JPH04366298A - Temporary sheathing work for cut face - Google Patents

Temporary sheathing work for cut face

Info

Publication number
JPH04366298A
JPH04366298A JP16745391A JP16745391A JPH04366298A JP H04366298 A JPH04366298 A JP H04366298A JP 16745391 A JP16745391 A JP 16745391A JP 16745391 A JP16745391 A JP 16745391A JP H04366298 A JPH04366298 A JP H04366298A
Authority
JP
Japan
Prior art keywords
propulsion
airbag
face
cut face
earth
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
JP16745391A
Other languages
Japanese (ja)
Inventor
Akio Ono
大野 彰雄
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Taisei Corp
Original Assignee
Taisei 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 Taisei Corp filed Critical Taisei Corp
Priority to JP16745391A priority Critical patent/JPH04366298A/en
Publication of JPH04366298A publication Critical patent/JPH04366298A/en
Pending legal-status Critical Current

Links

Landscapes

  • Excavating Of Shafts Or Tunnels (AREA)

Abstract

PURPOSE:To exactly shield a cut face by a simplified operation as needed. CONSTITUTION:In a method of closing a cut face on the tip of a tube having a cutting edge on its tip, which is being advanced under the ground, a rigid frame 3 is housed in the cutting edge 2 and an expandible air bag 4 made of a flexible, water-stopping material is positioned on the front of the frame inside of the cutting edge 2. A fluid is supplied into the air bag to expand it in order to close the cut face.

Description

【発明の詳細な説明】[Detailed description of the invention]

【0001】0001

【産業上の利用分野】本発明は、切羽土砂の管内流入を
効果的に阻止できる、切羽仮土留工法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a face temporary earth retaining method that can effectively prevent the inflow of face earth and sand into pipes.

【0002】0002

【従来の技術】帯水層や地下水層を対象に推進工法を採
用する場合は、ウェルポイント工法やデープウェル工法
を併用して推進レベルより下位に地下水位を下げておく
必要がある。これは、推進管内に水と共に大量の土砂が
流入するのを阻止するためである。
[Prior Art] When a propulsion method is used for an aquifer or a groundwater aquifer, it is necessary to lower the groundwater level below the propulsion level by using the well point method or the deep well method in combination. This is to prevent a large amount of earth and sand from flowing into the propulsion pipe together with water.

【0003】0003

【発明が解決しようとする問題点】揚水ポンプの故障或
いは停電事故が発生すると、故障箇所の修理や停電が復
旧するまでの間、揚水作業の中断を強いられる。修理や
復旧に時間がかかると、地下水の水位が推進管を越えて
上昇する場合がある。このような場合、推進管は土砂の
侵入を阻止する機能を具備しないために、推進管内へ大
量土砂の流入を許してしまい、地上の陥没事故を誘発す
る危険がある。
[Problems to be Solved by the Invention] When a water pump malfunctions or a power outage occurs, water pumping operations are forced to be suspended until the faulty part is repaired or the power is restored. If repairs and restoration take time, the groundwater level may rise above the propulsion pipe. In such a case, since the propulsion pipe does not have a function to prevent the intrusion of earth and sand, a large amount of earth and sand is allowed to flow into the propulsion pipe, and there is a risk of causing a ground cave-in accident.

【0004】0004

【本発明の目的】本発明は以上の点に鑑みてなされたも
ので、その目的とするところは、必要な時に簡易な操作
で確実に切羽を遮蔽できる、切羽仮土留工法を提供する
ことにある。
[Object of the present invention] The present invention has been made in view of the above points, and its purpose is to provide a face temporary earth retaining method that can reliably shield the face with simple operation when necessary. be.

【0005】[0005]

【問題点を解決するための手段】本発明は、先端に推進
用刃口を取り付けて地中を推進する管体の先端の切羽を
閉塞する方法であって、推進用刃口の内側に剛性の枠体
を収容し、推進用刃口の内側であって前記枠体の前方に
可撓性と止水性を有する素材で形成した膨縮自在のエア
バッグを位置させ、エアバッグに流体を供給して膨脹さ
せて切羽を閉塞する、切羽仮土留工法である。
[Means for Solving the Problems] The present invention is a method of closing the face at the tip of a tube for propelling underground by attaching a propulsion cutter to the tip, and in which the inside of the propulsion cutter has rigidity. An inflatable airbag made of a flexible and waterproof material is located inside the propulsion blade opening and in front of the frame, and fluid is supplied to the airbag. This is a face temporary earth retention method in which the earth is inflated and the face is closed.

【0006】[0006]

【本発明の構成】以下図面を参照しながら本発明につい
て説明する。
[Structure of the present invention] The present invention will be explained below with reference to the drawings.

【0007】<イ>仮土留手段 図1に切羽の土留手段の概念図を示す。推進管1の先端
に筒状の推進用刃口2を取り付けて、地中を推進させる
ことは従来と同様である。本発明は仮土留を必要とする
とき、推進用刃口2の内側に剛性の枠体3を組み立てる
か、或いは事前に取り付けておいた枠体3の前方に袋状
のエアバッグ4を位置させ、エアバッグ4にエアを供給
して膨脹させることで、推進管1の先端を閉塞する。
<A> Temporary Earth Retaining Means FIG. 1 shows a conceptual diagram of the earth retaining means for the face. A cylindrical propulsion blade 2 is attached to the tip of the propulsion tube 1 to propel the tube underground, as in the conventional case. In the present invention, when temporary soil retention is required, a rigid frame 3 is assembled inside the propulsion cutting edge 2, or a bag-shaped airbag 4 is positioned in front of the frame 3 that has been attached in advance. By supplying air to the air bag 4 and inflating it, the tip of the propulsion tube 1 is closed.

【0008】<ロ>枠体 枠体3は膨脹させたエアバッグ4の後退を阻止する部材
であると共に、推進用刃口2の補強部材としても機能す
る。また枠体は鋼材等を組み合わせて形成し、特別鋼材
の組み合わせ形状に制限を受けない。上記の他に枠体3
に要求されることは、推進用刃口2を通過できない外径
を有し、しかも推進中に土砂の取り込みを阻害しない構
造であれば良い。また枠体3は推進中は使用せず、エア
バッグ4を装着する際に鋼材を運び込み、推進用刃口2
の内側で組み立ててもよい。
<B> Frame The frame 3 is a member that prevents the inflated airbag 4 from retreating, and also functions as a reinforcing member for the propulsion blade 2. Furthermore, the frame is formed by combining steel materials, etc., and there are no restrictions on the shape of the combination of special steel materials. In addition to the above, frame 3
What is required is a structure that has an outer diameter that cannot pass through the propulsion blade opening 2 and does not inhibit the uptake of earth and sand during propulsion. In addition, the frame body 3 is not used during propulsion, and steel material is carried in when installing the airbag 4.
It can be assembled inside.

【0009】<ハ>エアバッグ エアバッグ4は土圧に対抗できる強度と防水性を備えた
素材を用いて、推進管1の径に応じて袋状に製作する。 エアバッグ4の一部には、エア等を供給できる供給ホー
スを取り付けておく。エアバッグ4は少なくとも膨脹し
たときに推進用刃口2の内周面に圧着できる寸法であれ
ば良い。エアバッグ4の膨脹流体は、エア等の気体の他
に水等の流体、或いは発泡性の材料を使用しても良い。
<C> Airbag The airbag 4 is manufactured in a bag shape according to the diameter of the propulsion tube 1 using a material that is strong enough to withstand earth pressure and waterproof. A supply hose capable of supplying air, etc. is attached to a part of the airbag 4. The size of the airbag 4 may be such that it can be pressed against the inner circumferential surface of the propulsion blade 2 at least when inflated. The inflation fluid of the airbag 4 may be a gas such as air, a fluid such as water, or a foaming material.

【0010】0010

【作用】つぎに推進工法を一例に刃口の土留方法につい
て説明する。
[Operation] Next, the method of retaining earth at the cutting edge will be explained using the propulsion method as an example.

【0011】<イ>推進 図2に推進時の切羽の断面図を示す。推進作業に先行し
てウェルポイント工法やデープウェル工法で推進レベル
より下位に地下水位を下げておく。そして、先端に推進
用刃口2を装着した推進管1の基端から推力を加えて図
面左側へ推進を続ける。推進用刃口2の開口から取り込
んだ土砂は、発進側へ運搬して排土する。
<A> Propulsion FIG. 2 shows a sectional view of the face during propulsion. Prior to the promotion work, lower the groundwater level below the promotion level using the well point construction method or deep well construction method. Then, thrust is applied from the base end of the propulsion tube 1, which has the propulsion blade 2 attached to the tip, to continue propulsion toward the left side of the drawing. The earth and sand taken in through the opening of the propulsion blade 2 is transported to the starting side and discharged.

【0012】<ロ>仮土留 揚水ポンプの故障や停電事故が発生して地下水の水位が
上昇してきたら、図1、3に示すように、折り畳んであ
るエアバッグ4を枠体3の前方に位置させ、エアバッグ
4から延びる供給ホース5の端にバルブ6を介して図示
しないコンプレッサー等の流体供給装置に配管する。そ
して、エアバッグ4にエアの供給を開始する。その結果
、折り畳んであるエアバッグ4が推進用刃口2の内側で
,かつ枠体2の前方で膨脹をはじめ、エアバッグ4の周
面が推進用刃口2の内周面に圧着して推進用刃口2を閉
塞する。したがって、切羽土砂はエアバッグ4によって
遮られるから、推進管1内への土砂の流入が阻止される
。この間に揚水ポンプの修理や送電の復旧作業を行う。
<B> If the underground water level rises due to a failure of the temporary storage pump or a power outage accident, the folded airbag 4 is placed in front of the frame 3 as shown in FIGS. 1 and 3. The end of the supply hose 5 extending from the airbag 4 is connected via a valve 6 to a fluid supply device such as a compressor (not shown). Then, supply of air to the airbag 4 is started. As a result, the folded airbag 4 begins to expand inside the propulsion blade 2 and in front of the frame 2, and the peripheral surface of the airbag 4 is pressed against the inner peripheral surface of the propulsion blade 2. The propulsion blade opening 2 is closed. Therefore, since the face earth and sand are blocked by the airbag 4, the earth and sand are prevented from flowing into the propulsion pipe 1. During this time, repairs to the water pump and restoration of power transmission will be carried out.

【0013】<ハ>仮土留解除 再び揚水して地下水位を下げたら、バルブ6を開いてエ
アバッグ4を収縮させて回収する。エアバッグ4を回収
したら推進作業を再開する。
<C> Release of temporary soil retention After the water is pumped up again to lower the groundwater level, the valve 6 is opened to deflate the airbag 4 and the water is recovered. After recovering airbag 4, propulsion work will resume.

【0014】[0014]

【その他の実施例】図4に示すように、推進用刃口2の
内周面と接触予定のエアバッグ4の周面に、連続して環
状シール41を接着等により取り付けても良い。環状シ
ール41は例えば厚さ5ミリ、幅100ミリ程度の軟質
ゴムを使用することができる。さらにまた、エアバッグ
4と推進用刃口2の前面を止水する環状のシール材43
を取り付けても良い。シール材43はエアバッグ4側に
接着剤等で固着しておく。
[Other Embodiments] As shown in FIG. 4, an annular seal 41 may be attached continuously to the inner circumferential surface of the propulsion cutting edge 2 and the circumferential surface of the airbag 4 which is to be in contact with it by adhesive or the like. The annular seal 41 can be made of soft rubber with a thickness of about 5 mm and a width of about 100 mm, for example. Furthermore, an annular sealing material 43 that seals off water between the airbag 4 and the front surface of the propulsion blade opening 2 is provided.
You can also attach it. The sealing material 43 is fixed to the airbag 4 side with adhesive or the like.

【0015】[0015]

【発明の効果】本発明は以上説明したようになるから次
のような効果を得ることができる。
[Effects of the Invention] Since the present invention is as explained above, the following effects can be obtained.

【0016】<イ>  小さく畳んであるエアバッグを
仮土留位置に位置させ、切羽で膨脹させるだけの簡単な
操作で、切羽土砂の侵入を確実に阻止することができる
[0016] <A> The intrusion of earth and sand into the face can be reliably prevented by a simple operation of placing a small folded air bag at the temporary soil retaining position and inflating it at the face.

【0017】<ロ>  エアバッグを萎ませて回収でき
るので、切羽の解放操作が簡単に行える。
<B> Since the airbag can be deflated and recovered, the face can be easily released.

【0018】<ハ>  エアバッグが可撓性を有するか
ら、管体の内周面との密着性が良好で、水密性に対する
信頼が高い。
<C> Since the airbag is flexible, it has good adhesion to the inner circumferential surface of the tube and is highly reliable in terms of watertightness.

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

【図1】  本発明の仮土留工法に使用する機材の説明
[Figure 1] Explanatory diagram of equipment used in the temporary earth retention method of the present invention

【図2】  推進時における切羽の断面図[Figure 2] Cross-sectional view of the face during propulsion

【図3】 
 仮土留時における切羽の断面図
[Figure 3]
Cross-sectional view of the face during temporary earth retention

【図4】  他の実施
例の説明図
[Figure 4] Explanatory diagram of another embodiment

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】    先端に推進用刃口を取り付けて地
中を推進する管体の先端の切羽を閉塞する方法であって
、推進用刃口の内側に剛性の枠体を収容し、推進用刃口
の内側であって前記枠体の前方に可撓性と止水性を有す
る素材で形成した膨縮自在のエアバッグを位置させ、エ
アバッグに流体を供給して膨脹させて切羽を閉塞する、
切羽仮土留工法。
Claim 1: A method of closing the face at the tip of a tube for propelling underground by attaching a propulsion cutter to the tip, the method comprising: housing a rigid frame inside the propulsion cutter; An inflatable airbag made of a flexible and waterproof material is positioned inside the cutting edge and in front of the frame, and fluid is supplied to the airbag to inflate it and close the face. ,
Face temporary earth retaining method.
JP16745391A 1991-06-13 1991-06-13 Temporary sheathing work for cut face Pending JPH04366298A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16745391A JPH04366298A (en) 1991-06-13 1991-06-13 Temporary sheathing work for cut face

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16745391A JPH04366298A (en) 1991-06-13 1991-06-13 Temporary sheathing work for cut face

Publications (1)

Publication Number Publication Date
JPH04366298A true JPH04366298A (en) 1992-12-18

Family

ID=15849975

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16745391A Pending JPH04366298A (en) 1991-06-13 1991-06-13 Temporary sheathing work for cut face

Country Status (1)

Country Link
JP (1) JPH04366298A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008163602A (en) * 2006-12-27 2008-07-17 Totetsu Kogyo Co Ltd Excavating element

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008163602A (en) * 2006-12-27 2008-07-17 Totetsu Kogyo Co Ltd Excavating element

Similar Documents

Publication Publication Date Title
US3618639A (en) Packer for sealing pipe leaks
CN102900848B (en) A kind of shield machine belt pressure warehouse entry airbag sealing unit and method
US4167358A (en) Open-channel flow control system
US8763688B2 (en) High pressure oil pipe bullet plug
KR0178146B1 (en) Method for everting a tubular liner bag
GB2030624A (en) Collapsible rubber dam
US5687771A (en) Temporarily blocking the bore of a pipe through which a fluid flows with a foamed plug removed by dissolving
JPH04366298A (en) Temporary sheathing work for cut face
CN210661351U (en) Air-filled sealing protective air bag of shield machine
JP4479591B2 (en) Rubber weir and repair method of rubber weir
CA2080046A1 (en) Device for temporarily obturating a pipeline carrying any fluid whatsoever
JP3986336B2 (en) Shaft seal device
JP2002180780A (en) Sealing method for shaft arrival of shield machine and its device
JP2020133650A (en) Water stop plug
CN218093038U (en) Sealing device for shield starting receiving machine
CN218063401U (en) Leading-in protective sealing device and heading machine
EP0368527B1 (en) Device and method for temporarily blocking the bore of a pipe through which a fluid flows
CN117569864A (en) Device and method for exhausting gas of road tunnel penetrating through steep coal seam
JP3628233B2 (en) Propulsion drilling method
JPS6027198Y2 (en) Shield tail seal device
JPH0220309Y2 (en)
JP2971900B2 (en) Tail seal replacement method for shield machine
JPH11100827A (en) Water stop joint and on-site repairing method for water stop material with it
JPH0438957B2 (en)
JPH03247897A (en) Method and device for emergency water stop in tail-sealing section of shielding machine