JP2000087683A - Shield machine, and tunnel execution method thereby - Google Patents

Shield machine, and tunnel execution method thereby

Info

Publication number
JP2000087683A
JP2000087683A JP25734898A JP25734898A JP2000087683A JP 2000087683 A JP2000087683 A JP 2000087683A JP 25734898 A JP25734898 A JP 25734898A JP 25734898 A JP25734898 A JP 25734898A JP 2000087683 A JP2000087683 A JP 2000087683A
Authority
JP
Japan
Prior art keywords
propulsion
excavator
machine
shield machine
bodies
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.)
Granted
Application number
JP25734898A
Other languages
Japanese (ja)
Other versions
JP3640537B2 (en
Inventor
Katsuya Sasaki
加津也 佐々木
Yoshiyuki Shimizu
賀之 清水
Koichiro Nakayama
耕一郎 中山
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.)
Hitachi Zosen Corp
Original Assignee
Hitachi Zosen Corp
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 Hitachi Zosen Corp filed Critical Hitachi Zosen Corp
Priority to JP25734898A priority Critical patent/JP3640537B2/en
Publication of JP2000087683A publication Critical patent/JP2000087683A/en
Application granted granted Critical
Publication of JP3640537B2 publication Critical patent/JP3640537B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Excavating Of Shafts Or Tunnels (AREA)

Abstract

PROBLEM TO BE SOLVED: To provide an execution method capable of easily changing the curvature by arranging a specified number of excavating and advancing machine bodies adjacent to each other while deviating them from one another in the longitudinal direction successively from one side to adjust the thrust of respectively provided propulsion jacks. SOLUTION: Cutter heads 1A-1C are provided adjacent to each other on a tip part of first to third excavating and advancing machine bodies 2A-2C of different length in a shield machine 1. The cutter heads 1A-1C are arranged at the position successively deviated backward by the difference in length of the first to third excavating and advancing machine bodies 2A-2C, and propulsion jacks 3-5 are arranged on the circumference with specified intervals. An auxiliary blade 6 to be advanced/retracted to/from the ground G side at a specified angle α is provided on a side part of the third excavating and advancing machine body 2C. A curved tunnel of different curvature can be executed while keeping a specified propulsion force by adjusting the propulsion force of the propulsion jacks 3-5, and the curvature can be easily changed. The smooth execution can be effected by projecting the auxiliary blade 6.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、シールド掘進機お
よびシールド掘進機におけるトンネル施工方法に関す
る。
The present invention relates to a shield machine and a tunnel construction method for the shield machine.

【0002】[0002]

【従来の技術】従来、三連式のシールド掘進機(三連式
マルチフェースシールド掘進機ともいう)は、図3およ
び図4に示すように、中央の面板20が先行し両側の面
板21,22が後行する構成となっており、幾何学的中
心(重心)Aが、中央のシールド23に存在している。
2. Description of the Related Art Conventionally, as shown in FIGS. 3 and 4, a triple shield excavator (also referred to as a triple multiface shield excavator) is arranged such that a central face plate 20 precedes and face plates 21 and 21 on both sides. 22, a geometric center (center of gravity) A exists in the central shield 23.

【0003】[0003]

【発明が解決しようとする課題】上記従来の三連式のシ
ールド掘進機では、中央の面板20が先行し両側の面板
21,22が後行する構成となっており、幾何学的中心
Aが、中央のシールド23に存在しているので、地山G
を曲線施工する場合、推進ジャッキの推進力の調節が必
要であった。
In the above-mentioned conventional triple shield excavator, the central face plate 20 precedes and the face plates 21 and 22 on both sides follow. , Because it exists in the central shield 23,
When performing the curve construction, it was necessary to adjust the propulsion force of the propulsion jack.

【0004】そこで、本発明は、上記課題を解決し得る
シールド掘進機およびシールド掘進機におけるトンネル
施工方法の提供を目的とする。
Accordingly, an object of the present invention is to provide a shield machine and a tunnel construction method for the shield machine capable of solving the above-mentioned problems.

【0005】[0005]

【課題を解決するための手段】本発明における課題解決
手段は、三個以上の掘進機本体を隣り合わせて設けると
ともに、一方の掘進機本体から他方の掘進機本体を順に
前後方向にずらして配置するよう構成している。
Means for Solving the Problems In the present invention, three or more excavator bodies are provided adjacent to each other, and one excavator body is sequentially shifted from the other excavator body in the front-rear direction. It is configured as follows.

【0006】また、両側の掘進機本体の少なくとも一方
に、掘進機本体に対して後方に向けて地山側に所定角度
で出没自在な補助翼が設けられている。上記構成におい
て、三個以上の掘進機本体を隣り合わせて設けるととも
に、一方の掘進機本体から他方の掘進機本体を順に前後
方向に配置するようし、各掘進機本体に等しい推進力を
付与して曲線施工をし、各掘進機本体に等しい推進力を
付与する代わりに異なった推進力を付与して曲線施工す
る曲率を変更する。
[0006] At least one of the excavator bodies on both sides is provided with an auxiliary wing that is capable of protruding and retracting at a predetermined angle on the ground side toward the rear with respect to the excavator body. In the above configuration, three or more excavator bodies are provided adjacent to each other, and one excavator body is arranged in the front-rear direction from the other excavator body in order to impart the same propulsive force to each excavator body. Curve construction is performed, and instead of imparting equal propulsion force to each excavator body, a different propulsion force is applied to change the curvature for curve construction.

【0007】[0007]

【発明の実施の形態】以下、本発明の実施の形態を図面
に基づいて説明する。図1の平面図に示すように、本発
明の実施の形態に係るシールド掘進機1は、長さの異な
る第一〜第三掘進機本体2A〜2Cの先端部に、カッタ
ーヘッド1A〜1Cを備え、第一〜第三掘進機本体2A
〜2Cは隣り合わせて配置されるとともに、前記カッタ
ーヘッド1A〜1Cは、第一〜第三掘進機本体2A〜2
Cの長さの異なる分だけ第一掘進機本体2Aのカッター
ヘッド1Aから第二掘進機本体2Bのカッターヘッド1
B、第三掘進機本体2Cのカッターヘッド1C順に後方
向にずれた位置に配置され、前記第一〜第三掘進機本体
2A〜2Cの後端面は、カッターヘッド1A〜1Cに平
行な所定の同一面内にある。また、第一〜第三掘進機本
体2A〜2Cには、それぞれ推進用ジャッキ3〜5が円
周上に所定間隔で複数個設けられている。
Embodiments of the present invention will be described below with reference to the drawings. As shown in the plan view of FIG. 1, a shield machine 1 according to an embodiment of the present invention includes cutter heads 1A to 1C at the distal ends of first to third machine bodies 2A to 2C having different lengths. Equipped, first to third machine 2A
2C are disposed adjacent to each other, and the cutter heads 1A to 1C are provided with first to third excavator bodies 2A to 2C.
From the cutter head 1A of the first machine 2A to the cutter head 1 of the second machine 2B by the length of C
B, the cutter head 1C of the third excavator main body 2C is disposed at a position shifted rearward in the order of the cutter head 1C, and the rear end surfaces of the first to third excavator main bodies 2A to 2C are arranged at predetermined positions parallel to the cutter heads 1A to 1C. They are in the same plane. The first to third excavator bodies 2A to 2C are provided with a plurality of propulsion jacks 3 to 5 at predetermined intervals on the circumference.

【0008】この構成により、シールド掘進機1の幾何
学的中心(重心)Pが、第一掘進機本体2A側に存在す
るよう構成されている。なお、第三掘進機本体2Cの側
部に、第三掘進機本体2Cに対して後方に向けて地山G
側に所定角度αで出没する補助翼6が設けられている。
With this configuration, the geometric center (center of gravity) P of the shield machine 1 is configured to be present on the first machine body 2A side. It should be noted that the ground G is provided on the side of the third machine body 2C toward the rear with respect to the third machine body 2C.
An auxiliary wing 6 that protrudes and disappears at a predetermined angle α is provided on the side.

【0009】また図2において、所定の推進用ジャッキ
(図では推進用ジャッキ3を示している)の推進力によ
って前記幾何学的中心に働くモーメントMは、M=F・
R・cosβによって表される。この式において、 F:所定の推進用ジャッキの推進力 R:幾何学的中心Pから所定の推進用ジャッキまでの距
離 β:幾何学的中心Pから所定の推進用ジャッキまでと水
平軸hとのなす角度 である。従って第一〜第三掘進機本体2A〜2Cの径を
設定し、各推進用ジャッキ3〜5の位置を決定し、Fを
決定することにより、幾何学的中心Pに働くモーメント
が算出されることになる。
In FIG. 2, the moment M acting on the geometric center by the propulsion force of a predetermined propulsion jack (the propulsion jack 3 is shown in the figure) is M = F ·
It is represented by R · cosβ. In this formula, F: the propulsion force of the predetermined propulsion jack R: the distance from the geometric center P to the predetermined propulsion jack β: the distance between the geometric center P and the predetermined propulsion jack and the horizontal axis h The angle to make. Therefore, the moment acting on the geometric center P is calculated by setting the diameters of the first to third excavator bodies 2A to 2C, determining the positions of the propulsion jacks 3 to 5, and determining F. Will be.

【0010】上記構成において、各第一〜第三掘進機本
体2A〜2Cに設けられた推進用ジャッキ3〜5のそれ
ぞれの合力が等しいとすると、例えば水平面内で地山G
を掘削する場合、シールド掘進機1は、図1の矢印Dで
示すように湾曲して掘進し、地山Gを湾曲施工すること
ができる。これは、シールド掘進機1が、第一掘進機本
体2Aから第二掘進機本体2B、第三掘進機本体2Cの
順に後方向にずらして配置されていることにより、シー
ルド掘進機1の幾何学的中心Pが第一掘進機本体2A側
に存在し、各推進用ジャッキ3〜5の推進力の合力が、
幾何学的中心Pからずれて(図1では第一掘進機本体2
Aの第二掘進機本体2B寄り)働くからである。また、
補助翼6を所定角度で突出させることで、より円滑に曲
線施工を行うことができる。
In the above configuration, assuming that the resultant forces of the propulsion jacks 3 to 5 provided in the first to third excavator main bodies 2A to 2C are equal, for example, the ground G
Excavation, the shield machine 1 can excavate in a curved manner as shown by an arrow D in FIG. This is because the shield machine 1 is displaced rearward in the order of the first machine body 2A, the second machine body 2B, and the third machine body 2C from the first machine body 2A. Target P exists on the first excavator main body 2A side, and the resultant force of the propulsion forces of the propulsion jacks 3 to 5 is as follows:
Deviated from the geometric center P (in FIG. 1, the first machine body 2
This is because the second excavator main body 2B of A works). Also,
By projecting the auxiliary wing 6 at a predetermined angle, it is possible to perform a curved construction more smoothly.

【0011】このように、各推進用ジャッキ3〜5の推
進力の合力が幾何学的中心Pに対してずれて働くこと
で、各推進用ジャッキ3〜5の推進力を特別に制御する
ことなく(各推進用ジャッキ3〜5の推進力を等しく設
定したとしても)、地山Gを湾曲して掘削することがで
きる。
As described above, since the resultant force of the propulsion jacks 3 to 5 is shifted with respect to the geometric center P, the propulsion force of each of the propulsion jacks 3 to 5 is specially controlled. (Even if the propulsion forces of the propulsion jacks 3 to 5 are set equal), the ground G can be curved and excavated.

【0012】また、両側の推進用ジャッキ3,5の推進
力を変更することで、幾何学的中心Pに働くモーメント
の大きさを変更して、掘削する曲線の曲率を容易に変更
することができる。
Also, by changing the propulsion force of the jacks 3 and 5 on both sides, the magnitude of the moment acting on the geometric center P can be changed to easily change the curvature of the excavated curve. it can.

【0013】例えば、推進用ジャッキ3〜5の本数をそ
れぞれ同一とし推進力も等しくした状態では、推進用ジ
ャッキ3〜5の推進力の合力に対する推進用ジャッキ4
の推進力の合力の割合は、(推進用ジャッキ4の本数)/
(推進用ジャッキ3〜5の総本数)となっている。そし
て、推進用ジャッキ4の推進力の合力をこの割合に保持
しておき、両側の推進用ジャッキ3および推進用ジャッ
キ5の推進力を調節することで、幾何学的中心Pに働く
モーメントの大きさを変化させ、これにより所定の推進
力を保持しながら、異なった曲率のトンネルの曲線施工
をすることができる。
For example, in the state where the number of the propulsion jacks 3 to 5 is the same and the propulsion force is equal, the propulsion jacks 4 with respect to the combined propulsion force of the propulsion jacks 3 to 5 are used.
The ratio of the resultant force of the propulsion is (number of propulsion jacks 4) /
(Total number of propulsion jacks 3 to 5). The resultant force of the propulsion jacks 4 is held at this ratio, and the propulsion forces of the propulsion jacks 3 and the propulsion jacks 5 on both sides are adjusted, so that the magnitude of the moment acting on the geometric center P is adjusted. In this way, it is possible to construct tunnels having different curvatures while maintaining a predetermined driving force.

【0014】例えば、推進用ジャッキ4の推進力の合力
を一定に保持したまま推進用ジャッキ3の推進力の合力
を所定量だけ低下させ、推進用ジャッキ5の推進力の合
力を同量だけ増加させるようにすれば、異なった曲率の
トンネルの曲線施工をすることができる。
For example, while keeping the resultant force of the propulsion jack 4 constant, the resultant force of the propulsion jack 3 is reduced by a predetermined amount, and the resultant force of the propulsion jack 5 is increased by the same amount. By doing so, it is possible to perform curved construction of tunnels having different curvatures.

【0015】そして、各推進用ジャッキ3〜5の推進力
の合力が幾何学的中心Pに働くモーメントを零になるよ
うに設定することにより、直線施工にも対応することも
可能になる。なお、各推進用ジャッキ3〜5の推進力の
油圧制御は、図示しないが配管に設けられたリリーフ
弁、減圧弁によって行われる。
By setting the resultant force of the propulsion forces of the propulsion jacks 3 to 5 so that the moment acting on the geometric center P becomes zero, it is possible to cope with straight-line construction. Although not shown, the hydraulic control of the propulsion force of each of the propulsion jacks 3 to 5 is performed by a relief valve and a pressure reducing valve provided in a pipe.

【0016】また、上記実施の形態では、三連式のシー
ルド掘進機1において説明したがこれに限定されるもの
ではなく、場合に応じて四連式あるいはそれ以上のカッ
ターヘッドおよび掘進機本体を有するシールド掘進機1
に適応させることもできる。これらの場合、シールド掘
進機1の幾何学的中心Pが第一掘進機本体2A側にある
ようにし、上記のように推進用ジャッキを等しい力で駆
動すると、シールド掘進機1によって曲線施工を行うこ
とができる。シールド掘進機1の幾何学的中心Pが、第
一掘進機本体2A側にずれて存在することで、各推進用
ジャッキ3〜5が推進する第一〜第三掘進機本体2A〜
2Cの推進力を等しいとすると、各推進用ジャッキ3〜
5の推進力を制御することなく地山Gを曲線施工するこ
とができる。
Further, in the above-described embodiment, the description has been given of the triple shield excavator 1. However, the present invention is not limited to this, and a quadruple or more cutter head and an excavator main body may be used as necessary. Shield machine 1
Can also be adapted. In these cases, when the geometric center P of the shield machine 1 is located on the first machine body 2A side, and the propulsion jack is driven with the same force as described above, the shield machine 1 performs a curved construction. be able to. Since the geometric center P of the shield machine 1 is shifted toward the first machine body 2A, the first to third machine bodies 2A to which the propulsion jacks 3 to 5 protrude.
Assuming that the propulsion of 2C is equal, each propulsion jack 3 ~
The curved ground G can be constructed without controlling the propulsion force of the fifth embodiment.

【0017】[0017]

【発明の効果】以上の説明から明らかな通り、本発明
は、三個以上の掘進機本体を隣り合わせて設けるととも
に、一方の掘進機本体から他方の掘進機本体を順に前後
方向にずらして配置するよう構成したので、各掘進機本
体に与える推進力を変更するとなく等しい推進力を付与
して曲線施工が容易にできる。
As is apparent from the above description, according to the present invention, three or more excavator bodies are provided adjacent to each other, and one excavator main body is sequentially shifted in the front-rear direction from the other excavator main body. With such a configuration, the same propulsion force is applied without changing the propulsion force applied to each of the excavator bodies, and the curve construction can be easily performed.

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

【図1】本発明の実施の形態を示すシールド掘進機の要
部概略平面図である。
FIG. 1 is a schematic plan view of a main part of a shield machine showing an embodiment of the present invention.

【図2】同じく正面図である。FIG. 2 is a front view of the same.

【図3】従来のシールド掘進機の要部概略平面図であ
る。
FIG. 3 is a schematic plan view of a main part of a conventional shield machine.

【図4】同じく平面図である。FIG. 4 is a plan view of the same.

【符号の説明】[Explanation of symbols]

1 シールド掘進機 2A 第一掘進機本体 2B 第二掘進機本体 2C 第三掘進機本体 3 推進用ジャッキ 4 推進用ジャッキ 5 推進用ジャッキ 6 補助翼 G 地山 P 幾何学的中心 Reference Signs List 1 shield excavator 2A first excavator main body 2B second excavator main body 2C third excavator main body 3 jack for propulsion 4 jack for propulsion 5 jack for propulsion 6 auxiliary wing G ground mountain P geometric center

───────────────────────────────────────────────────── フロントページの続き (72)発明者 中山 耕一郎 大阪府大阪市住之江区南港北1丁目7番89 号 日立造船株式会社内 Fターム(参考) 2D054 AA02 AB03 GA04 GA34 GA56 ──────────────────────────────────────────────────続 き Continuation of the front page (72) Inventor Koichiro Nakayama 1-89, Minami Kohoku, Suminoe-ku, Osaka-shi, Osaka F-term in Hitachi Zosen Corporation 2D054 AA02 AB03 GA04 GA34 GA34 GA56

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】 三個以上の掘進機本体を隣り合わせて設
けるとともに、一方の掘進機本体から他方の掘進機本体
を順に前後方向にずらして配置するよう構成したことを
特徴とするシールド掘進機。
1. A shield machine wherein three or more machine bodies are provided adjacent to each other, and one machine body is sequentially shifted from the other machine body in the front-rear direction.
【請求項2】 両側の掘進機本体の少なくとも一方に、
掘進機本体に対して後方に向けて地山側に所定角度で出
没自在な補助翼が設けられたことを特徴とする請求項1
記載のシールド掘進機。
2. At least one of the machine bodies on both sides,
2. An auxiliary wing, which is provided at a predetermined angle on the ground side toward the rear with respect to the excavator main body, and is capable of protruding and retracting at a predetermined angle.
The shield machine described.
【請求項3】 三個以上の掘進機本体を隣り合わせて設
けるとともに、一方の掘進機本体から他方の掘進機本体
を順に前後方向に配置するようし、各掘進機本体に等し
い推進力を付与して曲線施工をすることを特徴とするシ
ールド掘進機におけるトンネル施工方法。
3. An excavator body having three or more excavator bodies adjacent to each other, and one excavator body being disposed in order from the other excavator body in the front-rear direction so as to impart the same propulsion force to each excavator body. A tunnel construction method for a shield machine, wherein the tunnel construction is performed by a curved construction.
【請求項4】 各掘進機本体に等しい推進力を付与する
代わりに異なった推進力を付与して曲線施工する曲率を
変更することを特徴とする請求項3記載のシールド掘進
機におけるトンネル施工方法。
4. The tunnel construction method in a shield machine according to claim 3, wherein a different propulsion force is applied to each excavator body instead of applying the same propulsion force to change the curvature for performing the curve construction. .
JP25734898A 1998-09-11 1998-09-11 Shield machine and tunnel construction method in shield machine Expired - Fee Related JP3640537B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25734898A JP3640537B2 (en) 1998-09-11 1998-09-11 Shield machine and tunnel construction method in shield machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25734898A JP3640537B2 (en) 1998-09-11 1998-09-11 Shield machine and tunnel construction method in shield machine

Publications (2)

Publication Number Publication Date
JP2000087683A true JP2000087683A (en) 2000-03-28
JP3640537B2 JP3640537B2 (en) 2005-04-20

Family

ID=17305139

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25734898A Expired - Fee Related JP3640537B2 (en) 1998-09-11 1998-09-11 Shield machine and tunnel construction method in shield machine

Country Status (1)

Country Link
JP (1) JP3640537B2 (en)

Also Published As

Publication number Publication date
JP3640537B2 (en) 2005-04-20

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