JPS58138898A - Impact type propelling apparatus - Google Patents

Impact type propelling apparatus

Info

Publication number
JPS58138898A
JPS58138898A JP2015482A JP2015482A JPS58138898A JP S58138898 A JPS58138898 A JP S58138898A JP 2015482 A JP2015482 A JP 2015482A JP 2015482 A JP2015482 A JP 2015482A JP S58138898 A JPS58138898 A JP S58138898A
Authority
JP
Japan
Prior art keywords
propulsion
tip
chisel
head
tube
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
JP2015482A
Other languages
Japanese (ja)
Inventor
山門 憲雄
中原 「巌」
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.)
SHINGIJIYUTSU KAIHATSU KK
SHINGIJUTSU KAIHATSU KK
Original Assignee
SHINGIJIYUTSU KAIHATSU KK
SHINGIJUTSU KAIHATSU 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 SHINGIJIYUTSU KAIHATSU KK, SHINGIJUTSU KAIHATSU KK filed Critical SHINGIJIYUTSU KAIHATSU KK
Priority to JP2015482A priority Critical patent/JPS58138898A/en
Publication of JPS58138898A publication Critical patent/JPS58138898A/en
Pending legal-status Critical Current

Links

Landscapes

  • Excavating Of Shafts Or Tunnels (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】 本発明は、道路下、軌道下等の地中に管路を布設すると
きに採用される圧縮空気等を用いブこ衝″1ト式推進装
置に関し、特に直進精度に優れて、批准効率が高く、ま
た礫地盤でも容易に推1イ(できるようにした衝撃式推
進装置に関する。。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a single thrust type propulsion device using compressed air, etc., which is used when laying pipes underground under roads, tracks, etc. This invention relates to an impact type propulsion device that has excellent performance, high ratification efficiency, and can be easily thrust even on gravel ground.

従来、この種の圧縮空気等による衝撃式推進装置として
は、第1に本体に内蔵した、圧縮空気により作動するピ
ストン弐)・ンマで推進ヘッドの先端に設けたチゼルを
打撃し、これによりパ・ラド全体を地盤中に一定の方向
に向は圧入推進させるものがある。
Conventionally, in this type of impact-type propulsion device using compressed air, etc., the first step is to strike a chisel provided at the tip of the propulsion head with a piston built in the main body and operated by compressed air.・There is one that pushes the entire RAD into the ground in a fixed direction.

しかし、該衝撃式推進装置は、地盤を直接圧密排除して
前進するものであるから、周辺地盤との摩擦力が大きく
、さらに推進ヘット自体(佳回転しないで地盤中を前進
のみするものであるかCハ この部分と周辺地盤との摩
擦抵抗力は極めて人きくなり、推進能力にも問題がある
However, since the impact type propulsion device moves forward by directly consolidating and removing the ground, the frictional force with the surrounding ground is large, and the propulsion head itself (which only moves forward through the ground without rotating) The frictional resistance between this part and the surrounding ground is extremely strong, and there is also a problem with the propulsion ability.

1だ、第2の推進装面としては第1図に示す如く先端が
斜状に尖鋭々刃先Af:略同径の推進管Bと連結し、該
推進管Bが1チ「定・」゛法突出した態様で推進管Bの
外周に若干大径の埋設管c−4適宜な先端数句部材りに
より嵌着固定し、かつ刃先Aの先端に切羽Ei固定して
おき、刃先人が回転したとき掘削される地盤の径が上記
取付部材りの外径に等しくなるように構成し、刃先A及
び推進管Bi回転させながら前進させる方式のものが提
案されている。
1. As shown in Fig. 1, the second propulsion device has an oblique tip with a sharp cutting edge Af: connected to the propulsion tube B having approximately the same diameter, and the propulsion tube B has one tip. A buried pipe C-4 with a slightly larger diameter is fitted and fixed on the outer periphery of the propulsion pipe B in a protruding manner with an appropriate tip several pieces, and a face Ei is fixed to the tip of the cutting edge A, and the cutting edge is rotated. A system has been proposed in which the diameter of the ground to be excavated is equal to the outer diameter of the mounting member, and the cutting edge A and the propulsion pipe Bi are advanced while being rotated.

しかし、該第2の推進装置においても埋設管C自体は回
転せず、上記推進管の推力のみで前進するものであるか
ら、たとえ切羽Eで取付部材りの外径と同径の孔を掘削
しても、該埋設管Cの外周面全体が掘削土や周辺地盤と
の間に大きな摩擦力を牛じ、この摩擦力に打ち勝って全
体が前進するためには、立坑に設置される装置全体が非
常に大がかりなものとならざるを得ない。
However, even in the second propulsion device, the buried pipe C itself does not rotate and moves forward only by the thrust of the propulsion pipe. However, the entire outer circumferential surface of the buried pipe C exerts a large frictional force with the excavated soil and the surrounding ground, and in order to overcome this frictional force and move the entire device forward, it is necessary to must be extremely large-scale.

さらに、刃先Aと推進管Bとが同径であるため、刃先A
はこれに加えられる推力によって推進速度を増すと地盤
への刃先Aの貫入長が増すことから斜状刃先の影響によ
って刃先Aの径より若干犬き外径の孔で推進されてしま
うため、前進するに従って刃先が推進管の重量で下方向
に下がっていき目的とする方向より下向きに進んでいっ
てし1うことになる。
Furthermore, since the cutting edge A and the propulsion tube B have the same diameter, the cutting edge A
When the propulsion speed increases due to the thrust applied to this, the penetration length of the cutting edge A into the ground increases, and due to the influence of the slanted cutting edge, it is propelled through a hole with an outer diameter slightly larger than the diameter of the cutting edge A, so it cannot move forward. As the blade moves forward, the weight of the propulsion tube causes the cutting edge to move downward, and the cutting edge moves downward from the desired direction.

本発明は、上記のような従来の問題点を解決Iまたもの
で、その王たる目的は正確に目的方向に直進することが
でき、刃先と掘削地盤との抵抗を最も少なくし、丑だ推
進管と周辺地盤との摩擦抵抗も極力小さくなるようにし
た衝撃式推進装置を提供するにある。
The present invention solves the above-mentioned conventional problems, and its main purpose is to be able to move straight in the target direction accurately, to minimize the resistance between the cutting edge and the excavated ground, and to achieve efficient propulsion. To provide an impact type propulsion device in which the frictional resistance between a pipe and the surrounding ground is minimized.

このために本発明の衝撃式推進装置は、推進ヘッドに進
退可能に設けたチゼルの先端に先端斜状部を取り付け、
かつチゼルに対しエアー7・ンマにより打撃力を付与す
ると同時に、チゼル外周に」−記先端斜状部と所定距離
をおいて嵌着された拡孔部と該先端斜状部とで構成され
た先端刃先部ヲ」二記推進ヘッドとともに回転推進させ
るようにしたものである。
For this purpose, the impact type propulsion device of the present invention has a chisel provided on the propulsion head so as to be movable back and forth, and a sloped tip portion is attached to the tip of the chisel.
At the same time, a blowing force is applied to the chisel by air 7, and at the same time, the chisel is made up of an enlarged hole fitted at a predetermined distance from the slanted tip part on the outer periphery of the chisel, and the slanted tip part. The tip of the cutting edge is rotated and propelled together with the two propelling heads.

以下、本発明の実施例を図面について説明する。Embodiments of the present invention will be described below with reference to the drawings.

第2図は本発明にかかる衝撃式推進装置を道路下横断の
管路布設に適用した場合の全体図を示すもので、1は推
進ヘッド、2は推進ヘッド1の後端に連結した推進管で
あり、これら推進ヘッド1及び推進管2は、道路3を挾
んで形成した一方の立坑4(第2図では一方の立坑のみ
を示す)から道路3下の地盤中に道路3を横断する方向
に推進されるもので、その推進は、推進ヘッド1に内蔵
した圧縮空気式のノ・ンマ機構(後述する)により、推
進ヘッド1の先端に設けたチゼル12を打撃する作用と
、立坑4内に設置した回転推進装置60作用とにより行
なわれる。
FIG. 2 shows an overall view of the impact type propulsion device according to the present invention when it is applied to the installation of a pipe crossing under a road. 1 is a propulsion head, and 2 is a propulsion pipe connected to the rear end of the propulsion head 1. The propulsion head 1 and the propulsion pipe 2 are arranged in a direction that crosses the road 3 from one shaft 4 (only one shaft is shown in FIG. 2) formed between the roads 3 into the ground below the road 3. The propulsion is achieved by the action of striking a chisel 12 provided at the tip of the propulsion head 1 by a compressed air type nozzle mechanism (described later) built into the propulsion head 1, and by the action of hitting the chisel 12 provided at the tip of the propulsion head 1. This is carried out by the action of a rotary propulsion device 60 installed at.

上記回転推進装置6は、基台7上に進退可能に設置され
た本体8を有し、この本体8は、推進管2を道路下の地
盤中に推進できる姿勢にチャッキングする機能と、推進
ヘッド1を含めた推進管2全体を回転する機能を備え、
そして該本体8は、エアー等の流体圧ジヤツキ9によっ
て推進方向及び後退方向に移動しうるようになっている
The rotary propulsion device 6 has a main body 8 installed on a base 7 so as to be able to move forward and backward. Equipped with a function to rotate the entire propulsion tube 2 including the head 1,
The main body 8 can be moved in the forward and backward directions by a hydraulic jack 9 such as air.

第3図は、上記推進ヘッド1の詳細を示す断面図であっ
て、該推進ヘッド1は、所定長さの筒状ケーシング10
を有し、この筒状ケーシング10の先端には、筒状のチ
ゼル保持部材11の一端部が同軸に螺着されている。
FIG. 3 is a sectional view showing details of the propulsion head 1, which includes a cylindrical casing 10 of a predetermined length.
One end of a cylindrical chisel holding member 11 is coaxially screwed onto the tip of the cylindrical casing 10.

該保持部材11内には、チゼル12のヘッド側が保持部
材11の軸線方向にスライド可能に嵌合されているとと
もに、チゼン12のヘッド側段部12aと保持部材11
内の他端側段部11a間に該チゼル12と同心状に配置
した圧縮ノくネ13が介在され、これによりチゼル12
を後退する方向(矢線X方向)に付勢するようになって
いる。
The head side of the chisel 12 is fitted into the holding member 11 so as to be slidable in the axial direction of the holding member 11, and the head side step portion 12a of the chisel 12 and the holding member 11
A compression screw 13 arranged concentrically with the chisel 12 is interposed between the step portion 11a on the other end side of the inside, so that the chisel 12
is biased in the direction of retreat (direction of arrow X).

そして、チゼル】2のヘッド12bと対向する筒状ケー
シング10の内壁には、チゼル12の一定値以上の後退
を規制するストッパ14が取り付けられている。
A stopper 14 is attached to the inner wall of the cylindrical casing 10 facing the head 12b of the chisel 2 to prevent the chisel 12 from retreating beyond a certain value.

また、上記チゼル保持部材11の先端部には、チゼル1
2の保持部材11外方への突出部外周に水密に嵌合され
てチゼル12と一体になっている拡孔部15の一端部が
、軸線方向にスライド可能に嵌合されており、この拡孔
部15と保持部材11間は、複数個のピン16により軸
方向の移動を許容し、相対的な回転を阻止するように、
相互に連結されている。
Further, a chisel 1 is provided at the tip of the chisel holding member 11.
One end of the enlarged hole 15, which is watertightly fitted to the outer periphery of the outward protrusion of the holding member 11 of No. 2 and is integrated with the chisel 12, is fitted so as to be slidable in the axial direction. A plurality of pins 16 are provided between the hole 15 and the holding member 11 to allow movement in the axial direction and prevent relative rotation.
interconnected.

該拡、r1部15の夕1周は、先端に行くに従って階段
部15aにより径が小さくなる階段状に形成されている
The first round of the enlarged r1 portion 15 is formed into a step-like shape whose diameter decreases toward the tip due to a step portion 15a.

該拡孔部15の前方に突出したチゼル12の先端部12
cには、拡孔FBI! ] sと所定距離をおいて先端
斜状部17が一体に取り付けられている。
The tip portion 12 of the chisel 12 protrudes forward of the enlarged hole portion 15.
In c, hole enlarged FBI! ] A tip inclined portion 17 is integrally attached at a predetermined distance from s.

該先端斜状部17け、図示の如く円筒をその軸線と所定
角度をとって斜めに切断した尖鋭状の形状をなしており
、尖端17aは、チゼル12の軸線Yより外方に偏心し
たかたちになっている。
As shown in the figure, the tip slanted portion 17 has a sharp shape obtained by cutting a cylinder diagonally at a predetermined angle with the axis thereof, and the pointed end 17a is eccentrically outward from the axis Y of the chisel 12. It has become.

なお、本実施例では斜辺が軸線Yとなす角度は37度に
形成されている。
In this embodiment, the angle between the oblique side and the axis Y is 37 degrees.

1だ、拡孔部15と先端斜状部17との間のチゼル先端
部12cは、先端斜状部17の基端部17bよりも細径
にしてあり、該基端部17bと拡孔部15の先端との間
にD1定の凹陥部1.2 dが形成されている。
1, the chisel tip 12c between the enlarged hole part 15 and the inclined tip part 17 has a smaller diameter than the proximal end 17b of the inclined tip part 17, and the proximal end 17b and the enlarged hole part A concave portion 1.2 d having a constant D1 is formed between the tip of the tip 15 and the tip of the concave portion 1.2 d.

しかして、先端斜状部17メこれに続く凹陥部12d及
び拡孔部15とで先端刃先部zl構成するものである。
Thus, the tip inclined portion 17, the concave portion 12d following this, and the enlarged hole portion 15 constitute a tip cutting edge portion zl.

18は上記筒状ケーシング1o内のチゼルヘッド12 
b (Jjlに配設したエアーハンマで、そのハンマヘ
ッド18aは、筒状ケージツク10内にシール材19を
介して包密に嵌着したカイトF<1(材18bに筒状ケ
ーシング1oのlll1lI線方向に移動oJ能に案内
され、エアーハンマ18に供給される原綿空気により図
示しないピストンを動作させることでハンマヘッド18
aを介して上記チゼル]2に打撃ケ加えるようになって
いる3、 かかる構成の推進ヘッド1は、第4図に示すように、結
合機構20を介して推進管2の前端に結合され、推進管
2に力えられる回転力及びJff進カを推進ヘッド1に
伝達できるようになっている1、上記結合機構20は、
411進ヘツド用筒状ケーシング10の後端に着脱可能
に嵌合された筒状の連結部材21及び推進管2の前端に
着脱可能に嵌合される管部拐22を介して結合された筒
状の連結部材23′ff:有し、連結部材23は連結部
4421内に嵌挿され、この結合部材23の外周に第5
図に示す如く、90度の位相で軸線に平行な複数個(本
実施例では4個)の溝23aを形成している。
18 is a chisel head 12 inside the cylindrical casing 1o.
b (This is an air hammer installed in Jjl, and the hammer head 18a is connected to the lll1lI line of the cylindrical casing 1o to the kite F The hammer head 18 is moved in the direction by operating a piston (not shown) by the raw cotton air supplied to the air hammer 18.
3. The propulsion head 1 having such a configuration is coupled to the front end of the propulsion tube 2 via a coupling mechanism 20, as shown in FIG. 1, the coupling mechanism 20 is configured to be able to transmit the rotational force and Jff advance force applied to the propulsion tube 2 to the propulsion head 1.
A cylindrical connecting member 21 that is removably fitted to the rear end of the cylindrical casing 10 for the 411 helical head, and a cylinder that is connected to the front end of the propulsion tube 2 through a tube part 22 that is removably fitted to the front end of the propulsion tube 2. The connecting member 23'ff has a shape, and the connecting member 23 is fitted into the connecting part 4421, and a fifth
As shown in the figure, a plurality of grooves 23a (four in this embodiment) are formed parallel to the axis with a phase of 90 degrees.

また、連結部材21の外壁にも、90度の位相で4個の
穴21ai形成せしめ、この各穴21a内に遊動可能に
収容した鋼球20aiそれぞれ対応する上記台溝23a
に係合し、これにより連結部材21と23の軸方向への
相対移動を許可し、その相対回転を禁止することで、エ
アーハンマ18からチゼル12に加えられる衝撃力が推
進管2に伝達されないようにするとともに、推進管20
回転が推進ヘッド1に伝達できるようにしである。
Furthermore, four holes 21ai are formed in the outer wall of the connecting member 21 with a phase of 90 degrees, and the grooves 23a correspond to the steel balls 20ai that are movably accommodated in each hole 21a.
By engaging with the connecting members 21 and 23 and thereby permitting relative movement in the axial direction and prohibiting their relative rotation, the impact force applied from the air hammer 18 to the chisel 12 is not transmitted to the propulsion tube 2. In addition, the propulsion pipe 20
This allows rotation to be transmitted to the propulsion head 1.

また、上記推進管2円の軸線上には、給包管24が推進
管2の全長に亘り配置され、そしてサポータ25により
支持されているとともに、給気管24の推進管2内挿入
端には、継手部材26を介して上記エアーハンマ18に
連結される給気パイプ27の一端がスライド可能に、か
つ気密に結合されている。
Further, on the axis of the propulsion tube 2 circle, a supply tube 24 is arranged along the entire length of the propulsion tube 2, and is supported by a supporter 25, and at the insertion end of the air supply tube 24 into the propulsion tube 2, One end of an air supply pipe 27 connected to the air hammer 18 via a joint member 26 is slidably and airtightly connected.

さらに推進管2の後退開口から突出する給気管24の後
端には、スイベル28を介して圧縮空気源(図示せず)
と接続される給気ホース29が連結されている。
Furthermore, a compressed air source (not shown) is connected to the rear end of the air supply pipe 24 protruding from the retreat opening of the propulsion pipe 2 via a swivel 28.
An air supply hose 29 is connected to the air supply hose 29.

次に、上記のように構成された本実施例の月1・中推進
動作について説明する。
Next, the monthly promotion operation of this embodiment configured as described above will be explained.

推進ヘッド1及び推進管2が互いに・−直線」−に結合
され、そして推進ヘッド1が第2図に示すように道路3
下の地盤中にこれを横断する方向に侵入し、かつ推進ヘ
ッド1を含めた推進管2が、回転推進装置6により回転
及び推進力を受けている状態において、コンプレッサな
どからの用縮空気カホース29.スイベル28.給気管
211及び給気バイブ27を介してエアーハンマ18に
供給サレテ、ハンマ】8が作動して、このハンマヘッド
18aは、チゼル12のヘッド12b’i打撃する。
The propulsion head 1 and the propulsion tube 2 are connected to each other in a straight line, and the propulsion head 1 is connected to the road 3 as shown in FIG.
In a state where the propulsion pipe 2 including the propulsion head 1 is receiving rotation and propulsion force from the rotary propulsion device 6, the compressed air hose from the compressor etc. enters the ground below in a direction that crosses it, and the propulsion pipe 2 including the propulsion head 1 is receiving rotation and propulsion force from the rotary propulsion device 6. 29. Swivel 28. Air is supplied to the hammer 18 through the air supply pipe 211 and the air supply vibrator 27, and the hammer [8] operates, and the hammer head 18a strikes the head 12b'i of the chisel 12.

このため、チゼル12は保持部材11内を王縮バネ13
に抗して前進動され、該チゼル12先端の先端斜状部1
7がビットとしての機能を果たして地盤に貫入する。こ
れにより地盤を排除しながら地中に圧入前進されると同
時に、推進ヘッド1全体もエアーハンマ18の打撃力で
前進され、管路布設に必要な横穴が地中に形成されるこ
とになる3、 このとき、推進ヘッド】と推進管2とは溝23aと鋼球
20aにより結合されているため、推進ヘッド1がエア
ーハンマ18の打撃力で前進しても、その推進力は結合
機構20の部分で吸収され、推進管2に反力としては、
はとんど伝達されることがない3、 さらに本実施例の/h色としては、推進管2とともに」
二記先端刃先部Z全体が回転力と打撃推進力を受けてい
ることである。
For this reason, the chisel 12 holds the compression spring 13 inside the holding member 11.
The inclined tip portion 1 at the tip of the chisel 12 is moved forward against the
7 serves as a bit and penetrates into the ground. As a result, the propulsion head 1 is pushed forward into the ground while removing the ground, and at the same time, the entire propulsion head 1 is also moved forward by the impact force of the air hammer 18, and a horizontal hole necessary for laying the pipe is formed in the ground. , At this time, the propulsion head] and the propulsion tube 2 are connected by the groove 23a and the steel ball 20a, so even if the propulsion head 1 moves forward with the impact force of the air hammer 18, the propulsion force is not absorbed by the coupling mechanism 20. The reaction force is absorbed by the propulsion tube 2 as follows:
Furthermore, the /h color of this example is the same as the propulsion tube 2.
2. The entire cutting edge portion Z receives rotational force and impact propulsion force.

即ち、第6図に示す如く、先端刃先部2のうち先端斜状
部17が、上記打撃力とともに回転推進力を受けて、地
盤Fを回転切削し、先端斜状部17と同径で破砕された
円形の先導孔Gを形成していく。
That is, as shown in FIG. 6, the tip slanted portion 17 of the tip tip portion 2 receives the rotational driving force together with the above-mentioned impact force, rotatably cuts the ground F, and fractures the ground F with the same diameter as the tip slanted portion 17. Then, a circular pilot hole G is formed.

また、掘削、破砕された土は、凹陥部12dが形成され
ていることにより円滑に後方に排除されていき、次に階
段状に段部1・5aが形成されている拡孔部15により
、」二記先導孔Gは段階的に無理なく圧密拡孔されてい
き、最後には推進ヘッド10や推進管2と同径の孔に1
で拡孔されるため、推進管2はスムースに前進しうる。
In addition, the excavated and crushed soil is smoothly removed backwards due to the formation of the concave portion 12d, and then is removed by the hole expansion portion 15 having stepped portions 1 and 5a formed in a step-like manner. ” The second pilot hole G is expanded step by step without any difficulty, and finally a hole with the same diameter as the propulsion head 10 and the propulsion tube 2 is formed.
Since the hole is enlarged at , the propulsion tube 2 can move forward smoothly.

なお、この際推進管2自体も回転しつつ振動しているか
ら、管壁との摩擦抵抗も少なく、推進性能が高い。
In addition, since the propulsion tube 2 itself is also rotating and vibrating at this time, there is little frictional resistance with the tube wall, and the propulsion performance is high.

さらに、上記拡孔部15の作用により、推進ヘッド10
は中心軸線Yに平行に先導孔Gに沿って前進する特性を
示すようになるので、直進性の精度が格段に向上する。
Further, due to the action of the enlarged hole portion 15, the propulsion head 10
Since it exhibits the characteristic of advancing along the guide hole G parallel to the central axis Y, the accuracy of straightness is significantly improved.

また、本実施例で先端斜状部17を37度のfit度に
形成したのは、次の理由による1、即ち、斜状部先端に
圧縮された十くさびが発生してし捷う37度以上の先端
斜状角度においては先端圧入抵抗は大きく、旧状角度3
710以丁に1.・いては土くさびは発生し−ないが、
↑1状面の即擦抵抗が増して先端圧入抵抗が大きくなる
との結宋が出願人により測定された。つ捷り、先端を略
37度前後の鋭角としたものが最も小さな力で用人させ
ることができるためである。
In addition, the reason why the distal end slanted portion 17 is formed to have a fit degree of 37 degrees in this embodiment is due to the following reason. At the tip oblique angles above, the tip press-fit resistance is large;
710 to 1.・No soil wedge occurs, but
↑The applicant has measured that the instant friction resistance of the single-shaped surface increases and the tip press-fit resistance increases. This is because the blade can be twisted with the least amount of force if the tip is at an acute angle of about 37 degrees.

推進ヘッド1及び推進管2の地中への推進に伴い、推進
%;2の後端及び給気管24の後端には、それぞれ他の
■1進管2及び給気管24が順次結合さねる。Mi推進
後、給気管24を支持するサポータ25が推進管2と一
体に結合されてはいないので、給気管24と→ノ”ポー
タ25を引き抜くことができ、そして推進管2は管路と
して完成し利用される。
As the propulsion head 1 and the propulsion pipe 2 are propelled into the ground, the rear ends of the propulsion head 1 and the air supply pipe 24 are sequentially connected to the other single-advance pipes 2 and the air supply pipe 24, respectively. . After Mi propulsion, the supporter 25 that supports the air supply pipe 24 is not integrally connected to the propulsion pipe 2, so the air supply pipe 24 and the porter 25 can be pulled out, and the propulsion pipe 2 is completed as a conduit. and used.

さらに、推進・\ラド1及び推進管2の地中への推進に
伴い、推進方向が目的の軌道より外れた場合は、斜状部
17の胴面を軌道方向の逆に向け、推進ヘッド1を回転
せずに推進させることによって斜状部17の効果により
除々に推進ヘッド1の向きを変え方向を修正することが
できる。
Furthermore, if the propulsion direction deviates from the intended trajectory due to the propulsion of the propulsion/RAD 1 and propulsion tube 2 into the ground, the body surface of the slanted portion 17 is turned in the opposite direction of the trajectory, and the propulsion head 1 By propelling the propulsion head 1 without rotating, it is possible to gradually change the orientation of the propulsion head 1 and correct the direction due to the effect of the slanted portion 17.

上述した如く本発明によれば、推進ヘッドに進退可能に
設けたチゼルの先端に先端斜状部を取りイ1け、かつチ
ゼルに対しエアー7・ンマにより打撃力を何カすると同
時に、チゼル外周に先端斜状部と所定距#をおいて嵌着
された拡孔部と該先端斜状部とで構成された先端刃先g
(”fr上記推進ヘッドとともに回転推進させるように
したものであるため、直進精度が非常に高く、先端刃先
部と掘削地盤との抵抗が小さく、捷だ推進管と掘削上と
の摩擦抵抗も少なく推進性能が高い。さらに、礫が地中
に存在してもこれを容易に推進することができる。捷だ
、先端に設けた衝撃式推進ヘッドで推進管に振動ヲ刀え
ているので、推進管に与える回転力は小さくでき、しか
も衝撃式推進ヘット用自体も推進能力を有しているので
、推進力を小さくでき、立坑に設置される回転推進装置
の小型化、小パワー化が可能になるとともに推進長を増
大することができる々ど従来に々い画期的な効果を奏す
るものである。
As described above, according to the present invention, the tip of the chisel that is movably provided on the propulsion head is provided with a slanted tip, and at the same time, the outer periphery of the chisel is A cutting edge g that is composed of a hole enlarged part fitted at a predetermined distance # from the inclined tip part to the inclined tip part.
("fr) Since it is designed to be rotated and propelled together with the above propulsion head, the straightness is very high, the resistance between the tip of the cutting edge and the excavated ground is small, and the frictional resistance between the slender propulsion pipe and the excavation ground is also small. It has high propulsion performance.Furthermore, even if there is gravel underground, it can be easily propelled.The impact-type propulsion head installed at the tip of the propulsion tube prevents vibrations, so the propulsion tube The rotational force applied to the shaft can be reduced, and since the impact type propulsion head itself has propulsion capacity, the propulsion force can be reduced, making it possible to downsize and reduce the power of the rotary propulsion device installed in the shaft. At the same time, the propulsion length can be increased, which has a revolutionary effect compared to the conventional one.

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

第1図は従来の推進装置の概略断面図、第2図1は本発
明に係る衝撃式推進装置を道路下等の管路布設に適用し
た場合の全体構成図、第3図は、本発明の一実施例にお
ける推進ヘッドの詳細を示す断面図、第4図は該実施例
における推進ヘッドと推進管との結合構造の詳細を示す
断面図、第5は1は第4図のIV−IV線に沿う断面図
、第6図は、該実施例における先端刃先部の掘削態様を
示す詣1明図である1、 1・推進ヘッド、2・・推進管、12・・・チゼル、1
2d・・・凹陥部、】5・・拡孔部、17・・・先端斜
状部、」8・・エアーハンマ、Z・・・先端刃先部。
Fig. 1 is a schematic sectional view of a conventional propulsion device, Fig. 2 1 is an overall configuration diagram when the impact type propulsion device according to the present invention is applied to laying pipes under roads, etc., and Fig. 3 is a diagram of the present invention. FIG. 4 is a sectional view showing details of the propulsion head and propulsion tube in the embodiment; 5th is a sectional view showing details of the propulsion head and the propulsion tube in the embodiment; The cross-sectional view taken along the line, FIG. 6, is a clear view showing the excavation mode of the tip of the cutting edge in this embodiment. 1. Propulsion head, 2. Propulsion tube, 12. Chisel, 1
2d...Concave part, ]5... Enlarged hole part, 17... Slanted tip part, ``8... Air hammer, Z... Tip part.

Claims (3)

【特許請求の範囲】[Claims] (1)  進退可能に設けたチゼルと、該チゼルを打撃
して推進させるエアーハンマを内蔵した推進ヘッドとを
有し、上記チゼルの先端に取り付けた先端斜状部と、チ
ゼル外周に該先端斜状部と所定距離全おいて嵌着された
拡孔部とからなる先端刃先部全上記推進ヘッドとともに
回転する手段全備えてなる衝撃式推進装置−
(1) It has a chisel that can move forward and backward, and a propulsion head that has a built-in air hammer that propels the chisel by striking it, and has a slanted tip part attached to the tip of the chisel, and a slanted tip part on the outer periphery of the chisel. An impact-type propulsion device comprising: a cutting edge portion consisting of a shaped portion and a hole-enlarged portion fitted at a predetermined distance; and a means for rotating together with the propulsion head.
(2)上記先端斜状部は、37度前後の角度を有するこ
とを特徴とする特許請求の範囲第1項記載の衝撃式推進
装置。
(2) The impact type propulsion device according to claim 1, wherein the tip inclined portion has an angle of about 37 degrees.
(3)  上記先端斜状部と上記拡孔部との間の上記チ
ゼルは、該先端斜状部の基端より細径とされて凹陥部が
形成されている特許請求の範囲第1項または第2項記載
の衝撃式推進装置。
(3) The chisel between the slanted tip portion and the enlarged hole portion has a smaller diameter than the proximal end of the slanted tip portion to form a concave portion. The impact type propulsion device according to item 2.
JP2015482A 1982-02-10 1982-02-10 Impact type propelling apparatus Pending JPS58138898A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2015482A JPS58138898A (en) 1982-02-10 1982-02-10 Impact type propelling apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2015482A JPS58138898A (en) 1982-02-10 1982-02-10 Impact type propelling apparatus

Publications (1)

Publication Number Publication Date
JPS58138898A true JPS58138898A (en) 1983-08-17

Family

ID=12019232

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015482A Pending JPS58138898A (en) 1982-02-10 1982-02-10 Impact type propelling apparatus

Country Status (1)

Country Link
JP (1) JPS58138898A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0425736U (en) * 1990-06-26 1992-02-28

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4923410A (en) * 1972-06-28 1974-03-01
JPS56795B2 (en) * 1974-09-09 1981-01-09

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4923410A (en) * 1972-06-28 1974-03-01
JPS56795B2 (en) * 1974-09-09 1981-01-09

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0425736U (en) * 1990-06-26 1992-02-28

Similar Documents

Publication Publication Date Title
US6439319B1 (en) Method and apparatus for directional boring under mixed conditions
EP0657006B1 (en) Guided mole
US6371223B2 (en) Drill head for directional boring
JPH0317388A (en) Automatic propulsion type impact excavator
JPS58138898A (en) Impact type propelling apparatus
US3480092A (en) Rotary impact burrowing device
JP3726179B2 (en) Drilling device
JP2940424B2 (en) Forward search device for tunnel machine
JPS63503155A (en) A device that forms holes in the soil
JP2636207B2 (en) Pipe driving device
JPS59141696A (en) Impact type propelling apparatus
JP3406891B2 (en) Impact-type small-diameter thruster for gravel
JPH10259692A (en) Ground propulsive excavating device
JPH02289788A (en) Drilling device for forming slot on base rock
JPS58120987A (en) Mortising device
JPS6211154B2 (en)
JPH0626620Y2 (en) Cutter head
JPH08277691A (en) Excavating tool
JPS63147092A (en) Small-bore pipe propulsion method and device
JPH0417657Y2 (en)
JP2637014B2 (en) Ground drilling equipment
JPS5940996B2 (en) drilling equipment
JP2616933B2 (en) Land drilling tools and drilling methods
JPS6332215Y2 (en)
JPS6332216Y2 (en)