JP3142242B2 - Promotion method - Google Patents

Promotion method

Info

Publication number
JP3142242B2
JP3142242B2 JP25107596A JP25107596A JP3142242B2 JP 3142242 B2 JP3142242 B2 JP 3142242B2 JP 25107596 A JP25107596 A JP 25107596A JP 25107596 A JP25107596 A JP 25107596A JP 3142242 B2 JP3142242 B2 JP 3142242B2
Authority
JP
Japan
Prior art keywords
propulsion
head
receiving surface
bending
axis
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.)
Expired - Fee Related
Application number
JP25107596A
Other languages
Japanese (ja)
Other versions
JPH1061377A (en
Inventor
輝夫 壁内
正也 服部
孝志 十川
幸重 山田
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.)
Kubota Corp
Original Assignee
Kubota 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 Kubota Corp filed Critical Kubota Corp
Priority to JP25107596A priority Critical patent/JP3142242B2/en
Priority to US08/886,220 priority patent/US5878825A/en
Priority to EP97111234A priority patent/EP0816627B1/en
Priority to DE69725053T priority patent/DE69725053T2/en
Publication of JPH1061377A publication Critical patent/JPH1061377A/en
Application granted granted Critical
Publication of JP3142242B2 publication Critical patent/JP3142242B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Excavating Of Shafts Or Tunnels (AREA)

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、例えば、ガス管・
ケーブル管・水道管等の埋設管を地中に敷設するための
地中穴を形成する技術に関し、さらに詳しくは、ヘッド
軸芯に対して傾斜した受圧面部を備えた推進ヘッドを設
けると共に、前記推進ヘッドの後方に屈曲自在に連設し
た複数の推進管を設けて構成してある推進体を使用し、
この推進体に後方から押圧力を作用させて地中推進させ
る推進方法に関する。
[0001] The present invention relates to, for example,
Regarding technology for forming an underground hole for laying underground pipes such as cable pipes and water pipes in the ground, more specifically, a propulsion head having a pressure receiving surface portion inclined with respect to the head axis, Using a propulsion body that is configured by providing a plurality of propulsion tubes that are flexibly connected behind the propulsion head,
The present invention relates to a propulsion method in which a thrust is applied to the propulsion body from behind to propelle underground.

【0002】[0002]

【従来の技術】推進体は、推進に伴って受圧面部に作用
する地盤反力で、その作用方向に屈曲するように誘導さ
れながら地中を進んでいく訳であるが、従来、この種の
推進方法としては、予め、前記推進体をどの方向にも屈
曲できるように構成しておき、曲進推進部においては、
前記受圧面部を、曲げる方向とは反対側に向けたまま推
進させる方法をとっていた。また、直進推進部において
は、前記推進体の受圧面部を、所定推進サイクル毎に正
逆反転させて蛇行推進させ、計画直線に沿った蛇行線と
なるように推進制御を行う方法をとっていた。
2. Description of the Related Art A propelling body travels underground while being guided to bend in the direction of action by a ground reaction force acting on a pressure-receiving surface portion during propulsion. As a propulsion method, in advance, the propulsion body is configured so as to be able to bend in any direction.
A method has been adopted in which the pressure receiving surface portion is propelled while being directed to the side opposite to the bending direction. Further, in the straight propulsion unit, the pressure receiving surface portion of the propulsion body is meanderingly propelled by reversing the direction of the pressure every predetermined propulsion cycle, and the propulsion is controlled so as to form a meandering line along a planned straight line. .

【0003】[0003]

【発明が解決しようとする課題】従来の推進方法によれ
ば、推進体をどの方向にも屈曲できるように形成してあ
るから、どの方向にも屈曲推進させることができる反
面、前記受圧面部の向く方向が、本来向けなければなら
ない方向からずれていた場合、そのまま推進すれば予定
とする屈曲方向からずれた方向に推進体が進むことにな
り、推進の方向制御が複雑化し易いという問題点があ
る。この問題点は、曲線推進部のみならず、直線推進さ
せる際にも、不用意に推進体が屈曲し易いことから、同
様に懸念され、計画推進線から推進体がずれれば、それ
に伴って、計画推進線に推進経路を戻すための制御がそ
の都度必要となり、推進作業が煩雑になり易いという問
題点がある。
According to the conventional propulsion method, since the propulsion body is formed so as to be bent in any direction, it can be bent and propelled in any direction. If the heading direction deviates from the direction to which it should be directed, the propulsion body will advance in the direction deviating from the intended bending direction if propelled as it is, and the control of the propulsion direction tends to be complicated. is there. This problem is not only caused by the curved propulsion section, but also by the straight propulsion, because the propulsion body is easily carelessly bent. In addition, control for returning the propulsion route to the planned propulsion line is required each time, and there is a problem that the propulsion work tends to be complicated.

【0004】従って、本発明の目的は、前記問題点を解
消し、複雑な方向制御を実施しなくても、精度よく推進
体を推進させることができる推進方法を提供するところ
にある。
Accordingly, an object of the present invention is to solve the above-mentioned problems and to provide a propulsion method capable of accurately propelling a propulsion body without performing complicated direction control.

【0005】[0005]

【課題を解決するための手段】[Means for Solving the Problems]

〔構成〕請求項1の発明の特徴手段は、ヘッド軸芯に対
して傾斜した受圧面部を備えた推進ヘッドを設けると共
に、前記推進ヘッドの後方に屈曲自在に連設した複数の
推進管を設けて構成してある推進体を使用し、この推進
体に後方から押圧力を作用させて地中推進させるにあた
り、予め、前記推進管の屈曲軸芯が一軸になるように前
記推進体を構成しておき、前記受圧面部を、前記屈曲軸
芯周りの前記推進管の揺動方向に沿う方向に向けて推進
するところにある。
[Structure] The characteristic feature of the invention of claim 1 is to provide a propulsion head having a pressure receiving surface portion inclined with respect to the head axis, and a plurality of propulsion tubes connected to the back of the propulsion head so as to be freely bent. In the case of using a propulsion body configured as described above and applying a pressing force to the propulsion body from behind to perform underground propulsion, the propulsion body is configured in advance so that the bending axis of the propulsion pipe is uniaxial. In addition, the pressure receiving surface portion is propelled in a direction along the swing direction of the propulsion pipe around the bending axis.

【0006】請求項2の発明の特徴手段は、ヘッド軸芯
に対して傾斜した受圧面部を、ヘッド本体に対して前記
ヘッド軸芯周りに回転駆動自在に取り付た推進ヘッドを
設けると共に、前記推進ヘッドの後方に屈曲自在に連設
した複数の推進管を設けて構成してある推進体を使用
し、この推進体に後方から押圧力を作用させて地中推進
させるにあたり、予め、前記推進管の屈曲軸芯が一軸に
なるように前記推進体を構成しておき、曲進推進部にお
いては、前記受圧面部を、前記屈曲軸芯周りの前記推進
管の揺動方向に沿う方向に向けて推進し、直進推進部に
おいては、前記受圧面部を、前記屈曲軸芯方向に沿う方
向に向けて推進するところにある。
A second feature of the present invention is to provide a propulsion head having a pressure receiving surface portion inclined with respect to a head axis rotatably attached to a head main body so as to be rotatable around the head axis. A propulsion body having a plurality of bendable propulsion tubes provided behind the propulsion head is used, and when a thrust is applied to the propulsion body from behind to perform underground propulsion, the propulsion is performed in advance. The propulsion body is configured so that the bending axis of the pipe is uniaxial, and in the bending propulsion unit, the pressure receiving surface portion is oriented in a direction along the swing direction of the propulsion pipe around the bending axis. In the straight-moving propulsion part, the pressure receiving surface is propelled in a direction along the bending axis direction.

【0007】〔作用及び効果〕請求項1の発明の特徴手
段によれば、予め、前記推進管の屈曲軸芯が一軸になる
ように前記推進体を構成しておくから、推進に伴う推進
体の屈曲方向は、前記一軸の屈曲軸芯周りにのみ許容さ
れ、不用意に意図しない方向に屈曲推進されるのを防止
できる。そして、推進方向制御を簡単化することが可能
となる。更には、前記受圧面部を、前記屈曲軸芯周りの
前記推進管の揺動方向に沿う方向に向けて推進するか
ら、前記受圧面部に作用する土圧を、推進体の屈曲力に
効率よく作用させることが可能となる。即ち、複雑な方
向制御を実施しなくても、精度よく、且つ、効率よく推
進体を屈曲推進させることができる。
According to the first aspect of the present invention, the propulsion body is configured in advance so that the bending axis of the propulsion pipe is uniaxial. Is allowed only around the uniaxial bending axis, and can be prevented from being accidentally bent in an unintended direction. And it becomes possible to simplify propulsion direction control. Furthermore, since the pressure receiving surface portion is propelled in a direction along the swing direction of the propulsion pipe around the bending axis, the earth pressure acting on the pressure receiving surface portion efficiently acts on the bending force of the propulsion body. It is possible to do. In other words, the propulsion body can be bent and propelled accurately and efficiently without performing complicated direction control.

【0008】請求項2の発明の特徴手段によれば、予め
前記推進管の屈曲軸芯が一軸になるように前記推進体を
構成し、曲進推進部においては、前記受圧面部を、前記
屈曲軸芯周りの前記推進管の揺動方向に沿う方向に向け
て推進するから、従来のように予定しない方向に推進体
が曲るということを回避し易く、前記受圧面部に作用す
る地盤反力によって推進体が前記受圧面部の向く方向と
は反対側に、且つ、前記屈曲軸芯周りに屈曲し、予定ど
うり曲線推進させることができる。また、直進推進部に
おいては、前記受圧面部を、前記屈曲軸芯方向に沿う方
向に向けて推進するから、前記受圧面部に作用する地盤
反力の作用方向が、前記屈曲軸芯を含む面に沿うことに
なり、前記受圧面部に地盤反力が作用しても、その地盤
反力によって推進体が前記屈曲軸芯周りに屈曲すること
はなく、より直線的に推進させることが可能となる。そ
の結果、計画推進線から推進経路がずれ難くなり、且
つ、それに伴うズレ修正のための制御も頻繁に実施する
必要がなくなり、精度よく且つ効率よく推進することが
可能となる。
According to the characteristic feature of the second aspect of the present invention, the propulsion body is configured so that the bending axis of the propulsion tube is uniaxial in advance, and in the bending propulsion portion, the pressure receiving surface portion is formed by the bending. Since the propulsion is performed in the direction along the swinging direction of the propulsion pipe around the axis, it is easy to prevent the propulsion body from bending in an unexpected direction as in the related art, and the ground reaction force acting on the pressure receiving surface portion As a result, the propulsion body is bent on the opposite side to the direction in which the pressure-receiving surface portion faces and around the bending axis, and can be propelled in a predetermined curve. Further, in the straight running propulsion portion, since the pressure receiving surface portion is propelled in a direction along the bending axis center direction, the action direction of the ground reaction force acting on the pressure receiving surface portion is a surface including the bending axis center. Accordingly, even when a ground reaction force acts on the pressure receiving surface portion, the propulsion body does not bend around the bending axis due to the ground reaction force, and can be propelled more linearly. As a result, the propulsion route is less likely to deviate from the planned propulsion line, and it is not necessary to frequently perform the control for correcting the deviation, thereby enabling accurate and efficient propulsion.

【0009】[0009]

【発明の実施の形態】以下に本発明の実施の形態を図面
に基づいて説明する。
Embodiments of the present invention will be described below with reference to the drawings.

【0010】〔第一実施形態〕推進体Sは、図1〜図2
(複数の推進管の連結状態を示す図面)に示すように、
外面略円筒面状の推進ヘッド1と、その推進ヘッド1の
後方に連設した複数の推進管2とを設けた推進本体3で
構成し、前記推進本体3に、その長手方向に間隔をあけ
て複数の屈曲連結部R1と複数の非屈曲連結部R2とを
それぞれ設けてある。
[First Embodiment] FIG.
As shown in (a drawing showing the connection state of multiple propulsion pipes),
The propulsion head 3 includes a propulsion head 1 having a substantially cylindrical outer surface and a plurality of propulsion pipes 2 connected to the rear of the propulsion head 1. The propulsion main body 3 is spaced apart in its longitudinal direction. A plurality of bent connection portions R1 and a plurality of non-bend connection portions R2.

【0011】前記推進ヘッド1は、図2に示すように、
金属製の筒状体で形成してあると共に、先端部の閉塞部
分には、ヘッド軸芯Pに対して傾斜した受圧面部Fを一
体に形成してある。そして、推進に伴って受圧面部Fが
土圧を受けることによって、受圧面部Fが向く方向とは
反対側に推進ヘッド1が誘導され、方向転換していくよ
うになっている。また、推進ヘッド1の中間部には、前
記屈曲連結部R1の一つが設けてある。そして、この屈
曲連結部R1は、前記推進本体3の径方向に沿う横軸芯
(屈曲軸芯の一例)X周りにのみ屈曲自在に形成してあ
る。また、前記受圧面部Fは、前記横軸芯Xに直交する
方向に向けて形成してある。推進ヘッド1の基端部に
は、前記非屈曲連結部R2の一方の分割部4aが設けて
ある。
The propulsion head 1 is, as shown in FIG.
A pressure receiving surface portion F inclined with respect to the head axis P is formed integrally with a closed portion of the tip portion while being formed of a metal cylindrical body. Then, when the pressure receiving surface portion F receives the earth pressure with the propulsion, the propulsion head 1 is guided to the side opposite to the direction in which the pressure receiving surface portion F faces, and changes direction. In the middle part of the propulsion head 1, one of the bent connection portions R1 is provided. The bent connecting portion R1 is formed to be bendable only around a horizontal axis (an example of a bent axis) X along the radial direction of the propulsion main body 3. Further, the pressure receiving surface portion F is formed in a direction orthogonal to the horizontal axis X. At the base end of the propulsion head 1, one of the divided portions 4a of the non-flexible connecting portion R2 is provided.

【0012】前記推進管2は、例えば、口径が約50m
m程度又はそれ以下の極小口径金属筒で構成してあり、
その先端部(推進方向での前方端部)には、前記非屈曲
部連結部R2の一方の分割部4aと着脱自在な他方の分
割部4bを設けてある。また、推進管2の基端部(推進
方向での後方端部)には、前記推進ヘッド1と同様に一
方の分割部4aを設けてある。尚、前記一方の分割部4
aと他方の分割部4bとを連結させることで、連結状態
の非屈曲連結部R2が構成される。また、推進管2の中
間部には、図に示すように、二つの屈曲連結部R1を各
別に設けてある。従って、推進管2は、両端部に各別に
形成された両分割部4a・4bと、三つの推進管部2a
と、各推進管部2a間に形成された二つの屈曲連結部R
1とから構成されている。
The propulsion pipe 2 has, for example, a diameter of about 50 m.
m or less of a very small diameter metal cylinder,
At the tip (the front end in the propulsion direction), one split portion 4a of the non-bent portion connecting portion R2 and the other split portion 4b that is detachable are provided. At the base end (the rear end in the propulsion direction) of the propulsion pipe 2, one divided portion 4 a is provided similarly to the propulsion head 1. In addition, the one divided portion 4
By connecting a to the other divided portion 4b, a non-bend connecting portion R2 in a connected state is formed. As shown in the figure, two bent connecting portions R1 are separately provided in the intermediate portion of the propulsion pipe 2. Therefore, the propulsion pipe 2 has two divided sections 4a and 4b formed separately at both ends and three propulsion pipe sections 2a.
And two bent connecting portions R formed between the propulsion pipe portions 2a.
And 1.

【0013】前記屈曲連結部R1を、更に詳しく説明す
ると、図2〜図8に示すように、一方の推進管部2aの
端部(前端部)に筒状の球面嵌合部18を設け、他方の
推進管部2aの端部(後端部)に、前記球面嵌合部18
に内嵌係合自在な球状嵌合部7を設け、両嵌合部7・1
8どうしを嵌合させて構成してある。前記球面嵌合部1
8は、先窄み形状の筒部材(第一カバー筒部の一例)8
と、その筒部材8内周部の雌ネジ部8bに螺合して前記
一方の推進管部2aと連結する連結筒19とを設けて構
成してあり、前記筒部材8・連結筒19の一端部(前端
側)の内周面は、前記球状嵌合部7の外周面に沿う凹面
形状に形成してある。また、筒部材8の窄み部分の外周
面は、前記両推進管部2aどうしの屈曲芯を中心とした
凸状の曲面(球面)形状に形成してある。この凸状の曲
面形状部分を曲面部8aという(図5参照)。そして、
窄み部分の端面部(前端側)は、二平面からなる平面部
8dに形成してある。因に、前記筒部材8は、後述する
摺接筒部材17とで、屈曲連結部R1をカバーするよう
に構成してある。一方、前記球状嵌合部7は、その一端
部に、前記推進管部2aに内嵌状態に螺合自在な雄ネジ
部7aを形成してあり、他端部には、前記球面嵌合部1
8の一端部(前端側)の内周面に沿う形状の球状部7b
を設けてある。そして、球状嵌合部7と球面嵌合部18
とは、嵌合させた状態で、前記横軸芯X周りの屈曲揺動
が可能なように二つのピン9で連結してある。尚、前記
ピン9の一端部は、前記球状嵌合部7の外面の一部(相
対向する2箇所)に深さ方向が前記横軸芯Xに沿う状態
で形成された凹部7dに殆ど隙間なく挿入され、且つ、
前記ピン9の他端部は、前記球面嵌合部18の一部(前
記凹部7dに対応する位置2箇所)に貫通方向が前記横
軸芯Xに沿う状態で形成された貫通ネジ孔8eに螺合挿
入されるようになっており、そのピン9の両端部挿入に
基づく係合により、前記屈曲連結部R1の前記横軸芯X
周りの屈曲揺動が図6に示すように可能な構成となって
いる。尚、一本の推進管2に形成してある二つの屈曲連
結部R1は、それぞれの横軸芯Xどうしが平行になるよ
うに構成してある。
The bent connecting portion R1 will be described in more detail. As shown in FIGS. 2 to 8, a cylindrical spherical fitting portion 18 is provided at one end (front end) of one propulsion pipe portion 2a. The spherical fitting portion 18 is attached to the end (rear end) of the other propulsion tube 2a.
Are provided with spherical fitting portions 7 which can be internally fitted and engaged with each other.
8 are fitted together. The spherical fitting portion 1
Reference numeral 8 denotes a tapered cylindrical member (an example of a first cover cylindrical portion).
And a connecting tube 19 which is screwed to the female screw portion 8b of the inner peripheral portion of the cylindrical member 8 and is connected to the one propulsion tube portion 2a. The inner peripheral surface at one end (front end side) is formed in a concave shape along the outer peripheral surface of the spherical fitting portion 7. The outer peripheral surface of the constricted portion of the tubular member 8 is formed in a convex curved surface (spherical surface) centered on the bent core between the two propulsion pipes 2a. This convex curved surface portion is referred to as a curved surface portion 8a (see FIG. 5). And
The end face portion (front end side) of the constricted portion is formed in a flat portion 8d composed of two flat surfaces. Incidentally, the tubular member 8 is configured to cover the bent connection portion R1 with a sliding contact tubular member 17 described later. On the other hand, the spherical fitting portion 7 has, at one end thereof, a male screw portion 7a which can be screwed into the propulsion tube portion 2a in an internally fitted state, and the other end portion has the spherical fitting portion 7a. 1
8 has a spherical portion 7b along the inner peripheral surface at one end (front end side).
Is provided. Then, the spherical fitting portion 7 and the spherical fitting portion 18
Is connected by two pins 9 so as to be able to bend and swing around the horizontal axis X in the fitted state. Note that one end of the pin 9 is almost free from a concave portion 7d formed in a part (two opposing positions) of the outer surface of the spherical fitting portion 7 so that the depth direction is along the horizontal axis X. Inserted without
The other end of the pin 9 has a through screw hole 8e formed in a part of the spherical fitting portion 18 (at two positions corresponding to the concave portion 7d) with a penetrating direction along the horizontal axis X. The horizontal axis X of the bent connection portion R1 is engaged by the engagement based on the insertion of both ends of the pin 9.
As shown in FIG. 6, it is configured such that the surrounding bending and swinging is possible. The two bent connecting portions R1 formed on one propulsion pipe 2 are configured such that their respective horizontal axes X are parallel to each other.

【0014】また、前記球状嵌合部7を螺合させてある
方の推進管部2aの端部(後端部)には、前記筒部材8
に外嵌して屈曲連結部R1を覆う摺接筒部材17を延出
状態に設けてある。前記摺接筒部材17の端部(後端
部)の内周部には、前記筒部材8と摺接筒部材17とを
嵌合させた状態で前記曲面部8aに摺接して両推進管部
2a間の隙間を閉塞する摺接部10を設けてある。この
摺接部10は、前記曲面部8aと面接触するように構成
してある。一方、摺接筒部材17の端部(後端部)の外
周部は、図5に示すように、先窄み形状に構成してあ
り、この窄み部10aを設けてあることによって、前記
屈曲連結部R1の屈曲に伴って、周囲の土を傾斜に沿っ
て管外方側へ誘導することが可能となり、屈曲連結部R
1内空部への土の侵入防止を図っている。また、この推
進管部2aの端面部(前記摺接部10の内側に位置す
る)11は、平面に形成してあり、前記横軸芯X周りの
屈曲に伴って、前記球面嵌合部18の先端に形成してあ
る二つの平面部8dの何れか一面が面当接し、両推進管
部2aどうしの最大屈曲角度を規制するように構成して
ある。前記平面部8d及び前記端面部11は、共に角度
規制用対向部dに相当し、これら角度規制用対向部dの
対向方向は、前記推進管部2aの長手方向に沿って設定
してある。従って、角度規制状態での推進力は、推進管
部2aの長手方向に沿った圧縮力で両部間に伝達され、
曲げ力やセン断力が大きく作用するものに比べて効率よ
く応力伝達を叶えることが可能となる。また、前記平面
部8d及び端面部11を角度規制手段Dという。一方、
前記球状嵌合部7と、前記平面部8dと、前記端面部1
1との間の空間には、グリースGを充填してあり、屈曲
連結部R1外方から推進管2の内空部へ、両推進管部2
a間の境目を通して土や地下水が入り込むのを防ぐと共
に、屈曲するに伴う摩擦力の低減を図ってある。
The cylindrical member 8 is attached to the end (rear end) of the propulsion tube 2a on which the spherical fitting portion 7 is screwed.
The sliding contact cylindrical member 17 which is fitted to the outside and covers the bent connecting portion R1 is provided in an extended state. An inner peripheral portion of an end portion (rear end portion) of the sliding contact cylindrical member 17 is brought into sliding contact with the curved surface portion 8a in a state where the cylindrical member 8 and the sliding contact cylindrical member 17 are fitted to each other. A sliding contact portion 10 for closing a gap between the portions 2a is provided. The sliding contact portion 10 is configured to make surface contact with the curved surface portion 8a. On the other hand, as shown in FIG. 5, the outer peripheral portion of the end portion (rear end portion) of the sliding contact cylindrical member 17 is formed to have a tapered shape. With the bending of the bent connecting portion R1, the surrounding soil can be guided to the outside of the pipe along the slope, and the bent connecting portion R
1) Prevents intrusion of soil into the inner space. Further, an end face portion (located inside the sliding contact portion 10) 11 of the propulsion tube portion 2a is formed in a plane, and the spherical fitting portion 18 is bent with the bending around the horizontal axis X. Any one of the two flat portions 8d formed at the end of the protruding portion comes into surface contact with each other to regulate the maximum bending angle between the two propulsion pipe portions 2a. The flat portion 8d and the end surface portion 11 both correspond to an angle regulating opposing portion d, and the facing direction of the angle regulating opposing portion d is set along the longitudinal direction of the propulsion tube portion 2a. Therefore, the propulsion force in the angle-restricted state is transmitted between the propulsion pipe portion 2a by a compression force along the longitudinal direction,
It is possible to efficiently transmit the stress as compared with the one in which the bending force and the shearing force largely act. The flat portion 8d and the end surface portion 11 are referred to as angle restricting means D. on the other hand,
The spherical fitting portion 7, the flat portion 8d, and the end face portion 1
1 is filled with grease G, and from the outside of the bent connection portion R1 to the inner space of the propulsion tube 2, the two propulsion tube portions 2
In addition to preventing soil and groundwater from entering through the boundary between points a, the frictional force accompanying bending is reduced.

【0015】前記非屈曲連結部R2を説明すると、図9
に示すように、噛み合わせ一体化部12によって分離自
在に連結されており、必要に応じて(その必要性は、例
えば、前記推進本体3をできるだけコンパクトに巻き取
っておきたい場合等に生じる)分離できるようになって
いる。尚、前記噛み合わせ一体化部12においては、前
記一方の分割部4aに形成してある凸部12aと、前記
他方の分割部4bに形成してある凹部12bとの噛み合
わせ状態が、雄ネジ部(前記他方の分割部4bに形成し
てある)12dへの雌ネジ体(前記一方の分割部4aに
形成してある)12eの螺合固定により、前記分離自在
な連結が実行されるようになっている。また、前記凸部
12aと凹部12bとは、互いの嵌合状態が、推進管軸
芯周りに180度のみ位相ずれ可能な状態に形成してあ
る。従って、当該非屈曲連結部R2で連結された推進管
2の前記横軸芯Xは、互いに平行な状態になる。前記凸
部12aと凹部12bとで、位置決め機構13は構成し
てある。
The non-flexible connecting portion R2 will be described with reference to FIG.
As shown in FIG. 2, the propulsion body 3 is detachably connected by the meshing integrated portion 12 and can be separated as required (for example, the need arises when the propulsion main body 3 is to be wound up as compactly as possible). It has become. Incidentally, in the meshing integrated portion 12, the meshing state between the convex portion 12a formed on the one divided portion 4a and the concave portion 12b formed on the other divided portion 4b is an external thread. The separable connection is performed by screwing and fixing a female screw body (formed on the one divided portion 4a) 12e to a portion (formed on the other divided portion 4b) 12d. It has become. The convex portion 12a and the concave portion 12b are formed in such a state that their fitting state can be shifted only by 180 degrees around the axis of the propulsion pipe. Therefore, the horizontal axes X of the propulsion pipes 2 connected by the non-flexible connection portion R2 are in a state of being parallel to each other. The projection 12a and the recess 12b constitute a positioning mechanism 13.

【0016】上述の推進体Sを使用して実施される本実
施形態の推進は、図1に示すように、予め発進位置に形
成されたピットTから、前記ピットT内に配置した押込
装置Mで前記推進体Sを所定の方向(本実施形態では、
斜め上方)に向けて土中推進させる訳であるが、推進体
Sを最初にセットする時に、前記受圧面部Fが下方を向
く状態に推進ヘッド1を位置決めして、後は、その推進
ヘッド1に、前記非屈曲連結部R2で推進管2を連結す
れば、推進体Sの各屈曲連結部R1の屈曲軸芯が横姿勢
になって、押込装置Mで地中へ押し込むことによって、
推進体Sが斜め上方へ屈曲しながら、簡単にスピーディ
ーに曲線推進を実施することが可能となる。
As shown in FIG. 1, the propulsion according to the present embodiment, which is carried out by using the above-described propulsion body S, starts from a pit T formed at a starting position in advance and pushes in a pushing device M disposed in the pit T. In the predetermined direction (in the present embodiment,
This means that the propulsion head 1 is positioned so that the pressure receiving surface portion F faces downward when the propulsion body S is first set. When the propulsion pipe 2 is connected to the non-bending connection portion R2, the bending axis of each bending connection portion R1 of the propulsion body S is in a horizontal posture, and is pushed into the ground by the pushing device M.
While the propulsion body S bends obliquely upward, it is possible to easily and speedily perform curve propulsion.

【0017】〔第二実施形態〕推進体Sは、図10〜図
12に示すように、小口径(例えば、口径が100mm
程度又はそれ以下の小径)の推進管2の複数個を、前記
推進管2の軸芯方向と直交する横軸芯(屈曲軸芯の一
例)X周りに屈曲揺動自在な連結部Rを介して屈曲自在
に連結し、それら推進管2の最先端部に、外面略円筒面
状の推進ヘッド1を連結することにより構成されてい
る。尚、本実施形態においては、前記推進ヘッド1と推
進管2との連結部分も、前記複数の推進管2の相互間を
連結する連結部分も、ともに前記連結部Rで構成されて
いる。
[Second Embodiment] As shown in FIGS. 10 to 12, the propulsion body S has a small diameter (for example, a diameter of 100 mm).
A plurality of propulsion pipes 2 having a small diameter of the order of or less) are connected via a connecting portion R which is capable of bending and swinging around a horizontal axis (an example of a bending axis) X orthogonal to the axial direction of the propulsion pipe 2. The propulsion tube 2 is configured to be connected to a propelling head 1 having a substantially cylindrical outer surface at the foremost portion thereof. In the present embodiment, both the connection portion between the propulsion head 1 and the propulsion tube 2 and the connection portion for connecting the plurality of propulsion tubes 2 to each other are configured by the connection portion R.

【0018】前記連結部Rは、更に詳しくは、図10・
11・4に示すように、各推進管2の先端部に設けられ
た球状嵌合部7と、各推進管2の基端部に設けられて前
記球状嵌合部7を内嵌係合自在な球面嵌合部8とを、前
記横軸芯X周りの屈曲揺動が可能なようにピン9で連結
したものである。尚、前記ピン9の一端部は、前記球状
嵌合部7の外面の一部(相対向する2箇所)に深さ方向
が前記横軸芯Xに沿う状態で形成された凹部7dに殆ど
隙間なく挿入され、且つ、前記ピン9の他端部は、前記
球面嵌合部8の一部(前記凹部7dに対応する位置2箇
所)に貫通方向が前記横軸芯Xに沿う状態で形成された
貫通ネジ孔8eに螺合挿入されるようになっており、そ
のピン9の両端部挿入に基づく係合により、前記連結部
Rの前記横軸芯X周りの屈曲揺動が図12に示すように
可能な構成となっている。尚、前記ピン9の一端部の太
さを変えて、そのピン9の一端部を前記凹部7dへ十分
な隙間をあけて挿入するようにすれば、前記連結部R
は、前記隙間が許す限り、任意な屈曲揺動が行えるよう
になる。即ち、前記ピン9の差し替えで、前記連結部R
を、前記横軸芯X周りの屈曲揺動が可能な状態から、任
意な屈曲揺動が行える状態へ、容易に変更することがで
きるようになっている。
The connecting portion R is described in more detail in FIG.
As shown in 11.4, the spherical fitting portion 7 provided at the distal end portion of each propulsion tube 2 and the spherical fitting portion 7 provided at the base end portion of each propulsion tube 2 can be internally fitted and engaged. Are connected by a pin 9 so as to be able to bend and swing around the horizontal axis X. Note that one end of the pin 9 is almost free from a concave portion 7d formed in a part (two opposing positions) of the outer surface of the spherical fitting portion 7 so that the depth direction is along the horizontal axis X. And the other end of the pin 9 is formed in a part of the spherical fitting portion 8 (at two positions corresponding to the concave portion 7d) so that the penetration direction is along the horizontal axis X. FIG. 12 shows that the connecting portion R is bent and swung around the horizontal axis X by the engagement based on the insertion of both ends of the pin 9 into the through screw hole 8e. It has a possible configuration. If the thickness of one end of the pin 9 is changed and one end of the pin 9 is inserted into the recess 7d with a sufficient gap, the connecting portion R
Can perform arbitrary bending and swinging as long as the gap allows. That is, by replacing the pin 9, the connecting portion R
Can be easily changed from a state in which bending and swinging around the horizontal axis X is possible to a state in which arbitrary bending and swinging can be performed.

【0019】前記複数の推進管2の中から選択された幾
つかの推進管2の中間部は、第一実施形態で説明したも
のと同様の構成の噛み合わせ一体化部(図9参照)12
によって分離自在に連結してある。
An intermediate portion of some of the propulsion tubes 2 selected from the plurality of propulsion tubes 2 has a meshing integrated portion (see FIG. 9) 12 similar in configuration to that described in the first embodiment.
Are connected so that they can be separated.

【0020】前記推進ヘッド1は、図10に示すよう
に、その本体を構成する筒状のヘッド本体1Aと、駆動
流体(具体的には、作動油や滑材等)の供給に基づいて
推進ヘッドの軸芯(以後、単にヘッド軸芯という)P周
りに回転駆動自在な状態に前記ヘッド本体1Aに内嵌さ
れた駆動軸1Bと、前記駆動軸1Bの先端に取り付けら
れた先導体1Dとから構成されている。前記先導体1D
には、ヘッド軸芯Pに対して傾斜した受圧面部Fを形成
してあり、前記駆動軸1Bを回転駆動させることによっ
て、先導体1Dが適宜姿勢に回転駆動されて、前記受圧
面部Fが適宜方向を向く。そして、推進に伴って受圧面
部Fが土圧を受けることによって、推進管2と推進ヘッ
ド1とが前記横軸芯X周りに屈曲し、前記推進ヘッド1
が方向転換していくようになっている。その際、受圧面
部Fを前記横軸芯X方向に沿う方向に向けてあれば、土
圧は前記横軸芯Xに交わる方向に作用するから、推進体
Sを屈曲させずによりまっすぐに推進させることが可能
となる。因に、前記受圧面部Fの向いている方向は、図
には示さないが、推進ヘッド1に内蔵したセンサーによ
って検知できるように構成してある。
As shown in FIG. 10, the propulsion head 1 is propelled based on a cylindrical head main body 1A constituting the main body thereof and a supply of a driving fluid (specifically, hydraulic oil or a sliding material). A drive shaft 1B fitted inside the head body 1A so as to be rotatable around an axis P of the head (hereinafter simply referred to as a head axis) P, and a leading conductor 1D attached to the tip of the drive shaft 1B. It is composed of The tip conductor 1D
Is formed with a pressure receiving surface portion F inclined with respect to the head axis P, and by rotating the drive shaft 1B, the leading conductor 1D is rotationally driven to an appropriate posture, and the pressure receiving surface portion F is appropriately rotated. Turn in the direction. Then, the propulsion pipe 2 and the propulsion head 1 bend around the horizontal axis X when the pressure receiving surface portion F receives the earth pressure with the propulsion, and the propulsion head 1
Is changing directions. At this time, if the pressure receiving surface portion F is oriented in the direction along the horizontal axis X, the earth pressure acts in a direction intersecting with the horizontal axis X, so that the propulsion body S is propelled straight without bending. It becomes possible. The direction in which the pressure receiving surface portion F faces is not shown in the drawing, but is configured to be detected by a sensor built in the propulsion head 1.

【0021】上述の推進体Sを使用して実施される本実
施形態の推進は、図15に示すように、予め発進位置に
形成されたピットTから、前記ピットT内に配置した押
込装置Mで前記推進体Sを所定の方向に向けて土中推進
させる訳であるが、曲進推進部においては、図14に示
すように、前記受圧面部Fを、前記横軸芯X周りの前記
推進管2の揺動方向に沿う方向(上または下方向)に向
けて推進し、直進推進部においては、図13に示すよう
に、前記受圧面部Fを、前記横軸芯X方向に沿う方向
(横方向)に向けて推進するものである。
As shown in FIG. 15, the propulsion according to the present embodiment, which is carried out using the above-described propulsion body S, starts from a pit T formed in advance at a start position and pushes in a pushing device M disposed in the pit T. In this case, the propulsion body S is propelled under the ground in a predetermined direction. In the curved propulsion unit, as shown in FIG. Propulsion is performed in the direction (upward or downward) along the swinging direction of the pipe 2, and in the straight traveling propulsion section, as shown in FIG. 13, the pressure receiving surface portion F is moved in the direction along the horizontal axis X direction ( (Lateral direction).

【0022】〔別実施の形態〕以下に本発明の別の実施
形態を説明する。前記屈曲軸芯は、先の実施形態で説明
した横軸芯に限るものではなく、例えば、水平面内で右
カーブや左カーブの曲線推進を実施する場合には、前記
屈曲軸芯は縦軸芯に設定する必要がある。
[Another Embodiment] Another embodiment of the present invention will be described below. The bending axis is not limited to the horizontal axis described in the previous embodiment.For example, when performing curve propulsion of a right curve or a left curve in a horizontal plane, the bending axis is a vertical axis. Must be set to

【0023】尚、特許請求の範囲の項に図面との対照を
便利にするために符号を記すが、該記入により本発明は
添付図面の構成に限定されるものではない。
[0023] In the claims, reference numerals are provided for convenience of comparison with the drawings, but the present invention is not limited to the configuration of the attached drawings.

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

【図1】第一実施形態での推進状況を示す側面図FIG. 1 is a side view showing a state of propulsion in a first embodiment.

【図2】第一実施形態の推進体の要部を示す下面視断面
FIG. 2 is a cross-sectional view of a main part of the propulsion body of the first embodiment as viewed from below.

【図3】屈曲連結部の詳細縦断面図FIG. 3 is a detailed vertical sectional view of a bending connection portion.

【図4】屈曲連結部(又は、連結部)の詳細横断面図FIG. 4 is a detailed cross-sectional view of a bent connecting portion (or a connecting portion).

【図5】摺接部を示す断面図FIG. 5 is a sectional view showing a sliding contact portion.

【図6】屈曲連結部の作用説明図FIG. 6 is an explanatory diagram of an operation of a bending connection portion.

【図7】屈曲連結部の分解斜視図FIG. 7 is an exploded perspective view of a bent connection portion.

【図8】屈曲連結部の分解斜視図FIG. 8 is an exploded perspective view of a bent connection portion.

【図9】噛み合わせ一体化部を示す分解斜視図FIG. 9 is an exploded perspective view showing a meshing integrated portion.

【図10】第二実施形態の推進体の要部を示す下面視断
面図
FIG. 10 is a cross-sectional view seen from below showing a main part of the propulsion body of the second embodiment.

【図11】連結部の詳細縦断面図FIG. 11 is a detailed vertical sectional view of a connecting portion.

【図12】連結部の作用説明図FIG. 12 is an explanatory diagram of an operation of a connecting portion.

【図13】第二実施形態の直線部推進状況を示す上面図FIG. 13 is a top view showing a straight section propulsion state according to the second embodiment.

【図14】第二実施形態の曲線部推進状況を示す側面図FIG. 14 is a side view showing a curved part propulsion state of the second embodiment.

【図15】第二実施形態の推進状況を示す側面図FIG. 15 is a side view showing the promotion status of the second embodiment.

【符号の説明】[Explanation of symbols]

1 推進ヘッド 1A ヘッド本体 2 推進管 F 受圧面部 P ヘッド軸芯 S 推進体 X 屈曲軸芯 DESCRIPTION OF SYMBOLS 1 Propulsion head 1A Head main body 2 Propulsion pipe F Pressure receiving surface part P Head axis S Propulsion body X Bending axis

フロントページの続き (72)発明者 山田 幸重 兵庫県尼崎市浜1丁目1番1号 株式会 社クボタ 技術開発研究所内 (56)参考文献 特公 平7−68860(JP,B2) (58)調査した分野(Int.Cl.7,DB名) E21D 9/06 311 Continuing from the front page (72) Inventor Yukishige Yamada 1-1-1, Hama, Amagasaki-shi, Hyogo Pref. Kubota Technology Development Laboratory Co., Ltd. (56) References JP 7-68860 (JP, B2) (58) Survey Field (Int.Cl. 7 , DB name) E21D 9/06 311

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 ヘッド軸芯(P)に対して傾斜した受圧
面部(F)を備えた推進ヘッド(1)を設けると共に、
前記推進ヘッド(1)の後方に屈曲自在に連設した複数
の推進管(2)を設けて構成してある推進体(S)を使
用し、この推進体(S)に後方から押圧力を作用させて
地中推進させる推進方法であって、 予め、前記推進管(2)の屈曲軸芯(X)が一軸になる
ように前記推進体(S)を構成しておき、前記受圧面部
(F)を、前記屈曲軸芯(X)周りの前記推進管(2)
の揺動方向に沿う方向に向けて推進する推進方法。
1. A propulsion head (1) having a pressure receiving surface (F) inclined with respect to a head axis (P) is provided.
A propulsion body (S) having a plurality of bendable propulsion tubes (2) provided behind the propulsion head (1) is used, and a pressing force is applied to the propulsion body (S) from behind. A propulsion method for underground propulsion by acting, wherein the propulsion body (S) is configured so that the bending axis (X) of the propulsion pipe (2) is uniaxial in advance, and the pressure receiving surface portion ( F), the propulsion pipe (2) around the bending axis (X).
A propulsion method for propelling in the direction along the rocking direction of
【請求項2】 ヘッド軸芯(P)に対して傾斜した受圧
面部(F)を、ヘッド本体(1A)に対して前記ヘッド
軸芯(P)周りに回転駆動自在に取り付た推進ヘッド
(1)を設けると共に、前記推進ヘッド(1)の後方に
屈曲自在に連設した複数の推進管(2)を設けて構成し
てある推進体(S)を使用し、この推進体(S)に後方
から押圧力を作用させて地中推進させる推進方法であっ
て、 予め、前記推進管(2)の屈曲軸芯(X)が一軸になる
ように前記推進体(S)を構成しておき、曲進推進部に
おいては、前記受圧面部(F)を、前記屈曲軸芯(X)
周りの前記推進管(2)の揺動方向に沿う方向に向けて
推進し、直進推進部においては、前記受圧面部(F)
を、前記屈曲軸芯(X)方向に沿う方向に向けて推進す
る推進方法。
2. A propulsion head having a pressure receiving surface portion (F) inclined with respect to a head axis (P) rotatably mounted on the head body (1A) around the head axis (P). 1) and a propulsion body (S) having a plurality of propulsion pipes (2) arranged to bend freely behind the propulsion head (1) is used. A propulsion method in which a pushing force is applied from behind to the ground to propell underground, wherein the propulsion body (S) is configured in advance so that the bending axis (X) of the propulsion pipe (2) is uniaxial. In the bending propulsion unit, the pressure receiving surface (F) is connected to the bending axis (X).
The propulsion is performed in the direction along the swinging direction of the surrounding propulsion pipe (2), and in the linear propulsion section, the pressure receiving surface section (F)
A propulsion method for propelling in a direction along the bending axis (X) direction.
JP25107596A 1996-06-10 1996-09-24 Promotion method Expired - Fee Related JP3142242B2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP25107596A JP3142242B2 (en) 1996-06-10 1996-09-24 Promotion method
US08/886,220 US5878825A (en) 1996-07-03 1997-07-01 Underground propelling method
EP97111234A EP0816627B1 (en) 1996-07-03 1997-07-03 Underground drilling method
DE69725053T DE69725053T2 (en) 1996-07-03 1997-07-03 Underground drilling

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP8-146896 1996-06-10
JP14689696 1996-06-10
JP25107596A JP3142242B2 (en) 1996-06-10 1996-09-24 Promotion method

Publications (2)

Publication Number Publication Date
JPH1061377A JPH1061377A (en) 1998-03-03
JP3142242B2 true JP3142242B2 (en) 2001-03-07

Family

ID=26477594

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25107596A Expired - Fee Related JP3142242B2 (en) 1996-06-10 1996-09-24 Promotion method

Country Status (1)

Country Link
JP (1) JP3142242B2 (en)

Also Published As

Publication number Publication date
JPH1061377A (en) 1998-03-03

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