JP2008274584A - Anchor device setting method and anchor device - Google Patents

Anchor device setting method and anchor device Download PDF

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JP2008274584A
JP2008274584A JP2007117037A JP2007117037A JP2008274584A JP 2008274584 A JP2008274584 A JP 2008274584A JP 2007117037 A JP2007117037 A JP 2007117037A JP 2007117037 A JP2007117037 A JP 2007117037A JP 2008274584 A JP2008274584 A JP 2008274584A
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wing
anchor
wing device
construction method
lower wing
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JP4912208B2 (en
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Akitoshi Tsurumi
明俊 鶴見
Nobuhide Asai
信秀 浅井
Yoshitaka Shimada
祥敬 嶋田
Yusuke Nozaki
裕介 野▲崎▼
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JFE Metal Products and Engineering Inc
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Abstract

<P>PROBLEM TO BE SOLVED: To provide an anchor device setting method which allows correct driving of an anchor device, facilitates coping with a trouble of difficult driving of a blade device, and facilitates transportation thereof. <P>SOLUTION: According to the anchor device setting method, the blade device 1 consisting of a cylinder portion 10 and a blade portion 20 is driven into the natural ground 8 by a driving means, not shown in Fig. Thereafter, an anchor shaft 2 is inserted into the cylinder portion 10 of the blade device 1 which has already been driven, and driven into the natural ground 8. Further the blade device 1 is formed by combining an upper blade device and a lower blade device with each other. When the blade device is driven into the natural ground, first the lower blade device is driven, and then the upper blade device is driven, followed by combining the former and the latter with each other in the natural ground 8. Thereafter the anchor shaft 2 is driven into the natural ground 8 while penetrating an upper cylinder portion of the upper blade device and a lower cylinder portion of the lower blade device. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

本発明はアンカー装置の施工方法、特に、羽体を具備するアンカー装置の施工方法およびアンカー装置に関する。   The present invention relates to an anchor device construction method, and more particularly, to an anchor device construction method and anchor device having a wing.

従来、法面(斜面)における落石対策施設のロープ(ワイヤ)構造物を固定するために用いるアンカー(アンカーロッド、アンカーパイプ等、本発明において「アンカー装置」と総称する)の施工方法は、
(あ)一般に、地表(地面)に直接打ち込む方法、
(い)あるいは、地面に据削孔を予め形成し、この掘削孔にアンカー装置を挿入する方法、
(う)また、前記掘削孔にアンカー装置を挿入すると共に、モルタル、セメント、樹脂などの凝結効果を有する凝固剤を流しこむことでアンカー装置を地中に定着させる方法(このとき、アンカー装置によって、凝固剤とアンカーの挿入時期は前後するが地中部を定着層と位置づけ、定着層は主には岩盤層、安定した土層などの比較的安定した層で形成される)、がある。
そして、この様に設置されたアンカー装置の地表より上部に露出したアンカー上端部に、金具などで構成されたクリップを介してロープが固定される。
Conventionally, the construction method of an anchor (anchor rod, anchor pipe, etc., collectively referred to as “anchor device” in the present invention) used to fix a rope (wire) structure of a rockfall countermeasure facility on a slope (slope),
(Ah) Generally, the method of driving directly on the ground (ground),
(Ii) Or, a method of forming a pre-installation hole in the ground in advance and inserting an anchor device into the excavation hole,
(Iii) A method of fixing the anchor device in the ground by inserting an anchor device into the excavation hole and pouring a coagulant having a setting effect such as mortar, cement, resin, etc. Although the timing of insertion of the coagulant and anchor is around, the underground part is positioned as a fixing layer, and the fixing layer is mainly formed by a relatively stable layer such as a rock layer or a stable soil layer).
And a rope is fixed to the anchor upper end exposed above the ground surface of the anchor device installed in this way via a clip made of metal fittings or the like.

また、従来の技術では、少なくとも地山が安定した土層で形成される斜面の場合か、あるいは地表が不安定な土層で、地中が岩盤層で形成される様な二つ以上の性質が異なる層から形成されるなどの斜面の場合に、アンカー自身の固定(抜けだしを防止する固定)については、比較的安定していると考えられる。
しかし、地表部に不安定な層が存在している斜面の場合には、アンカー装置と概ね直行する方向の荷重に対して耐力的な要素を望めないことから、場合によればアンカー上端部が荷重作用方向に傾くと考えられる。すなわち、アンカー上端部に取り付けられたクリップおよびロープがアンカー上端部と同様の挙動を示し、落石対策施設としての構造に余分な負荷が生じることになる。
このため、前記アンカー装置の倒れの防止を目的として、アンカーロッドまたはアンカーパイプ(本発明において「アンカー軸」と総称する)を打設後、アンカー軸が貫通した状態で、アンカー軸に沿って、スリーブ(本発明において「筒部」と称す)および羽部を有する羽装置を設置する発明が開示されている(例えば、特許文献1参照)。
In addition, in the conventional technology, at least two characteristics such as the case where the ground is a slope formed by a stable soil layer, or the soil surface is unstable and the ground is formed by a rock layer. In the case of a slope such as formed from different layers, it is considered that the anchor itself is fixed (fixing to prevent pulling out) relatively stable.
However, in the case of a slope with an unstable layer on the ground surface, it is not possible to expect a load bearing element against the load in a direction generally perpendicular to the anchor device. It is thought that it tilts in the direction of load application. That is, the clip and the rope attached to the upper end of the anchor exhibit the same behavior as that of the upper end of the anchor, and an extra load is generated in the structure as a rockfall countermeasure facility.
For this reason, for the purpose of preventing the anchor device from collapsing, an anchor rod or an anchor pipe (generally referred to as “anchor shaft” in the present invention) is placed, and then the anchor shaft passes through the anchor shaft, An invention in which a wing device having a sleeve (referred to as “cylinder portion” in the present invention) and a wing portion is installed is disclosed (for example, see Patent Document 1).

特開2001−226961号公報(第4−5頁、図9)Japanese Patent Laid-Open No. 2001-226916 (page 4-5, FIG. 9)

しかしながら、特許文献1に開示された技術は、アンカー軸を先に打設し、その後に、打羽装置を、既に打設されているアンカー軸に筒部が案内された状態で打設するものであるため、以下のような問題があった。
(イ)アンカー軸は長尺であるため地山に対して打設角度の管理が難しいことから、アンカー軸が地山の表面に対して垂直に打設されない場合には、打羽装置の筒部は地山の表面に対して傾くことになり、打羽装置の羽部の一部が地山の表面から突出する「浮き」が生じ、傾き防止効果が阻害され、目的を満足しない。
(ロ)また、アンカー軸は打設された後、羽装置の打設が困難になって(例えば、小石や礫等に衝突して)打設を断念した場合、羽装置の回収は比較的容易であるものの、アンカー軸の回収(引き抜き)が容易でないため、回収作業に所定の装置と相当の時間とを必要とし、施工コストの上昇や工期の延長の原因になる。
(ハ)さらに、筒部と複数の羽部から構成された羽装置は、相当の重量と見掛け上の嵩とを有することから、トラック輸送の際の積載できる数量が少ないため、運搬コストが上昇する原因や、法面(斜面)の高い位置にまで持ち上げる作業が容易でないため、施工コストの上昇や工期の延長の原因になっていた。
However, in the technique disclosed in Patent Document 1, the anchor shaft is driven first, and then the wing device is driven in a state where the cylindrical portion is guided to the anchor shaft that has already been driven. Therefore, there were the following problems.
(B) Since the anchor shaft is long and it is difficult to control the driving angle with respect to the natural ground, when the anchor shaft is not driven perpendicular to the surface of the natural ground, The part is inclined with respect to the surface of the natural ground, and a part of the wing part of the struck device is caused to “float” protruding from the surface of the natural ground, so that the tilt prevention effect is hindered and the purpose is not satisfied.
(B) In addition, after the anchor shaft is driven, if it becomes difficult to drive the wing device (for example, it collides with pebbles or gravel), the wing device is relatively recovered. Although it is easy, it is not easy to recover (draw out) the anchor shaft, so that a predetermined device and a considerable time are required for the recovery operation, which causes an increase in construction cost and an extension of the construction period.
(C) In addition, since the wing device composed of a cylindrical portion and a plurality of wing portions has a considerable weight and an apparent bulk, the amount that can be loaded during truck transportation is small, so the transportation cost increases. It is not easy to lift up to a position with a high slope (slope), which causes an increase in construction cost and extension of construction period.

本発明は、このような問題を解決するためになされたものであり、正確な打設が可能になると共に、羽装置の打設が困難になった場合でも容易に対応することができ、さらに、運搬が容易になるアンカー装置、およびその施工方法を提供することを目的とする。   The present invention has been made to solve such a problem, and enables accurate placement, and can easily cope with the case where it is difficult to place the wing device. An object of the present invention is to provide an anchor device that can be easily transported, and a construction method thereof.

(1)本発明に係るアンカー装置の施工方法は、筒部および該筒部の外周に固定された羽部からなる羽装置と、前記筒部を貫通自在な棒状または管状のアンカー軸と、からなるアンカー装置の施工方法であって、
前記羽装置を地山に打設する工程と、
前記アンカー軸を、前記打設されている羽装置の筒部に挿入して地山に打設する工程と、を有する。
(1) A construction method of an anchor device according to the present invention comprises: a wing device comprising a tubular portion and a wing portion fixed to the outer periphery of the tubular portion; and a rod-like or tubular anchor shaft that can penetrate the tubular portion. An anchor device construction method comprising:
Placing the wing device on a natural ground;
Inserting the anchor shaft into the cylindrical portion of the wing device that has been driven and driving the anchor shaft into a natural ground.

(2)前記(1)において、前記羽部が前記筒部の軸心を含む面内に配置され、
前記羽装置の上縁が地山の表面と略同一面になるように打設することを特徴とする。
(2) In the above (1), the wing portion is disposed in a plane including the axial center of the cylindrical portion,
The upper edge of the wing device is placed so as to be substantially flush with the surface of the natural ground.

(3)また、本発明に係るアンカー装置の施工方法は、下筒部および該下筒部の外周に固定された下羽部からなる下羽装置と、
上筒部および該上筒部の外周に固定された上羽部からなる上羽装置と、
前記下筒部および前記上筒部を貫通自在な棒状または管状のアンカー軸と、からなるアンカー装置の施工方法であって、
前記下筒部の軸心と前記上筒部の軸心とが一致した状態で、前記下羽装置と前記上羽装置とを一体化する工程と、
前記一体化された前記下羽装置および前記上羽装置を地山に打設する工程と、
前記アンカー軸を、前記一体化されて打設されている上羽装置の上筒部と下羽装置の下筒部とに挿入して地山に打設する工程と、
を有する。
(3) Moreover, the construction method of the anchor device according to the present invention includes a lower wing device composed of a lower tube portion and a lower wing portion fixed to the outer periphery of the lower tube portion,
An upper wing device comprising an upper cylinder portion and an upper wing portion fixed to the outer periphery of the upper cylinder portion;
An anchor device construction method comprising a rod-like or tubular anchor shaft that can pass through the lower cylinder part and the upper cylinder part,
A step of integrating the lower wing device and the upper wing device in a state where the axis of the lower cylinder portion and the axis of the upper cylinder portion coincide with each other;
Placing the integrated lower wing device and the upper wing device on a natural ground;
Inserting the anchor shaft into the upper cylinder part of the upper wing device and the lower cylinder part of the lower wing device that are integrally driven, and driving the ground shaft into a natural ground;
Have

(4)また、前記(3)において、前記上羽装置の上筒部の長さが前記上羽部の上下方向の長さの略半分であって、前記上筒部が前記上羽部の略上半分の範囲に固定され、
前記下羽装置の下筒部の長さが前記下羽部の上下方向の長さの略半分であって、前記下筒部が前記下羽部の略下半分の範囲に固定される、
前記下羽装置の上縁と前記上羽装置の上縁とが略同一面になるように一体化することを特徴とする。
(4) In the above (3), the length of the upper tube portion of the upper wing device is substantially half of the length of the upper wing portion in the vertical direction, and the upper tube portion is the upper wing portion. Fixed in the upper half of the range,
The length of the lower cylinder part of the lower wing device is approximately half of the length of the lower wing part in the vertical direction, and the lower cylinder part is fixed in a range of approximately the lower half of the lower wing part,
The upper edge of the lower wing device and the upper edge of the upper wing device are integrated so as to be substantially flush with each other.

(5)さらに、前記(3)または(4)において、前記上羽装置の上筒部の外周に、前記下羽装置の下羽部が侵入自在な上位置決め手段が設けられ、
前記下羽装置の下筒部の外周に、前記上羽装置の上羽部が侵入自在な下位置決め手段が設けられ、
前記上羽部が前記下位置決め手段に、前記下羽根が前記上位置決め手段に、それぞれ侵入した状態で一体化することを特徴とする。
(5) Further, in (3) or (4), an upper positioning means is provided on the outer periphery of the upper tube portion of the upper wing device so that the lower wing portion of the lower wing device can enter,
On the outer periphery of the lower tube portion of the lower wing device, a lower positioning means is provided that allows the upper wing portion of the upper wing device to enter,
The upper wing part is integrated with the lower positioning means, and the lower wing is integrated with the upper positioning means, respectively.

(6)また、本発明に係るアンカー装置の施工方法は、下筒部および該下筒部の外周に固定された下羽部からなる下羽装置と、
上筒部および該上筒部の外周に固定された上羽部からなる上羽装置と、
前記下筒部および前記上筒部を貫通自在な棒状または管状のアンカー軸と、からなるアンカー装置の施工方法であって、
前記下羽装置を地山に打設する工程と、
前記上羽装置を、前記上筒部の軸心が前記打設されている下羽装置の下筒部の軸心と一致するように打設する工程と、
前記アンカー軸を、前記打設されている上羽装置の上筒部と前記打設されている下羽装置の下筒部とに挿入して地山に打設する工程と、
を有するアンカー装置の施工方法。
(6) Moreover, the construction method of the anchor device according to the present invention includes a lower wing device including a lower cylinder portion and a lower wing portion fixed to the outer periphery of the lower cylinder portion;
An upper wing device comprising an upper cylinder portion and an upper wing portion fixed to the outer periphery of the upper cylinder portion;
An anchor device construction method comprising a rod-like or tubular anchor shaft that can pass through the lower cylinder part and the upper cylinder part,
Placing the lower wing device on a natural ground;
Placing the upper wing device such that the axial center of the upper tubular portion coincides with the axial center of the lower tubular portion of the lower wing device,
Inserting the anchor shaft into the upper cylinder portion of the placed upper wing device and the lower cylinder portion of the placed lower wing device, and placing the anchor shaft on a natural ground;
An anchor device construction method having

(7)前記(6)において、前記上羽装置の上筒部の長さが前記上羽部の上下方向の長さの略半分であって、前記上筒部が前記上羽部の略上半分の範囲に固定され、
前記下羽装置の下筒部の長さが前記下羽部の上下方向の長さの略半分であって、前記下筒部が前記下羽部の略下半分の範囲に固定され、
前記下羽装置の上縁が地山の表面と略同一面になるように打設し、前記上羽装置の上縁が地山の表面と略同一面になるように打設することを特徴とする。
(7) In the above (6), the length of the upper tube portion of the upper wing device is substantially half of the length of the upper wing portion in the vertical direction, and the upper tube portion is substantially above the upper wing portion. Fixed to half the range,
The length of the lower cylinder part of the lower wing device is approximately half of the length in the vertical direction of the lower wing part, and the lower cylinder part is fixed in a range of substantially lower half of the lower wing part,
The lower wing device is placed so that the upper edge is substantially flush with the surface of the natural ground, and the upper wing device is placed so that the upper edge is substantially flush with the surface of the natural ground. And

(8)前記(6)または(7)において、前記上羽装置の上筒部の外周に、前記下羽装置の下羽部が侵入自在な上位置決め手段が設けられ、
前記下羽装置の下筒部の外周に、前記上羽装置の上羽部が侵入自在な下位置決め手段が設けられ、
前記上羽装置を、前記打設されている下羽装置の下位置決め手段に、前記上羽部が侵入するように打設することを特徴とする。
(8) In the above (6) or (7), an upper positioning means is provided on the outer periphery of the upper tube portion of the upper wing device so that the lower wing portion of the lower wing device can enter,
On the outer periphery of the lower tube portion of the lower wing device, a lower positioning means is provided that allows the upper wing portion of the upper wing device to enter,
The upper wing device is placed such that the upper wing portion enters the lower positioning means of the placed lower wing device.

(9)前記(3)乃至(8)の何れかにおいて、前記上羽装置において、前記上羽部が前記上筒部の軸心を含む面内に配置され、
前記下羽装置において、前記下羽部が前記下筒部の軸心を含む面内に配置されることを特徴とする。
(9) In any one of the above (3) to (8), in the upper wing device, the upper wing portion is disposed in a plane including the axis of the upper tube portion,
In the lower wing device, the lower wing portion is disposed in a plane including an axis of the lower cylinder portion.

(10)前記(3)乃至(9)の何れかにおいて、前記上羽装置の上羽部および上位置決め手段が、それぞれ一対であって、前記上羽部が前記上筒部の軸心に対して互いに対称に配置され、前記上位置決め手段が前記上羽部に対して垂直の位置に設けられ、
前記下羽装置の下羽部および下位置決め手段が、それぞれ一対であって、前記下羽部が前記下筒部の軸心に対して互いに対称に配置され、前記下位置決め手段が前記下羽部に対して垂直の位置に設けられ、
前記打設されている下羽装置の一対の下羽部と前記打設されている上羽装置の一対の上羽部とが互いに垂直に位置決めされた状態で、前記アンカー軸を、前記打設されている上羽装置の上筒部と前記打設されている下羽装置の下筒部に挿入して地山に打設する工程と、を有することを特徴とする。
(10) In any one of (3) to (9), the upper wing portion and the upper positioning means of the upper wing device are each a pair, and the upper wing portion is relative to the axis of the upper cylinder portion. Are arranged symmetrically with each other, and the upper positioning means is provided at a position perpendicular to the upper wing part,
The lower wing device includes a pair of lower wing portions and lower positioning means, the lower wing portions are arranged symmetrically with respect to the axis of the lower cylinder portion, and the lower positioning means is the lower wing portion. In a position perpendicular to the
In the state where the pair of lower wing portions of the placed lower wing device and the pair of upper wing portions of the placed upper wing device are positioned perpendicular to each other, the anchor shaft And a step of inserting into the upper cylinder portion of the upper wing device and the lower cylinder portion of the lower wing device that has been placed, and placing in a natural ground.

(11)前記(1)または(2)において、前記羽装置に係止自在な天板を、前記羽部の上面に載置する工程を有することを特徴とする。   (11) The method according to (1) or (2), further comprising a step of placing a top plate that can be locked to the wing device on an upper surface of the wing portion.

(12)前記(3)乃至(10)の何れかにおいて、前記上羽装置および前記下羽装置に係止自在な天板を、前記上羽部の上面および前記下羽部の上面に載置する工程を有することを特徴とする。   (12) In any one of (3) to (10), the top plate that can be locked to the upper wing device and the lower wing device is placed on the upper surface of the upper wing portion and the upper surface of the lower wing portion. It has the process to perform.

(13)前記(3)乃至(10)の何れかにおいて、前記上羽装置の上羽部の上縁に係止用突起部が設けられ、
前記下羽装置の下羽部の上縁に係止用突起部が設けられ、
円周方向で4箇所等分配置され、前記係止用突起部が係止自在な係止用溝部が形成された天板を用意する工程と、
前記打設されている下羽装置の下羽部に設けられた係止用突起部および前記打設されている上羽装置の上羽部に設けられた係止用突起部が、前記係止用溝部に係止するように前記天板を載置する工程と、
を有することを特徴とする。
(13) In any one of (3) to (10), a locking projection is provided on an upper edge of the upper wing of the upper wing device,
A locking projection is provided on the upper edge of the lower wing portion of the lower wing device,
A step of preparing a top plate that is arranged in four equal parts in the circumferential direction and in which a locking groove portion on which the locking projection portion can be freely locked is formed;
The locking projection provided on the lower wing portion of the placed lower wing device and the locking projection provided on the upper wing portion of the placed upper wing device are Placing the top plate so as to be engaged with the groove portion,
It is characterized by having.

(14)また、本発明に係るアンカー装置は、下筒部および該下筒部の外周に固定された下羽部からなる下羽装置と、
上筒部および該上筒部の外周に固定された上羽部からなる上羽装置と、
前記下筒部および前記上筒部を貫通自在な棒状または管状のアンカー軸と、を有する。
(15)前記(14)において、前記上羽装置および前記下羽装置に係止自在な天板を有することを特徴とする。
(14) Further, the anchor device according to the present invention includes a lower wing device including a lower cylinder portion and a lower wing portion fixed to the outer periphery of the lower cylinder portion,
An upper wing device comprising an upper cylinder portion and an upper wing portion fixed to the outer periphery of the upper cylinder portion;
A rod-like or tubular anchor shaft that can pass through the lower cylinder part and the upper cylinder part.
(15) In the above (14), a top plate that can be locked to the upper wing device and the lower wing device is provided.

本発明に係るアンカー装置の施工方法は以上の構成であるから、以下の効果を奏する。
(i)本発明に係るアンカー装置の施工方法は、まず、羽装置を地山に打設する工程を実行し、これに続いて、既に打設されている羽装置の筒部にアンカー軸を挿入して、かかる挿入した状態でアンカー軸を地山に打設するから、(a)アンカー軸が地山の表面に対して垂直に打設されない場合であっても、既に打設されている打羽装置が倒されることがないから、羽装置の「浮き」が生じることがなく、目的が満足される。(b)また、羽装置の打設が困難になって打設を断念した場合であっても、まだ、アンカー軸は打設されていないから、羽装置のみを容易に回収(引き抜き)するだけで済み、対処が容易かつ迅速である。(c)さらに、アンカー軸を倒すような力が作用した場合でも、羽部が抵抗体として機能するから、アンカー装置の倒れが防止される。
なお、アンカーロッドまたはアンカーパイプ等は、単に「アンカー」と称すことができるものであるが、これと羽装置とからなる「アンカー装置」との混同を防止するため、本発明においては便宜上、「アンカー軸」と称す。
Since the construction method of the anchor device according to the present invention has the above configuration, the following effects can be obtained.
(I) In the anchor device construction method according to the present invention, first, the step of placing the wing device on the ground is executed, and subsequently, the anchor shaft is attached to the tube portion of the already-installed wing device. Since the anchor shaft is driven into the natural ground in the inserted state, (a) the anchor shaft is already driven even if the anchor shaft is not driven perpendicular to the surface of the natural ground. Since the squirting device is not overturned, the “floating” of the wing device does not occur and the object is satisfied. (B) Even if it is difficult to place the wing device and it has been abandoned, since the anchor shaft has not yet been placed, only the wing device is easily recovered (pulled out). It is easy and quick to deal with. (C) Further, even when a force that tilts the anchor shaft is applied, the wing portion functions as a resistor, so that the anchor device is prevented from falling.
The anchor rod, the anchor pipe, or the like can be simply referred to as “anchor”, but in order to prevent confusion between the “anchor device” composed of this and the wing device, It is called “anchor shaft”.

(ii)羽部が筒部の軸心を含む面内に配置され、羽装置の上縁が地山の表面と略同一面になるように打設するから、羽部にかかる力が筒部に確実に伝達され、羽装置の「浮き」が防止される。
なお、羽装置の上縁とは、羽部の上縁が筒部の軸心に対して垂直である場合には当該上縁を、羽部の上縁が筒部から離れるほど下がるように筒部の軸心に対して傾斜する場合には、上縁の羽部と筒部との接続位置を、羽部の上縁が筒部から離れるほど上がるように筒部の軸心に対して傾斜する場合には、上縁の筒部から最も離れた位置を、それぞれ意味している。
(Ii) Since the wing portion is arranged in a plane including the axis of the tube portion and the upper edge of the wing device is placed substantially flush with the surface of the natural ground, the force applied to the wing portion is the tube portion. The wing device is prevented from “floating”.
The upper edge of the wing device means that the upper edge of the wing part is perpendicular to the axis of the cylinder part, and the upper edge of the wing part is lowered so that the upper edge of the wing part moves away from the cylinder part. When tilting with respect to the axial center of the head part, tilt the connection position between the upper wing part and the cylindrical part with respect to the axial center of the cylindrical part so that the upper edge of the wing part rises away from the cylindrical part. In this case, the position farthest from the upper edge cylinder portion is meant.

(iii)また、まず下羽装置を打設し、次に、上羽装置を打設し、最後にアンカー軸を、既に打設されている上羽装置の上筒部と既に打設されている下羽装置の下筒部とに挿入して、かかる挿入した状態でアンカー軸を打設するから、前記(i)における(a)、(b)および(c)の効果が得られると共に、(d)下羽装置および上羽装置それぞれが、嵩張らずに軽量になる。   (Iii) Also, first the lower wing device is placed, then the upper wing device is placed, and finally the anchor shaft is already placed with the upper cylinder portion of the already placed upper wing device. Since the anchor shaft is driven in the inserted state with the lower cylinder portion of the lower wing device, the effects (a), (b) and (c) in (i) can be obtained, (D) Each of the lower wing device and the upper wing device is light without being bulky.

(iv)さらに、下羽装置の上縁と上羽装置の上縁とが略同一面になるように一体化するから、一体化した状態において下羽装置の上縁と上羽装置の上縁とに高低差がなく、打設された状態において地山への納まりがよい。
なお、下羽部の上縁および上羽部の上縁とは、それぞれ前記(ii)の羽装置の上縁に準じる。
(v)さらに、上羽部が下位置決め手段に、下羽根が上位置決め手段に、それぞれ侵入した状態で一体化するから、上羽部と下羽根との配置が正確になると共に、配置された位置が変動することがないため、アンカー装置の倒れが確実に防止される。
(Iv) Furthermore, since the upper edge of the lower wing device and the upper edge of the upper wing device are integrated so that they are substantially flush with each other, the upper edge of the lower wing device and the upper edge of the upper wing device are integrated. There is no difference in height between the two, and it is easy to fit in the natural ground when placed.
Note that the upper edge of the lower wing part and the upper edge of the upper wing part correspond to the upper edge of the wing device of (ii), respectively.
(V) Furthermore, since the upper wing part is integrated with the lower positioning means and the lower blade is integrated with the upper positioning means in an invading state, the arrangement of the upper wing part and the lower wing becomes accurate and arranged. Since the position does not change, the anchor device is reliably prevented from falling.

(vi)下羽装置と上羽装置とを、それぞれ別個に打設するから、打設が容易である。
(vii)さらに、下羽装置の上縁と上羽装置の上縁とが略同一面になるように打設するから、打設した状態において、下羽装置の上縁と上羽装置の上縁とに高低差がなく地山への納まりがよい。
なお、下羽装置の上縁および上羽装置の上縁とは、それぞれ前記(ii)の羽装置の上縁に準じる。
(Vi) Since the lower wing device and the upper wing device are driven separately, the driving is easy.
(Vii) Furthermore, since the upper edge of the lower wing device and the upper edge of the upper wing device are placed so that they are substantially flush with each other, the upper edge of the lower wing device and the upper edge of the upper wing device are There is no difference in height with the edge, and it fits in the natural ground.
The upper edge of the lower wing device and the upper edge of the upper wing device are the same as the upper edge of the wing device of (ii), respectively.

(viii)上羽装置を、既に打設されている下羽装置の下位置決め手段に、上羽部が侵入するように打設するから、(f)下羽装置の下羽部と上羽装置の上羽部との配置が正確になる。   (Viii) Since the upper wing device is driven so that the upper wing portion enters the lower positioning means of the already placed lower wing device, (f) the lower wing portion and the upper wing device of the lower wing device. The placement with the upper wing part becomes accurate.

(ix)また、上羽部が上筒部の軸心を含む面内に配置され、下羽部が下筒部の軸心を含む面内に配置されるから、上羽部および下羽部にかかる力が上筒部および下筒部に確実に伝達され、羽装置の「浮き」が防止される。
(x)さらに、下羽装置の一対の下羽部と上羽装置の一対の上羽部とが十字状に配置されるように打設されるから、アンカー装置の倒れが防止される(前記(c)参照)。また、一対の下羽部、および一対の上羽部は、いずれも平面を形成するから、下羽装置および上羽装置の見掛け上の嵩が大幅に小さくなり、運搬がさらに容易になる(前記(d)参照)。
(Ix) Since the upper wing portion is arranged in a plane including the axis of the upper cylinder portion and the lower wing portion is arranged in a plane including the axis of the lower cylinder portion, the upper wing portion and the lower wing portion The force applied to is reliably transmitted to the upper tube portion and the lower tube portion, and “floating” of the wing device is prevented.
(X) Furthermore, since the pair of lower wing portions of the lower wing device and the pair of upper wing portions of the upper wing device are placed so as to be arranged in a cross shape, the anchor device is prevented from falling (see above). (See (c)). In addition, since the pair of lower wing parts and the pair of upper wing parts form a flat surface, the apparent bulk of the lower wing apparatus and the upper wing apparatus is significantly reduced, and transportation is further facilitated (see above). (See (d)).

(xi)また、天板を羽部の上面に載置するから、羽部の配置が正確になる。
(xii)同様に、天板を上羽部の上面および下羽部の上面に載置するから、両者の配置が正確になる。
(Xi) Moreover, since the top plate is placed on the upper surface of the wing portion, the wing portion is accurately arranged.
(Xii) Similarly, since the top plate is placed on the upper surface of the upper wing portion and the upper surface of the lower wing portion, the arrangement of the two becomes accurate.

(xiii)下羽装置の下羽部および上羽装置の上羽部が、これに係止する天板によって位置決めされるから、配置された位置が変動することがないため、アンカー装置の倒れが確実に防止される(前記(c)参照)。   (Xiii) Since the lower wing portion of the lower wing device and the upper wing portion of the upper wing device are positioned by the top plate locked to the upper wing device, the arranged position does not change, and the anchor device falls down. This is surely prevented (see (c) above).

(xiv)また、本発明に係るアンカー装置は、下羽装置と、上羽装置と、アンカー軸と、を有するから、運搬が容易になる。
(xv)さらに、下羽装置および上羽装置に係止自在な天板を有するから、両者の配置が正確になる。
(Xiv) Moreover, since the anchor apparatus which concerns on this invention has a lower wing apparatus, an upper wing apparatus, and an anchor shaft, conveyance becomes easy.
(Xv) Further, since the lower wing device and the upper wing device have a top plate that can be locked, the arrangement of the two becomes accurate.

[実施の形態1:一体タイプ]
図1は本発明の実施の形態1に係るアンカー装置の施工方法を工程を追って説明する模式図である。
図1の(a)において、筒部10と、筒部10の外周に固定された羽部20からなる羽装置1を、予め試掘7が実施され後記するアンカー軸2を打設することが可能であることが確認された地山8の表面(以下、「地表面」と称す)9の施工地点に位置決めする。
なお、図中、羽部20は台形状であって、左右に一対だけ図示しているが、本発明はその形状や数量を限定するものではない。たとえば、4枚の羽部を十字状に設けてもよい。
[Embodiment 1: Integrated type]
FIG. 1 is a schematic view for explaining the anchor device construction method according to Embodiment 1 of the present invention step by step.
In FIG. 1A, it is possible to place an anchor shaft 2, which will be described later, in which a trial digging 7 is performed in advance on a wing device 1 including a cylinder portion 10 and a wing portion 20 fixed to the outer periphery of the cylinder portion 10. It is positioned at the construction point of the surface 9 (hereinafter referred to as “the ground surface”) 9 of the natural ground 8 confirmed to be.
In addition, in the figure, the wing | blade part 20 is trapezoid shape, Comprising: Although only one pair is shown in figure on the right and left, this invention does not limit the shape and quantity. For example, four wings may be provided in a cross shape.

図1の(b)において、羽装置1を図示しない打設手段によって地山8に打設する。このとき、羽部20の上縁(位置ハと位置ニとを結ぶ線に同じ)は筒部10に垂直であって、地表面9と略同一面になるまで打設する。
なお、羽部20の下縁(位置イと位置ロとを結ぶ線に同じ)は筒部10に近づくほど下方に突出するように傾斜しているため、打設が容易である。また、羽部20の上下方向の長さ(位置イと位置ニとの距離に同じ)は比較的短いため、打設中に傾くことがないだけでなく、羽部20が石や礫等に衝突して打設を中止せざるを得ない場合でも、羽装置1を容易に回収(引き抜く)ことができる。
また、打設手段は限定するものではなく、さらに、羽装置1にアダプタ(打設面が形成されている)を載置して、これを介して羽装置1を打設してもよい。
In FIG. 1B, the wing device 1 is driven on the ground 8 by a driving means (not shown). At this time, the upper edge of the wing portion 20 (same as the line connecting the position c and the position d) is perpendicular to the cylindrical portion 10 and is placed until it is substantially flush with the ground surface 9.
In addition, since the lower edge of the wing part 20 (same as the line connecting the position A and the position B) is inclined so as to protrude downward as it approaches the cylinder part 10, it is easy to place. In addition, since the vertical length of the wing part 20 (same as the distance between the position A and the position D) is relatively short, the wing part 20 is not tilted during placement, but the wing part 20 is made of stone or gravel. Even in the case where it is necessary to stop driving due to a collision, the wing device 1 can be easily recovered (pulled out).
In addition, the placing means is not limited, and an adapter (a placement surface is formed) may be placed on the wing device 1 and the wing device 1 may be placed therethrough.

図1の(c)において、アンカー軸2を、既に打設されている羽装置1の筒部10に挿入して地山8に打設する。すなわち、アンカー軸2と羽装置1とによってアンカー装置100が形成される。
このとき、アンカー軸2の打設地点は、試掘7によって打設可能であることが確認されているから、アンカー軸2は所定の深さに打設することができる。また、仮に、アンカー軸c2の打設方向が偏位した(傾いた)としても、羽装置1は既に打設されているため、羽装置1の姿勢が変動する(傾く)ことがない。すなわち、羽部20の一部が地表面9から突出する「浮き」が生じることがない。
In FIG. 1C, the anchor shaft 2 is inserted into the cylinder portion 10 of the wing device 1 that has already been driven and driven into the ground 8. That is, the anchor device 100 is formed by the anchor shaft 2 and the wing device 1.
At this time, since it has been confirmed that the anchoring point of the anchor shaft 2 can be driven by the test excavation 7, the anchor shaft 2 can be driven to a predetermined depth. Further, even if the driving direction of the anchor shaft c2 is deviated (tilted), the wing device 1 has already been driven, so that the posture of the wing device 1 does not change (tilt). That is, “floating” in which a part of the wing portion 20 protrudes from the ground surface 9 does not occur.

なお、アンカー軸2の長さや形状は限定するものではなく、管、棒あるいはこれに外周リブが形成されたもの等何れであってもよい。また、打設手段は限定するものではなく、さらに、アンカー軸2の状態にアダプラ(打設面が形成されている)を載置して、これを介してアンカー軸2を打設してもよい。
また、図1において、羽装置1の上縁が羽部20の上縁(図1の(b)において位置ハと位置ニとを結ぶ線に同じ)に同じであって、かかる上縁が、筒部10に軸心に対して垂直になっているが、本発明はこれに限定するものではなく、上縁が傾斜してもよい。
例えば、羽部20の上縁が筒部10から離れるほど下がるように筒部の軸心に対して傾斜する(ハ字状を呈す)場合には、羽部20と筒部10との接続位置(位置二)を羽装置1の上縁とし、反対に、羽部20の上縁が筒部10から離れるほど上がるように筒部の軸心に対して傾斜する(V字状を呈す)場合には、筒部10から最も離れた位置(位置ハ)を羽装置1の上縁とする。
The length and shape of the anchor shaft 2 are not limited, and may be any of a tube, a rod, or an outer peripheral rib formed thereon. Further, the placing means is not limited. Further, even if the adapter shaft (having a placement surface) is placed on the anchor shaft 2 and the anchor shaft 2 is placed therethrough. Good.
In FIG. 1, the upper edge of the wing device 1 is the same as the upper edge of the wing portion 20 (the same as the line connecting position c and position d in FIG. 1B), and the upper edge is Although the cylinder portion 10 is perpendicular to the axis, the present invention is not limited to this, and the upper edge may be inclined.
For example, in the case where the upper edge of the wing part 20 is inclined with respect to the axis of the cylinder part so as to move away from the cylinder part 10 (having a C shape), the connection position between the wing part 20 and the cylinder part 10 When (position 2) is the upper edge of the wing device 1 and, conversely, the upper edge of the wing part 20 is inclined with respect to the axis of the cylinder part so as to move away from the cylinder part 10 (presents a V shape). In this case, the position (position c) farthest from the cylinder portion 10 is defined as the upper edge of the wing device 1.

[実施の形態2:組立タイプ]
図2は本発明の実施の形態2に係るアンカー装置の施工方法に用いられる羽装置を説明する、(a)は羽装置を構成する下羽装置を模式的に示す斜視図、(b)は羽装置を構成する上羽装置を模式的に示す斜視図、(c)は羽装置を模式的に示す斜視図である。
なお、実施の形態1(図1)と同じ部分または相当する部分には同じ符号を付し、一部の説明を省略する。
[Embodiment 2: Assembly type]
2A and 2B illustrate a wing device used in the anchor device construction method according to Embodiment 2 of the present invention, FIG. 2A is a perspective view schematically showing a lower wing device constituting the wing device, and FIG. The perspective view which shows typically the upper wing apparatus which comprises a wing | blade apparatus, (c) is a perspective view which shows a wing apparatus typically.
In addition, the same code | symbol is attached | subjected to the part which is the same as that of Embodiment 1 (FIG. 1), or an equivalent part, and one part description is abbreviate | omitted.

(下羽装置)
図2の(a)において、下羽装置1aは、下筒部10aと、下筒部10aの外周に固定された一対の下羽部20aとからなる。
下筒部10aは、アンカー軸2が貫通自在な内径を具備する円筒であって、外周の下端寄りで軸心を挟んで対称位置に一対の下位置決め用突起11aと、外周の上段寄りで軸心を挟んで対称位置に一対の下位置決め用溝12aとが設けられている。一対の下位置決め用突起11aと一対の下位置決め用溝12aとは、何れも円周方向の同一位相に配置され、説明の便宜上、これらは、3時および9時の位置に配置されていると称す。
(Lower feather device)
In FIG. 2A, the lower wing device 1a includes a lower cylinder portion 10a and a pair of lower wing portions 20a fixed to the outer periphery of the lower cylinder portion 10a.
The lower cylinder portion 10a is a cylinder having an inner diameter through which the anchor shaft 2 can pass, and a pair of lower positioning projections 11a at a symmetrical position with the shaft centered near the lower end of the outer periphery, A pair of lower positioning grooves 12a are provided at symmetrical positions across the center. The pair of lower positioning projections 11a and the pair of lower positioning grooves 12a are both arranged in the same phase in the circumferential direction. For convenience of explanation, they are arranged at the 3 o'clock and 9 o'clock positions. Call it.

一対の下羽部20aは何れも、略台形状の板材であって、上下方向の長さが下筒部10aの長さの略2倍の長さになっている。そして、下端(位置イに同じ)が上筒部10bの下端に一致しているから、下羽部20aは上下方向の下縁寄りの略半分の範囲(位置ヌと位置イを結ぶ線に同じ)において、下筒部10aの12時および6時の位置に固定されている。
すなわち、一対の下位置決め用突起11a(一対の下位置決め用溝12aに同じ)と一対の下羽部20aとは、交互に、直交する面内配置されている(円周方向で等分に配置されている)。
Each of the pair of lower wing portions 20a is a substantially trapezoidal plate member, and the length in the vertical direction is approximately twice the length of the lower tube portion 10a. And since the lower end (same as position i) coincides with the lower end of the upper cylinder part 10b, the lower wing part 20a is the same as the line connecting the position n and position i in the substantially half range near the lower edge in the vertical direction. ) At the 12:00 and 6 o'clock positions of the lower tube portion 10a.
That is, the pair of lower positioning protrusions 11a (same as the pair of lower positioning grooves 12a) and the pair of lower wings 20a are alternately arranged in an orthogonal plane (equally arranged in the circumferential direction). Have been).

また、かかる固定された範囲の上方に、下筒部10a側に突出する下位置決め用突起部21a(位置リと位置ヌとを結ぶ線に同じ)が設けられている。すなわち、下位置決め用突起部21aは側縁(位置トと位置チとを結ぶ線、および位置ルと位置イとを結ぶ線に同じ)に対して、段差(位置チと位置リとを結ぶ線、および位置ヌと位置ルとを結ぶ線に同じ)分だけ、突出している。
さらに、上縁に突出するように下係止用突起部22a(位置ハ、位置ニ、位置ホ、位置ヘにて囲まれた範囲に同じ)が設けられ、下係止用突起部22aには下係止用貫通孔23aが形成されている。
Further, a lower positioning projection 21a (same as the line connecting the position and the position) is provided above the fixed range and protrudes toward the lower cylinder portion 10a. That is, the lower positioning projection 21a has a step (a line connecting the position H and the position R) with respect to the side edge (the same as the line connecting the position G and the position H and the line connecting the position L and the position A). , And the line connecting position n and position le).
Furthermore, a lower locking projection 22a (same as the range surrounded by position c, position d, position e, and position f) is provided so as to protrude to the upper edge, and the lower locking projection 22a A lower locking through hole 23a is formed.

(上羽装置)
図2の(b)において、上羽装置1bは、上筒部10bと、上筒部10bの外周に固定された一対の上羽部20bとからなる。
上筒部10bは、アンカー軸2が貫通自在な内径を具備する円筒であって、外周の上端寄りで軸心を挟んで対称位置に一対の上位置決め用突起11bと、外周の下段寄りで軸心を挟んで対称位置に一対の上位置決め用溝12bとが設けられている。一対の上位置決め用突起11bと一対の上位置決め用溝12bとは、何れも円周方向の同一位相に配置され、説明の便宜上、これらは、12時および6時の位置に配置されていると称す。
(Upper feather device)
In FIG. 2B, the upper wing device 1b includes an upper tube portion 10b and a pair of upper wing portions 20b fixed to the outer periphery of the upper tube portion 10b.
The upper cylinder portion 10b is a cylinder having an inner diameter through which the anchor shaft 2 can pass, and a pair of upper positioning projections 11b in a symmetrical position with the axis centered near the upper end of the outer periphery and a shaft near the lower stage of the outer periphery. A pair of upper positioning grooves 12b are provided at symmetrical positions across the center. The pair of upper positioning projections 11b and the pair of upper positioning grooves 12b are both arranged in the same phase in the circumferential direction, and for convenience of explanation, they are arranged at the 12 o'clock and 6 o'clock positions. Call it.

一対の上羽部20bは何れも、略台形状の板材であって、上下方向の長さが上筒部10bの長さの略2倍の長さになっている。そして、上縁(位置ヘと位置トとを結ぶ線に同じ)が上筒部10bの上端と同一面を形成しているから、上羽部20bは上下方向の上縁寄りの略半分の範囲(位置トと位置チとを結ぶ線に同じ)において、上筒部10bの3時および9時の位置に固定されている。
すなわち、一対の上位置決め用突起11b(一対の上位置決め用溝12bに同じ)と一対の上羽部20bとは、交互に、直交する面内配置されている(円周方向で等分に配置されている)。
Each of the pair of upper wing portions 20b is a substantially trapezoidal plate material, and the length in the vertical direction is approximately twice the length of the upper tube portion 10b. Since the upper edge (same as the line connecting the position f and position g) forms the same surface as the upper end of the upper tube portion 10b, the upper wing portion 20b is in a substantially half range near the upper edge in the vertical direction. (It is the same as the line connecting position G and position H) and is fixed at the 3 o'clock and 9 o'clock positions of the upper tube portion 10b.
That is, the pair of upper positioning protrusions 11b (same as the pair of upper positioning grooves 12b) and the pair of upper wing portions 20b are alternately arranged in an orthogonal plane (equally arranged in the circumferential direction). Have been).

また、かかる固定された範囲の下方に、上筒部10b側に突出する上位置決め用突起部21b(位置リと位置ヌとを結ぶ線に同じ)が設けられている。すなわち、上位置決め用突起部21bは側縁(位置トと位置チとを結ぶ線、および位置ルと位置イとを結ぶ線に同じ)に対して、段差(位置チと位置リとを結ぶ線、および位置ヌと位置ルとを結ぶ線に同じ)分だけ、突出している。
さらに、上縁に突出するように上係止用突起部22b(位置ハ、位置ニ、位置ホ、位置ヘにて囲まれた範囲に同じ)が設けられ、上係止用突起部22bには上係止用貫通孔23bが形成されている。
Further, below the fixed range, an upper positioning projection 21b (same as a line connecting the position and the position) protruding to the upper tube portion 10b side is provided. That is, the upper positioning projection 21b has a step (a line connecting the position H and the position R) with respect to the side edge (the same as the line connecting the position G and the position H and the line connecting the position L and the position A). , And the line connecting position n and position le).
Further, an upper locking projection 22b (same as the range surrounded by the position c, position d, position e, and position f) is provided so as to protrude to the upper edge, and the upper locking projection 22b An upper locking through hole 23b is formed.

(組立羽装置)
図2の(c)において、下羽装置1aと上羽装置1bとを組み立て、一体にしている。なお、説明の便宜上、かかる一体化されたものを組立羽装置4と称す。
すなわち、下筒部10aの軸心と上筒部10bの軸心とが一致した状態で、両者を重ねている。このとき、下羽装置1aの下羽部20aは上羽装置1bの上位置決め用突起11bに挾持され、下羽装置1aの下位置決め用突起部21aは上羽装置1bの上位置決め用溝12bに侵入している。同様に、上羽装置1bの上羽部20bは下羽装置1aの下位置決め用突起11aに挾持され、上羽装置1bの上位置決め用突起部21bは下羽装置1aの下位置決め用溝12aに侵入している。
したがって、合計4枚の下羽部20aおよび上羽部20bは堅固に位置決めされた状態で、それぞれ直交する面内に配置されている(円周方向で等分に配置されている)。
なお、本発明において「挾持」とは、下羽部20a両面に上位置決め用突起11bが当接するものに限定する意味ではなく、所定の間隔を設けて両者が対峙し、下羽部20aと上位置決め用突起11bとの相対位置が、所定の距離だけ変動するものを含む意味である(実施の形態3においても同様)。
(Assembly feather device)
In FIG. 2 (c), the lower wing device 1a and the upper wing device 1b are assembled and integrated. For convenience of explanation, the integrated unit is referred to as an assembly blade device 4.
That is, both are overlapped in a state where the axis of the lower cylinder portion 10a coincides with the axis of the upper cylinder portion 10b. At this time, the lower wing portion 20a of the lower wing device 1a is held by the upper positioning protrusion 11b of the upper wing device 1b, and the lower positioning protrusion 21a of the lower wing device 1a is formed in the upper positioning groove 12b of the upper wing device 1b. Invaded. Similarly, the upper wing portion 20b of the upper wing device 1b is held by the lower positioning projection 11a of the lower wing device 1a, and the upper positioning projection 21b of the upper wing device 1b is inserted into the lower positioning groove 12a of the lower wing device 1a. Invaded.
Therefore, a total of four lower wing portions 20a and upper wing portions 20b are arranged in a plane orthogonal to each other while being firmly positioned (equally arranged in the circumferential direction).
In the present invention, “holding” does not mean that the upper positioning protrusions 11b are in contact with both surfaces of the lower wing portion 20a. This means that the relative position with respect to the positioning projection 11b includes a value that varies by a predetermined distance (the same applies to the third embodiment).

(施工方法)
実施の形態2に係るアンカー装置の施工方法、下羽装置1aと上羽装置1bとを組み立て、予め両者を一体化した組立羽装置4を完成した後、組立羽装置4を地山8に打設するものである。すなわち、打設の要領は、実施の形態1(図1)における羽装置1を組立羽装置4に置き換えたものに同じであるから、説明を省略する。つまり、アンカー軸2と組立羽装置4とによってアンカー装置(図示しない)が形成される。
(Construction method)
The anchor device construction method according to the second embodiment, the lower wing device 1a and the upper wing device 1b are assembled, and the assembled wing device 4 in which the two are integrated in advance is completed, and then the assembled wing device 4 is hit on the ground 8 It is to be established. That is, the procedure for placing is the same as that of the first embodiment (FIG. 1) in which the wing device 1 is replaced with the assembly wing device 4, and the description thereof is omitted. That is, an anchor device (not shown) is formed by the anchor shaft 2 and the assembly blade device 4.

したがって、実施の形態2にかかるアンカー装置の施工方法は、実施の形態1と同様の効果(組立羽装置4の姿勢が変動する(傾く)ことがなく、打設不能への対応が容易)を奏すると共に、設置地点において組み立てることができるから、搬送が容易になる。
特に、下羽装置1aは一対の下羽部20aが平面を形成し、同様に上羽装置1bの上羽部20bも平面を形成しているから、トラック等への積み込み時に嵩張ることがなく、搬送効率が向上する。また、法面の高い位置に持ち上げる際、一体化された組立羽装置4の重量の略半分の重量である下羽装置1aと上羽装置1bとを、それぞれ持ち上げれば済むため、持ち上げのための装置を小型にすることができたり、作業者の負担を軽減したりすることができる。
Therefore, the construction method of the anchor device according to the second embodiment has the same effect as the first embodiment (the posture of the assembly blade device 4 does not fluctuate (tilt), and it is easy to cope with the placement failure). Since it can play and it can assemble in an installation point, conveyance becomes easy.
In particular, the lower wing device 1a has a pair of lower wing portions 20a that form a flat surface, and similarly, the upper wing portion 20b of the upper wing device 1b also forms a flat surface. Conveyance efficiency is improved. Moreover, when lifting to a high slope position, the lower wing device 1a and the upper wing device 1b, which are approximately half the weight of the integrated assembly wing device 4, only have to be lifted. The apparatus can be reduced in size, and the burden on the operator can be reduced.

なお、また、図2において、上羽装置1bの上縁および下羽装置1aの上縁とは、図2において位置ヘと位置トとを結ぶ線に同じであって、かかる上縁が、筒部10bおよび筒部10aに軸心に対して垂直になっているが、本発明はこれに限定するものではなく、上縁が傾斜してもよい。
例えば、上羽部20bの上縁が上筒部10bから離れるほど下がるように上筒部10bの軸心に対して傾斜する(ハ字状を呈す)場合には、上羽部20bと上筒部10bとの接続位置(位置ト)を上羽装置1bの上縁とし、反対に、上羽部20bの上縁が上筒部10bから離れるほど上がるように上筒部10bの軸心に対して傾斜する(V字状を呈す)場合には、上筒部10bから最も離れた位置(位置へ、上係止用突起22bを除く)を上羽装置1bの上縁とする。
In FIG. 2, the upper edge of the upper wing device 1b and the upper edge of the lower wing device 1a are the same as the line connecting the position to the position in FIG. Although the part 10b and the cylinder part 10a are perpendicular to the axis, the present invention is not limited to this, and the upper edge may be inclined.
For example, when the upper wing portion 20b is inclined with respect to the axial center of the upper tube portion 10b so as to be lowered as the upper edge of the upper wing portion 20b is separated from the upper tube portion 10b (presents a C shape), the upper wing portion 20b and the upper tube The connection position (position G) with the portion 10b is the upper edge of the upper wing device 1b, and, conversely, with respect to the axis of the upper tube portion 10b so that the upper edge of the upper wing portion 20b moves away from the upper tube portion 10b. When it is inclined (presents a V shape), the position farthest from the upper tube portion 10b (excluding the upper locking projection 22b) is set as the upper edge of the upper wing device 1b.

[実施の形態3:分割タイプ]
図3〜図6は本発明の実施の形態3に係るアンカー装置の施工方法を説明するものであって、図3および図4は工程を追って説明する模式図、図5は施工終了時の様子を模式的に示す斜視図、図6はアンカー装置を構成する天板を示す平面図である。なお、実施の形態1(図1)および実施の形態2(図2)と同じ部分または相当する部分には同じ符号を付し、一部の説明を省略する。
[Embodiment 3: Division type]
FIGS. 3 to 6 illustrate the construction method of the anchor device according to the third embodiment of the present invention. FIGS. 3 and 4 are schematic diagrams illustrating the steps, and FIG. FIG. 6 is a plan view showing a top plate constituting the anchor device. Note that the same or corresponding portions as those in the first embodiment (FIG. 1) and the second embodiment (FIG. 2) are denoted by the same reference numerals, and a part of the description is omitted.

図3の(a)において、下筒部10aと下羽部20aを具備する下羽装置1aを、予め試掘7が実施されアンカー軸2を打設することが可能であることが確認された地山8の表面の地表面9の施工地点に位置決めする。   In FIG. 3 (a), it is confirmed that the lower wing device 1a having the lower cylinder portion 10a and the lower wing portion 20a is preliminarily subjected to the test excavation 7 and can be anchored. Position at the construction point of the ground surface 9 on the surface of the mountain 8.

図3の(b)において、下羽装置1aを図示しない打設手段によって地山8に打設する。このとき、下羽部20aの上縁が地表面9と略同一面になるまで打設する。
なお、打設手段は限定するものではなく、また、下羽装置1aにアダプタ(打設面が形成されている)を載置して、これを介して下羽装置1aを打設してもよい。
In FIG. 3 (b), the lower wing device 1a is driven on the ground 8 by a driving means (not shown). At this time, it is driven until the upper edge of the lower wing portion 20a is substantially flush with the ground surface 9.
The placing means is not limited, and an adapter (having a placement surface) is placed on the lower wing device 1a, and the lower wing device 1a is placed through the adapter. Good.

図3の(c)において、打設しようとする上羽装置1bの上筒部10bの軸心と既に打設されている下羽装置1aの下筒部10aの軸心とを一致させ、上筒部10bの上羽部20b(3時および9時の位置に固定されている)と既に打設されている下羽装置1aの下筒部10aの下羽部20a(12時および6時の位置に固定されている)とが互いに垂直になるように配置して、上羽装置1bを地山8に打設する。
そうすると、下降する上羽装置1bの上羽部20bは、既に打設されている下羽装置1aの下位置決め用突起11aに挾持され、上位置決め用突起部21bは下羽装置1aの下位置決め用溝12aに侵入する。同時に、既に打設されている下羽装置1aの下羽部20aは、下降する上羽装置1bの上位置決め用突起11bに挾持され、下位置決め用突起部21aは上位置決め用溝12bに侵入する。やがて、上羽装置1bの上筒部10bの下端が下羽装置1aの下筒部10aの上端に当接する。
In FIG. 3 (c), the axis of the upper cylinder part 10b of the upper wing device 1b to be placed is aligned with the axis of the lower cylinder part 10a of the lower wing apparatus 1a already placed. The upper wing portion 20b (fixed at the 3 o'clock and 9 o'clock positions) of the tubular portion 10b and the lower wing portion 20a (at 12 o'clock and 6 o'clock) of the lower tubular portion 10a of the lower wing device 1a that has already been placed. The upper wing device 1b is placed on the natural ground 8 so as to be perpendicular to each other.
Then, the upper wing portion 20b of the lower wing device 1b that descends is held by the lower positioning protrusion 11a of the already placed lower wing device 1a, and the upper positioning protrusion 21b is used for lower positioning of the lower wing device 1a. It penetrates into the groove 12a. At the same time, the lower wing portion 20a of the lower wing device 1a that has already been driven is held by the upper positioning protrusion 11b of the lower wing device 1b that descends, and the lower positioning protrusion 21a enters the upper positioning groove 12b. . Eventually, the lower end of the upper tube portion 10b of the upper wing device 1b comes into contact with the upper end of the lower tube portion 10a of the lower wing device 1a.

すなわち、実施の形態3では、下羽装置1aと上羽装置1bとがそれぞれ別々に地山8に打設されることによって、地山8の中で組立羽装置4が完成する。
よって、下羽装置1aおよび上羽装置1bが何れも一対の下羽部20aおよび上羽部20bを具備するだけであるため、合計4枚の羽部を具備する組立羽装置4の打設に比較して、地山8から受ける摩擦抵抗が略半減する。したがって、下羽装置1aおよび上羽装置1bをそれぞれ別個に打設するための容量(荷重)が略半減する。すなわち、打設のための装置が小型になり、特に、傾斜のきつい法面における設置や運搬(上下方向および水平方向)が容易になるため、施工が迅速になる。
また、下羽装置1aまたは上羽装置1bが打設不能にあった場合であっても、打設不能になった一方だけ、あるいは両方を別個に回収(引き抜く)すれば済み、しかも、何れも一対の羽部を具備するだけであるから、地山8の摩擦抵抗が小さく、回収(引き抜き)が容易である。
That is, in the third embodiment, the lower wing device 1 a and the upper wing device 1 b are separately placed on the ground 8 to complete the assembly blade device 4 in the ground 8.
Therefore, since both the lower wing device 1a and the upper wing device 1b only have a pair of lower wing portion 20a and upper wing portion 20b, the assembly wing device 4 having a total of four wing portions can be placed. In comparison, the frictional resistance received from the natural ground 8 is substantially halved. Therefore, the capacity (load) for placing the lower wing device 1a and the upper wing device 1b separately is substantially halved. That is, the apparatus for placing is reduced in size, and in particular, installation and transportation (vertical direction and horizontal direction) on a slope with a steep slope become easy, so that the construction is quick.
Further, even when the lower wing device 1a or the upper wing device 1b cannot be placed, it is sufficient to collect (pull out) only one or both of which cannot be placed, and both of them. Since only a pair of wings is provided, the frictional resistance of the natural ground 8 is small and recovery (pulling) is easy.

図4の(a)において、アンカー軸2を、既に打設されている上羽装置1bの上筒部10bと打設されている下羽装置1aの下筒部10aとに挿入して地山8に打設する。
よって、実施の形態2と同様に、地中で組み立てられた組立羽装置4の姿勢が変動する(傾く)ことがない。
In FIG. 4A, the anchor shaft 2 is inserted into the upper cylinder portion 10b of the upper wing device 1b that has already been driven and the lower cylinder portion 10a of the lower wing device 1a that has been driven. Place in 8.
Therefore, as in the second embodiment, the posture of the assembly blade device 4 assembled in the ground does not change (tilt).

図4の(b)において、アンカー軸2が貫通した状態で、組立羽装置4の上に天板3を載置する。すなわち、下羽装置1aと上羽装置1bとアンカー軸2と天板3とによってアンカー装置300が形成される。
図6の(a)において、天板3は、中心に貫通孔32が形成された円盤30であって、円盤30の外周に到達する係止用溝部31が4箇所に設けられている。貫通孔32はアンカー軸2が貫通自在な内径を具備している。係止用溝部31は互いに直交する放射線上に配置され、下係止用突起部22aおよび上係止用突起部22bが侵入自在な幅と長さを具備している。
In FIG. 4B, the top plate 3 is placed on the assembly blade device 4 with the anchor shaft 2 penetrating. That is, the anchor device 300 is formed by the lower wing device 1 a, the upper wing device 1 b, the anchor shaft 2, and the top plate 3.
6A, the top plate 3 is a disk 30 having a through-hole 32 formed at the center, and is provided with four locking groove portions 31 that reach the outer periphery of the disk 30. In FIG. The through hole 32 has an inner diameter through which the anchor shaft 2 can pass. The locking groove 31 is disposed on the radiation orthogonal to each other, and has a width and a length that allow the lower locking projection 22a and the upper locking projection 22b to enter.

図5の(a)において、下羽装置1aと上羽装置1bとが一体化した組立羽装置4の中心を、アンカー軸2が貫通し、これに天板3が載置されている。このとき、下係止用突起部22aおよび上係止用突起部22bはそれぞれ係止用溝部31に係止して、円盤30の上方に突出している。したがって、下羽装置1aの下羽部20aと上羽装置1bの上羽部20bとは、一層堅固に位置決めされることになる。
なお、下係止用突起部22aおよび上係止用突起部22bにそれぞれ形成された下係止用貫通孔23aおよび上係止用貫通孔23bに、ボルトまたピン(図示しない)を挿入して天板3が離脱しないようにしてもよい。このとき、地表面9が盛り上がろうとした際、天板3はかかる盛り上がりの防止に寄与することになる。
In FIG. 5A, the anchor shaft 2 passes through the center of the assembly blade device 4 in which the lower blade device 1a and the upper blade device 1b are integrated, and the top plate 3 is placed thereon. At this time, the lower locking projection 22 a and the upper locking projection 22 b are locked to the locking groove 31 and protrude above the disk 30. Therefore, the lower wing portion 20a of the lower wing device 1a and the upper wing portion 20b of the upper wing device 1b are positioned more firmly.
A bolt or a pin (not shown) is inserted into the lower locking through hole 23a and the upper locking through hole 23b formed in the lower locking protrusion 22a and the upper locking protrusion 22b, respectively. The top plate 3 may not be detached. At this time, when the ground surface 9 is going to rise, the top plate 3 contributes to prevention of the rise.

図6の(b)において、天板3xは、中心に貫通孔32xが形成された矩形板30xであって、矩形板30xの角に到達する係止用溝部31xが4箇所に設けられている。貫通孔32xはアンカー軸2が貫通自在な内径を具備している。係止用溝部31xは互いに直交する放射線上に配置され、下係止用突起部22aおよび上係止用突起部22bが侵入自在な幅と長さを具備している。
図6の(c)において、天板3yは、中心に貫通孔32yが形成された十字状板30yであって、十字状板30yの先端到達する係止用溝部31yが4箇所に設けられている。貫通孔32yはアンカー軸2が貫通自在な内径を具備している。係止用溝部31yは互いに直交する放射線上に配置され、下係止用突起部22aおよび上係止用突起部22bが侵入自在な幅と長さを具備している。
In FIG. 6B, the top plate 3x is a rectangular plate 30x having a through hole 32x formed at the center, and four locking grooves 31x that reach the corners of the rectangular plate 30x are provided. . The through hole 32x has an inner diameter through which the anchor shaft 2 can pass. The locking groove 31x is disposed on radiation that is orthogonal to each other, and has a width and a length that allow the lower locking projection 22a and the upper locking projection 22b to enter.
In FIG. 6 (c), the top plate 3y is a cross-shaped plate 30y having a through hole 32y formed at the center, and there are four locking grooves 31y that reach the tip of the cross-shaped plate 30y. Yes. The through hole 32y has an inner diameter through which the anchor shaft 2 can pass. The locking groove 31y is disposed on radiation that is orthogonal to each other, and has a width and a length that allow the lower locking projection 22a and the upper locking projection 22b to enter.

なお、本発明において、天板の形態は図示するものに限定するものではなく、前記係止機能を奏する物である限り何れの形態であってもよい。
また、以上は、下羽部20aと上羽部20bとが十字状を呈する場合について説明しているが、本発明はこれに限定するものではないから、下羽部20aまたは上羽部20bの配置形態(枚数や配置角度)が変更された場合には、かかる変更された形態に合わせて天板の形状および係止用溝部の数量は変更されるものである。
In the present invention, the form of the top plate is not limited to that shown in the figure, and any form may be used as long as it has the locking function.
In addition, the above describes the case where the lower wing portion 20a and the upper wing portion 20b have a cross shape. However, the present invention is not limited to this, and the lower wing portion 20a or the upper wing portion 20b When the arrangement form (the number of sheets and the arrangement angle) is changed, the shape of the top plate and the number of the locking grooves are changed according to the changed form.

本発明は以上の構成であるから、横方向の倒れが防止されると共に、正確な打設が可能になり、かつ打設不能時の対応が容易であるから、様々な法面や平面に施工される各種寸法のアンカー装置の施工方法として広く利用することができる。   Since the present invention has the above-described configuration, it can be prevented from falling down in the lateral direction, can be accurately placed, and can be easily handled when placement is impossible. It can be widely used as a construction method for various anchor devices.

本発明の実施の形態1に係るアンカー装置の施工方法を説明する模式図。The schematic diagram explaining the construction method of the anchor apparatus which concerns on Embodiment 1 of this invention. 本発明の実施の形態2に係るアンカー装置の施工方法に用いられる羽装置を説明する斜視図等。The perspective view etc. which explain the wing | blade apparatus used for the construction method of the anchor apparatus which concerns on Embodiment 2 of this invention. 本発明の実施の形態3に係るアンカー装置の施工方法を説明する模式図。The schematic diagram explaining the construction method of the anchor apparatus which concerns on Embodiment 3 of this invention. 本発明の実施の形態3に係るアンカー装置の施工方法を説明する模式図。The schematic diagram explaining the construction method of the anchor apparatus which concerns on Embodiment 3 of this invention. 図4に示す施工終了時の様子を模式的に示す斜視図。The perspective view which shows typically the mode at the time of completion | finish of construction shown in FIG. 図3に示すアンカー装置を構成する天板を示す平面図。The top view which shows the top plate which comprises the anchor apparatus shown in FIG.

符号の説明Explanation of symbols

1 羽装置
1a 下羽装置
1b 上羽装置
2 アンカー軸
3 天板
3x 天板
3y 天板
4 組立羽装置
7 試掘
8 地山
9 地表面
10 筒部
10a 下筒部
10b 上筒部
11a 下位置決め用突起
11b 上位置決め用突起
12a 下位置決め用溝用溝
12b 上位置決め用溝用溝
20 羽部
20a 下羽部
20b 上羽部
21a 下位置決め用突起部
21b 上位置決め用突起部
22a 下係止用突起部
22b 上係止用突起部
23a 下係止用貫通孔
23b 上係止用貫通孔
30 円盤
30x 矩形板
30y 十字状板
31 係止用溝部
31x 係止用溝部
31y 係止用溝部
32 貫通孔
32x 貫通孔
32y 貫通孔
100 アンカー装置(実施の形態1)
300 アンカー装置(実施の形態3)
DESCRIPTION OF SYMBOLS 1 Wing device 1a Lower wing device 1b Upper wing device 2 Anchor shaft 3 Top plate 3x Top plate 3y Top plate 4 Assembly wing device 7 Exploration 8 Ground mountain 9 Ground surface 10 Tube portion 10a Lower tube portion 10b Upper tube portion 11a For lower positioning Protrusion 11b Upper positioning protrusion 12a Lower positioning groove groove 12b Upper positioning groove groove 20 Wings 20a Lower wings 20b Upper wings 21a Lower positioning protrusions 21b Upper positioning protrusions 22a Lower locking protrusions 22b Upper locking projection 23a Lower locking through hole 23b Upper locking through hole 30 Disc 30x Rectangular plate 30y Cross plate 31 Locking groove 31x Locking groove 31y Locking groove 32 Through hole 32x Through Hole 32y Through-hole 100 Anchor device (Embodiment 1)
300 Anchor device (Embodiment 3)

Claims (15)

筒部および該筒部の外周に固定された羽部からなる羽装置と、前記筒部を貫通自在な棒状または管状のアンカー軸と、からなるアンカー装置の施工方法であって、
前記羽装置を地山に打設する工程と、
前記アンカー軸を、前記打設されている羽装置の筒部に挿入して地山に打設する工程と、
を有するアンカー装置の施工方法。
A construction method of an anchor device comprising a wing device composed of a tubular portion and a wing portion fixed to the outer periphery of the tubular portion, and a rod-like or tubular anchor shaft that can penetrate the tubular portion,
Placing the wing device on a natural ground;
Inserting the anchor shaft into the cylindrical portion of the installed wing device and driving it into a natural ground;
An anchor device construction method having
前記羽部が前記筒部の軸心を含む面内に配置され、
前記羽装置の上縁が地山の表面と略同一面になるように打設することを特徴とする請求項1記載のアンカー装置の施工方法。
The wing portion is disposed in a plane including the axis of the cylindrical portion;
2. The anchor device construction method according to claim 1, wherein an upper edge of the wing device is placed so as to be substantially flush with a surface of a natural ground.
下筒部および該下筒部の外周に固定された下羽部からなる下羽装置と、
上筒部および該上筒部の外周に固定された上羽部からなる上羽装置と、
前記下筒部および前記上筒部を貫通自在な棒状または管状のアンカー軸と、からなるアンカー装置の施工方法であって、
前記下筒部の軸心と前記上筒部の軸心とが一致した状態で、前記下羽装置と前記上羽装置とを一体化する工程と、
前記一体化された前記下羽装置および前記上羽装置を地山に打設する工程と、
前記アンカー軸を、前記一体化されて打設されている上羽装置の上筒部と下羽装置の下筒部とに挿入して地山に打設する工程と、
を有するアンカー装置の施工方法。
A lower wing device comprising a lower cylinder part and a lower wing part fixed to the outer periphery of the lower cylinder part;
An upper wing device comprising an upper cylinder portion and an upper wing portion fixed to the outer periphery of the upper cylinder portion;
An anchor device construction method comprising a rod-like or tubular anchor shaft that can pass through the lower cylinder part and the upper cylinder part,
A step of integrating the lower wing device and the upper wing device in a state where the axis of the lower cylinder portion and the axis of the upper cylinder portion coincide with each other;
Placing the integrated lower wing device and the upper wing device on a natural ground;
Inserting the anchor shaft into the upper cylinder part of the upper wing device and the lower cylinder part of the lower wing device that are integrally driven, and driving the ground shaft into a natural ground;
An anchor device construction method having
前記上羽装置の上筒部の長さが前記上羽部の上下方向の長さの略半分であって、前記上筒部が前記上羽部の略上半分の範囲に固定され、
前記下羽装置の下筒部の長さが前記下羽部の上下方向の長さの略半分であって、前記下筒部が前記下羽部の略下半分の範囲に固定される、
前記下羽装置の上縁と前記上羽装置の上縁とが略同一面になるように一体化することを特徴とする請求項3記載のアンカー装置の施工方法。
The length of the upper tube portion of the upper wing device is approximately half of the length of the upper wing portion in the vertical direction, and the upper tube portion is fixed in a range of approximately the upper half of the upper wing portion,
The length of the lower cylinder part of the lower wing device is approximately half of the length of the lower wing part in the vertical direction, and the lower cylinder part is fixed in a range of approximately the lower half of the lower wing part,
4. The anchor device construction method according to claim 3, wherein the upper edge of the lower wing device and the upper edge of the upper wing device are integrated so as to be substantially flush with each other.
前記上羽装置の上筒部の外周に、前記下羽装置の下羽部が侵入自在な上位置決め手段が設けられ、
前記下羽装置の下筒部の外周に、前記上羽装置の上羽部が侵入自在な下位置決め手段が設けられ、
前記上羽部が前記下位置決め手段に、前記下羽根が前記上位置決め手段に、それぞれ侵入した状態で一体化することを特徴とする請求項3または4記載のアンカー装置の施工方法。
On the outer periphery of the upper cylinder portion of the upper wing device, an upper positioning means is provided so that the lower wing portion of the lower wing device can enter,
On the outer periphery of the lower tube portion of the lower wing device, a lower positioning means is provided that allows the upper wing portion of the upper wing device to enter,
5. The anchor device construction method according to claim 3, wherein the upper wing portion is integrated with the lower positioning means and the lower blade is integrated with the upper positioning means in a state of entering.
下筒部および該下筒部の外周に固定された下羽部からなる下羽装置と、
上筒部および該上筒部の外周に固定された上羽部からなる上羽装置と、
前記下筒部および前記上筒部を貫通自在な棒状または管状のアンカー軸と、からなるアンカー装置の施工方法であって、
前記下羽装置を地山に打設する工程と、
前記上羽装置を、前記上筒部の軸心が前記打設されている下羽装置の下筒部の軸心と一致するように打設する工程と、
前記アンカー軸を、前記打設されている上羽装置の上筒部と前記打設されている下羽装置の下筒部とに挿入して地山に打設する工程と、
を有するアンカー装置の施工方法。
A lower wing device comprising a lower cylinder part and a lower wing part fixed to the outer periphery of the lower cylinder part;
An upper wing device comprising an upper cylinder portion and an upper wing portion fixed to the outer periphery of the upper cylinder portion;
An anchor device construction method comprising a rod-like or tubular anchor shaft that can pass through the lower cylinder part and the upper cylinder part,
Placing the lower wing device on a natural ground;
Placing the upper wing device such that the axial center of the upper tubular portion coincides with the axial center of the lower tubular portion of the lower wing device,
Inserting the anchor shaft into the upper cylinder portion of the placed upper wing device and the lower cylinder portion of the placed lower wing device, and placing the anchor shaft on a natural ground;
An anchor device construction method having
前記上羽装置の上筒部の長さが前記上羽部の上下方向の長さの略半分であって、前記上筒部が前記上羽部の略上半分の範囲に固定され、
前記下羽装置の下筒部の長さが前記下羽部の上下方向の長さの略半分であって、前記下筒部が前記下羽部の略下半分の範囲に固定され、
前記下羽装置の上縁が地山の表面と略同一面になるように打設し、前記上羽装置の上縁が地山の表面と略同一面になるように打設することを特徴とする請求項6記載のアンカー装置の施工方法。
The length of the upper tube portion of the upper wing device is approximately half of the length of the upper wing portion in the vertical direction, and the upper tube portion is fixed in a range of approximately the upper half of the upper wing portion,
The length of the lower cylinder part of the lower wing device is approximately half of the length in the vertical direction of the lower wing part, and the lower cylinder part is fixed in a range of substantially lower half of the lower wing part,
The lower wing device is placed so that the upper edge is substantially flush with the surface of the natural ground, and the upper wing device is placed so that the upper edge is substantially flush with the surface of the natural ground. The construction method of the anchor apparatus of Claim 6.
前記上羽装置の上筒部の外周に、前記下羽装置の下羽部が侵入自在な上位置決め手段が設けられ、
前記下羽装置の下筒部の外周に、前記上羽装置の上羽部が侵入自在な下位置決め手段が設けられ、
前記上羽装置を、前記打設されている下羽装置の下位置決め手段に、前記上羽部が侵入するように打設することを特徴とする請求項6または7記載のアンカー装置の施工方法。
On the outer periphery of the upper cylinder portion of the upper wing device, an upper positioning means is provided so that the lower wing portion of the lower wing device can enter,
On the outer periphery of the lower tube portion of the lower wing device, a lower positioning means is provided that allows the upper wing portion of the upper wing device to enter,
The anchor device construction method according to claim 6 or 7, wherein the upper wing device is placed so that the upper wing portion enters the lower positioning means of the placed lower wing device. .
前記上羽装置において、前記上羽部が前記上筒部の軸心を含む面内に配置され、
前記下羽装置において、前記下羽部が前記下筒部の軸心を含む面内に配置されることを特徴とする請求項3乃至8の何れかに記載のアンカー装置の施工方法。
In the upper wing device, the upper wing portion is disposed in a plane including the axis of the upper tube portion,
The anchor device construction method according to any one of claims 3 to 8, wherein, in the lower wing device, the lower wing portion is disposed in a plane including an axis of the lower cylinder portion.
前記上羽装置の上羽部および上位置決め手段が、それぞれ一対であって、前記上羽部が前記上筒部の軸心に対して互いに対称に配置され、前記上位置決め手段が前記上羽部に対して垂直の位置に設けられ、
前記下羽装置の下羽部および下位置決め手段が、それぞれ一対であって、前記下羽部が前記下筒部の軸心に対して互いに対称に配置され、前記下位置決め手段が前記下羽部に対して垂直の位置に設けられ、
前記打設されている下羽装置の一対の下羽部と前記打設されている上羽装置の一対の上羽部とが互いに垂直に位置決めされた状態で、前記アンカー軸を、前記打設されている上羽装置の上筒部と前記打設されている下羽装置の下筒部に挿入して地山に打設する工程と、
を有することを特徴とする請求項3乃至9の何れかに記載のアンカー装置の施工方法。
The upper wing part and the upper positioning means are a pair, and the upper wing part is arranged symmetrically with respect to the axis of the upper cylinder part, and the upper positioning means is the upper wing part. In a position perpendicular to the
The lower wing device includes a pair of lower wing portions and lower positioning means, the lower wing portions are arranged symmetrically with respect to the axis of the lower cylinder portion, and the lower positioning means is the lower wing portion. In a position perpendicular to the
In the state where the pair of lower wing portions of the placed lower wing device and the pair of upper wing portions of the placed upper wing device are positioned perpendicular to each other, the anchor shaft Inserting into the upper cylinder portion of the upper wing device being placed and the lower cylinder portion of the lower wing device being placed, and placing in the natural ground;
The anchor device construction method according to claim 3, wherein the anchor device has a structure.
前記羽装置に係止自在な天板を、前記羽部の上面に載置する工程を有することを特徴とする請求項1または2記載のアンカー装置の施工方法。   3. The anchor device construction method according to claim 1, further comprising a step of placing a top plate that can be locked to the wing device on an upper surface of the wing portion. 前記上羽装置および前記下羽装置に係止自在な天板を、前記上羽部の上面および前記下羽部の上面に載置する工程を有することを特徴とする請求項3乃至10の何れかに記載のアンカー装置の施工方法。   11. The method according to claim 3, further comprising: placing a top plate that can be locked to the upper wing device and the lower wing device on an upper surface of the upper wing portion and an upper surface of the lower wing portion. The construction method of the anchor apparatus as described in a crab. 前記上羽装置の上羽部の上縁に係止用突起部が設けられ、
前記下羽装置の下羽部の上縁に係止用突起部が設けられ、
円周方向で4箇所等分配置され、前記係止用突起部が係止自在な係止用溝部が形成された天板を用意する工程と、
前記打設されている下羽装置の下羽部に設けられた係止用突起部および前記打設されている上羽装置の上羽部に設けられた係止用突起部が、前記係止用溝部に係止するように前記天板を載置する工程と、
を有することを特徴とする請求項3乃至10の何れかに記載のアンカー装置の施工方法。
A locking projection is provided on the upper edge of the upper wing portion of the upper wing device,
A locking projection is provided on the upper edge of the lower wing portion of the lower wing device,
A step of preparing a top plate that is arranged in four equal parts in the circumferential direction and in which a locking groove portion on which the locking projection portion can be freely locked is formed;
The locking projection provided on the lower wing portion of the placed lower wing device and the locking projection provided on the upper wing portion of the placed upper wing device include the locking projection. Placing the top plate so as to be engaged with the groove portion,
The anchor device construction method according to claim 3, wherein the anchor device construction method comprises:
下筒部および該下筒部の外周に固定された下羽部からなる下羽装置と、
上筒部および該上筒部の外周に固定された上羽部からなる上羽装置と、
前記下筒部および前記上筒部を貫通自在な棒状または管状のアンカー軸と、を有するアンカー装置。
A lower wing device comprising a lower cylinder part and a lower wing part fixed to the outer periphery of the lower cylinder part;
An upper wing device comprising an upper cylinder portion and an upper wing portion fixed to the outer periphery of the upper cylinder portion;
An anchor device having a rod-like or tubular anchor shaft that can pass through the lower cylinder part and the upper cylinder part.
前記上羽装置および前記下羽装置に係止自在な天板を有することを特徴とする請求項14記載のアンカー装置。   15. The anchor device according to claim 14, further comprising a top plate that can be locked to the upper wing device and the lower wing device.
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JP2010248841A (en) * 2009-04-17 2010-11-04 Tokyo Seiko Co Ltd Underground anchor
JP2011074738A (en) * 2009-10-02 2011-04-14 Jfe Metal Products & Engineering Inc Anchor and construction method thereof
JP2013023873A (en) * 2011-07-20 2013-02-04 Raiteku:Kk Installation method for anchor device

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JPS5493207A (en) * 1977-12-29 1979-07-24 Nakano Reitoki Seisakusho Compensating gear among compressors of refrigerating circuit provided with plurality of compressors
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Publication number Priority date Publication date Assignee Title
JP2010248841A (en) * 2009-04-17 2010-11-04 Tokyo Seiko Co Ltd Underground anchor
JP2011074738A (en) * 2009-10-02 2011-04-14 Jfe Metal Products & Engineering Inc Anchor and construction method thereof
JP2013023873A (en) * 2011-07-20 2013-02-04 Raiteku:Kk Installation method for anchor device

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