcher, 9...φ/converter,
, 10. .. 10□...Data transmitter/receiver, 11...
...Calculating section, 12...Data setting section, 13...Display section. Patent applicant: Mitsui Engineering & Shipbuilding Co., Ltd. Zenitaka Co., Ltd. Agent: Masaki Yamakawa (and one other person) Figure 2A1 vA2 Figure 3 Figure 4 Figure 5

Claims (1)

【特許請求の範囲】 直列に配設された推進管を元押しジヤツキによって進行
方向に押圧しながらその先端部に設けられたシールド掘
進機によってトンネルの掘進を行なう時、そのシールド
掘進機の位置を検出するためのシールド掘進機の位置検
出方法において、國接する推進管の接続部のうち対向す
る管壁に生ずる隙間間隔を測定し、この隙間間隔データ
と元押しジヤツキ側推進管方位から進行側推進管の方位
をめ、元押しジヤツキ側推進管位置および方位。 進行側推進管方位から進行側推進管位置をめ、このめら
れた推進管位1劃を基に順次進行側推進管の位置をめる
ことによってシールド掘進機の位置を検出するシールド
掘進機の位置検出方法。
[Scope of Claims] When excavating a tunnel using a shield excavator installed at the tip of the propulsion tubes arranged in series while pushing them in the advancing direction by a pusher jack, the position of the shield excavator is determined. In the method for detecting the position of a shield tunneling machine, the gap interval that occurs between the opposing pipe walls at the joints of the adjacent propulsion pipes is measured, and this gap interval data is used to determine the position of the advancing side propulsion from the direction of the main thrust jack side propulsion tube. Determine the direction of the tube, and determine the position and direction of the main push jack side propulsion tube. The position of the shield tunneling machine is detected by determining the position of the traveling side propulsion pipe from the direction of the traveling side propulsion pipe and sequentially adjusting the position of the traveling side propulsion pipe based on the determined propulsion pipe position. Location detection method.
JP18489083A 1983-10-03 1983-10-03 Positional detection of shield drilling machine Pending JPS6078096A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18489083A JPS6078096A (en) 1983-10-03 1983-10-03 Positional detection of shield drilling machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18489083A JPS6078096A (en) 1983-10-03 1983-10-03 Positional detection of shield drilling machine

Publications (1)

Publication Number Publication Date
JPS6078096A true JPS6078096A (en) 1985-05-02

Family

ID=16161100

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18489083A Pending JPS6078096A (en) 1983-10-03 1983-10-03 Positional detection of shield drilling machine

Country Status (1)

Country Link
JP (1) JPS6078096A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0538519U (en) * 1991-10-29 1993-05-25 三菱重工業株式会社 Attitude measuring device for tunnel excavator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0538519U (en) * 1991-10-29 1993-05-25 三菱重工業株式会社 Attitude measuring device for tunnel excavator

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