JP6618689B2 - Drilling and stirring device with co-rotation prevention wing - Google Patents

Drilling and stirring device with co-rotation prevention wing Download PDF

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JP6618689B2
JP6618689B2 JP2015042397A JP2015042397A JP6618689B2 JP 6618689 B2 JP6618689 B2 JP 6618689B2 JP 2015042397 A JP2015042397 A JP 2015042397A JP 2015042397 A JP2015042397 A JP 2015042397A JP 6618689 B2 JP6618689 B2 JP 6618689B2
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blade
rotation
rotation prevention
excavation
wing
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JP2016160706A (en
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福田 厚生
厚生 福田
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Tenox Kyusyu Corp
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Description

本発明は、深層混合処理工法などの地盤改良工法に使用され、掘削土が掘削翼や撹拌翼と共に回転する事態を防止する共回り防止翼付き掘削撹拌装置に関するものである。   The present invention relates to an excavation and agitation apparatus with a co-rotation prevention blade that is used in a ground improvement method such as a deep mixing treatment method, and prevents the excavation soil from rotating together with the excavation blade and the agitation blade.

土壌の粘性が高い(例えば、粘土やシルト等)場合、掘削された土砂及び固化材ミルクが掘削翼の回転につれて共回りしようとするが、共回り現象が発生すると、固化材ミルクと土砂の撹拌が不足して不均質なコラムが造成されてしまうため、共回り防止翼が必要となる。   If the soil is highly viscous (for example, clay, silt, etc.), the excavated earth and sand and the solidified milk will try to rotate along with the rotation of the drilling blades. As a result, a non-homogeneous column will be created and a co-rotation prevention wing will be required.

具体的には、特許文献1(特許第1197295号公報)に開示されるように、回転軸の下端部に掘削翼を設けたオーガ式の掘削装置では、掘削翼の回転外径である掘削径よりも、大径の共回り防止翼を、回転軸に遊嵌させるのが望ましい。   Specifically, as disclosed in Patent Document 1 (Japanese Patent No. 1197295), in an auger type drilling device in which a drilling blade is provided at the lower end portion of a rotating shaft, a drilling diameter which is a rotating outer diameter of the drilling blade. It is more desirable to loosely fit the large-diameter co-rotation preventing wing to the rotating shaft.

このようにすると、地中において、駆動手段により回転軸が盛んに回転する一方、共回り防止翼の先端部は周囲の地山に触れているので、共回り防止翼は地中でほとんど回転しない。言い換えると、回転軸と共回り防止翼とにおいて、大きな角速度差が生じることになり、この角速度差により、共回り防止翼を境界として、その上側と下側(掘削翼側)の土壌が縁切りされることになる。   In this way, while the rotating shaft is actively rotated by the driving means in the ground, the tip of the co-rotation preventing wing touches the surrounding ground, so the co-rotation preventing wing hardly rotates in the ground. . In other words, a large angular velocity difference is generated between the rotating shaft and the co-rotation prevention blade, and this angular velocity difference causes the soil on the upper side and the lower side (excavation blade side) to be bordered with the co-rotation prevention blade as a boundary. It will be.

本明細書において、掘削翼の掘削作用が及ぶ領域を「操作体積」と呼ぶと、共回り防止翼は、操作体積の境界部分に位置することになり、共回りしようとする土壌から見ると、共回りを妨げる邪魔板のような働きをする。このような働きにより、操作体積は一定範囲に限定されることとなり、結果として、掘削翼による混練が良好となる。   In this specification, when the area to which the excavation action of the excavation blade extends is referred to as “operation volume”, the co-rotation prevention blade is located at the boundary portion of the operation volume. It works like a baffle that prevents co-rotation. By such a function, the operation volume is limited to a certain range, and as a result, the kneading by the excavating blade is good.

昨今、建物の建て替え時に地盤改良を行う例が増えており、埋め土や盛土等の地盤が改良の対象となることが多い。このような地盤には、土のみでなく、しばしば異物(例えば、コンクリートガラ、アスファルトガラ、岩砕、岩塊、玉石、大礫、木屑等、通常、直径約10センチメートル〜50センチメートル程度のもの)が含まれている。   Recently, there are increasing examples of ground improvement at the time of rebuilding a building, and ground such as buried soil and embankment is often targeted for improvement. In such ground, not only soil, but often foreign matters (for example, concrete galley, asphalt galley, crushed rocks, boulders, cobblestones, gravels, wood chips, etc.) are usually about 10 to 50 centimeters in diameter. Stuff).

地盤に異物が含まれていると、異物が掘削翼と共回り防止翼との間に挟まり、これらの翼が変形あるいは損傷するおそれがある。さらには、異物が掘削翼と共回り防止翼との間に挟まったままとなると、本来上記角速度差を発生させるべきこれらの翼が、異物で接続されることにより、一体的に回転し、共回り防止翼の縁切り作用が果たされなくなってしまう。こうなると、地盤改良体の品質が著しく低下する。もともとは、異物はソイルセメントを上回る強度を有することが多いから、異物が地盤改良体内に残存しても、地盤改良体の品質は損なわれないのであるが、共回り防止翼の縁切り作用が無効にされてはならない。
特許第1197295号公報 特開2010−180647号公報 特開2005−325548号公報 特開2001−40651号公報
If foreign matter is contained in the ground, the foreign matter may be caught between the excavation blade and the co-rotation prevention blade, and these blades may be deformed or damaged. Furthermore, if the foreign object remains sandwiched between the excavating blade and the co-rotation preventing blade, these blades, which should generate the angular velocity difference, rotate together as a result of being connected by the foreign material. The edge-cutting action of the anti-rotation wing will not be fulfilled. If it becomes like this, the quality of the ground improvement body will fall remarkably. Originally, foreign matter often has a strength exceeding that of soil cement, so even if the foreign matter remains in the ground improvement body, the quality of the ground improvement body is not impaired, but the edge cutting action of the co-rotation prevention wing is ineffective. Must not be
Japanese Patent No. 1197295 JP 2010-180647 A JP 2005-325548 A JP 2001-40651 A

そこで本発明は、異物が存在してもその悪影響を抑制できる共回り防止翼付き掘削撹拌装置を提供することを目的とする。   Then, an object of this invention is to provide the excavation stirring apparatus with a co-rotation prevention wing | blade which can suppress the bad influence even if a foreign material exists.

第1の発明に係る共回り防止翼付き掘削撹拌装置は、地中で回転する回転軸と、回転軸の下端部に突設され土砂を掘削する掘削翼と、回転軸において掘削翼よりも所定距離だけ上方に設けられ、回転軸を周回し回転軸に対して遊嵌されるボス部を有する共回り防止翼とを備える共回り防止翼付き掘削撹拌装置であって、共回り防止翼は、ボス部に近接する基端部に比べ、先端部が掘削翼から遠ざかる形状をなすように形成されている。   According to a first aspect of the present invention, there is provided a rotating shaft that rotates in the ground, a rotating shaft that rotates in the ground, a drilling blade that projects from the lower end of the rotating shaft, and excavates earth and sand. An excavation and stirring device with a co-rotation prevention wing provided with a co-rotation prevention wing provided at a distance above and having a boss portion that circulates around the rotation shaft and is loosely fitted to the rotation shaft, Compared to the proximal end portion close to the boss portion, the distal end portion is formed to be away from the excavation blade.

共回り防止翼の形状は、滑らかな曲線で形成されていてもよい。あるいは、共回り防止翼の形状は、階段状に折れ曲がる複数の直線群により形成されていてもよい。   The shape of the co-rotation preventing wing may be formed with a smooth curve. Or the shape of a co-rotation prevention wing | wing may be formed of the several linear group bent in step shape.

この構成において、共回り防止翼は、ボス部に近接する基端部に比べ、先端部が掘削翼から遠ざかる形状をなすように形成されているため、共回り防止翼と掘削翼との近傍に異物が存在していたとしても、共回り防止翼と掘削翼とがなす角が大きく、異物は、共回り防止翼にカラムの外周側へ向けて押し出され、掘削翼と共回り防止翼との間に異物が挟まりにくくなる。   In this configuration, the co-rotation preventing wing is formed so that the tip portion is away from the excavation wing compared to the base end portion close to the boss portion. Even if there is a foreign object, the angle formed by the co-rotation prevention blade and the drilling blade is large, and the foreign object is pushed out by the co-rotation prevention blade toward the outer periphery of the column. Foreign matter is less likely to be caught between them.

よって、共回り防止翼と掘削翼とが一体的に回転する事態が回避され、共回り防止翼による縁切り効果が維持される。その結果、良質な地盤改良体を形成できる。   Therefore, the situation where the co-rotation preventing blade and the excavation blade rotate together is avoided, and the edge cutting effect by the co-rotation preventing blade is maintained. As a result, a good ground improvement body can be formed.

本発明によれば、共回り防止翼をボス部に近接する基端部に比べ、先端部が掘削翼から遠ざかる形状をなすように形成したため、異物がカラムの外周側へ押し出され、異物が掘削翼と共回り防止翼とに挟まらないようにすることができる。その結果、共回り防止翼による縁切り効果を維持して、良質な地盤改良体を形成できる。   According to the present invention, the anti-rotation blade is formed so that the tip portion is away from the excavation blade compared to the base end portion close to the boss portion, so that the foreign matter is pushed out to the outer peripheral side of the column and the foreign matter is excavated. It is possible to prevent the blade from being caught between the wing and the co-rotation prevention wing. As a result, it is possible to maintain the edge cutting effect by the co-rotation preventing wing and to form a good ground improvement body.

(比較例)
本発明の実施の形態を説明するに先立ち、比較例における異物による悪影響について、図9〜図10を参照しながら説明する。ここで、図9は、比較例における掘削撹拌装置の側面図、図10は、図9のA−A線断面図である。
(Comparative example)
Prior to the description of the embodiment of the present invention, adverse effects due to foreign substances in the comparative example will be described with reference to FIGS. Here, FIG. 9 is a side view of the excavation and stirring device in the comparative example, and FIG. 10 is a cross-sectional view taken along line AA in FIG.

図9において、回転軸2は、中心線1を有し、中心線1を中心に矢印N方向又はその逆方向に図示しない駆動手段による回転力を印加され、正転又は逆転する。なお、正転/逆転は、駆動手段により下降又は上昇する動作を考慮して切り替えられる。地中において、土壌の抵抗や振動などにより、中心線1の位置が若干変動することはあるが、以下、中心線1の位置は固定されていることを前提として説明を行う。   In FIG. 9, the rotation shaft 2 has a center line 1, and a rotation force by a driving means (not shown) is applied to the center line 1 in the arrow N direction or in the opposite direction to rotate forward or reverse. Note that the forward / reverse rotation is switched in consideration of the operation of descending or ascending by the driving means. Although the position of the center line 1 may slightly fluctuate due to soil resistance or vibration in the ground, the following description is based on the assumption that the position of the center line 1 is fixed.

中心線1が固定されているので、回転軸2の下端部に設けられる掘削翼3の先端縁は、中心線1を中心とする円軌道(これは、コラム外周9となる。)を描く。より具体的には、掘削翼3の下側には複数の爪3aが設けられており、これらの爪3aが土壌に食い込みながら回転することにより、掘削が進行する。   Since the center line 1 is fixed, the tip edge of the excavation blade 3 provided at the lower end of the rotating shaft 2 describes a circular orbit (this is the column outer periphery 9) centered on the center line 1. More specifically, a plurality of claws 3a are provided on the lower side of the excavation blade 3, and excavation proceeds by rotating the claws 3a while biting into the soil.

共回り防止翼7は、回転軸2において掘削翼3よりも所定距離だけ上方に設けられる。具体的には、共回り防止翼7の中心部(基端部)は、回転軸2を周回し回転軸に対して遊嵌されるボス部7aとなっており、ボス部7aの上下には、回転軸2から外径方向にフランジ上に設けられる上ストッパ5と下ストッパ6とが位置する。   The co-rotation prevention blade 7 is provided above the excavation blade 3 by a predetermined distance on the rotary shaft 2. Specifically, the central portion (base end portion) of the co-rotation preventing wing 7 is a boss portion 7a that circulates around the rotation shaft 2 and is loosely fitted to the rotation shaft. The upper stopper 5 and the lower stopper 6 provided on the flange in the outer diameter direction from the rotary shaft 2 are positioned.

上ストッパ5よりもさらに上方には、掘削翼3に直交する(但し、直交することは必須でなく任意事項である。)撹拌翼4の基端部が固着される。   A base end portion of the stirring blade 4 that is orthogonal to the excavation blade 3 (however, it is not essential and is optional) is further fixed above the upper stopper 5.

上述したように、回転軸2が回転すると、それと一体的に撹拌翼4と掘削翼3が回転するが、共回り防止翼7はほとんど静止し、大きな角速度差が生じる。この角速度差により、上述した縁切り作用が奏される。   As described above, when the rotating shaft 2 rotates, the stirring blade 4 and the excavation blade 3 rotate integrally therewith, but the co-rotation preventing blade 7 is almost stationary and a large angular velocity difference is generated. Due to this angular velocity difference, the edge cutting action described above is achieved.

上述した操作体積は、カラム外周9内の面積に、共回り防止翼7と掘削翼3との間隔t1と掘削翼3の高さとの和を乗じたものである。この面積は、掘削翼3の直径により固定されるものであるから、一定と考えて良い。したがって、操作体積を小さくして混練の効果を高めるためには、間隔t1を小さく設定するしかない。   The operation volume described above is obtained by multiplying the area in the column outer periphery 9 by the sum of the interval t1 between the co-rotation prevention blade 7 and the excavation blade 3 and the height of the excavation blade 3. Since this area is fixed by the diameter of the excavating blade 3, it can be considered to be constant. Therefore, in order to reduce the operation volume and increase the kneading effect, the interval t1 must be set small.

比較例の共回り防止翼7は、平面視において掘削翼3とほぼ同様に直線状に形成されている。ほぼ静止している共回り防止翼7に対して、掘削翼3が回転すると、共回り防止翼7と掘削翼3とは、小さな角をなし、あたかもハサミのように間隔t1にある土壌を切り裂くような動きをする。   The co-rotation prevention wing 7 of the comparative example is formed in a straight line in substantially the same manner as the excavation wing 3 in plan view. When the excavation blade 3 rotates with respect to the substantially stationary anti-rotation blade 7, the anti-rotation blade 7 and the excavation blade 3 form a small corner, and cut through the soil at the interval t1 like scissors. It moves like this.

ここで、間隔t1を上回る高さを有する異物8が共回り防止翼7と掘削翼3との間に近づくと、図10に示すように、これらの翼7、3の間に、異物8が挟まり込んでしまう。   Here, when the foreign object 8 having a height exceeding the interval t1 approaches between the co-rotation prevention blade 7 and the excavation blade 3, the foreign material 8 is interposed between the blades 7 and 3 as shown in FIG. It gets caught.

運良く、異物8が切断されれば良いが、通常では、異物8が掘削翼3と共回り防止翼7とを接続する接続具のような役割を果たしてしまい、その結果、共回り防止翼7が掘削翼3により強制的に回転させられてしまう。こうなると、縁切り作用はほとんど果たされなくなり、地盤改良体の品質が著しく低下することになる。   Fortunately, the foreign object 8 only needs to be cut, but normally, the foreign object 8 plays a role as a connecting tool for connecting the excavation blade 3 and the co-rotation prevention blade 7, and as a result, the co-rotation prevention blade 7. Is forcibly rotated by the excavating blade 3. In this case, the edge cutting action is hardly achieved, and the quality of the ground improvement body is significantly deteriorated.

(実施の形態1)
以下図面を参照しながら、本発明の実施の形態を説明する。図1は本発明の一実施の形態における掘削撹拌装置の側面図、図2は図1のB−B線断面図である。
(Embodiment 1)
Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a side view of an excavating and agitating apparatus according to an embodiment of the present invention, and FIG. 2 is a sectional view taken along line BB in FIG.

図1、図2において、比較例を示す図9、図10と同様の要素については、同一符号を付すことにより、重複する説明を省略する。なお、図1、図2では、共回り防止翼10と掘削翼3あるいは共回り防止翼10と撹拌翼4の各ペアを一段のみ図示しているが、勿論、これらを複数段上下に設ける場合にも、本発明は同様に適用できるものであって、このような場合も本発明の保護範囲に包含される。   In FIG. 1 and FIG. 2, the same elements as those in FIG. 9 and FIG. In FIGS. 1 and 2, each pair of the co-rotation prevention blade 10 and the excavation blade 3 or the co-rotation prevention blade 10 and the stirring blade 4 is shown in a single stage. In addition, the present invention can be similarly applied, and such a case is also included in the protection scope of the present invention.

本発明の特徴は、共回り防止翼10の平面視の形状にある。即ち、図2に示すように、共回り防止翼10は、ボス部10aに近接する基端部に比べ、先端部が掘削翼3から遠ざかる形状をなすように形成されている。このため、平面視で共回り防止翼10と掘削翼3とが近づいた状態においても、共回り防止翼10と掘削翼3との接点付近がなす角が大きい(この点は、図10と図2とを比較して参照されたい。)。   A feature of the present invention resides in the shape of the co-rotation preventing wing 10 in plan view. That is, as shown in FIG. 2, the co-rotation preventing wing 10 is formed so that the tip portion is away from the excavation wing 3 compared to the base end portion close to the boss portion 10 a. For this reason, even when the co-rotation preventing blade 10 and the excavation blade 3 are close to each other in plan view, the angle formed by the vicinity of the contact point between the co-rotation prevention blade 10 and the excavation blade 3 is large (this point is illustrated in FIGS. See 2 for comparison).

このような関係があることにより、異物8は、共回り防止翼10と掘削翼3との間に挟まらず掘削翼3の上又は下をすり抜けるような動きをなし、図2矢印で示すように、カラムの外周側へ押し出されることになる。このため、本発明によれば、比較例の間隔t1よりもさらに小さな間隔t2を採用することができ、その結果、操作体積をより小さく設定して高品質な地盤改良体を構築できると共に、異物8が掘削翼3と共回り防止翼10との間に挟まらないようにすることができる。このように、間隔を縮めると地盤改良体の品質を向上できる一方、異物の挟み込みの危険が増加するという、トレードオフの関係にある問題を一気に解決できるものである。   Due to this relationship, the foreign object 8 moves so as not to be sandwiched between the co-rotation prevention blade 10 and the excavation blade 3 and to pass through the upper or lower excavation blade 3, as indicated by arrows in FIG. Then, it is pushed out to the outer peripheral side of the column. For this reason, according to the present invention, it is possible to employ an interval t2 that is smaller than the interval t1 of the comparative example. As a result, it is possible to construct a high-quality ground improvement body by setting the operation volume smaller, 8 can be prevented from being sandwiched between the excavation blade 3 and the co-rotation prevention blade 10. As described above, when the interval is shortened, the quality of the ground improvement body can be improved, while the problem of a trade-off relationship that the risk of foreign matter being caught increases can be solved at a time.

共回り防止翼10は、図2では2枚を一対としているが、一枚あるいは三枚以上とすることもできる。   In FIG. 2, two of the co-rotation preventing blades 10 are paired, but may be one or three or more.

さらに、図3〜図8に例示するように、共回り防止翼10を平面視した形状は、種々変更できる。例えば、図3に示すように、基端部がボス部10aと接するようにスタートし、ある曲率で滑らかに湾曲する曲線状としてもよい。   Furthermore, as illustrated in FIGS. 3 to 8, the shape of the co-rotation preventing wing 10 in plan view can be variously changed. For example, as shown in FIG. 3, the base end portion may start so as to be in contact with the boss portion 10 a and may have a curved shape that curves smoothly with a certain curvature.

あるいは、図4に示すように、図3よりも曲率を大きくして、先端部が内側を向くようにしても良い。   Alternatively, as shown in FIG. 4, the curvature may be larger than that in FIG. 3 so that the tip portion faces inward.

あるいは、図5に示すように、階段状に折れ曲がる複数の直線群で構成しても良い。   Or as shown in FIG. 5, you may comprise by the some straight line group bent in step shape.

あるいは、図6に示すように、基端部を回転軸2に直交させ先端部を掘削翼3から遠ざかるように曲げても良い。   Alternatively, as shown in FIG. 6, the base end portion may be bent so as to be orthogonal to the rotating shaft 2 and the tip end portion away from the excavation blade 3.

あるいは、図7に示すように、基端部側をやや図7の上側にふくらませても良い。   Alternatively, as shown in FIG. 7, the base end side may be slightly inflated to the upper side of FIG.

さらには、図8に示すように、基端部をボス部10aに直交させ、それから図8右向きに折り曲げ、さらに曲線部を連続させて先端部へ至るように形成しても良い。   Furthermore, as shown in FIG. 8, the base end portion may be orthogonal to the boss portion 10a, then bent to the right in FIG. 8, and the curved portion may be continued to reach the distal end portion.

図3〜図8の各種形状には、それぞれ一長一短があるが、いずれの形状を採用しても、一定の効果があるから、これらの形状は、当然全て本発明に包含されるし、本発明の趣旨を変更しない限り、図示されていない形状をも本発明の保護範囲に属する。   Each of the various shapes in FIGS. 3 to 8 has advantages and disadvantages. However, any shape can be used to achieve certain effects. Therefore, these shapes are naturally included in the present invention. Unless the meaning of the above is changed, shapes not shown in the drawings also belong to the protection scope of the present invention.

本発明に係る共回り防止翼付き掘削撹拌装置は、例えば、地盤改良等を行う分野において好適に利用できる。   The excavation and stirring device with a co-rotation preventing blade according to the present invention can be suitably used in, for example, the field of ground improvement.

本発明の一実施の形態における掘削撹拌装置の側面図The side view of the excavation stirring apparatus in one embodiment of this invention 図1のB−B線断面図BB sectional view of FIG. 本発明の第1例における共回り防止翼の形状を示す断面図Sectional drawing which shows the shape of the co-rotation prevention blade in the 1st example of this invention 本発明の第2例における共回り防止翼の形状を示す断面図Sectional drawing which shows the shape of the co-rotation prevention blade in the 2nd example of this invention 本発明の第3例における共回り防止翼の形状を示す断面図Sectional drawing which shows the shape of the co-rotation prevention wing | blade in the 3rd example of this invention 本発明の第4例における共回り防止翼の形状を示す断面図Sectional drawing which shows the shape of the co-rotation prevention blade in the 4th example of this invention 本発明の第5例における共回り防止翼の形状を示す断面図Sectional drawing which shows the shape of the co-rotation prevention wing | blade in the 5th example of this invention 本発明の第6例における共回り防止翼の形状を示す断面図Sectional drawing which shows the shape of the co-rotation prevention blade in the 6th example of this invention 比較例における掘削撹拌装置の側面図Side view of excavating and stirring device in comparative example 図9のA−A線断面図AA line sectional view of FIG.

1 中心線
2 回転軸
3 掘削翼
3a 爪
4 撹拌翼
5 上ストッパ
6 下ストッパ
7、10 共回り防止翼
7a、10a ボス部
8 異物
9 コラム外周
t1、t2 間隔
DESCRIPTION OF SYMBOLS 1 Centerline 2 Rotating shaft 3 Excavation blade 3a Claw 4 Agitation blade 5 Upper stopper 6 Lower stopper 7, 10 Co-rotation prevention blade 7a, 10a Boss part 8 Foreign material 9 Column outer periphery t1, t2 space | interval

Claims (3)

地中で回転する回転軸と、
前記回転軸の下端部に突設され土砂を掘削する掘削翼と、
前記回転軸において前記掘削翼よりも所定距離だけ上方に設けられ、前記回転軸を周回し前記回転軸に対して遊嵌されるボス部を有する共回り防止翼とを備える共回り防止翼付き掘削撹拌装置であって、
前記共回り防止翼は、平面視において前記ボス部に近接する基端部に比べ、先端部が前記掘削翼から遠ざかる形状をなすように形成することにより、前記共回り防止翼と前記掘削翼とがいずれも直線状である場合よりも前記共回り防止翼と前記掘削翼とがなす角を拡大し、前記共回り防止翼が異物をカラムの外周側へ押し出すように構成したことを特徴とする共回り防止翼付き掘削撹拌装置。
A rotating shaft that rotates in the ground,
A drilling wing projecting at the lower end of the rotary shaft and excavating earth and sand;
Excavation with a co-rotation prevention wing provided with a co-rotation prevention wing provided at a predetermined distance above the excavation wing on the rotation shaft and having a boss portion that circulates around the rotation shaft and is loosely fitted to the rotation shaft A stirring device,
The co-rotation preventing wing than the base end portion close to the boss portion in a plan view, by the leading end portion is formed so as to form the shape away from the drilling blade, and the drilling blade and the co-rotation prevention wings The angle between the co-rotation prevention blade and the excavation blade is expanded as compared with the case where both are linear , and the co-rotation prevention blade is configured to push out foreign matter to the outer peripheral side of the column. Drilling and stirring device with co-rotation prevention blade.
前記形状は、滑らかな曲線で形成されている請求項1記載の共回り防止翼付き掘削撹拌装置。 The excavation and stirring apparatus with a co-rotation prevention wing according to claim 1, wherein the shape is formed by a smooth curve. 前記形状は、階段状に折れ曲がる複数の直線群により形成されている請求項1記載の共回り防止翼付き掘削撹拌装置。 The excavation and agitation device with anti-rotation blades according to claim 1, wherein the shape is formed by a plurality of straight line groups that are bent in a step shape.
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JPS5432010U (en) * 1977-08-05 1979-03-02
US5411353A (en) * 1993-09-01 1995-05-02 Taki; Osamu Soil solidification apparatus with a shear blade of adjustable length and rotation speed for creating a ribbed soil-cement pile
JP2010180647A (en) * 2009-02-06 2010-08-19 Machine Service:Kk Agitating head of excavating and agitating machine
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