JP2813687B2 - Propulsion device for propulsion method - Google Patents

Propulsion device for propulsion method

Info

Publication number
JP2813687B2
JP2813687B2 JP28998690A JP28998690A JP2813687B2 JP 2813687 B2 JP2813687 B2 JP 2813687B2 JP 28998690 A JP28998690 A JP 28998690A JP 28998690 A JP28998690 A JP 28998690A JP 2813687 B2 JP2813687 B2 JP 2813687B2
Authority
JP
Japan
Prior art keywords
propulsion
connecting portion
state
soil
head
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
JP28998690A
Other languages
Japanese (ja)
Other versions
JPH04161696A (en
Inventor
輝夫 壁内
勝彦 向野
高 大島
正也 服部
等真 川端
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.)
Furukawa Electric Co Ltd
Tokyo Electric Power Co Inc
Kubota Corp
Original Assignee
Furukawa Electric Co Ltd
Tokyo Electric Power Co Inc
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 Furukawa Electric Co Ltd, Tokyo Electric Power Co Inc, Kubota Corp filed Critical Furukawa Electric Co Ltd
Priority to JP28998690A priority Critical patent/JP2813687B2/en
Publication of JPH04161696A publication Critical patent/JPH04161696A/en
Application granted granted Critical
Publication of JP2813687B2 publication Critical patent/JP2813687B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、推進工法において使用される推進体装置に
関する。
The present invention relates to a propulsion device used in a propulsion method.

〔従来の技術〕[Conventional technology]

かかる推進体装置は、推進体を土中において直線的に
推進させる場合のみならず、推進体を土中において曲線
的に推進させる場合にも使用される。そこで、推進体を
土中において曲線的に推進させる場合に使用できるよう
な推進体装置として、互いに隣接する推進体同士を屈曲
自在に連結した連結部を複数備えたものがある。具体的
には、互いに隣接する推進体同士の連結部の構造を屈曲
自在となすために、その両推進体の対向する端面間に前
記屈曲を許容する隙間を設けたものがある。
Such a propulsion device is used not only when the propulsion body is linearly propelled in the soil but also when the propulsion body is propelled in a curve in the soil. Therefore, as a propulsion body device that can be used when the propulsion body is curvedly propelled in the soil, there is a propulsion body device that includes a plurality of connecting portions that connect adjacent propulsion bodies to bend freely. Specifically, in order to make the structure of the connection portion between the propulsion bodies adjacent to each other bendable, there is a type in which a gap that allows the bending is provided between opposing end faces of both propulsion bodies.

しかし、前記隙間は、推進体を土中にて曲線的に推進
させる推進工法の施工時において前記屈曲を確保する有
効な空間となる反面、そこに土砂等の異物が侵入して詰
まり易く、その詰まりが生じると前記屈曲を困難にして
しまうという不都合を生む空間ともなる。
However, the gap is an effective space for securing the bending at the time of the construction of the propulsion method for propelling the propulsion body in a curved manner in the soil, but is liable to be clogged by foreign matter such as earth and sand entering the space. If clogging occurs, it also becomes a space that creates a disadvantage that the bending becomes difficult.

そこで、本発明者等は、互いに隣接する前記両推進体
の対向する端面間に弾性変形自在なシール部材を圧入
し、そのシール部材の弾性変形能によって前記屈曲を可
能ならしめると共にそのシール部材の存在によって土砂
等の異物の侵入を防止して前記不都合が生じるのを回避
する構造簡素な推進体装置を先に開発した。
Then, the present inventors press-fit an elastically deformable seal member between opposing end faces of the two propulsion bodies adjacent to each other, and make the bending possible by the elastic deformability of the seal member, and at the same time, A propulsion device having a simple structure for preventing the inconvenience caused by preventing the intrusion of foreign matters such as earth and sand by its existence has been previously developed.

〔発明が解決しようとする課題〕[Problems to be solved by the invention]

然るに、本発明者等が先に開発した前記推進体装置に
おいても、以下に述べるような改良すべき問題がある。
However, the propulsion device developed by the present inventors has problems to be improved as described below.

即ち、前記推進体装置を巻装ドラムに巻取収納する場
合等においては、前記連結部の構造ではその屈曲の程度
が不十分となって前記推進体装置をコンパクトに巻取収
納することができないことがあるという改良すべき問題
がある。そこで、前記屈曲自在な連結部の数を増やすこ
とも考えられるが、その数を単純に増やすと、今度は、
推進体を土中にて直線的に推進させる場合に円滑な推進
ができなくなるという問題が生じることとなる。
That is, in the case where the propulsion device is wound up and stored in a winding drum, the degree of bending of the structure of the connecting portion is insufficient, and the propulsion device cannot be wound up and stored compactly. There are problems that need to be improved. Therefore, it is conceivable to increase the number of the flexible connecting portions, but if the number is simply increased, this time,
When the propelling body is propelled linearly in the soil, a problem arises in that smooth propulsion cannot be performed.

本発明はかかる事情に鑑みてなされたものであり、前
記隙間内に土砂等の異物の侵入を防止して前記不都合が
生じるという問題を回避できると共に、推進体を巻装ド
ラムに巻取収納する場合においてもコンパクトに巻取収
納することができ、更に推進体を土中にて直線的に推進
させる場合においても円滑な推進が可能な、構造簡素な
推進体装置を提供することを目的としている。
SUMMARY OF THE INVENTION The present invention has been made in view of the above circumstances, and can prevent a problem that the inconvenience occurs by preventing intrusion of foreign matter such as earth and sand into the gap, and at the same time, winds and stores a propulsion body on a winding drum. It is an object of the present invention to provide a propulsion device having a simple structure that can be wound up and stored compactly even in a case, and that can smoothly propell even when the propulsion body is linearly propelled in the soil. .

〔課題を解決するための手段〕[Means for solving the problem]

本発明に係る推進工法用推進体装置の特徴構成は、 前記複数の連結部の一部を、互いに隣接する前記両推
進体の対向する端面間に弾性変形自在なシール部材を圧
入してなる第1連結部にて構成すると共に、 前記複数の連結部の残部を、連結部の屈曲姿勢を許容
する第1状態とその屈曲姿勢を禁止して直線状姿勢に保
持する第2状態とに切り換える切換え手段を備える第2
連結部にて構成してある点にあり、その作用・効果は次
の通りである。
The characteristic configuration of the propulsion device for a propulsion method according to the present invention is as follows. A part of the plurality of connecting portions is formed by press-fitting an elastically deformable seal member between opposing end surfaces of the adjacent two propulsion members. A switch configured to include one connecting portion and to switch the remaining portions of the plurality of connecting portions between a first state in which the bending posture of the connecting portion is allowed and a second state in which the bending posture is prohibited and held in a straight posture. Second with means
The operation and effect are as follows.

〔作 用〕(Operation)

かかる推進工法用推進体装置にあっては、前記第1連
結部において、前記両推進体の対向する端面間に圧入し
た弾性変形自在なシール部材の存在によって土砂等の異
物の侵入が防止される。
In the propulsion device for a propulsion method, the presence of the elastically deformable seal member press-fitted between the opposed end surfaces of the two propulsion members at the first connecting portion prevents intrusion of foreign matter such as earth and sand. .

更に、推進体を土中にて曲線的に推進させたり、推進
体を巻装ドラムにコンパクトに巻取収納したりすべく、
前記推進体装置を適宜屈曲させたい場合、前記第1連結
部においては、そこに設けた弾性変形自在なシール部材
の弾性変形性により、その連結部での屈曲を可能とする
と共に、前記第2連結部においては、前記切換え手段を
用いて連結部を屈曲姿勢を許容する第1状態に切り換え
ることにより、その連結部での屈曲を可能とし、もって
いずれの連結部においても前記推進体装置を適宜屈曲さ
せ得るようになる。
Furthermore, in order to propel the propelling body in the ground in a curved manner, or to compactly wind and store the propelling body on the winding drum,
When it is desired to bend the propulsion device appropriately, the first connecting portion can be bent at the connecting portion by the elastic deformability of an elastically deformable seal member provided thereon, and the second connecting portion can be bent at the second connecting portion. In the connecting part, the connecting part is switched to the first state in which the bending posture is allowed by using the switching means, thereby enabling the bending at the connecting part. It can be bent.

更に、推進体を土中において直線的に推進させたい場
合、前記第2連結部において、前記切換え手段を用いて
連結部を直線状姿勢に保持する第2状態に切り換えるこ
とにより、その連結部での屈曲を阻止し、推進体を土中
にて円滑に直進させることができるようになる。
Further, when it is desired to propel the propelling body linearly in the soil, the second connecting portion is switched to the second state in which the connecting portion is maintained in the linear posture by using the switching means, so that the connecting portion is connected to the second connecting portion. Of the propulsion body, and the propelling body can smoothly advance straight in the soil.

〔発明の効果〕〔The invention's effect〕

従って、本発明の推進体装置によれば、前記第1連結
部において前記隙間内に土砂等の異物の侵入を防止して
前記不都合が生じるという問題を回避できると共に、推
進体を巻装ドラムに巻取収納する場合等においてもコン
パクトに巻取収納することができ、更に推進体を土中に
て直進的に推進させる場合においても円滑な推進が可能
となる。しかも、本発明の推進体装置においては、その
連結部の一部が前記隙間に前記シール部材が圧入された
だけの構造であって簡素な構造となる。
Therefore, according to the propulsion device of the present invention, it is possible to prevent the problem that the inconvenience occurs by preventing foreign matters such as earth and sand from entering the gap in the first connection portion, and to connect the propulsion device to the winding drum. It can be wound up and stored compactly even when it is wound up and stored, and smooth propulsion is possible even when the propelling body is propelled straight in the ground. Moreover, in the propulsion device of the present invention, a part of the connecting portion has a structure in which the seal member is merely press-fitted into the gap, and has a simple structure.

〔実施例〕〔Example〕

以下、本発明の実施例を図面に基づいて説明する。 Hereinafter, embodiments of the present invention will be described with reference to the drawings.

本発明に係る推進体装置を構成する複数の推進体
(B)‥は、第5図に示す如く、推進用ヘッド(1)と
複数の推進管(2)‥との組合せよりなり、それらは連
結部(J)を介して予め連結されている。
As shown in FIG. 5, the plurality of propulsion bodies (B) ‥ constituting the propulsion body apparatus according to the present invention are composed of a combination of a propulsion head (1) and a plurality of propulsion pipes (2) ‥. They are connected in advance via a connecting portion (J).

かかる推進体(B)‥は、推進機によって土中へ推進
されるが、その推進機は、以下に詳述するように構成さ
れている。
The propulsion body (B) # is propelled into the soil by a propulsion device, and the propulsion device is configured as described in detail below.

即ち、施工ピット(5)内に、前記推進管(2)‥を
保持しつつ押圧して、その先端に連結した推進用ヘッド
(1)を土中推進させるべく、推進管(2)‥を土中に
押し込む推進用ヘッド(1)推進用の押圧装置(3)が
設けられると共に、複数の推進管(2)‥を土中に侵入
させる箇所近くでその各軸芯が略直線上に並ぶ状態に保
持しながら土中に案内するガイド部材(4)が設けられ
ている。また施工ピット(5)の上部外方に、推進管
(2)‥を巻取収納する巻装用ドラム(6)が設けられ
ている。尚、図中の(14)は、施工ピット(5)が崩れ
ないようにその側壁を内側から支持する支持ジャッキで
あり、また図中の(15)は、前記巻装用ドラム(6)か
ら繰り出される推進体(B)‥を支持して押圧部材(1
7)に案内するガイドローラーである。
In other words, the propulsion pipe (2) ‥ is pushed into the construction pit (5) while holding the propulsion pipe (2) ‥ while holding the propulsion head (1) connected to the tip thereof in the soil. A propulsion head (1) for pushing into the ground is provided with a pressing device (3) for propulsion, and the respective axes of the plurality of propulsion pipes (2) ‥ are arranged substantially in a straight line near a place where the propulsion pipes (2) ‥ enter the soil. A guide member (4) is provided for guiding into the soil while maintaining the state. A winding drum (6) for winding and storing the propulsion pipe (2) # is provided outside the upper part of the construction pit (5). Incidentally, (14) in the figure is a support jack for supporting the side wall of the construction pit (5) from the inside so as not to collapse, and (15) in the figure is extended from the winding drum (6). Pressing member (1) supporting the propelling body (B)
It is a guide roller to guide to 7).

前記推進用ヘッド(1)は、例えば50〜70mmの小径の
ヘッド本体(1A)と、ヘッド本体(1A)と同径でヘッド
本体(1A)に対して推進体軸芯(P)(推進用ヘッド軸
芯(P))周りに回転自在に先端側に取り付けてある掘
削部(1B)とからなる。
The propulsion head (1) has a head body (1A) having a small diameter of, for example, 50 to 70 mm, and a propelling body axis (P) (propulsion body) having the same diameter as the head body (1A) and having a diameter equal to that of the head body (1A). And a digging part (1B) rotatably mounted on the tip side around the head axis (P).

前記掘削部(1B)には、推進用ヘッド(1)を土中推
進させるに伴って土圧を受けて、その土圧を受けた方向
に推進用ヘッド(1)の推進方向を片寄らせるための受
圧面(F)を、先端側ほど前記軸芯(P)に近接する傾
斜面に形成して設けてある。そして、前記推進用ヘッド
(1)を直進させるときには、ヘッド本体(1A)に対し
て掘削部(1B)を回転させながら推進させる一方、旋回
させるときには、旋回させるべき側とは反対側に受圧面
(F)を向けて推進させ、その受圧面(F)が受ける土
圧にて、推進用ヘッド(1)の推進方向が受圧面(F)
と反対側に向けられるようになる。
The excavation part (1B) receives the earth pressure in accordance with the propulsion of the propulsion head (1) in the soil and shifts the propulsion direction of the propulsion head (1) to the direction in which the earth pressure is received. The pressure receiving surface (F) is formed on an inclined surface closer to the axis (P) toward the tip end. When the propulsion head (1) is moved straight, the excavation portion (1B) is propelled while rotating with respect to the head body (1A), and when the propulsion head (1) is turned, the pressure receiving surface is located on the side opposite to the side to be turned. (F), and the propulsion direction of the propulsion head (1) is changed to the pressure receiving surface (F) by the earth pressure received by the pressure receiving surface (F).
Will be turned to the opposite side.

前記複数の推進体(B)のうちの隣接するもの同士を
屈曲自在に連結する連結部(J)、即ち、前記推進用ヘ
ッド(1)と前記推進管(2)とを屈曲自在に連結する
連結部(J)、及び前記推進管(2)の隣接するもの同
士を屈曲自在に連結する連結部(J)は、以下に詳述す
るように構成されている(第1図〜第4図参照。) 即ち、前記連結部(J)においては、後方(第1図〜
第4図においては、左方が後方に相当)の推進体(B)
の端部(B2)に形成された継手取付部(B4)の内面に、
継手部材(12)を螺合固定すると共に、その推進体
(B)の前方に隣接の推進体(B)の端部(B1)に、前
記継手部材(12)を推進体芯(P)と直交する方向に揺
動自在に受け入れる嵌合受部(13)を形成してある。前
記継手部材(12)は、推進体(B)の長手方向に沿う姿
勢で設けてあり、後部に形成された軸部(12a)とその
前部に形成された球状継手部(12b)との組合せからな
る。その軸部(12a)は前記後方の推進体(B)の前部
に螺合固定してあり、その球状継手部(12b)は前記前
方の推進体(B)の後部に設けた嵌合受部(13)に揺動
自在に内嵌してある。
A connecting portion (J) for connecting adjacent ones of the plurality of propulsion bodies (B) to bend freely, that is, for connecting the propulsion head (1) and the propulsion tube (2) to bend freely. The connecting portion (J) and the connecting portion (J) for connecting adjacent ones of the propulsion pipes (2) so as to bend freely are configured as described in detail below (FIGS. 1 to 4). That is, in the connecting portion (J), the rear portion (FIG. 1 to FIG.
In FIG. 4, the left side corresponds to the rear) (B)
On the inner surface of the joint mounting part (B 4 ) formed at the end (B 2 ) of
With a coupling member (12) is fixedly screwed, the propellant propellant adjacent the front of the (B) end of the (B) to (B 1), propellant core the coupling member (12) (P) A fitting receiving portion (13) for swingably receiving in a direction perpendicular to the direction is formed. The joint member (12) is provided in a posture along a longitudinal direction of the propulsion body (B), and is formed by a shaft portion (12a) formed at a rear portion and a spherical joint portion (12b) formed at a front portion thereof. Consist of combinations. The shaft part (12a) is screwed and fixed to the front part of the rear propulsion body (B), and the spherical joint part (12b) is provided on a fitting receiver provided at the rear part of the front propulsion body (B). Part (13) is swingably fitted inside.

前記複数の連結部(J)の一部は、第1図及び第2図
(A),(B)に示すように、互いに隣接する前記両推
進体(B),(B)の対向する端面間に弾性変形自在な
シール部材(10)を圧入してなる第1連結部(J1)にて
構成されている。かかる第1連結部(J1)においては、
前記シール部材(10)の弾性変形能により第2図(A)
に示す屈曲姿勢をとり得るようになっている。しかも、
前記シール部材(10)の存在によって土砂等の異物の侵
入が防止されるようになっている。
As shown in FIGS. 1 and 2 (A) and (B), a part of the plurality of connecting portions (J) are opposed end faces of the two propulsion bodies (B) and (B) adjacent to each other. The first connecting portion (J 1 ) is formed by press-fitting an elastically deformable seal member (10) therebetween. In the first connecting portion (J 1 ),
FIG. 2 (A) shows the elastic deformation capability of the seal member (10).
The bending posture shown in FIG. Moreover,
The presence of the seal member (10) prevents entry of foreign matter such as earth and sand.

また、前記複数の連結部(J)の残部は、第1図、第
3図及び第4図に示すように、連結部(J)の屈曲姿勢
を許容する第1状態とその屈曲姿勢を禁止して直線状姿
勢に保持する第2状態とに切り換える切換え手段(K)
を備える第2連結部(J2)にて構成されている。
Further, as shown in FIGS. 1, 3 and 4, the remaining portion of the plurality of connecting portions (J) is in a first state in which the connecting portion (J) is allowed to bend and its bending posture is prohibited. Switching means (K) for switching to the second state of maintaining the linear posture
And a second connecting portion (J 2 ) provided with:

その切換え手段(K)は、具体的には、前記前方の推
進体(B)の端部(B1)に接当して前記第2状態を実現
する突っ張り部(8a)を有するリング状のストッパー
(8)を備えてなる。尚、本実施例においては、前記突
っ張り部(8a)が前記第2状態で前記後方の推進体
(B)の端部(B2)にも接当するようになっている。
The switching means (K) is, specifically, a ring-shaped member having a strut (8a) which comes into contact with the end (B 1 ) of the forward propulsion body (B) to realize the second state. A stopper (8) is provided. In the present embodiment, the strut portion (8a) is adapted to Setto to end (B 2) of said rear propellant in the second state (B).

そのストッパー(8)はその後方の端面が凹凸状態と
なっていて、その凸部に相当する部分が幅広となって前
記突っ張り部(8a)を形成している。そして、そのスト
ッパー(8)は、前記継手取付部(B4)の外面にスライ
ド部材及びすべり軸受として機能するブッシュ(21)を
介して外嵌されており、そのブッシュ(21)の存在によ
り、推進体軸芯(P)方向への摺動及び推進体軸芯
(P)周りでの回動が円滑に行われるようになってい
る。尚、そのブッシュ(21)は、例えば焼結合金やテフ
ロン等を素材とするスライドベアリングよりなる。ま
た、前記ストッパー(8)の突っ張り部(8a)の前記端
部(B1)からの退避を許容する空間部(S)が、前記後
方の推進体(B)の前方の端部(B2)に形成されてい
る。
The stopper (8) has an uneven rear end surface, and a portion corresponding to the convex portion is widened to form the strut portion (8a). The stopper (8) is externally fitted to the outer surface of the joint mounting portion (B 4 ) via a bush (21) functioning as a slide member and a slide bearing. Due to the presence of the bush (21), Sliding in the direction of the propulsion body axis (P) and rotation around the propulsion body axis (P) are performed smoothly. The bush (21) is made of a slide bearing made of, for example, a sintered alloy or Teflon. Further, a space (S) allowing the retraction of the strut (8a) of the stopper (8) from the end (B 1 ) is formed at the front end (B 2 ) of the rear propulsion body (B). ) Is formed.

かかるストッパー(8)によれば、それを推進体芯
(P)周りに適宜回動させてその突っ張り部(8a)を前
記隣接する推進体(B),(B)の端部(B1),(B2
夫々に接当させ、その両推進体(B),(B)の連結部
(J)が屈曲姿勢にならないように突っ張らせることに
より、前記第2状態を実現する一方、それを再度、推進
体芯(P)周りに適宜回動させた上でその突っ張り部
(8a)を前記空間部(S)に退避させることにより、前
記両推進体(B),(B)の連結部(J)が屈曲姿勢を
とり得るようにすることにより、前記第1状態を実現す
ることができる。
According to the stopper (8), which propellant core (P) as appropriate the strut portion is rotated (8a) of the adjacent propellant around (B), the end of the (B) (B 1) , (B 2 )
The second state is realized by bringing the propulsion body into contact with each of the propulsion bodies (B) and (B) so that the connecting portion (J) of the propulsion bodies (B) does not assume a bent posture. By appropriately rotating around the core (P) and retracting the strut (8a) into the space (S), the connecting portion (J) between the two propulsors (B) and (B) is connected. The first state can be realized by being able to assume a bending posture.

更に、前記空間部(S)が設けられた前記後方の推進
体(B)の端部(B2)には、その空間部(S)を覆う被
覆部(B3)が形成されている。更に詳しくは、前記後方
の推進体(B)の端部(B2)には、その前方に向かっ
て、内径が前記ストッパー(8)の外径よりも大径で且
つ外径が推進体本体の外径にほぼ等しいリング状の被覆
部(B3)が推進体本体から延設され、その被覆部(B3
によって前記空間部(S)が取り巻かれ、外から覆われ
ている。尚、その被覆部(B3)は、前記後方の推進体
(B)の端部(B2)がストッパー(8)に対して前記第
2状態において接当する端面をも覆う程度に推進体本体
から延設されている。また、その被覆部(B3)と前記ス
トッパー(8)との摺接部には、、円環状のシール部材
(22)が介装されており、そのシール部材(22)の存在
によって土砂等の侵入が防止されるようになっている。
Further, a covering portion (B 3 ) that covers the space (S) is formed at an end (B 2 ) of the rear propulsion body (B) provided with the space (S). More specifically, the end (B 2 ) of the rear propulsion body (B) has an inner diameter larger than the outer diameter of the stopper (8) and an outer diameter toward the front toward the front. A ring-shaped covering portion (B 3 ) approximately equal to the outer diameter of the protruding body extends from the propelling body body, and the covering portion (B 3 )
Surrounds the space (S) and is covered from the outside. Note that the covering portion (B 3 ) has such an extent that the end portion (B 2 ) of the rear propulsion body (B) also covers the end surface that contacts the stopper (8) in the second state. It extends from the body. An annular seal member (22) is interposed at the sliding contact portion between the covering portion (B 3 ) and the stopper (8). Intrusion is prevented.

かくして推進体(B)の連結部(J)が構成されてい
る場合は、前記空間部(S)が設けられた推進体(B)
の端部(B2)にその空間部(S)を覆う被覆部(B3)が
形成されているために、その被覆部(B3)の存在によ
り、前記第2状態を実現した状態における前記空間部
(S)の開放状態が遮蔽されるようになる。従って、そ
の部分において土砂等の異物が外から侵入するのが防止
されるようになる。
When the connecting portion (J) of the propulsion body (B) is configured as described above, the propulsion body (B) provided with the space portion (S).
Since the covering portion (B 3 ) that covers the space portion (S) is formed at the end portion (B 2 ), the presence of the covering portion (B 3 ) causes the second state to be realized. The open state of the space (S) is blocked. Therefore, foreign matter such as earth and sand can be prevented from entering the portion from the outside.

尚、本実施例においては、前記被覆部(B3)が前記第
2状態において前記後方の推進体(B)の端部(B2)と
接当する接当端面をも覆う程度に推進体本体から延設さ
れているため、前記第2状態における前記接当端面が外
から遮蔽され、その部分においても土砂等の異物が外か
ら侵入するのが防止されるようになる。
In the present embodiment, the propulsion body is in such a degree that the covering portion (B 3 ) also covers the contact end face of the rear propulsion body (B) which contacts the end (B 2 ) of the rear propulsion body (B) in the second state. Since it extends from the main body, the contact end surface in the second state is shielded from the outside, and foreign matter such as earth and sand can be prevented from entering from the outside also in that portion.

〔別実施例〕 前記切換え手段(K)が、第6図に示すように、前記
前方の推進体(B)の端部(B1)に接当して前記第2状
態を実現する接当部(18a)を有するナット状のストッ
パー(18)よりなる実施例も考えられる。尚、前記接当
部(18a)における前記第2状態と前記第1状態との切
換えは、前記後方の推進体(B)の端部(B2)外周に形
成された螺合部と、それに螺合される前記ストッパー
(18)内周に形成された螺合部との螺合量調整によって
行われるようになっている。
[Another Embodiment] As shown in FIG. 6, the switching means (K) contacts the end (B 1 ) of the forward propulsion body (B) to realize the second state. An embodiment comprising a nut-shaped stopper (18) having a part (18a) is also conceivable. The switching between the second state and the first state in the contact portion (18a) is performed by a screwing portion formed on an outer periphery of an end (B 2 ) of the rear propulsion body (B), The adjustment is performed by adjusting the screwing amount with a screwing portion formed on the inner periphery of the stopper (18) to be screwed.

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

【図面の簡単な説明】 第1図〜第5図は本発明に係る推進工法用推進体装置の
一実施例を示し、第1図は前記推進体装置の第1連結部
及び第2連結部の双方を示す縦断面図、第2図(A),
(B)は前記推進体装置の第1連結部を第1状態と第2
状態とに分けて示す縦断面図、第3図は前記推進体装置
の第2連結部を示すべく第1図中のIII−III線にて切断
して示す断面図、第4図はその要部を示す分解斜視図、
第5図は前記推進体装置を備える推進機の全体を示す側
面図、第6図は本発明に係る推進工法用推進体装置の別
実施例を示す縦断面図である。 (10)……シール部材、(B)……推進体、(K)……
切換え手段、(J)……連結部、(J1)……第1連結
部、(J2)……第2連結部。
BRIEF DESCRIPTION OF THE DRAWINGS FIGS. 1 to 5 show an embodiment of a propulsion device for a propulsion method according to the present invention, and FIG. 1 shows a first connection portion and a second connection portion of the propulsion device. FIG. 2 (A)
(B) shows that the first connecting portion of the propulsion device is in the first state and the second state.
FIG. 3 is a cross-sectional view taken along line III-III in FIG. 1 to show a second connecting portion of the propulsion device, and FIG. Exploded perspective view showing a part,
FIG. 5 is a side view showing the entire propulsion device including the propulsion device, and FIG. 6 is a longitudinal sectional view showing another embodiment of the propulsion device for a propulsion method according to the present invention. (10) Seal member, (B) Propeller, (K)
Switching means, (J) ...... connecting portion, (J 1) a first coupling part ......, (J 2) ...... second coupling portion.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 向野 勝彦 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 (72)発明者 大島 高 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 (72)発明者 服部 正也 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 (72)発明者 川端 等真 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 特開 平2−161095(JP,A) 特開 平2−161094(JP,A) (58)調査した分野(Int.Cl.6,DB名) E21D 9/06 311──────────────────────────────────────────────────続 き Continuing on the front page (72) Katsuhiko Mukai, 1-1-1, Hama, Amagasaki-shi, Hyogo Inside Kubota Technology Development Laboratory Co., Ltd. (72) Takashi Oshima 1-1-1, Hama, Amagasaki-shi, Hyogo Shares Inside the Kubota Research Institute of Technology (72) Inventor Masaya Hattori 1-1-1, Hama, Amagasaki-shi, Hyogo Prefecture Inside the Kubota Research Institute of Technology, Inc. (72) Tomonori Kawabata 1-1-1 Hama, Amagasaki-shi, Hyogo No. In Kubota Technology Development Laboratory Co., Ltd. (56) References JP-A-2-161095 (JP, A) JP-A-2-1611094 (JP, A) (58) Fields investigated (Int. Cl. 6 , DB (Name) E21D 9/06 311

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】互いに隣接する推進体(B),(B)同士
を屈曲自在に連結した連結部(J)を複数備えた推進工
法用推進体装置であって、 前記複数の連結部(J)の一部を、互いに隣接する前記
両推進体(B),(B)の対向する端面間に弾性変形自
在なシール部材(10)を圧入してなる第1連結部(J1
にて構成すると共に、 前記複数の連結部(J)の残部を、連結部(J)の屈曲
姿勢を許容する第1状態とその屈曲姿勢を禁止して直線
状姿勢に保持する第2状態とに切り換える切換え手段
(K)を備える第2連結部(J2)にて構成してある推進
工法用推進体装置。
1. A propulsion body device for a propulsion method comprising a plurality of connecting portions (J) in which mutually adjacent protruding bodies (B) and (B) are flexibly connected to each other, wherein the plurality of connecting portions (J) are provided. ), A first connecting portion (J 1 ) formed by press-fitting an elastically deformable seal member (10) between opposing end faces of the two propulsion bodies (B) and (B) adjacent to each other.
And a second state in which the remaining portions of the plurality of connecting portions (J) are allowed to be bent in the connecting portion (J), and a second state in which the bent portions are prohibited and held in a linear position. A propulsion device for a propulsion method, comprising a second connecting portion (J 2 ) provided with a switching means (K) for switching between the two.
JP28998690A 1990-10-25 1990-10-25 Propulsion device for propulsion method Expired - Fee Related JP2813687B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP28998690A JP2813687B2 (en) 1990-10-25 1990-10-25 Propulsion device for propulsion method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP28998690A JP2813687B2 (en) 1990-10-25 1990-10-25 Propulsion device for propulsion method

Publications (2)

Publication Number Publication Date
JPH04161696A JPH04161696A (en) 1992-06-05
JP2813687B2 true JP2813687B2 (en) 1998-10-22

Family

ID=17750300

Family Applications (1)

Application Number Title Priority Date Filing Date
JP28998690A Expired - Fee Related JP2813687B2 (en) 1990-10-25 1990-10-25 Propulsion device for propulsion method

Country Status (1)

Country Link
JP (1) JP2813687B2 (en)

Also Published As

Publication number Publication date
JPH04161696A (en) 1992-06-05

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