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JP6427477B2 - Expanded hole drilling head - Google Patents
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JP6427477B2 - Expanded hole drilling head - Google Patents

Expanded hole drilling head Download PDF

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JP6427477B2
JP6427477B2 JP2015186775A JP2015186775A JP6427477B2 JP 6427477 B2 JP6427477 B2 JP 6427477B2 JP 2015186775 A JP2015186775 A JP 2015186775A JP 2015186775 A JP2015186775 A JP 2015186775A JP 6427477 B2 JP6427477 B2 JP 6427477B2
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expansion
blade
shaft
wing
enlarged
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JP2017061787A (en
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佐藤 啓
啓 佐藤
喜代満 畠山
喜代満 畠山
辰弥 駒澤
辰弥 駒澤
和男 駒澤
和男 駒澤
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NIHON BASE CO.,LTD.
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NIHON BASE CO.,LTD.
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Description

本発明は拡大孔掘削用ヘッドに係り、特に土木工事において球根部を有する基礎鋼管杭又はコンクリート杭を構築する場合に使用する拡大孔掘削用ヘッドに関する。   The present invention relates to an enlarged hole drilling head, and more particularly to an enlarged hole drilling head used when constructing a foundation steel pipe pile or a concrete pile having a bulb portion in civil engineering work.

基礎鋼管杭又はコンクリート杭を構築するためには、アースドリルやスクリューオーガ等で地中孔を掘削し、基礎鋼管杭又はコンクリート杭を建込む。この際、基礎鋼管杭等の支持力を高めるために、地中孔の底部を所要深さ位置で拡径掘削し、地中孔の下端部を球根状に拡幅することが行われる。   In order to construct a foundation steel pipe pile or a concrete pile, the underground hole is excavated with an earth drill, a screw auger or the like, and a foundation steel pipe pile or a concrete pile is constructed. At this time, in order to increase the supporting force of the foundation steel pipe pile or the like, the bottom of the underground hole is excavated at a required depth position to widen the lower end of the underground hole in a bulbous shape.

このように、地中孔の下端部に球根状の拡幅部を形成する手段としては、例えば特開平11ー350473号公報に開示されているような拡大掘削刃を備えた掘削ヘッドや、実開平1−75194号公報に開示されている拡大掘削装置などがある。 Thus, as means for forming a bulb-like widening portion at the lower end portion of the underground hole, for example, a digging head provided with an expanding digging blade as disclosed in JP-A-11-350473, and the like expanding large drilling apparatus disclosed in 1-75194 JP.

前記特開平11ー350473号公報に開示されている発明は、鋼管杭の先端が支持層に達した時点で、鋼管杭の内部に挿入したオーガースクリューを逆転させ、該オーガースクリューの下端部に縮径状態で挿入した拡大ビットを拡径させると同時に上下動させることにより、前記鋼管杭の先端が位置する部分を拡削する方法である。   According to the invention disclosed in the above-mentioned JP-A-11-350473, when the tip of the steel pipe pile reaches the support layer, the auger screw inserted into the inside of the steel pipe pile is reversed to be contracted at the lower end of the auger screw This is a method of expanding the portion where the tip of the steel pipe pile is located by expanding and simultaneously moving the expanding bit inserted in the diameter state.

また、前記実開平1−75194号公報の拡大掘削装置は、掘削羽根を地山に食い込ませて回転を拘束したうえで掘削ロッドを逆転し、押圧ノックの先端を拡大刃の後端部に向かって突き出してこれを押圧することにより拡大刃を外方に強制的に回転させ、広がった拡大刃により拡大掘削するようにしている。   Further, in the magnifying and excavating apparatus disclosed in Japanese Utility Model Application Laid-Open No. 1-75194, the excavating blade is inserted into the ground to restrain the rotation and then the excavating rod is reversed to move the tip of the pressure knock toward the rear end of the expanding blade. The expansion blade is forced to rotate outward by pushing out and pushing this out, and it is made to carry out expansion excavation by the spread expansion blade.

これらの掘削ヘッドや拡大掘削装置では、拡大孔を掘削するには、正回転(時計回り方向)から逆回転(反時計回り方向)に操作を変更しなければならない。その場合、オーガヘッドの先端や掘削羽根は逆向きで回転するため、地中孔の底部を掘削する能力は著しく低下し、作業能率も著しく低下する。また、拡大掘削装置においては掘削ロッドの正回転時において、拡大刃をロックする手段がないため、正回転時に拡大刃と押圧ノックとの間に岩石等が進入して拡大刃を回転させて、不用意に拡大孔を掘削することとなる惧れもある。   In these drilling heads and expansion drilling devices, in order to drill an enlarged hole, the operation must be changed from positive rotation (clockwise direction) to reverse rotation (counterclockwise direction). In that case, since the tip of the auger head and the cutting blade rotate in the opposite direction, the ability to dig the bottom of the underground hole is significantly reduced, and the working efficiency is also significantly reduced. In addition, in the case of the expansion drilling apparatus, there is no means for locking the expansion blade at the time of forward rotation of the drilling rod, so rock etc. enter between the expansion blade and the press knock at the time of forward rotation to rotate the expansion blade, There is also the possibility that the expanded hole will be dug carelessly.

そこで、発明者らは、特許第2711236号公報および特許第4945603号公報に記載の発明のように、拡大孔を掘削するときも正回転で行え、拡大孔を所望の深さに形成できるとともに、正回転時に拡大刃が不用意に拡開するのを防止した拡大孔掘削用ヘッドが提案されている。すなわち、特許2711236号公報に記載の拡大孔掘削用ヘッドは、拡大孔を掘削するとき、掘削用刃を孔底部に食い込ませて外筒体を固定した後駆動軸を逆回転させると、シャフトがキー部とキー溝が遊嵌する範囲内で逆回転して蹴飛ばしピンが拡大刃から外れ、拡大刃を半径方向外方へ押すことにより拡開させる。   Therefore, as in the inventions described in Japanese Patent No. 2711236 and Japanese Patent No. 4945603, the inventors can perform positive rotation even when digging the expanded hole, and can form the expanded hole to a desired depth, An expanded hole drilling head has been proposed which prevents the expanded blade from being expanded inadvertently during forward rotation. That is, in the case of the enlarged hole excavating head disclosed in Japanese Patent No. 2711236, when the enlarged hole is excavated, the excavating blade bites into the hole bottom to fix the outer cylindrical body, and then the drive shaft is reversely rotated. In the range in which the key portion and the key groove are loosely fitted, the kicking pin is released from the expanding blade by reverse rotation, and the expanding blade is expanded by pushing it radially outward.

そして、駆動軸を正回転させると、拡大刃は土の抵抗を受けて完全に拡開し、掘削用刃とともに土を掘削する。そして、所定深さの掘削孔を穿削した後は、駆動軸を逆回転させながら上方へ引き上げると、拡大刃は土の抵抗を受けて回動しながら折り畳まれ、蹴飛ばしピンが拡大刃に係合して当初の状態に復帰する。   Then, when the drive shaft is rotated forward, the expansion blade receives the resistance of the soil and is completely expanded, and excavates the soil with the digging blade. Then, after drilling a wellbore having a predetermined depth, if the drive shaft is pulled up while being reversely rotated, the expanding blade is folded while rotating due to the resistance of the soil, and the kicking pin engages with the expanding blade Return to the original state.

また特許第4945603号公報に記載の拡大孔掘削用ヘッドでは、拡大孔を掘削する際に、拡大翼操作部材により掘削用刃の半径内に折り畳状態に保持されている拡大翼の径縮保持の解除と、拡大翼を外方向へ蹴り出して拡径させる動作をほぼ同時に行うことで、拡大翼の径縮,拡径の動作を確実に行え、また上部シャフトの逆回転時に、拡大翼操作部材の蹴り出し部が、拡大翼の先端部が前記掘削用刃の半径から突出する位置まで強制的に拡大翼を外方向へ押し広げることで、粘性土地盤の場合でも掘削用刃の半径の外に位置するまで確実に拡径できる。   In the case of the enlarged hole excavating head disclosed in Japanese Patent No. 4945603, when the enlarged hole is excavated, the diameter reduction holding of the expanded vane held in the folded state within the radius of the digging blade by the enlarged wing operating member By releasing the expansion blade and pushing the expansion blade outward almost simultaneously, the expansion and contraction of the expansion blade can be reliably performed. At the same time, when the upper shaft is reversely rotated, the expansion blade is operated. The kicker of the member forcibly pushes the expanding wing outward to a position where the tip of the expanding wing projects from the radius of the digging blade, thereby making the radius of the digging blade even in the case of a viscous ground. The diameter can be reliably expanded to the outside.

さらに拡大翼が所定角度まで押し拡げられた際、拡大翼の軸部近傍の内側面がストッパーと当接するため、前記拡大翼が所定角度まで押し拡げられて拡径した状態が保持され、所望径の拡大孔を確実に掘削することができるものとしている。   Furthermore, when the expansion wing is pushed and expanded to a predetermined angle, the inner surface in the vicinity of the shaft portion of the expansion wing abuts against the stopper, so the expansion wing is pushed and expanded to a predetermined angle and the diameter expanded state is maintained. It is assumed that the expanded hole of the can be duly drilled.

特開平11ー350473号公報Japanese Patent Application Laid-Open No. 11-350473 実開平1−75194号公報Japanese Utility Model Publication No. 1-75194 特許第2711236号公報Patent No. 2711236 gazette 特許第4945603号公報Patent No. 4945603

しかし、上記発明では、粘性土地盤にでも対応する構造としているため、拡大孔掘削用ヘッドの構造が複雑になる一方、掘削径の大きな大径杭の施工では耐久性が低下して、頻繁に掘削用ヘッドを補修する必要が生じるなど使用上の制限があった。また掘削抵抗(N値)の大きなN値の高い礫質地盤では掘削自体が困難になる等の不都合も生じていた。   However, in the above invention, the construction is made to cope with the viscous land, so the structure of the expanded hole drilling head becomes complicated, but in the construction of a large diameter pile with a large diameter, the durability decreases and it is frequently There were limitations in use such as the need to repair the drilling head. In addition, in the case of a high quality N soil soil having a large drilling resistance (N value), problems such as difficulty in drilling itself have occurred.

本発明は、上記のような従来技術の欠点を克服するために、拡大翼の拡径・縮径の操作を簡素な構造で実現することができるとゝもに、耐久性の向上を図り、掘削抵抗の大きな地盤であっても確実に拡大孔を形成できる拡大孔掘削用ヘッドを提供することを目的としたものである。   In order to overcome the drawbacks of the prior art as described above, the present invention improves the durability as well, since the operation of diameter expansion and diameter reduction of the expansion wing can be realized with a simple structure, It is an object of the present invention to provide an enlarged hole excavating head capable of reliably forming an enlarged hole even in a ground having a large excavation resistance.

上記の目的を達成するため、本願の第1の発明は、上端部に駆動軸と連結する連結部を備えた上部シャフトの下端部に、所定角度正逆回転可能となるように下部シャフトを接続するとゝもに、前記下部シャフトには、直径方向で相対向する少なくとも二つの位置においてそれぞれ拡大翼を所定角度内で回動可能に軸支する上部ブラケット及び下部ブラケットからなる拡大翼支持部材を、前記上部シャフトには、その正回転時に、一端が前記拡大翼のアーム部の後端と当接して、前記拡大翼を前記下部シャフトに装着した掘削用刃の半径内に折り畳み状態に保持するトルク伝達部として、又逆回転時に、他端が前記拡大翼の先端部と衝当して、前記拡大翼の前記先端部が前記掘削用刃の半径から突出する位置まで前記拡大翼を強制的に外方向へ拡径する蹴り出し部としてそれぞれ機能する拡大翼操作部材を装着した拡大孔掘削用ヘッドであって、前記上部シャフトの正回転時に前記拡大翼の前記アーム部の内側面が当接して前記拡大翼が拡径することを防止するストッパーとして、又前記上部シャフトの逆回転時には前記拡大翼の前記アーム部の前記内側面が当接してせん断破断され、前記拡大翼の拡径を検知する検知部としてそれぞれ機能する拡大翼検知手段を、前記拡大翼支持部材の前記上部ブラケット及び前記下部ブラケット間に備え、前記拡大翼の前記アーム部の外側面と当接して前記拡大翼が拡径及び縮径する動きを制限するストッパー部材を前記拡大翼支持部材に備えたことを特徴とする拡大孔掘削用ヘッドである。 In order to achieve the above object, according to a first aspect of the present invention, a lower shaft is connected to a lower end portion of an upper shaft provided with a connecting portion connected with a drive shaft at an upper end portion so as to be rotatable forward and reverse by a predetermined angle. Then, the lower shaft is an enlarged wing support member composed of an upper bracket and a lower bracket pivotally supporting the expansion wings at a predetermined angle at at least two diametrically opposed positions, One end of the upper shaft abuts on the rear end surface of the arm portion of the expanding blade during normal rotation, and the expanding blade is held in a folded state within the radius of the digging blade attached to the lower shaft as the torque transmission unit, also during the reverse rotation, the other end to the distal end portion and the strike of the expansion blades, forcing the expansion wings to a position where the tip of the expanded wings protrudes from the radius of the excavating blade Outward direction An enlarged hole drilling head equipped with expansion blades operating members respectively function as a kick-out portion for diameter expansion, the expansion wings inner surface of the arm portion of the expansion blades during forward rotation of the upper shaft abuts As a stopper that prevents the diameter of the expansion shaft from expanding, and when the upper shaft rotates in reverse, the inner surface of the arm portion of the expansion blade abuts and is sheared , and a detection unit that detects the expansion diameter of the expansion blade the expansion wings detection means which function respectively, provided between the upper bracket and the lower bracket of the expansion wing support member, the expansion wings are expanded and contracted in contact with the larger blade outer surface of the arm portion of the person The enlarged blade support member is provided with a stopper member for restricting the movement .

また、本願の請求項2に記載の発明は、前記拡大翼検知手段が、前記拡大翼支持部材の前記上部ブラケット及び前記下部ブラケットに上下両端部をそれぞれ固定したボルトであって、前記拡大翼の軸部近傍の厚さより大きい間隔をおいて、せん断誘導溝を上下2ヶ所に備えたことを特徴とする。 The invention of claim 2 of the present application, the expanded wings detecting means, a said upper bracket and a bolt which upper and lower end portions were respectively fixed to the lower bracket of the expansion wing support member, for the expansion wings at a yet larger than the thickness of intervals of the shaft portion near to comprising the shear guide grooves in upper and lower two places.

さらに、本願の請求項に記載の発明は、前記下部シャフトに装着した前記掘削用刃に、ほぼ杭外径まで拡径する補助拡大翼と位置決め部材を設けたことを特徴とする。 The present invention as described in claim 3 of the present application, the excavating blade mounted on the lower shaft, characterized in that a substantially and the auxiliary expansion vanes whose diameter increases until Kuigai diameter positioning member.

本発明では、前記拡大翼支持部材の上部ブラケット及び下部ブラケットに、拡大翼のアーム部の内側面が上部シャフトの正回転時に当接して前記拡大翼が拡径することを防止するストッパーとして、又前記上部シャフトの逆回転時には前記拡大翼のアーム部の内側面が衝当してせん断破断され、前記拡大翼の拡径を検知する検知部としてそれぞれ機能する検知手段からなる拡大翼操作部材を備えた構造とすることで構造を簡素化することができ、この結果構成部材厚を大きくして耐久性を高めることができる。 In the present invention, the upper bracket and the lower bracket of the expansion wing support member are used as a stopper for preventing the expansion wing from expanding due to the inner surface of the arm portion of the expansion wing coming into contact when the upper shaft rotates forward. When the upper shaft is reversely rotated, the inner surface of the arm portion of the expansion blade collides and is sheared, and an expansion wing operation member comprising detection means functioning as a detection unit for detecting the expansion diameter of the expansion wing is provided. With this structure, the structure can be simplified, and as a result, the thickness of the component members can be increased to enhance the durability.

また、拡大翼のアーム部の外側面と当接して拡大翼が拡径する動きを制限するストッパー部材を拡大翼支持部材に備えた構造とすることで、拡大翼の回転半径を一定に保つことができ、地中孔の下部において所望の径の大きさの掘削孔を確実に掘削することができる。In addition, the expansion wing supporting member has a structure in which the expansion wing supporting member is provided with a stopper member that abuts on the outer surface of the arm portion of the expansion wing to limit the expansion movement of the expansion wing, thereby keeping the rotation radius of the expansion wing constant. It is possible to reliably drill a drill hole of the desired diameter size at the bottom of the underground hole.

また、拡大翼支持部材に備えたストッパー部材は、拡大翼のアーム部の外側面と当接して拡大翼が縮径する動きを制限するため、拡大翼が下部シャフト側に入り込みすぎないようにすることができる。  In addition, the stopper member provided on the expansion wing support member is in contact with the outer surface of the arm portion of the expansion wing to restrict the diameter reduction of the expansion wing, so that the expansion wing does not enter the lower shaft side too much be able to.

また、本発明では、前記拡大翼検知手段を観察することで拡大翼が確実に拡径し、拡径した状態で所定径の拡大孔が穿削されたことを確認することができる。   Further, in the present invention, by observing the expanded blade detection means, it is possible to confirm that the expanded blade is expanded in diameter surely and the expanded hole having a predetermined diameter is drilled in the expanded state.

また、本発明では、前記拡大翼検知手段が、前記拡大翼支持部材の上部ブラケット及び下部ブラケットに上下両端部をそれぞれ固定したボルトであって、前記拡大翼の軸部近傍の厚さより大きい間隔をおいて、せん断誘導溝を上下2ヶ所に備えた構成とすることで、前記ボルトが圧力を受けた場合に前記せん断誘導溝の位置で確実にせん断され、拡大翼の拡径が阻害されることがなく、拡大翼を拡径させたいときに確実に拡径させることができる。 In the present invention, the expansion wings detecting means, a bolt which is fixed to the upper bracket and the lower bracket upper and lower end portions of the expanding blade support member, not greater than the shank thickness of the vicinity of the larger wing spacing By providing the shear guiding grooves at two places in the upper and lower sides, when the bolt is subjected to pressure, it is surely sheared at the position of the shear guiding groove and the diameter expansion of the expansion wing is inhibited. Therefore, when it is desired to expand the diameter of the expansion blade, the diameter can be reliably expanded.

また、本発明によれば、下部シャフトに装着した掘削用刃に、ほぼ杭外径まで拡径する補助拡大翼と位置決め部材を設けたことから、掘削抵抗が大きなN値の高い礫質地盤でも拡大孔の掘削が容易となる。 Further, according to the present invention, the excavating blade mounted on the lower shaft, substantially an auxiliary expansion vanes whose diameter increases to Kuigai diameter from the provision of the positioning member, a high drilling resistance of large N value gravelly soil But drilling of the expanded hole becomes easy.

本発明に係る拡大孔掘削用ヘッドの正面図である。It is a front view of the head for the extended hole excavation concerning the present invention. 同拡大孔掘削用ヘッドの右側面図である。It is a right view of the head for the same expansion hole excavation. 同拡大孔掘削用ヘッドの補助拡大翼が拡径した状態の正面図である。It is a front view in the state where the auxiliary expansion wing of the head for the same expansion hole excavation was diameter-expanded. 図1のC−C線断面図である。It is the CC sectional view taken on the line of FIG. 図1のB−B線断面図である。It is the BB sectional drawing of FIG. 拡大翼の拡径操作開始時の図1のC−C線断面図である。It is CC sectional view taken on the line of FIG. 1 at the time of the diameter expansion operation start of an expansion wing | blade. 同拡大翼の拡径操作開始時の図1のB−B線断面図である。It is the BB sectional drawing of FIG. 1 at the time of the diameter expansion operation start of the same expansion wing | blade. 同拡大翼の拡径操作第1段階時の図1のC−C線断面図である。It is CC sectional view taken on the line of FIG. 1 at the time of diameter expansion operation 1st step of the expansion blade. 同拡大翼の拡径操作第1段階時の図1のB−B線断面図である。It is the BB sectional drawing of FIG. 1 at the time of diameter expansion operation 1st step of the expansion blade. 同拡大翼の拡径操作第2段階時の図1のC−C線断面図である。It is CC sectional view taken on the line of FIG. 1 at the time of expansion operation 2nd step of the expansion blade. 同拡大翼が最大まで拡径した状態のC−C線断面図である。FIG. 7 is a cross-sectional view taken along the line C-C in a state where the diameter of the expansion blade is expanded to the maximum. 補助拡大翼が最大まで拡径した状態の底面図である。It is a bottom view in the state where diameter of an auxiliary expansion wing was expanded to the maximum. 図2のD部分の拡大図である。It is an enlarged view of D part of FIG. 図2のD部分のシャーピンせん断後の拡大図である。It is the enlarged view after shear pin shear of D part of FIG. 拡大孔掘削時の縦断面説明図である。It is longitudinal cross-section explanatory drawing at the time of an expanded hole excavation.

以下、本発明を図1乃至図15に示す実施例により詳細に説明する。図において、1は本発明に係る拡大孔掘削用ヘッドで、2は上端部に駆動軸101との連結部3を有する上部シャフトである。4,4は前記上部シャフト2の軸孔5の内周面に形成したキー溝で、軸方向Aに延びている前記キー溝4,4は、前記上部シャフト2の直径方向で相対向する位置にそれぞれ形成されている。なお、図中6は前記上部シャフト2の下部外周面に設けたらせん状の掘削刃である。 It will be described in detail below by examples showing the present invention in FIG. 1 to FIG. In the figure, reference numeral 1 is a head for drilling an enlarged hole according to the present invention, and 2 is an upper shaft having a connecting portion 3 with a drive shaft 101 at an upper end portion. Reference numerals 4 and 4 denote key grooves formed on the inner peripheral surface of the shaft hole 5 of the upper shaft 2, and the key grooves 4 and 4 extending in the axial direction A are opposed to each other in the diameter direction of the upper shaft 2. Are respectively formed. In the figure, reference numeral 6 denotes a spiral digging blade provided on the lower outer peripheral surface of the upper shaft 2.

8は下部シャフトで、その上端部の外周面には前記上部シャフト2の軸孔5内のキー溝4,4に遊嵌して係合するキー部9,9を、下部シャフトの下部の外周面にはらせん状の掘削用刃10をそれぞれ備えており、前記下部シャフト8の上端部を前記上部シャフト2の下部の軸孔5内に挿入して前記両シャフト2,8が連結されている。 Reference numeral 8 denotes a lower shaft, and on the outer peripheral surface of the upper end portion of the lower portion of the lower shaft 8 , key portions 9, 9 loosely engaged with key grooves 4 in the shaft hole 5 of the upper shaft 2 are engaged. A spiral digging blade 10 is provided on the outer peripheral surface, and the upper end portion of the lower shaft 8 is inserted into the lower shaft hole 5 of the upper shaft 2 to connect the both shafts 2 and 8 There is.

そして、前記上部シャフト2と下部シャフト8は、前記キー溝4とキー部9が遊嵌する範囲内、例えば本実施例にあっては、上部シャフト2が下部シャフト8に対して中心角が60度の範囲内で正回転(時計方向)及び逆回転(反時計方向)できる構造としている。なお、図中11は前記掘削用刃10の下端部に一列に設けた複数本の掘削刃先である。   The upper shaft 2 and the lower shaft 8 have a central angle 60 with respect to the lower shaft 8 in the range where the key groove 4 and the key portion 9 are loosely fitted, for example, in the present embodiment. It can be rotated forward (clockwise) and reverse (counterclockwise) within a range of degrees. In the figure, reference numeral 11 denotes a plurality of cutting edges provided in a line at the lower end portion of the cutting blade 10.

12は前記下部シャフト8の上部に固定した拡大翼支持部材で、上下に離間して装着した平面視が横長方形状の上部ブラケット12a及び下部ブラケット12bで構成されており、この上部・下部両ブラケット12a,12bの両端の側面12c付近にあって、前記下部シャフト8の直径方向で相対向する二つの位置に、後述するボルト13aを取り付けるための挿入孔14が形成されている。 An enlarged wing support member 12 fixed to the upper portion of the lower shaft 8 is composed of an upper bracket 12a and a lower bracket 12b which are horizontally separated from each other in plan view mounted separately from each other in the vertical direction. Insertion holes 14 for attaching bolts 13a, which will be described later, are formed near two side surfaces 12c at both ends of 12a and 12b and opposite to each other in the diameter direction of the lower shaft 8.

15は拡大翼で、耐久性を高めるために幅や厚さが大きく形成されたアーム部18とその先端に設けた先端刃19とから構成されており、前記アーム部18の内側面18a側に折れ曲がる後端部近傍で、前記上部・下部両ブラケット12a,12b間の両端部付近に円柱状の軸部16,16によって回動可能となるように設置されている。   An enlarged wing 15 is composed of an arm 18 formed to have a large width and / or thickness to improve durability and a tip blade 19 provided at the tip thereof, and on the side of the inner side surface 18a of the arm 18 It is installed in the vicinity of both ends between the upper and lower brackets 12a and 12b in the vicinity of the bent rear end so as to be pivotable by cylindrical shaft portions 16 and 16.

20は前記上部シャフト2にプレート21を介して装着された拡大翼操作部材で、前記プレート21の外周面21aにおいて前記上部シャフト2の直径方向で相対向する位置からそれぞれ垂下する正面視が横台形状の板材でそれぞれ形成されており、一側端20aは一方の拡大翼15のアーム部18の後端面18b側を向き、他側端20bは他方の拡大翼15の先端刃19側を向くように前記プレート21に固定され、上部シャフト2を中心として円周方向に回動可能に設置されている。   An enlarged wing control member 20 mounted on the upper shaft 2 via a plate 21 is a horizontal base in a front view in which each of the outer shaft 21a of the plate 21 is suspended from the diametrically opposite position of the upper shaft 2 The one side end 20a is directed to the rear end face 18b side of the arm portion 18 of one expansion wing 15 and the other side end 20b is directed to the tip blade 19 side of the other expansion wing It is fixed to the plate 21 and installed so as to be rotatable in the circumferential direction about the upper shaft 2.

上記構成により、前記上部シャフト2を正回転させ、拡大翼操作部材20の一側端20aを一方の拡大翼15のアーム部18の後端面18bに当接させることで、この拡大翼15の軸部16を中心とした拡径する動きを阻止することができる。また、前記上部シャフト2を逆回転させ、拡大翼操作部材20の他側端20bを他方の拡大翼15の先端刃19の内側部19aに衝当させることで、軸部16を中心として拡大翼15を強制的に拡径させることができる。 With the above configuration, the shaft of the enlarged wing 15 is rotated by positively rotating the upper shaft 2 and bringing one end 20 a of the enlarged wing operating member 20 into contact with the rear end face 18 b of the arm portion 18 of one enlarged wing 15. The diameter-expanding movement centering on the part 16 can be prevented. Further, the upper shaft 2 is reversely rotated, and the other side end 20b of the expansion wing operation member 20 is abutted against the inner side 19a of the tip end blade 19 of the other expansion wing 15, whereby the expansion wing around the shaft portion 16 is enlarged. 15 can be forcibly expanded.

13は前記拡大翼15が不用意に拡径するのを防止するストッパーとしての機能と、前記拡大翼15が拡径した場合にこれを検知する拡大翼検知手段として機能するシャーピンで、その外周面に前記拡大翼15の軸部近傍の厚さよりやや大きな間隔をおいて、上下に離間して二本のせん断誘導溝13c,13cを形成したボルト13aで形成されている。なお、図中13bは前記下部ブラケット12aの下面側からボルト13aに螺合せしめたナットであり、前記シャーピン13は前記上部・下部両ブラケット12a,12bの間にかけ渡すように固定されている。 The outer peripheral surface 13 has a function as a stopper for preventing the expansion blade 15 from being inadvertently expanded and a shear pin as expansion blade detection means for detecting the expansion blade 15 when the diameter is expanded. The bolt 13a has two shear guiding grooves 13c and 13c spaced apart vertically at a distance slightly larger than the thickness in the vicinity of the shaft portion of the expansion blade 15. In the figure, reference numeral 13b denotes a nut screwed to the bolt 13a from the lower surface side of the lower bracket 12a, and the shear pin 13 is fixed so as to extend between the upper and lower brackets 12a and 12b.

22は前記上部・下部両ブラケット12a,12bの両端付近の側面12cに装着したストッパー部材で、前記拡大翼15の軸部近傍のアーム部18の外側面18c付近に配置されている。このストッパー部材22は、前記下部シャフト8の直径方向で相対向する位置に二つ配置されているとゝもに、上部・下部両ブラケット12a,12bの間に橋渡すように固定されている。 A stopper 22 is mounted on the side surface 12c near both ends of the upper and lower brackets 12a and 12b, and is disposed near the outer surface 18c of the arm 18 near the shaft of the enlarged wing 15. The stopper member 22, the the are two arranged in opposite position at a diameter direction of the lower shaft 8ゝmonitor, upper and lower two brackets 12a, it is fixed to HashiWataru Suyo during 12b.

上記構成により、まず前記拡大翼15が掘削用刃6,10の半径R内に折り畳まれた状態のときに、前記拡大翼15の軸部近傍のアーム部18の外側面18cが前記ストッパー部材22の斜面22aと当接しているため、前記拡大翼15が前記軸部16を中心として下部シャフト8側に必要以上に縮径する動きを制限し、拡大翼15が下部シャフト8側に入り込みすぎないようになっている。 With the above configuration, when the enlarged wing 15 is first folded within the radius R of the digging blades 6 and 10, the outer surface 18c of the arm 18 near the shaft of the enlarged wing 15 is the stopper member 22. The expanding wing 15 restricts the movement of the diameter of the expanding wing 15 toward the lower shaft 8 more than necessary around the shaft portion 16 so that the expanding wing 15 does not enter the lower shaft 8 too much. It is supposed to be.

また、前記拡大翼15が前記軸部16を中心として外方向へ拡径し、拡大翼15のアーム部18の内側面18aによって前記シャーピン13が強い圧力を受けた場合、前記シャーピン13は前記上下二条のせん断誘導溝13c,13c間でせん断され、前記拡大翼15が拡径したことを検知することができる。前記シャーピン13がせん断された後は、前記拡大翼15のアーム部18の後端部が前記上部・下部両ブラケット12a,12bに残ったシャーピン13,13の間を自由に通過できるようになる。 Also, if the expansion blades 15 are expanded outwardly around the shaft portion 16, which receives the pressure stronger the shear pin 13 by the inner side surface 18a of the arm portion 18 of the expansion blades 15, the shear pins 13 are the upper and lower It is possible to detect that the diameter of the expanding blade 15 is increased by shearing between the two shear guide grooves 13c and 13c. After the shear pin 13 is sheared, the rear end portion of the arm portion 18 of the expansion wing 15 can freely pass between the shear pins 13 and 13 left on the upper and lower brackets 12a and 12b .

前記上部・下部両ブラケット12a,12bに残ったシャーピン13,13の間をアーム部18の後端部が通過し、前記拡大翼15が軸部16を中心として最大限拡径した時、すなわち、前記下部シャフト8の直径方向で相対向する二つの前記拡大翼15,15が一直線となる位置までそれぞれが拡径した時、前記拡大翼15,15の軸部近傍のアーム部18の外側面18cが前記ストッパー部材22の先端面22bと当接し、前記拡大翼15の拡径の動きが止められ、前記軸部16を中心とした拡大翼15のそれ以上の拡径が阻止される。 When the rear end portion of the arm portion 18 passes between the shear pins 13 and 13 left on the upper and lower brackets 12a and 12b and the expanding wing 15 is maximally expanded in diameter about the shaft portion 16, that is, The outer surface 18c of the arm portion 18 in the vicinity of the shaft portion of the enlarged wings 15, 15 when the diameter of the lower shaft 8 respectively expands to a position where the two enlarged wings 15, 15 opposed to each other in the diametrical direction become straight. Is abutted with the tip end surface 22b of the stopper member 22, the expansion movement of the expansion wing 15 is stopped, and the diameter expansion of the expansion wing 15 around the shaft portion 16 is prevented.

23は前記下部シャフト8の掘削用刃10の外周付近に設けられた補助拡大翼で、位置決め部材であるL字状のブラケット24の内側に、前記掘削用刃10を挟むようにして両面にボルト25a及びナット25bによって回動自在に支持されている。この補助拡大翼23は、前記掘削用刃10の半径R内に折り畳まれた状態から、前記補助拡大翼23の側面部23aが前記ブラケット24の上辺部24aに当接する状態までボルト25aを中心として拡径することができ、その拡径した二本の補助拡大翼23,23によって地中孔111の下部において拡大孔を掘削することができる。   Reference numeral 23 denotes an auxiliary expansion wing provided near the outer periphery of the excavating blade 10 of the lower shaft 8 so as to sandwich the excavating blade 10 inside an L-shaped bracket 24 which is a positioning member. It is rotatably supported by a nut 25b. The auxiliary enlarged wing 23 is centered on the bolt 25 a from the state where it is folded within the radius R of the digging blade 10 until the side portion 23 a of the auxiliary enlarged wing 23 abuts on the upper side 24 a of the bracket 24. The diameter can be expanded, and the enlarged diameter can be excavated at the lower part of the underground hole 111 by the two enlarged auxiliary diameters 23 and 23.

また、通常時は前記補助拡大翼23が不用意に拡径しないように、折り畳まれた状態で点溶接により前記掘削用刃10に固定されている。また、前記補助拡大翼23は最大まで拡径した場合の回転半径r1が前記拡大翼15が最大まで拡径した場合の回転半径r2よりもやや小さくなるように、前記補助拡大翼23の長さは設定されている。 In addition, in a normal state, the auxiliary enlarged wing 23 is fixed to the digging blade 10 by point welding in a folded state so that the diameter of the auxiliary enlarged wing 23 is not inadvertently increased. The auxiliary expansion blades 23 are rotated radius r1 in the case of diameter up, the so enlarged wing 15 is slightly smaller than the rotation radius r2 in the case of diameter up to the length of the auxiliary expansion blades 23 Is set.

次に、拡大孔掘削用ヘッド1の動作について説明すると、地面から所定の深さの地中孔111を掘削する場合は、駆動軸101を正回転(時計方向に回転)させることで、駆動軸101に連結部3を介して連結されている上部シャフト2、および上部シャフト2にプレート21を介して装着された拡大翼操作部材20がそれぞれ同方向に回転する。   Next, the operation of the enlarged hole excavating head 1 will be described. When excavating the underground hole 111 of a predetermined depth from the ground, the drive shaft 101 is rotated forward (rotated clockwise) to drive the drive shaft. The upper shaft 2 connected to the connector 101 via the connector 3 and the enlarged wing operating member 20 mounted on the upper shaft 2 via the plate 21 rotate in the same direction.

拡大翼操作部材20が正回転することで、図4及び図5に示すように、拡大翼操作部材20の垂下部の一側端20aが拡大翼15のアーム部18の後端面18bと当接する。その結果、拡大翼15の軸部16を中心とした拡径する動きが阻止され、拡大翼15は掘削用刃6,10の半径R内に折り畳まれた状態が保持される。 As shown in FIG. 4 and FIG. 5, when the expansion wing operation member 20 rotates forward, one end 20 a of the hanging portion of the expansion wing operation member 20 abuts on the rear end face 18 b of the arm portion 18 of the expansion wing 15. . As a result, the expansion movement around the shaft portion 16 of the expansion wing 15 is blocked, and the expansion wing 15 is maintained in the folded state within the radius R of the digging blades 6 and 10.

同時に、拡大翼15の軸部近傍のアーム部18の外側面18cがストッパー部材22の斜面22aと当接し、拡大翼15の軸部16を中心とした下部シャフト8側への更なる動き(縮径する動き)も阻止されている。その結果、拡大翼15は軸部16を中心に回動することができず掘削用刃6,10の半径R内に折り畳まれた状態が固定される。 At the same time, the outer surface 18c of the arm 18 near the shaft of the expansion wing 15 abuts on the slope 22a of the stopper member 22 to further move the expansion wing 15 toward the lower shaft 8 about the shaft 16 (contraction Drooping movement is also blocked. As a result, the magnifying wing 15 can not rotate about the shaft portion 16 and the folded state is fixed within the radius R of the digging blades 6 and 10.

ここで、何らかの不具合により、上部シャフト2が逆回転し、図6及び図7に示すように、拡大翼操作部材20の一側端20aが拡大翼15のアーム部18の後端面18bからやや離れた場合であっても、拡大翼15のアーム部18の内側面18aがシャーピン13に当接し、拡大翼15の軸部16を中心とした拡径する動きが阻止され、拡大翼15は掘削用刃10の半径R内に折り畳まれた状態が保持される。 Here, due to some problem, the upper shaft 2 is reversely rotated, and as shown in FIGS. 6 and 7, one end 20a of the enlarged wing operating member 20 is slightly separated from the rear end face 18b of the arm portion 18 of the enlarged wing 15. even when an inner side surface 18a of the arm portion 18 of the expansion blades 15 abuts the shear pin 13, movement of the enlarged diameter shaft portion 16 around the expansion blades 15 is prevented, for expanding wings 15 drilled The folded state is maintained within the radius R of the blade 10.

上部シャフト2および上部シャフト2にプレート21を介して装着された拡大翼操作部材20がそれぞれ正回転し、図5に示すように、上部シャフト2の軸孔5のキー溝4の正回転方向側の端面4aが下部シャフト8のキー部9と当接する。そして、上部シャフト2が更に正回転すると下部シャフト8は上部シャフト2と一緒に正回転する。   The enlarged wing operating member 20 mounted on the upper shaft 2 and the upper shaft 2 via the plate 21 rotates forward, and as shown in FIG. 5, the positive rotation direction side of the key groove 4 of the shaft hole 5 of the upper shaft 2 The end face 4 a of the lower shaft 8 abuts on the key portion 9 of the lower shaft 8. Then, when the upper shaft 2 further rotates forward, the lower shaft 8 rotates forward together with the upper shaft 2.

それにより、上部シャフト2及び下部シャフト8の外周面に装着した掘削用刃6,10及び掘削刃先11が同一方向に回転するので、駆動軸101によって上部シャフト2を介して下部シャフト8に対して軸方向Aの押し込み力を加えることにより、地面113に所定深さの地中孔111を掘削することができる。 Thereby, since the excavating blade 6, 10 and the drilling edge 11 is mounted on the outer peripheral surface of the upper shaft 2 and a lower shaft 8 rotates in the same direction, relative to the lower shaft 8 via the upper shaft 2 by a drive shaft 101 By applying a pressing force in the axial direction A, the underground hole 111 of a predetermined depth can be excavated on the ground 113.

次に、地中孔111が地面から所定の深さまで達した後、地中孔111の下部に拡大孔112を形成する場合は、駆動軸101の回転を一旦停止するとゝもに、駆動軸101によって上部シャフト2を介して下部シャフト8に対して軸方向Aの押し込み力を加えることにより、下部シャフト8の掘削用刃10の下端部に設けられた掘削刃先11を孔底114に食い込ませ、下部シャフト8を孔底114に固定する。   Next, after the underground hole 111 reaches a predetermined depth from the ground, when forming the expanded hole 112 in the lower part of the underground hole 111, once the rotation of the drive shaft 101 is stopped, the drive shaft 101 is also driven. The cutting edge 11 provided at the lower end of the digging blade 10 of the lower shaft 8 is made to bite into the hole bottom 114 by applying pressing force in the axial direction A to the lower shaft 8 via the upper shaft 2 by the The lower shaft 8 is fixed to the hole bottom 114.

そして、下部シャフト8が孔底114に固定された状態で駆動軸101を逆回転(反時計方向に回転)させ、駆動軸101に連結されている上部シャフト2を逆回転させる。すなわち、上部シャフト2を図4及び図5に示す状態から、上部シャフト2のキー溝4と下部シャフト8のキー部9とが遊嵌する範囲内、例えば本実施例では60度の範囲内で上部シャフト2を逆回転させることで、上部シャフト2のキー溝4の逆回転方向側の端面4bが下部シャフト8のキー部9と図9に示す状態で衝当する。   Then, in a state where the lower shaft 8 is fixed to the hole bottom 114, the drive shaft 101 is reversely rotated (counterclockwise rotation), and the upper shaft 2 connected to the drive shaft 101 is reversely rotated. That is, within the range in which the key groove 4 of the upper shaft 2 and the key portion 9 of the lower shaft 8 are loosely fitted from the state shown in FIG. 4 and FIG. By rotating the upper shaft 2 in the reverse direction, the end surface 4b on the reverse rotation direction side of the key groove 4 of the upper shaft 2 strikes the key portion 9 of the lower shaft 8 in the state shown in FIG.

上部シャフト2が逆回転することにより、上部シャフト2にプレート21を介して装着された拡大翼操作部材20の垂下部の一側端20aは、一方の拡大翼15のアーム部18の後端面18bと当接する図4に示す状態から離れる。そして、上部シャフト2の逆回転を続けることで、拡大翼操作部材20は円弧を描きながら他方の拡大翼15に近づいてゆき、図8に示すように、拡大翼操作部材20の垂下部の他側端20bが拡大翼15の先端刃19の内側部19aと当接する。   When the upper shaft 2 is reversely rotated, one end 20 a of the hanging portion of the expansion wing operating member 20 attached to the upper shaft 2 via the plate 21 is the rear end face 18 b of the arm 18 of one expansion wing 15. And abut from the state shown in FIG. Then, by continuing the reverse rotation of the upper shaft 2, the expansion wing operation member 20 approaches the other expansion wing 15 while drawing a circular arc, and as shown in FIG. The side end 20 b abuts on the inside portion 19 a of the tip blade 19 of the enlarged wing 15.

そして、上部シャフト2のキー溝4の逆回転方向側の端面4bが下部シャフト8のキー部9と衝当した図9に示す状態の後も上部シャフト2を逆回転させると、拡大翼操作部材20の垂下部の他側端20bが拡大翼15の先端刃19の内側部19aの位置まで移動する(図8参照)。これに伴い拡大翼15の先端刃19は拡大翼操作部材20によって強制的に押し出され、軸部16を中心として反時計方向に回転して先端刃19の外側部19bが掘削用刃6,10の半径Rの外側に突出する位置まで移動(拡径)する。   Then, when the upper shaft 2 is reversely rotated even after the state shown in FIG. 9 in which the end face 4b on the reverse rotation direction side of the key groove 4 of the upper shaft 2 collides with the key portion 9 of the lower shaft 8, the enlarged wing operation member The other end 20b of the hanging portion 20 moves to the position of the inner side 19a of the tip blade 19 of the expansion blade 15 (see FIG. 8). Accordingly, the end blade 19 of the expansion wing 15 is forcibly pushed out by the expansion wing operation member 20 and rotates counterclockwise around the shaft portion 16 so that the outer portion 19 b of the end blade 19 is the digging blade 6, 10 Move to a position where it protrudes outside the radius R of the (diameter expansion).

上記のように、拡大翼操作部材20によって拡大翼15が軸部16を中心として反時計方向(外方向)へ拡径することにより、二つの拡大翼15,15のアーム部18の後端部も軸部16を中心として反時計方向に回転する。その結果、図13に示すように、上部・下部両ブラケット12a,12bの間にかけ渡すように固定されているシャーピン13がアーム部18の内側面18aによって圧力を受け、図14に示すように、せん断誘導溝13c,13cの位置でせん断される。そして、上部・下部両ブラケット12a,12bに残ったシャーピン13のせん断誘導溝13c,13c間を拡大翼15のアーム部18の後端部が自由に通過でき、拡大翼15が拡径できるようになる。 As described above, the enlarged wing 15 is expanded in the counterclockwise direction (outward direction) around the shaft portion 16 by the enlarged wing operation member 20, whereby the rear end portions of the arm portions 18 of the two enlarged wings 15, 15 Also, it rotates counterclockwise around the shaft portion 16. As a result, as shown in FIG. 13, the shear pin 13 fixed so as to bridge between the upper and lower brackets 12a and 12b is subjected to pressure by the inner side surface 18a of the arm portion 18, and as shown in FIG. Shearing is performed at the position of the shear guiding grooves 13c, 13c. Then, the rear end portion of the arm portion 18 of the expansion wing 15 can freely pass between the shear guiding grooves 13c, 13c of the shear pin 13 left in the upper and lower brackets 12a, 12b so that the expansion wing 15 can expand in diameter. Become.

次に、図8に示す状態から駆動軸101を正回転させる。それに伴い、駆動軸101に連結されている上部シャフト2も同方向に回転し、図に示すように、キー溝4の正回転方向側の端面4aが下部シャフト8のキー部9と当接する。そして、駆動軸101を更に正回転させると、下部シャフト8は駆動軸101に連結されている上部シャフト2を介して駆動軸101と同方向に回転する。 Next, the drive shaft 101 is rotated forward from the state shown in FIG. Along with this, also the upper shaft 2 is connected to the drive shaft 101 rotates in the same direction, as shown in FIG. 5, the end surface 4a of the forward rotation direction of the key groove 4 comes into contact with the key portion 9 of the lower shaft 8 . Then, when the drive shaft 101 is further positively rotated, the lower shaft 8 is rotated in the same direction as the drive shaft 101 via the upper shaft 2 connected to the drive shaft 101.

下部シャフト8が正回転することで、掘削用刃6,10の半径Rの外側に突出する位置まで移動している拡大翼15の先端刃19が掘削土の抵抗を受け、拡大翼15は軸部16を中心として徐々に拡径する(図8,図10参照)。そして、上記のように上部・下部両ブラケット12a,12bに残ったシャーピン13のせん断誘導溝13c,13c間を拡大翼15のアーム部18の後端部が通過し、図11に示すように、下部シャフト8の直径方向で相対向する二つの拡大翼15,15はそのアーム部18,18が一直線になるまで拡径する。 The forward rotation of the lower shaft 8 causes the tip blade 19 of the expansion blade 15 moving to a position projecting outward of the radius R of the digging blade 6, 10 to the resistance of the excavated soil, and the expansion blade 15 has an axis The diameter is gradually enlarged centering on the portion 16 (see FIGS. 8 and 10). Then, the rear end portion of the arm portion 18 of the expansion wing 15 passes between the shear guiding grooves 13c, 13c of the shear pin 13 left in the upper and lower brackets 12a, 12b as described above, as shown in FIG. expansion wings 15, 15 two of you opposed in radial direction of the lower shaft 8 is expanded to the arm portions 18, 18 thereof in alignment.

そのとき、拡大翼15の軸部近傍のアーム部18の外側面18cがストッパー部材22の先端面22bと当接するため、拡大翼15のそれ以上の拡径する動きが阻止される。そのため、駆動軸101の正回転を持続させて掘り進めることで、図15に示すように、所望深さの地中孔111の下部において拡大翼15の先端刃19によって拡大孔112を掘削することができる。 At this time, the outer surface 18 c of the arm 18 near the shaft of the expansion wing 15 abuts on the end surface 22 b of the stopper member 22, so that the further expansion movement of the expansion wing 15 is blocked. Therefore, by continuing the normal rotation of the drive shaft 101 and digging, as shown in FIG. 15, the enlarged hole 112 is excavated by the tip blade 19 of the enlarged wing 15 at the lower part of the underground hole 111 of the desired depth. Can.

所望深さの地中孔111の下部に拡大孔112を掘削する作業が終了した場合には、駆動軸101を今度は逆回転させる。それに伴い、駆動軸101に連結されている上部シャフト2も同方向に回転するため、図9示すように、上部シャフト2のキー溝4の逆回転方向側の端面4bが下部シャフト8のキー部9と当接し、下部シャフト8が上部シャフト2と同方向に徐々に逆回転していく。 When the operation of excavating the enlarged hole 112 below the underground hole 111 of the desired depth is completed, the drive shaft 101 is reversely rotated. Along with that, the upper shaft 2 connected to the drive shaft 101 also rotates in the same direction, so as shown in FIG. 9 , the end face 4 b on the reverse rotation direction side of the key groove 4 of the upper shaft 2 is the key portion of the lower shaft 8 The lower shaft 8 is in reverse rotation in the same direction as the upper shaft 2.

そして、下部シャフト8が逆回転することで、掘削用刃6,10の半径Rの外側に突出する位置まで拡径している拡大翼15の先端刃19は、そのアーム部18の外側面18cが掘削土の抵抗を受け、拡大翼15は軸部16を中心として徐々に縮径していき、掘削用刃6,10の半径Rの内側まで回転移動する。 The tip end blade 19 of the expansion blade 15 whose diameter is expanded to a position protruding outward of the radius R of the digging blades 6 and 10 by the reverse rotation of the lower shaft 8 is the outer surface 18 c of the arm portion 18. Due to the resistance of the excavated soil, the expanding wing 15 gradually reduces its diameter around the shaft portion 16 and rotationally moves to the inside of the radius R of the digging blades 6 and 10.

上記のように、拡大翼15の先端刃19が掘削用刃6,10の半径Rの内側まで回転移動した時点で駆動軸101を今度は正回転させる。それに伴い、駆動軸101に連結されている上部シャフト2も同方向に回転し、拡大翼操作部材20の垂下部の一側端20aが拡大翼15のアーム部18の後端面18bと当接する。その結果、拡大翼15の軸部16を中心とした拡径する動きが阻止され、拡大翼15は掘削用刃6,10の半径R内に折り畳まれた状態が保持される。 As described above, at the time when the tip end blade 19 of the expansion blade 15 rotationally moves to the inside of the radius R of the digging blades 6 and 10, the drive shaft 101 is rotated forward. Accordingly, the upper shaft 2 connected to the drive shaft 101 is also rotated in the same direction, and one end 20 a of the hanging portion of the expansion wing operation member 20 abuts on the rear end surface 18 b of the arm 18 of the expansion wing 15. As a result, the expansion movement around the shaft portion 16 of the expansion wing 15 is blocked, and the expansion wing 15 is maintained in the folded state within the radius R of the digging blades 6 and 10.

ここで、上部・下部両ブラケット12a,12bには、図13及び図14に示すように拡大翼15が拡径したことを検知するためのシャーピン13が固定されているため、拡大孔112の掘削作業が終了した後、拡大孔掘削用ヘッド1を上方へ引き上げ、シャーピン13の状態を観察することで、拡大翼15が拡径したか否かを検知することができる。 Here, as shown in FIGS. 13 and 14, the shear pin 13 for detecting that the enlarged wing 15 has expanded is fixed to both the upper and lower brackets 12a and 12b, so that digging of the enlarged hole 112 is performed. after the work is completed, pulling the enlarged hole drilling head 1 upwards, by observing the state of the shear pin 13 can be enlarged wing 15 detects whether or not expanded.

したがって、拡大孔掘削用ヘッド1が上方へ引き上げられた際に拡大翼15が折り畳まれた状態であったとしても、シャーピン13がせん断誘導溝13cの位置でせん断されていれば、拡大孔112の掘削時に拡大翼15が実際に拡径したと検知することができ、また地中孔111の下部に拡大孔112を掘削できたことを把握することができる。   Therefore, if the shear pin 13 is sheared at the position of the shear guiding groove 13c even if the enlarged wing 15 is in a folded state when the expanded hole excavating head 1 is pulled upward, At the time of excavation, it can be detected that the expansion wing 15 has actually expanded in diameter, and it can be grasped that the expansion hole 112 can be excavated at the lower part of the underground hole 111.

また、試験掘りによって地盤が硬く拡大翼15だけでは拡大孔112の掘削が困難と判断した場合は、補助拡大翼23の上記点溶接による固定を解除する。それにより、駆動軸101とともに下部シャフト8が正回転することで、補助拡大翼23が掘削用刃6,10の半径R内に折り畳まれた図2に示す状態から、補助拡大翼23の先端部23bが掘削土の抵抗を受けてボルト25aを中心として徐々に拡径する。 Further, when it is determined that the ground is hard due to the test digging and it is difficult to dig the enlarged hole 112 only by the enlarged wing 15, the fixing of the auxiliary enlarged wing 23 by the point welding is released. As a result, when the lower shaft 8 rotates forward with the drive shaft 101, the tip portion of the auxiliary enlarged wing 23 is obtained from the state shown in FIG. 2 in which the auxiliary enlarged wing 23 is folded within the radius R of the digging blade 6, 10. The diameter 23 b gradually expands around the bolt 25 a due to the resistance of the excavated soil.

そして、補助拡大翼23の側面部23aがブラケット24の上辺部24aに当接する図3及び図12に示す状態まで補助拡大翼23が拡径するため、拡大孔112を掘削することが可能となる。 Then, since the diameter of the auxiliary expansion wing 23 is expanded to the state shown in FIGS. 3 and 12 in which the side surface portion 23a of the auxiliary expansion wing 23 abuts on the upper side portion 24a of the bracket 24, the expanded hole 112 can be excavated. .

また、拡大孔112の掘削作業が終了し、拡大孔掘削用ヘッド1が上方へ引き上げられる際、上記のように下部シャフト8は駆動軸101と共に逆回転するため、補助拡大翼23は掘削土の抵抗を受けて徐々に縮径していき、図2に示すように、掘削用刃6,10の半径R内に折り畳まれた状態に戻る。 In addition, when the drilling operation of the enlarged hole 112 is finished and the enlarged hole excavating head 1 is pulled upward, the lower shaft 8 is reversely rotated with the drive shaft 101 as described above, so the auxiliary enlarged wing 23 is made of excavated soil Under the resistance, the diameter is gradually reduced, and as shown in FIG. 2, the state returns to the state of being folded within the radius R of the digging blade 6, 10.

ここで、仮に拡大孔掘削用ヘッド1を引き上げる途中で土砂を噛んで補助拡大翼23が折り畳まれなくなった場合には、補助拡大翼23が固定されている位置の掘削用刃10の肉厚は上記のように他の位置に比べて薄く上下方向の抵抗に対して弱い構造であるため、強引に拡大孔掘削用ヘッド1を上方へ引き上げて掘削用刃10の補助拡大翼23が固定されている薄い位置を破壊しながら引き上げる。 Here, if the auxiliary expansion wing 23 is not folded by biting earth and sand while pulling up the expansion hole excavating head 1, the thickness of the digging blade 10 at the position where the auxiliary expansion wing 23 is fixed is As described above, since it is a thin structure that is weak against resistance in the vertical direction compared to other positions, the auxiliary enlarged wing 23 of the digging blade 10 is fixed by forcibly pulling up the enlarged hole drilling head 1 upward. It pulls up while destroying a thin position.

また、掘削用刃10に補助拡大翼23を回動自在に支持しているボルト25aに、引張抵抗の弱いボルト25aを使用してもよい。こうすることで、土砂が噛んで補助拡大翼23が折り畳まれなくなった場合に、強引に拡大孔掘削用ヘッド1を上方へ引き上げてボルト25aを破断し、補助拡大翼23を掘削用刃10から脱落させながら拡大孔掘削用ヘッド1を上方へ引き上げることができる。   In addition, a bolt 25a that is weak in tensile resistance may be used as the bolt 25a that rotatably supports the auxiliary expansion wing 23 on the digging blade 10. By doing this, when the earth and sand bite and the auxiliary expansion wing 23 does not fold, the head 1 for expanding hole drilling is forcibly pulled upward and the bolt 25 a is broken, and the auxiliary expansion wing 23 from the cutting blade 10 The extended hole drilling head 1 can be pulled up while dropping off.

1 拡大孔掘削用ヘッド
2 上部シャフト
3 連結部
4 キー溝
5 軸孔
6 掘削用刃
7 軸部近傍部
8 下部シャフト
9 キー部
10 掘削用刃
11 掘削刃先
12 拡大翼支持部材
12a 上部ブラケット
12b 下部ブラケット
12c 側面
13 シャーピン
13a ボルト
13c せん断誘導溝
14 挿入孔
15 拡大翼
16 軸部
18 アーム部
18a 内側面
18b 後端面
19 先端刃
19a 内側面
20 拡大翼操作部材
20a 一側端
20b 他側端
21 プレート
22 ストッパー部材
22a 斜面
22b 先端面
23 補助拡大翼
24 ブラケット
DESCRIPTION OF SYMBOLS 1 Expansion hole excavating head 2 upper shaft 3 connection part 4 key groove 5 axial hole 6 drilling blade 7 axial part vicinity 8 lower shaft 9 key part 10 drilling blade 11 cutting edge 12 expanding blade support member 12a upper bracket 12b lower part Bracket 12c Side 13 Shear pin 13a Bolt 13c Shear guiding groove 14 Insertion hole 15 Enlarged wing 16 Shaft 18 Arm part 18a Inner side 18b Rear end face 19 Tip blade 19a Inner side 20 Expansion wing control member 20a One side end 20b Other side end 21 Plate 22 Stopper member 22a Slope 22b Tip face 23 Auxiliary expansion wing 24 Bracket

Claims (3)

上端部に駆動軸と連結する連結部を備えた上部シャフトの下端部に、所定角度正逆回転可能となるように下部シャフトを接続するとゝもに、前記下部シャフトには、直径方向で相対向する少なくとも二つの位置においてそれぞれ拡大翼を所定角度内で回動可能に軸支する上部ブラケット及び下部ブラケットからなる拡大翼支持部材を、前記上部シャフトには、その正回転時に、一端が前記拡大翼のアーム部の後端と当接して、前記拡大翼を前記下部シャフトに装着した掘削用刃の半径内に折り畳み状態に保持するトルク伝達部として、又逆回転時に、他端が前記拡大翼の先端部と衝当して、前記拡大翼の前記先端部が前記掘削用刃の半径から突出する位置まで前記拡大翼を強制的に外方向へ拡径する蹴り出し部としてそれぞれ機能する拡大翼操作部材を装着した拡大孔掘削用ヘッドであって、前記上部シャフトの正回転時に前記拡大翼の前記アーム部の内側面が当接して前記拡大翼が拡径することを防止するストッパーとして、又前記上部シャフトの逆回転時には前記拡大翼の前記アーム部の前記内側面が当接してせん断破断され、前記拡大翼の拡径を検知する検知部としてそれぞれ機能する拡大翼検知手段を、前記拡大翼支持部材の前記上部ブラケット及び前記下部ブラケット間に備え、前記拡大翼の前記アーム部の外側面と当接して前記拡大翼が拡径及び縮径する動きを制限するストッパー部材を前記拡大翼支持部材に備えたことを特徴とする拡大孔掘削用ヘッド。 When the lower shaft is connected to the lower end of the upper shaft provided with the connecting part connected with the drive shaft at the upper end so as to be able to rotate forward and reverse by a predetermined angle, the lower shaft is diametrically opposed And the upper shaft includes an upper bracket and a lower bracket for pivotally supporting the expansion wing within a predetermined angle, and the upper shaft has one end thereof when the positive rotation is performed. As a torque transmission part in contact with the rear end face of the arm part to hold the widening blade in a folded state within the radius of the digging blade attached to the lower shaft, and at the other time the other end is the widening blade expansion of in tip and impinge, respectively function as the forced out kick diameter increases outward portion of the enlarged blade to a position where the tip projects from the radius of the drilling blade of the expansion wings An enlarged hole drilling head equipped with a control member, as a stopper for the inner surface of the arm portion of the expansion blades during forward rotation of the upper shaft to prevent the expansion wing abuts it is enlarged, also When the upper shaft is reversely rotated, the inner surface of the arm portion of the expanding blade abuts and is sheared, and the expanding blade detecting means functioning as a detecting unit for detecting the diameter expansion of the expanding blade is the expanding blade the upper bracket and provided between the lower bracket, the arm portion of the outer surface and in contact with the enlarged wing support member a stopper member for limiting movement of the expansion blades are expanded and contracted in the expansion wing of the support member An expanded hole drilling head characterized by being provided in . 前記拡大翼検知手段が、前記拡大翼支持部材の前記上部ブラケット及び前記下部ブラケットに上下両端部をそれぞれ固定したボルトであって、前記拡大翼の軸部近傍の厚さより大きい間隔をおいて、せん断誘導溝を上下2ヶ所に備えたことを特徴とする請求項1に記載の拡大孔掘削用ヘッド。 The larger blade detecting means, a said upper bracket and a bolt which upper and lower ends are fixed respectively to the lower bracket of the expansion wing support member, at a not greater than the thickness of intervals of the shaft portion near the enlarged wing, The enlarged hole drilling head according to claim 1, characterized in that shear guiding grooves are provided at upper and lower two places. 前記下部シャフトに装着した前記掘削用刃に、ほぼ杭外径まで拡径する補助拡大翼と位置決め部材を設けたことを特徴とする請求項1又は2に記載の拡大孔掘削用ヘッド。 Wherein the excavating blade mounted on the lower shaft, enlarged pores drilling head according to claim 1 or 2, characterized in that a positioning member and the auxiliary expansion vanes whose diameter increases to approximately Kuigai diameter.
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JPS5634068Y2 (en) * 1977-12-05 1981-08-12
JP2688622B2 (en) * 1990-01-18 1997-12-10 新日本製鐵株式会社 Auger for soil cement composite pile construction and soil cement composite pile construction method
JP3859817B2 (en) * 1997-06-17 2006-12-20 旭化成建材株式会社 Expansion head for excavation
GB2400869B (en) * 2003-04-22 2006-11-15 Cie Du Sol Threading equipment
JP4945603B2 (en) * 2009-07-03 2012-06-06 前田製品販売株式会社 Expanded hole drilling head

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