JP7274697B1 - Rotating buried tip enlarged wing pile - Google Patents

Rotating buried tip enlarged wing pile Download PDF

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JP7274697B1
JP7274697B1 JP2023019539A JP2023019539A JP7274697B1 JP 7274697 B1 JP7274697 B1 JP 7274697B1 JP 2023019539 A JP2023019539 A JP 2023019539A JP 2023019539 A JP2023019539 A JP 2023019539A JP 7274697 B1 JP7274697 B1 JP 7274697B1
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秋男 田中
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Abstract

【課題】 従来の杭は、軸管の先端付近の外周に螺旋翼が螺旋状に突設されているため、地中への貫入時に、軸管の周囲の掘削土が、軸管の外周面からの突出部位にてほぐされたり、かき乱されることにより、安定した杭保持が実現できないおそれがある。【解決手段】 本発明は、円筒杭本体と、円筒杭本体の先端側軸心に立設する筒状掘削刃と、筒状掘削刃の外周に沿って回動連結具を介して回動自在に配設する複数の拡大翼と、を備え、各拡大翼の表面には、正転方向側を下に傾斜する推進翼が突設され、各拡大翼は、正転方向側の一部が他の拡大翼の逆転方向側の一部で被覆され、正転方向に回転する状態では、各拡大翼の全てが回転埋設先端拡大翼杭の外径内に収容され、逆転方向に回転する状態では、各拡大翼の一部が回転埋設先端拡大翼杭の外径外に突出されることを特徴とした回転埋設先端拡大翼杭である。【選択図】 図9[Problem] In conventional piles, since spiral blades protrude in a spiral shape on the outer periphery near the tip of the shaft pipe, when the pile is penetrated into the ground, the excavated soil around the shaft pipe is pushed into the outer peripheral surface of the shaft pipe. There is a risk that stable pile holding cannot be realized by being loosened or disturbed by the protruding part from the empty pile. SOLUTION: The present invention comprises a cylindrical pile main body, a cylindrical excavating blade erected on the tip side axial center of the cylindrical pile main body, and rotatable along the outer periphery of the cylindrical piling blade via a rotary connector. and a plurality of expansion wings disposed on the surface of each expansion wing, each expansion wing has a propulsion wing inclined downward on the forward rotation direction side, and each expansion wing has a part on the forward rotation direction side In a state in which a part of the other expansion wing on the reverse direction side is covered and rotates in the normal direction, each expansion wing is entirely housed within the outer diameter of the rotary-embedded tip expansion wing pile and rotates in the reverse direction. is a rotating embedded tip expanding wing pile characterized in that a part of each expanding wing protrudes outside the outer diameter of the rotating embedded tip expanding wing pile. [Selection drawing] Fig. 9

Description

本発明は、回転埋設先端拡大翼杭、より具体的には、軸回りの一方向の回転により地盤に貫入し、所望の地盤まで貫入埋設されたら、逆方向の回転によって突出する拡大翼で地盤支持力等を増強させることによって地盤に強固に立てることができる回転埋設先端拡大翼杭に関する。 The present invention relates to a rotating buried tip enlarged wing pile, more specifically, an enlarged wing that penetrates into the ground by rotating in one direction around the axis, and when it is penetrated and buried to a desired ground, rotates in the opposite direction to protrude from the ground. The present invention relates to a rotating buried tip expanded wing pile that can be firmly erected on the ground by increasing the bearing capacity and the like.

鋼管杭を地中に埋め込む施工方法としては、各種ハンマー等による打込み工法がある。この打込み工法は、杭の先端部が支持層に達するまで杭の後端部(頭部)をハンマー等で打撃する工法であるため、杭の打撃に伴う振動、騒音等により、特に住宅密集地においては施工が困難な場合がある。そこで、回転貫入工法が好んで用いられている。この回転貫入工法は、螺旋状の羽根等の鋼片を下端部外周面に設けた鋼管杭を地面に配置し、該鋼管杭を回転させながら地中に押し込むことによって該鋼管杭を地中に埋め込むものである。
このような回転貫入工法で用いられる鋼管杭に関する文献の一例として、特許文献1が挙げられる。
As a construction method for embedding steel pipe piles in the ground, there are driving methods using various hammers and the like. In this driving method, the rear end (head) of the pile is hit with a hammer until the tip of the pile reaches the bearing layer, so the vibration and noise associated with the hitting of the pile can cause damage, especially in densely populated residential areas. In some cases, construction is difficult. Therefore, the rotary penetration method is preferably used. In this rotary penetration method, a steel pipe pile having a steel piece such as a spiral blade on the outer peripheral surface of the lower end is placed on the ground, and the steel pipe pile is pushed into the ground while rotating. It is embedded.
Patent document 1 is mentioned as an example of the document regarding the steel pipe pile used by such a rotary penetration method.

文献1に係る発明は、少なくとも1つの螺旋翼が先端付近の外周に螺旋状に突設され、少なくとも1つの切欠部が先端に形成された鋼管製の軸管と、この軸管の内径より外径が少し小さい鋼管製で、底板が先端に固着され、前記軸管内に前記底板を軸管の先端側に向けて挿入された内管とを備えたことを特徴とする鋼管杭で、地盤に対する先端支持力を向上できるものである。 The invention according to Document 1 comprises a steel shaft tube having at least one helical blade spirally protruding from the outer periphery near the tip and at least one notch formed at the tip, and an outer diameter of the shaft tube. A steel pipe pile having a slightly smaller diameter, a bottom plate fixed to the tip, and an inner pipe inserted into the shaft pipe with the bottom plate facing the tip side of the shaft pipe. It is possible to improve the tip support force.

特開2003-176536JP 2003-176536

しかし、文献1に係る発明は、鋼管製の軸管の先端付近の外周に螺旋翼が螺旋状に突設されているため、地中への貫入時に、軸管の周囲の掘削土が、軸管の外周面からの突出部位にてほぐされたり、かき乱されることにより、地中に貫入された状態下においては、軸管の外周面摩擦力が十分効果的に確保されない。このようなことから、軸管のぐらつきが生じ、安定した杭保持が実現できない。 However, in the invention according to Document 1, since the helical blades are protruding spirally from the outer periphery near the tip of the steel pipe shaft pipe, when the shaft pipe is penetrated into the ground, the excavated soil around the shaft pipe When the tube is penetrated into the ground, the frictional force on the outer peripheral surface of the axial tube cannot be sufficiently effectively secured because the protruding portion from the outer peripheral surface of the tube loosens or disturbs the tube. For this reason, the shaft tube wobbles, and stable pile holding cannot be achieved.

そこで、本発明は、軸回りの一方向の正転方向の回転により地盤に貫入し、所望の地盤まで貫入埋設されたら、逆方向の逆転方向の回転によって突出する拡大翼で地盤支持力等を増強させることによって地盤に強固に確保することができる回転埋設先端拡大翼杭を提供するものである。 Therefore, the present invention penetrates into the ground by rotating in the forward direction in one direction around the axis, and when the ground is penetrated and embedded to the desired ground, the expanding wings projecting by rotating in the reverse direction in the opposite direction increase the ground bearing force. To provide a rotating buried tip enlarged wing pile that can be firmly secured to the ground by reinforcing it.

請求項1の発明は、正転方向の回転によって地盤に貫入される回転埋設先端拡大翼杭であって、円筒杭本体と、円筒杭本体の先端側軸心に立設する筒状掘削刃と、筒状掘削刃の外周に沿って回動連結具を介して回動自在に配設する複数の拡大翼と、を備え、各拡大翼の表面には、正転方向側を下に傾斜する推進翼が突設され、各拡大翼は、正転方向側の一部が他の前記拡大翼の逆転方向側の一部で被覆され、正転方向に回転する状態では、各拡大翼の全てが回転埋設先端拡大翼杭の外径内に収容され、逆転方向に回転する状態では、各拡大翼の一部が回転埋設先端拡大翼杭の外径外に突出されることを特徴とした回転埋設先端拡大翼杭である。 The invention of claim 1 is a rotating embedded tip expanding wing pile that penetrates into the ground by rotating in the normal direction, comprising a cylindrical pile main body and a cylindrical excavating blade erected at the tip side axial center of the cylindrical pile main body. , and a plurality of enlarging wings rotatably arranged along the outer periphery of the cylindrical excavating blade via a rotating connector, and the surface of each enlarging wing is inclined downward in the normal rotation direction. Propulsion blades are protruded, and each expansion wing has a part on the forward rotation side covered with a part of the other expansion wing on the reverse rotation direction side, and in a state of rotating in the normal rotation direction, all of each expansion wing is accommodated within the outer diameter of the rotary embedded tip enlarged wing pile, and in a state of rotating in the reverse direction, a part of each enlarged blade protrudes outside the outer diameter of the rotary embedded tip enlarged wing pile. It is a buried tip expanded wing pile.

請求項2の発明は、回転埋設先端拡大翼杭の先端側又は拡大翼の表面にストッパーを備えたことを特徴とする、請求項1に記載の回転埋設先端拡大翼杭である。 The invention of claim 2 is the rotary embedded tip enlarged wing pile according to claim 1, characterized in that a stopper is provided on the tip side of the rotary embedded tip enlarged wing pile or on the surface of the enlarged wing.

請求項3の発明は、拡大翼の逆転方向側の一部を外側に折曲げた折曲部としたことを特徴とする、請求項1又は請求項2に記載の回転埋設先端拡大翼杭である。 The invention of claim 3 is the rotating embedded tip expansion wing pile according to claim 1 or claim 2, characterized in that a part of the expansion wing on the reverse direction side is bent outward. be.

本発明の回転埋設先端拡大翼杭によれば、主に次のような効果を奏することができる。 ADVANTAGE OF THE INVENTION According to the rotary embedded tip enlarged wing pile of the present invention, the following effects can be mainly exhibited.

回転埋設先端拡大翼杭本体が、一方向への回転によって地中に所定の深さまで貫入された状態下で、地中への貫入時とは逆の方向に回転させることにより、拡大翼が、杭本体の先端部の外周縁から径方向外側に突出されることから、地中に貫入された回転埋設先端拡大翼杭本体を、地中への貫入時とは逆方向に回転させるだけの極めて簡単な作業を行うだけで、掘削片にて掘削された地中の掘削土に対する杭本体の先端部の接触面積が、杭本体の先端部の外周縁からの回動部材の突出部位の面積分だけ有利に増大する。 Under the state in which the main body of the rotary-buried tip expanded wing pile has been penetrated into the ground to a predetermined depth by rotating in one direction, by rotating in the opposite direction to the time of penetration into the ground, the expanded wing is Since it protrudes radially outward from the outer peripheral edge of the tip of the pile body, the rotating buried tip enlarged wing pile body penetrated into the ground is rotated in the opposite direction to the time of penetration into the ground. By performing simple work, the contact area of the tip of the pile body with the excavated soil excavated by the excavated fragments is the surface area of the protruding part of the rotating member from the outer peripheral edge of the tip of the pile body. increases favorably.

地中への貫入状態下で、外周面摩擦力と、杭本体の先端部での掘削土との接触面積とが、何れも十分な大きさにおいて確保され得て、杭本体の外周面の全体において発揮される支持力と、杭本体の先端部において発揮される先端支持力の両方が、効果的に高められ得ることとなる。そして、その結果として、上部荷重を、より安定的に且つ確実に支持することが可能となり、以て、例えば、住宅等の基礎杭として使用された場合等において、かかる住宅等の不同沈下等の発生を、より一層効果的に防止することができる。しかも、そのような支持力の増大効果を得る上において、面倒な作業が強いられることもない。 Under the state of penetrating into the ground, both the outer peripheral surface frictional force and the contact area between the tip of the pile body and the excavated soil can be secured at a sufficient size, and the entire outer peripheral surface of the pile body can be secured. Both the bearing force exerted at the tip of the pile body and the tip bearing force exerted at the tip of the pile body can be effectively enhanced. As a result, it is possible to more stably and reliably support the upper load, and thus, for example, when used as foundation piles for houses, etc., uneven settlement of such houses, etc. occurrence can be prevented more effectively. Moreover, troublesome work is not forced to obtain such an effect of increasing the supporting force.

回転埋設先端拡大翼杭本体が一方向に回転させられて、地中に貫入せしめられるときに、複数の回動部材(拡大翼)と筒状掘削刃とが、杭本体の先端部の外周縁よりも径方向内側に収容位置し、杭本体の先端部の外周縁からの突出しないように配置されているため、例えば、杭本体の一方向への回転時に、かかる突出部位が地中の石等の障害物に接触し、それによって、当初設定していた杭打ち位置からずれてしまう芯ずれ(水平誤差)が生ずるようなことが、効果的に防止される。 When the rotary-buried tip enlarged wing pile body is rotated in one direction and penetrated into the ground, the plurality of rotating members (enlarging wings) and the cylindrical excavating blades move along the outer peripheral edge of the tip of the pile body. Since it is housed radially inside the pile body and is arranged so as not to protrude from the outer peripheral edge of the tip of the pile body, for example, when the pile body rotates in one direction, such a protruding part will be a stone in the ground. It is possible to effectively prevent misalignment (horizontal error) in which the piling position is shifted from the initially set piling position due to contact with an obstacle such as the piling.

複数の回動部材(拡大翼)が、軸心方向への回動により、回転埋設先端拡大翼杭本体の先端部の外周縁よりも内側に収容されることから、例えば、運搬時等において、複数の回動部材(拡大翼)を、かかる内側への収容位置に配置させておけば、多数のものをまとめて運ぶ際にもかさばるようなことがなく、優れた取扱性が、有利に発揮される。 Since the plurality of rotating members (expansion wings) are accommodated inside the outer peripheral edge of the tip of the rotation-buried tip expansion wing pile body by rotating in the axial direction, for example, during transportation, etc., By arranging a plurality of rotating members (enlarged wings) in such an inwardly accommodated position, it does not become bulky when carrying a large number of items at once, and excellent handleability can be advantageously exhibited. be done.

円筒杭本体と先端板の装着状態を示す斜視図である。It is a perspective view which shows the mounting state of a cylindrical pile main body and a tip plate. 先端板の平面図である。Fig. 2 is a plan view of the tip plate; 筒状掘削刃の側面図である。Fig. 2 is a side view of a tubular digging edge; 筒状掘削刃の底面図である。It is a bottom view of a cylindrical digging edge. 拡大翼を表面側から見た図である。It is the figure which looked at the expansion wing from the surface side. 折曲部を備えた拡大翼を表面側から見た図である。It is the figure which looked at the expansion wing provided with the bending part from the surface side. 回転埋設先端拡大翼杭を先端から見た図である。It is the figure which looked at the rotary buried tip expansion wing pile from the tip. 回転埋設先端拡大翼杭の先端側の拡大翼が縮小した状態の図で、(a)は側面図、(b)は後端側から見た一部透視図である。It is a figure of the state where the expansion wing by the side of the tip of the rotary buried tip expansion wing pile has contracted, (a) is a side view, and (b) is a partially transparent view seen from the rear end side. 回転埋設先端拡大翼杭の先端側の拡大翼が拡大した状態の図で、(a)は側面図、(b)は後端側から見た一部透視図である。It is a figure of the state where the expansion wing of the tip side of the rotary buried tip expansion wing pile was expanded, (a) is a side view, (b) is a partially perspective view seen from the rear end side. 回転埋設先端拡大翼杭を後端側から見た各拡大翼の位置関係を示す一部透視図である。FIG. 4 is a partial perspective view showing the positional relationship of each expansion wing viewed from the rear end side of the rotary-buried tip expansion wing pile.

本発明の回転埋設先端拡大翼杭(以下、単に「杭」とする場合がある。)1は、正転方向Aの回転によって杭1径のまま地盤に埋設し、逆転方向Bの回転によって杭1先端に達する支持層にて拡大翼50が拡大することによって、地盤支持力を増強させることができるものである。 A rotating embedded tip enlarged wing pile (hereinafter, sometimes simply referred to as a "pile") 1 of the present invention is embedded in the ground with a pile diameter of 1 by rotating in the forward rotation direction A, and by rotating in the reverse direction B, the pile By expanding the expanding wings 50 at the support layer reaching one tip, the ground bearing capacity can be enhanced.

具体的には、地盤の杭1打ち箇所において、軸回りの一方向をなす正転方向Aの回転によって、筒状掘削刃30による地盤掘削で杭1径の外径1оの幅のまま地中に貫入し、所望の地盤まで貫入埋設されたら、軸回りの反対方向をなす逆転方向Bの回転によって突出する拡大翼50により、杭1と地盤の間に先端支持力、摩擦力(外周面摩擦力、内周面摩擦力)、水平垂直力が働くことにより、地盤、特に軟弱地盤等における杭工事に強固に対応するための回転埋設先端拡大翼杭1を提供する。 Specifically, at a place where one pile is driven in the ground, by rotating in the forward rotation direction A that forms one direction around the axis, the cylindrical excavation blade 30 excavates the ground while maintaining the width of the outer diameter 1o of the pile 1 diameter. When it is penetrated and embedded to the desired ground, the tip support force and frictional force (outer peripheral surface friction Provided is a rotating buried tip expanded wing pile 1 for firmly coping with pile work in the ground, especially in soft ground, etc., by the action of horizontal and vertical forces.

各図で図示するように、本発明の回転埋設先端拡大翼杭1は、円筒杭本体10、先端板20、筒状掘削刃30、回動連結具40、推進翼60が突設された拡大翼50等が組み合わさって構成されている。以下、本発明である回転埋設先端拡大翼杭1の各実施形態について説明する。 As shown in each figure, the rotating embedded tip enlarged wing pile 1 of the present invention includes a cylindrical pile body 10, a tip plate 20, a tubular excavating blade 30, a rotary connector 40, and a propelling blade 60. Wings 50 and the like are combined together. Hereinafter, each embodiment of the rotating embedded tip enlarged wing pile 1 of the present invention will be described.

円筒杭本体10は、内部に空洞13を備えた長尺な円筒状の筒体である。円筒杭本体10としては、鋼管杭が挙げられるが、その他、PC杭(プレストレストコンクリート杭)、PHC杭(高強度プレストレストコンクリート杭)、PRC杭(プレストレスト鉄筋コンクリート杭)、SC杭(外殻鋼管付きコンクリート杭)等のコンクリート杭であってもよい。また、単杭であっても継ぎ杭であってもよい。また、円筒杭本体10の長さ、内径、外径等も問わない。 The cylindrical pile main body 10 is a long cylindrical tubular body having a cavity 13 inside. As the cylindrical pile body 10, a steel pipe pile can be mentioned, but in addition, PC pile (prestressed concrete pile), PHC pile (high strength prestressed concrete pile), PRC pile (prestressed reinforced concrete pile), SC pile (concrete with outer shell steel pipe) piles) and other concrete piles. Moreover, it may be a single pile or a joint pile. Moreover, the length, inner diameter, outer diameter, etc. of the cylindrical pile main body 10 are not limited.

円筒杭本体10の先端側Xには、先端板20が備わる(図1参照)。この先端板20は、中心位置に穴22が穿設された円盤状の部材(鋼材円板)で、円筒杭本体10の外径10оに合致した外径20оを備え、円筒杭本体10の先端面11に溶接等によって取り付けられる。円筒杭本体10の空洞13と先端板20の穴22は連通することとなる。 A tip plate 20 is provided on the tip side X of the cylindrical pile body 10 (see FIG. 1). This tip plate 20 is a disc-shaped member (steel disc) with a hole 22 drilled at the center position, and has an outer diameter 20 о that matches the outer diameter 10 о of the cylindrical pile body 10, and the tip of the cylindrical pile body 10 It is attached to the surface 11 by welding or the like. The cavity 13 of the cylindrical pile body 10 and the hole 22 of the tip plate 20 are communicated.

先端板20の外径20оと円筒杭本体10の外径10оは同径又は略同径が望ましいが、先端板20の外径20оが円筒杭本体10の外径10оよりも小径であってもよく、したがって、例えば、先端板20を円筒杭本体10の空洞13内(内壁面)に固設する構成であってもよい。 The outer diameter 20' of the tip plate 20 and the outer diameter 10' of the cylindrical pile body 10 are preferably the same or substantially the same, but even if the outer diameter 20' of the tip plate 20 is smaller than the outer diameter 10' of the cylindrical pile body 10 Well, therefore, for example, the structure which fixes the tip plate 20 in the cavity 13 (inner wall surface) of the cylindrical pile main body 10 may be sufficient.

円筒杭本体10と先端板20が別部材で円筒杭本体10の先端面11に先端板20が固設される構成の他、円筒杭本体10と先端板20が一体成形される構成であってもよい。また、筒状掘削刃30や拡大翼50が円筒杭本体10の先端面11に備えることができれば、先端板20を備えない構成であってもよい。 In addition to the configuration in which the cylindrical pile body 10 and the tip plate 20 are separate members and the tip plate 20 is fixed to the tip surface 11 of the cylindrical pile body 10, the cylindrical pile body 10 and the tip plate 20 are integrally molded. good too. Further, if the tubular excavating edge 30 and the expanding wing 50 can be provided on the tip surface 11 of the cylindrical pile main body 10, the tip plate 20 may not be provided.

先端板20の材質は、鋼材製等の耐久性が高いものであればどのような材質であってもよい。また、肉厚、穴の内径等も問わない。 The material of the tip plate 20 may be any material, such as steel, as long as it has high durability. Moreover, the wall thickness, the inner diameter of the hole, etc. are not limited.

円筒杭本体10の先端側X軸心には、筒状掘削刃30が備えられている。具体的には、先端板20の表面21軸心から筒状掘削刃30が立設する構成である。なお、筒状掘削刃30は先端板20を介して備える他、上述のように、先端板20を介さずに円筒杭本体10の先端面11軸心から直接筒状掘削刃30が立設してもよい。 A cylindrical excavating edge 30 is provided at the tip side X-axis center of the cylindrical pile main body 10 . Specifically, the cylindrical digging blade 30 is erected from the axis of the surface 21 of the tip plate 20 . The cylindrical excavating blade 30 is provided via the tip plate 20, and as described above, the cylindrical excavating blade 30 is erected directly from the axis of the tip surface 11 of the cylindrical pile body 10 without the tip plate 20 interposed therebetween. may

この筒状掘削刃30は、図3等で図示するように、先端に鋸刃形状の刃部33を備え、内部に空洞39を備えた筒体で、本体31と本体上方の刃部33に分けることができ、主に刃部33によって地盤を掘削するものである。各図では円筒状の筒体で説明している。 As shown in FIG. 3 and the like, this tubular excavating blade 30 is a tubular body having a sawtooth-shaped blade portion 33 at its tip and a cavity 39 inside. It can be divided into two parts, and excavates the ground mainly by the blade portion 33 . In each figure, a cylindrical cylinder is used for explanation.

刃部33は複数の山形状の山刃部37、谷形状の谷刃部38が組み合わさって構成されている。刃部33の形状、構成は山刃部37、谷刃部38が繰り返し組み合わさって構成されていればどのようなものであってもよい。したがって、山刃部37の高さ、谷刃部38の深さ、数、角度、形状等も問わないため、各山刃部37の高さが略同じであっても段違いであってもよい。また、図示しないが、山刃部37、谷刃部38をさらに鋸刃形状としてもよい。 The blade portion 33 is configured by combining a plurality of mountain-shaped peak blade portions 37 and valley-shaped valley blade portions 38 . The blade portion 33 may have any shape and configuration as long as the blade portion 37 and the valley blade portion 38 are repeatedly combined. Therefore, since the height of the mountain edge portions 37 and the depth, number, angle, shape, etc. of the valley edge portions 38 do not matter, the height of each mountain edge portion 37 may be substantially the same or uneven. . Moreover, although not shown, the ridge portion 37 and the trough portion 38 may be formed in a serrated shape.

筒状掘削刃30(本体31)は、先端板20の穴22の内径20iに略合致した内径30iを備えており、先端板20の穴22の縁(表面21)に筒状掘削刃30(本体31)が溶接等によって取り付けられている。円筒杭本体10の空洞13と先端板20の穴22と筒状掘削刃30の空洞39は連通することとなる。 The tubular digging blade 30 (main body 31) has an inner diameter 30i that substantially matches the inner diameter 20i of the hole 22 of the tip plate 20, and the tubular digging blade 30 (main body 31) is attached to the edge (surface 21) of the hole 22 of the tip plate 20. A main body 31) is attached by welding or the like. The cavity 13 of the cylindrical pile body 10, the hole 22 of the tip plate 20 and the cavity 39 of the tubular excavating blade 30 are communicated.

先端板20の穴22の内径20iと筒状掘削刃30(本体31)の空洞39の内径30iは同径又は略同径が望ましいが、筒状掘削刃30の空洞39の内径30iが先端板20の穴22の内径20iよりも大径であってもよい。また、筒状掘削刃30の空洞39の内径30iが先端板20の穴22の内径20iよりも小径であってもよい。したがって、例えば、筒状掘削刃30(本体31の外周35)を先端板20の穴22内(内壁面)に固設する構成であってもよい。 The inner diameter 20i of the hole 22 of the tip plate 20 and the inner diameter 30i of the cavity 39 of the tubular digging blade 30 (main body 31) are preferably the same or substantially the same diameter, but the inner diameter 30i of the cavity 39 of the tubular digging blade 30 is larger than the tip plate. It may be larger than the inner diameter 20i of the hole 22 of 20 . Also, the inner diameter 30i of the cavity 39 of the tubular digging blade 30 may be smaller than the inner diameter 20i of the hole 22 of the tip plate 20 . Therefore, for example, the tubular digging blade 30 (the outer periphery 35 of the main body 31) may be fixed inside the hole 22 (inner wall surface) of the tip plate 20. As shown in FIG.

筒状掘削刃30と先端板20が別部材で先端板20の表面21に筒状掘削刃30が固設される構成の他、筒状掘削刃30と先端板20が一体成形される構成であってもよい。 In addition to the configuration in which the tubular excavation blade 30 and the tip plate 20 are separate members and the tubular excavation blade 30 is fixed to the surface 21 of the tip plate 20, there is also a configuration in which the tubular excavation blade 30 and the tip plate 20 are integrally formed. There may be.

筒状掘削刃30の材質は、鋼材製等の掘削性や耐久性が高いものであればどのような材質であってもよい。また、長さ、内径、外径等も問わない。筒状掘削刃30は、各図で図示したような円筒状の他、図示しないが三角状、四角状、五角形状、六角形状等の多角形状であってもよい。なお、筒状掘削刃30の形状に合わせて、拡大翼50の数、形状等が適応される。 The cylindrical excavating blade 30 may be made of any material such as steel, as long as it has high excavating properties and durability. Also, the length, inner diameter, outer diameter, etc. are not limited. The cylindrical excavating blade 30 may have a cylindrical shape as shown in each drawing, or may have a polygonal shape such as a triangular, quadrangular, pentagonal, or hexagonal shape (not shown). The number, shape, etc. of the expanding blades 50 are adapted according to the shape of the tubular excavating blade 30 .

円筒杭本体10の先端側Xには、推進翼60が突設された拡大翼50が回動自在に配設されている。この拡大翼50は、筒状掘削刃30の外周35に沿って回動連結具40を介して回動自在に軸支されており、正転方向Aへの回転では縮小状態(図7、図8(b)参照)に、逆転方向Bへの回転では拡大状態(図9(b)参照)となる。 On the tip end side X of the cylindrical pile body 10, an enlarged wing 50 having a propulsion wing 60 is rotatably arranged. The expanding blade 50 is rotatably supported along the outer circumference 35 of the cylindrical digging blade 30 via a rotary coupling 40, and is contracted when rotated in the forward rotation direction A (FIGS. 7 and 8). 8(b)), and the rotation in the reverse direction B results in an enlarged state (see FIG. 9(b)).

拡大翼50は、所定の肉厚を備えた湾曲状の鋼板である。各拡大翼50の形状は、各拡大翼50が縮小状態のときに各拡大翼50全体で筒状掘削刃30の外周35を囲繞、換言すれば、筒状掘削刃30の本体31を包み込むようにできればどのような形状であってもよく、図5等で図示した形状以外であってもよい。また、図示しないが、各拡大翼50は、正転方向側50fの角部分、端面又は逆転方向側50rの角部分、端面を面取りしてもよい。このような面取りを行うことにより、各拡大翼50が引っ掛かることなくスムーズに拡大又は縮小することができる。 The expansion wing 50 is a curved steel plate with a predetermined thickness. The shape of each expansion wing 50 is such that when each expansion wing 50 is contracted, the entire expansion wing 50 surrounds the outer circumference 35 of the tubular excavating blade 30 , in other words, wraps around the main body 31 of the tubular excavating blade 30 . Any shape may be used as long as it is possible, and shapes other than those illustrated in FIG. 5 and the like may be used. Although not shown, each enlarging wing 50 may be chamfered at the corners and end faces of the forward rotation side 50f or at the corners and end faces of the reverse rotation direction side 50r. By performing such chamfering, each expansion wing 50 can be expanded or contracted smoothly without being caught.

拡大翼50は複数枚で配設構成されている。図7等では、四枚、具体的には、第一の拡大翼51、第二の拡大翼52、第三の拡大翼53、第四の拡大翼54で配置構成されているが、拡大翼50は二枚、三枚、または五枚以上であってもよい。安定度からすれば、三枚以上が杭1の先端5にかかる安定力が増加するため望ましい。なお、配置構成される拡大翼50の枚数によっては、各拡大翼50の長手方向の長さが異なることは勿論である。本実施形態ではより望ましい四枚の例で説明する。 The enlarging wings 50 are arranged in plural. In FIG. 7 and the like, four expansion wings, specifically, a first expansion wing 51, a second expansion wing 52, a third expansion wing 53, and a fourth expansion wing 54, are arranged. 50 may be two, three, or five or more. In terms of stability, three or more piles are desirable because the stabilizing force applied to the tip 5 of the pile 1 increases. It goes without saying that the length of each expansion wing 50 in the longitudinal direction differs depending on the number of expansion wings 50 arranged. In the present embodiment, a more desirable example of four sheets will be described.

第一の拡大翼51乃至第四の拡大翼54は、筒状掘削刃30の外周35(先端板20の外周)に沿って等間隔で配置されている。図7では、第一の拡大翼51と第三の拡大翼53が対角線上に配置され、第二の拡大翼52と第四の拡大翼54が対角線上に配置されている。 The first to fourth expansion wings 51 to 54 are arranged at equal intervals along the outer circumference 35 of the tubular digging edge 30 (the outer circumference of the tip plate 20). In FIG. 7, the first expansion wing 51 and the third expansion wing 53 are arranged diagonally, and the second expansion wing 52 and the fourth expansion wing 54 are arranged diagonally.

第一の推進翼61の逆転方向側51rの端部から第三の推進翼63の逆転方向側53rの端部を結ぶ仮想線C1と、第二の推進翼62の逆転方向側52rの端部から第四の推進翼64の逆転方向側54rの端部を結ぶ仮想線C2によって十字を形成する(図10参照)。このように、第一の拡大翼51乃至第四の拡大翼54はバランス良く均等に配置構成されるのが望ましい。 An imaginary line C1 connecting the end of the reverse direction side 51r of the first propeller blade 61 to the end of the reverse direction side 53r of the third propeller blade 63, and the end of the reverse direction side 52r of the second propeller blade 62 to the end of the reverse direction side 54r of the fourth propeller blade 64 to form a cross (see FIG. 10). In this way, it is desirable that the first to fourth expansion wings 51 to 54 are evenly arranged in a well-balanced manner.

回転埋設先端拡大翼杭1が地中に貫入する際の各拡大翼50が縮小した状態では、各拡大翼50同士が一部重なって配置、すなわち、各拡大翼50は、正転方向側50fの一部が他の拡大翼50の逆転方向側50rの一部で被覆される。具体的には、回転埋設先端拡大翼杭1を先端5から見た図7によれば、第一の拡大翼51の正転方向側51fの一部が第四の拡大翼54の逆転方向側54rで被覆され、第二の拡大翼52の正転方向側52fの一部が第一の拡大翼51の逆転方向側51rで被覆され、第三の拡大翼53の正転方向側53fの一部が第二の拡大翼52の逆向方向側rで被覆され、第四の拡大翼54の正転方向側54fの一部が第三の拡大翼53の逆転方向側53rで被覆される。このように、一部重なり合う第一の拡大翼51乃至第四の拡大翼54が風車状に配置される。 In the contracted state of the expansion wings 50 when the rotary-buried tip expansion wing pile 1 penetrates into the ground, the expansion wings 50 are partially overlapped with each other. is covered with a part of the reverse direction side 50r of the other expanding wing 50. As shown in FIG. Specifically, according to FIG. 7 , which is a view of the rotary-buried tip expansion wing pile 1 viewed from the tip 5 , a part of the forward rotation direction side 51 f of the first expansion wing 51 is the reverse rotation direction side of the fourth expansion wing 54 . A portion of the forward rotation side 52f of the second expansion wing 52 is covered with the reverse rotation side 51r of the first expansion wing 51, and a part of the forward rotation side 53f of the third expansion wing 53 is covered with A part of the forward rotation side 54 f of the fourth expansion wing 54 is covered with the reverse rotation side 53 r of the third expansion wing 53 . In this manner, the first to fourth expanding blades 51 to 54 that are partially overlapped are arranged like a windmill.

また、各拡大翼50が縮小状態では、第一の拡大翼51乃至第四の拡大翼54は、筒状掘削刃30に凭れ掛るように傾斜状態で支持される。拡大翼50の上端50tが筒状掘削刃30の外周35に当接又は対峙した状態となる。具体的には、第一の拡大翼51の上端51tが筒状掘削刃30の外周35の一部に当接又は対峙し、第二の拡大翼52の上端52tが筒状掘削刃30の外周35の一部に当接又は対峙し、第三の拡大翼53の上端53tが筒状掘削刃30の外周35の一部に当接又は対峙し、第四の拡大翼54の上端54tが筒状掘削刃30の外周35の一部に当接又は対峙する。このように、拡大翼50の上端50tが筒状掘削刃30の外周35に当接又は対峙した位置が拡大翼50の最縮小の範囲となる。各拡大翼50が縮小した状態では、各拡大翼50は杭1径の外径1оの幅内に収められ、杭1径の外径1оよりも外に出ることはない。 Further, when each expansion wing 50 is contracted, the first expansion wing 51 to the fourth expansion wing 54 are supported in an inclined state so as to lean against the cylindrical digging blade 30 . The upper end 50t of the expanding wing 50 comes into contact with or faces the outer circumference 35 of the tubular digging blade 30. As shown in FIG. Specifically, the upper end 51t of the first expanding wing 51 abuts or faces a part of the outer circumference 35 of the tubular excavating blade 30, and the upper end 52t of the second expanding wing 52 35, the upper end 53t of the third enlarging wing 53 abuts or faces a part of the outer circumference 35 of the tubular digging blade 30, and the upper end 54t of the fourth enlarging wing 54 is in contact with or confronting a part of the outer circumference 35 of the tubular excavating blade 30. abuts or faces a portion of the outer circumference 35 of the shaped digging edge 30 . Thus, the position where the upper end 50t of the expanding wing 50 abuts or faces the outer circumference 35 of the tubular digging blade 30 is the range in which the expanding wing 50 is contracted the most. When each expansion wing 50 is contracted, each expansion wing 50 is accommodated within the width of the outer diameter 1o of the pile 1 diameter and does not protrude beyond the outer diameter 1o of the pile 1 diameter.

拡大翼50は全体的に内側に湾曲しているが、逆転方向側50rの一部を外側に折曲げた折曲部50zとしてもよい(図6参照)。拡大翼50に折曲部50zを形成することによって、各拡大翼50が縮小した状態では、拡大翼50と拡大翼50との間にはスペースが介在することとなる。具体的には、第一の拡大翼51の折曲部51zと第二の拡大翼52の正転方向側52fにはスペースが介在し、第二の拡大翼52の折曲部52zと第三の拡大翼53の正転方向側53fにはスペースが介在し、第三の拡大翼53の折曲部53zと第四の拡大翼54の正転方向側54fにはスペースが介在し、第四の拡大翼54の折曲部54zと第一の拡大翼51の正転方向側51fにはスペースが介在する。回転埋設先端拡大翼杭1を逆転方向Bに回転する際においては、これらの各スペースから地盤(掘削土)が入り込むことによって拡大翼50を押し広げることができるため、より少ない力で拡大翼50を拡大させることができる。 Although the enlarging wing 50 is curved inward as a whole, it may be a bent portion 50z in which a part of the reverse direction side 50r is bent outward (see FIG. 6). By forming the bent portion 50z in the expansion wings 50, a space is interposed between the expansion wings 50 when the expansion wings 50 are contracted. Specifically, a space is provided between the bent portion 51z of the first expansion wing 51 and the forward rotation direction side 52f of the second expansion wing 52, and the bent portion 52z of the second expansion wing 52 and the third expansion wing 52 are separated from each other. A space is interposed on the forward rotation direction side 53f of the expansion wing 53, and a space is interposed between the bent portion 53z of the third expansion wing 53 and the forward rotation direction side 54f of the fourth expansion wing 54. A space is interposed between the bent portion 54z of the expanding blade 54 and the forward rotation direction side 51f of the first expanding blade 51 . When rotating the rotary-buried tip expanding wing pile 1 in the reverse direction B, the expanding wing 50 can be expanded by the ground (excavated soil) entering from each of these spaces, so that the expanding wing 50 can be expanded with less force. can be expanded.

各拡大翼50の表面50aには平面視弧状(略三日月状)で形成される推進翼60が突設されている。具体的には、第一の拡大翼51の表面51aには第一の推進翼61が突設され、第二の拡大翼52の表面52aには第二の推進翼62が突設され、第三の拡大翼53の表面53aには第三の推進翼63が突設され、第四の拡大翼54の表面54aには第四の推進翼64が突設されている。推進翼60は、平面視弧状(略三日月状)以外の形状でもよく、地盤に対する杭1の貫入性や推進性を考慮して各図で図示した形状とは異なる形状を選択することもできる。 A propulsion wing 60 formed in an arc shape (substantially crescent shape) in plan view protrudes from the surface 50a of each expansion wing 50 . Specifically, a first propeller wing 61 protrudes from the surface 51a of the first expansion wing 51, and a second propeller wing 62 protrudes from the surface 52a of the second expansion wing 52. A surface 53a of the third expanding wing 53 is provided with a third propelling blade 63, and a surface 54a of the fourth expanding wing 54 is provided with a fourth propelling blade 64. As shown in FIG. The propulsion blade 60 may have a shape other than an arc shape (substantially crescent shape) in a plan view, and a shape different from the shape shown in each figure may be selected in consideration of the penetrability and propelability of the pile 1 with respect to the ground.

拡大翼50に備えた推進翼60には第一作用面60a、第一作用面60aの裏側に第二作用面60bを備える。具体的には、第一の拡大翼51に備えた第一の推進翼61には第一作用面61a、第一作用面61aの裏側に第二作用面61bを備える。第二の拡大翼52に備えた第二の推進翼62には第一作用面62a、第一作用面62aの裏側に第二作用面62bを備える。第三の拡大翼53に備えた第三の推進翼63には第一作用面63a、第一作用面63aの裏側に第二作用面63bを備える。第四の拡大翼54に備えた第四の推進翼64には第一作用面64a、第一作用面64aの裏側に第二作用面64bを備える。なお、推進翼60は、回転埋設先端拡大翼杭1の正転方向Aへの回転又は逆転方向Bへの回転を推進させることができれば、長手方向の長さや短手方向の高さ等は問わない。 The propulsion blade 60 provided in the expansion wing 50 has a first working surface 60a and a second working surface 60b behind the first working surface 60a. Specifically, the first propulsion wing 61 provided in the first expanding wing 51 has a first working surface 61a, and the second working surface 61b is provided on the back side of the first working surface 61a. The second propulsion wings 62 provided in the second expansion wings 52 are provided with a first working surface 62a and a second working surface 62b behind the first working surface 62a. A third propulsion wing 63 provided in the third expanding wing 53 has a first working surface 63a and a second working surface 63b behind the first working surface 63a. A fourth propulsion wing 64 provided on the fourth expanding wing 54 has a first working surface 64a and a second working surface 64b behind the first working surface 64a. The propulsion blade 60 may have any length in the longitudinal direction or height in the width direction, as long as it can propel the rotation of the rotary embedded tip enlarged wing pile 1 in the forward rotation direction A or in the reverse rotation direction B. do not have.

推進翼60は、拡大翼50の表面50aに溶接等により固設されており、拡大翼50の表面50aに対して垂直に設けてもよく、また、傾斜して設けてもよい。 The propeller blades 60 are fixed to the surface 50a of the expansion wing 50 by welding or the like, and may be provided perpendicular to the surface 50a of the expansion wing 50, or may be provided at an angle.

推進翼60の配置角度、向き等については、図5、図6で図示したように、拡大翼50に対して軸回りの一方向をなす正転方向側60fが下となるように傾斜、具体的には、水平に対して例えば、20°から60°、概ね30°や45°下に向かって傾斜させるのが望ましい。なお、推進翼60は、回転埋設先端拡大翼杭1の正転方向Aへの回転又は逆転方向Bへの回転を推進させることができれば配置角度等については問わない。 As shown in FIGS. 5 and 6, the propulsion blades 60 are inclined so that the forward rotation direction side 60f forming one direction around the axis of the expansion blades 50 is downward. Practically, it is desirable to incline downward from the horizontal by, for example, 20° to 60°, generally 30° or 45°. In addition, if the propeller blade 60 can propel the rotation in the forward rotation direction A or the rotation in the reverse rotation direction B of the rotationally buried tip enlarged wing pile 1, the arrangement angle and the like do not matter.

各拡大翼50が縮小した状態で全体として第一の推進翼61乃至第四の推進翼64を回転埋設先端拡大翼杭1の先端5から見ると螺旋状をなすように配置される。また、各拡大翼50の表面50aから各推進翼60が鍔状に突出しているが、第一の推進翼61乃至第四の推進翼64は回転埋設先端拡大翼杭1の杭1径(外径1о)より突出せず杭1径内(外径1о内)に収まる構成となっている。 The first propeller blades 61 to the fourth propeller blades 64 as a whole are arranged in a helical shape when viewed from the tip end 5 of the rotating embedded tip expander pile 1 in a state where each expansion blade 50 is contracted. Each propelling blade 60 protrudes like a flange from the surface 50 a of each expanding blade 50 . It is configured so that it does not protrude from the diameter 1o) and fits within 1 diameter of the pile (within 1o outside diameter).

各拡大翼50が縮小した状態で回転埋設先端拡大翼杭1を側面視した場合、各推進翼60の位置関係については、同じ位置であっても、異なる位置であってもよい。すなわち、第一の拡大翼51乃至第四の拡大翼54が全て同じ位置であってもよい。また、第一の拡大翼51に備えた第一の推進翼61よりも第二の拡大翼52に備えた第二の推進翼62のほうが高くてもよく、第三の拡大翼53に備えた第三の推進翼63よりも第四の拡大翼54に備えた第四の推進翼64のほうが高くてもよい。 When the rotating embedded leading end expanding wing pile 1 is viewed from the side with the expanding wings 50 contracted, the positional relationship of the propelling wings 60 may be the same or different. That is, the first to fourth expansion wings 51 to 54 may all be in the same position. Further, the second propelling wings 62 provided on the second expanding wings 52 may be higher than the first propelling wings 61 provided on the first expanding wings 51, and the third propelling wings provided on the third expanding wings 53 may be higher. The fourth propelling wings 64 provided on the fourth expanding wings 54 may be higher than the third propelling wings 63 .

推進翼60の材質は、鋼材製等掘削性や耐久性が高いものであればどのような材質であってもよい。また、拡大翼50と推進翼60が別部材で拡大翼50の表面50aに推進翼60が固設される構成の他、拡大翼50と推進翼60が一体成形される構成であってもよい。 The material of the propulsion blades 60 may be any material such as steel, as long as it has high excavability and durability. In addition to the configuration in which the expansion wing 50 and the propelling wing 60 are separate members and the propelling wing 60 is fixed to the surface 50a of the expanding wing 50, the expansion wing 50 and the propelling wing 60 may be integrally molded. .

このように、各拡大翼50が縮小した状態においては、回転埋設先端拡大翼杭1の先端5の第一の拡大翼51乃至第四の拡大翼54が風車状に配置され、また、第一の推進翼61乃至第四の推進翼64が螺旋状に配置されることとなる(図7参照)。 In this way, in the state in which each expansion blade 50 is contracted, the first expansion blade 51 to the fourth expansion blade 54 at the tip 5 of the rotating embedded tip expansion blade pile 1 are arranged in a windmill shape, and the first 61 to 64 are spirally arranged (see FIG. 7).

回転埋設先端拡大翼杭1の先端側Xには回動連結具40を介して拡大翼50が連結されている。具体的には、拡大翼50は、回動連結具40の支軸48を支点として拡大方向(外径方向OD)に拡大し、また、回動連結具40の支軸48を支点として縮小方向(軸心方向AX)に縮小する。 An enlarged wing 50 is connected to the tip end side X of the rotating embedded tip enlarged wing pile 1 via a rotary connector 40 . Specifically, the expansion wing 50 expands in the expansion direction (outer diameter direction OD) with the support shaft 48 of the rotation coupling 40 as the fulcrum, and also expands in the contraction direction with the support shaft 48 of the rotation coupling 40 as the fulcrum. (Axial direction AX).

この回動連結具40は、拡大翼50が回動自在に連結されていればどのような構成であってもよい。したがって、耐久性に問題がなければヒンジ、丁番等の連結部材を使用してもよい。以下、回動連結具40の実施形態の一例を説明する。 The rotary connector 40 may have any structure as long as the expansion wings 50 are rotatably connected. Therefore, connecting members such as hinges and hinges may be used as long as there is no problem in durability. An example of an embodiment of the pivotal coupling 40 will be described below.

筒状掘削刃30の下方の外周35からリブ41が突設する。このリブ41は、一枚の拡大翼50に対して何本でもよい。したがって、図8(b)や図9(b)のように一枚の拡大翼50に対して二本でもよく、また、図示しないが、一本、又は三本以上の複数本であってもよい。各リブ41の先端側には支軸48を挿通するための穴を穿設している。 A rib 41 protrudes from the lower outer circumference 35 of the tubular digging edge 30 . Any number of ribs 41 may be provided for one enlarged wing 50 . Therefore, as shown in FIG. 8(b) or FIG. 9(b), one expanding wing 50 may be provided with two, or although not shown, may be provided with one or a plurality of three or more. good. A hole for inserting a support shaft 48 is bored in the tip side of each rib 41 .

一方、拡大翼50の裏面50b、具体的には、第一の拡大翼51の裏面51b、第二の拡大翼52の裏面52b、第三の拡大翼53の裏面53b、第四の拡大翼54の裏面54bにはリブ46を固設する。これらのリブ46の固設については、第一の拡大翼51の裏面51b、第二の拡大翼52の裏面52b、第三の拡大翼53の裏面53b、第四の拡大翼54の裏面54bにベース49を設け、リブ46の一端側をこのベース49に固設する構成であってもよい。各リブ46の先端側には支軸48を挿通するための穴を穿設している。 On the other hand, the rear surface 50b of the expansion wing 50, specifically, the rear surface 51b of the first expansion wing 51, the rear surface 52b of the second expansion wing 52, the rear surface 53b of the third expansion wing 53, and the fourth expansion wing 54 A rib 46 is fixed on the rear surface 54b of the . These ribs 46 are fixed to the rear surface 51b of the first expansion wing 51, the rear surface 52b of the second expansion wing 52, the rear surface 53b of the third expansion wing 53, and the rear surface 54b of the fourth expansion wing 54. A configuration in which a base 49 is provided and one end side of the rib 46 is fixed to this base 49 may be employed. A hole for inserting a support shaft 48 is drilled in the tip side of each rib 46 .

拡大翼50の裏面50bに固設したリブ46の穴と筒状掘削刃30から突設したリブ41の穴を合わせ、両穴に支軸48を挿通することによって、支軸48を支点として拡大翼50が回動可能となる。支軸48は、どのような構成のものであってもよい。例えば、強化ボルト、超硬ボルト等を使用してもよい。ボルトに関しては、有効ネジ溝がない半ネジを使用するのが望ましい。 The hole of the rib 46 fixed to the back surface 50b of the enlarging wing 50 is aligned with the hole of the rib 41 protruding from the cylindrical digging blade 30, and by inserting the support shaft 48 into both holes, the expansion is performed using the support shaft 48 as a fulcrum. The wing 50 becomes rotatable. The support shaft 48 may have any configuration. For example, reinforced bolts, cemented carbide bolts, etc. may be used. As for the bolts, it is desirable to use a half thread that does not have an effective thread.

他の構成としては、図示しないが、例えば、拡大翼50の裏面50bに、支軸48を挿通するための穴を穿設した第一挟持板及び第二挟持板を併設し、第一挟持板と第二挟持板の間に拡大翼50の裏面50bに固設したリブ46を配置し、拡大翼50に固設したリブの穴と第一挟持板及び第二挟持板の穴を合わせ、各穴に支軸48を挿通することによって、支軸48を支点として拡大翼50が回動自在となる構成が挙げられる。 As another configuration (not shown), for example, a first clamping plate and a second clamping plate having a hole for inserting the support shaft 48 are provided on the rear surface 50b of the expansion wing 50, and the first clamping plate The rib 46 fixed to the rear surface 50b of the expanding wing 50 is arranged between the and second holding plate, the hole of the rib fixed to the expanding wing 50 is aligned with the hole of the first holding plate and the second holding plate, and each hole is By inserting the support shaft 48, the expansion wing 50 can rotate freely with the support shaft 48 as a fulcrum.

このように、拡大翼50は回動連結具40を介して、具体的には、回動連結具40の支軸48により回動自在に軸支されている。すなわち、正転方向Aに回転する状態では、拡大翼50が軸心方向AX、すなわち、筒状掘削刃30に向かって回動することによって、拡大翼50の全てが杭1の外径1о内に収容された状態とされ、逆転方向Bに回転する状態では、拡大翼50が杭1の外径1о方向に回動することによって、拡大翼50の一部が杭1の外径1о外に突出した状態とされる。なお、拡大翼50が拡大状態の場合、図9(b)のように、拡大翼50の一部が他の拡大翼50の一部と重なり合う場合もあるが、重なり合わない構成としてもよい。 In this manner, the expanding wing 50 is rotatably supported via the pivotal connector 40 , specifically, by the support shaft 48 of the pivotal connector 40 . That is, when rotating in the forward rotation direction A, the expanding blade 50 rotates in the axial direction AX, that is, toward the cylindrical excavating blade 30, so that the expanding blade 50 is entirely within the outer diameter 1o of the pile 1. In the state of rotating in the reverse direction B, the expansion wing 50 rotates in the direction of the outer diameter 1o of the pile 1, so that a part of the expansion wing 50 moves outside the outer diameter 1o of the pile 1. It is in a protruded state. When the expansion wing 50 is in the expanded state, a part of the expansion wing 50 may overlap with a part of the other expansion wing 50 as shown in FIG. 9(b).

軸回りの反対方向をなす逆転方向Bの回転によって拡大した拡大翼50の表面50aが円筒杭本体10の先端面11等に当接することによって、この先端面11等がストッパーの役目を有することとなる。したがって、ストッパーで止まる位置が拡大翼50の最大拡大範囲となる。 The surface 50a of the enlarging wing 50, which is enlarged by the rotation in the reverse direction B which is the opposite direction around the axis, abuts against the tip surface 11 of the cylindrical pile body 10, etc., and the tip surface 11, etc. serve as a stopper. Become. Therefore, the maximum expansion range of the expansion wings 50 is the position where the stopper stops.

ストッパーとしては、例えば、円筒杭本体10の先端外周縁を突環状部12とし、この突環状部12をストッパーとすることができる。具体的には、円筒杭本体10の空洞13内に先端板20を備える構成によれば、円筒杭本体10の先端外周縁に突環状部12が形成される。突環状部12の高さは問わない。したがって、突環状部12の高さによって拡大翼50の開く角度を調節することができる。 As a stopper, for example, the tip outer peripheral edge of the cylindrical pile main body 10 can be used as a projecting annular portion 12, and this projecting annular portion 12 can be used as a stopper. Specifically, according to the configuration in which the tip plate 20 is provided in the cavity 13 of the cylindrical pile main body 10 , the projecting annular portion 12 is formed at the tip outer peripheral edge of the cylindrical pile main body 10 . The height of the projecting annular portion 12 does not matter. Therefore, the opening angle of the expanding wings 50 can be adjusted by the height of the projecting annular portion 12 .

その他、拡大翼50の表面50aに別途ストッパー(不図示)を設けてもよい。具体的には、ストッパーを拡大翼50の表面50aに溶接等により固設されることによって拡大翼50の表面50aから突設する。ストッパーの形状、長さ、高さ等は問わない。したがって、ストッパーの高さによって拡大翼50の開く角度を調節することができる。 In addition, a separate stopper (not shown) may be provided on the surface 50a of the expanding wing 50. FIG. Specifically, the stopper is fixed to the surface 50a of the expansion wing 50 by welding or the like so as to protrude from the surface 50a of the expansion wing 50 . The shape, length, height, etc. of the stopper do not matter. Therefore, the opening angle of the expanding wings 50 can be adjusted by adjusting the height of the stopper.

また、筒状掘削刃30の外周35、具体的には、拡大翼50の上端50tが当たる位置にストッパーを設けてもよい。このストッパーを設けることによって拡大翼50の最縮小の範囲を調節することができる。 Further, a stopper may be provided at the outer circumference 35 of the tubular digging blade 30, specifically at a position where the upper end 50t of the expansion wing 50 abuts. By providing this stopper, it is possible to adjust the minimum contraction range of the expansion wings 50 .

本発明の回転埋設先端拡大翼杭1に使用方法の一例について説明する。まず、回転埋設先端拡大翼杭1を貫入する地盤の掘削箇所において、所定の施工機械等(不図示)を用いて、回転埋設先端拡大翼杭1の先端5を下側にした状態で地盤上に直立させる。なお、杭1の打ち込み位置を出すためには、主に筒状の先端支持具(不図示)を用いて行われる。具体的には、打ち込み位置に先端支持具を設置し、この先端支持具の空洞内に回転埋設先端拡大翼杭1の先端5を入れて回転させることによって施工を行う。これにより、打ち込み位置に回転埋設先端拡大翼杭1の杭芯を合わせることができる。その他の周知の杭芯合わせにより行ってもよいことは勿論である。 An example of how to use the rotating embedded tip enlarged wing pile 1 of the present invention will be described. First, at an excavation point of the ground where the rotary buried tip enlarged wing pile 1 is to be penetrated, a predetermined construction machine (not shown) is used to place the tip 5 of the rotary buried tip enlarged wing pile 1 on the ground. upright on the In addition, in order to determine the driving position of the pile 1, a tubular end support (not shown) is mainly used. Specifically, a tip support is installed at the driving position, and the tip 5 of the rotating embedded tip enlarged wing pile 1 is inserted into the cavity of the tip support and rotated. As a result, the pile core of the rotationally buried tip enlarged wing pile 1 can be aligned with the driving position. Of course, other well-known pile centering may be used.

その後、図示しない施工機械に設けられる回転駆動装置により、回転埋設先端拡大翼杭1に対して、図7にて示される正転方向Aに回転力が与えられて、回転埋設先端拡大翼杭1が筒状掘削刃30と共に、右回りに一体回転させられる。これにより、筒状掘削刃30によって、地中が掘削されつつ、回転埋設先端拡大翼杭1が先端5側から徐々に地中に貫入せしめられる。すなわち、軸回りの一方向をなす正転方向Aに回転埋設先端拡大翼杭1を回転させることによって、回転埋設先端拡大翼杭1の先端5に突設する筒状掘削刃30等で地盤を掘削し、これにより回転埋設先端拡大翼杭1が地中深くに貫入する。 After that, a rotating force is applied to the rotary embedded tip enlarged wing pile 1 in the forward rotation direction A shown in FIG. is integrally rotated clockwise together with the tubular digging blade 30 . As a result, while the ground is being excavated by the tubular excavating blade 30 , the rotating embedded tip-expanding wing pile 1 is gradually penetrated into the ground from the tip 5 side. That is, by rotating the rotary embedded tip enlarged wing pile 1 in the forward rotation direction A that is one direction around the axis, the ground is excavated by the tubular excavating edge 30 or the like protruding from the tip 5 of the rotary embedded tip enlarged wing pile 1. Excavation is carried out, and as a result, the rotating embedded tip enlarged wing pile 1 penetrates deep into the ground.

軸回りの一方向をなす正転方向Aの回転による地盤を掘削する状態、すなわち、各拡大翼50が縮小状態では、隣接する第一の拡大翼51乃至第四の拡大翼54は他の拡大翼50によって一部被覆された状態を保持しながら地中に貫入するが、この状態においては、第一の拡大翼51乃至第四の拡大翼54の全てが、円筒杭本体10の外径10о方向内側に収容される位置に維持されている。 When the ground is excavated by rotation in the forward rotation direction A around the axis, that is, when each expansion wing 50 is contracted, the adjacent first expansion wing 51 to fourth expansion wing 54 are in the other expansion state. It penetrates into the ground while maintaining a state partially covered by the wing 50. In this state, all of the first expanding wing 51 to the fourth expanding wing 54 have an outer diameter of 10° of the cylindrical pile main body 10. It is maintained in a position stowed inwards.

軸回りの一方向をなす正転方向Aの回転で抵抗(応力)を掛けることによって、地盤に埋設される。具体的には、第一の拡大翼51に備えた第一の推進翼61の第一作用面61a(正転方向側61fから徐々に)、第二の拡大翼52に備えた第二の推進翼62の第一作用面62a(正転方向側62fから徐々に)、第三の拡大翼53に備えた第三の推進翼63の第一作用面63a(正転方向側63fから徐々に)、第四の拡大翼54に備えた第四の推進翼64の第一作用面64a(正転方向側64fから徐々に)に抵抗(応力)が掛かり、回転埋設先端拡大翼杭1が地盤に埋設される。 It is embedded in the ground by applying resistance (stress) by rotating in the forward rotation direction A which is one direction around the axis. Specifically, the first action surface 61a (gradually from the forward rotation direction side 61f) of the first propelling blade 61 provided on the first expanding blade 51, the second propelling blade provided on the second expanding blade 52 A first acting surface 62a of the blade 62 (gradually from the forward rotation direction side 62f), and a first acting surface 63a of the third propelling blade 63 provided in the third expansion wing 53 (gradually from the forward rotation direction side 63f) , Resistance (stress) is applied to the first action surface 64a (gradually from the forward rotation direction side 64f) of the fourth propulsion blade 64 provided in the fourth expansion wing 54, and the rotary buried tip expansion wing pile 1 is placed on the ground. Buried.

そして、回転埋設先端拡大翼杭1が所望の地盤(支持層)まで埋設されたら、今度は施工機械に設けられる回転駆動装置により回転埋設先端拡大翼杭1を軸回りの反対方向をなす逆転方向B、すなわち、左回りに回転させることによって拡大翼50が杭1径よりも突出する。すなわち、拡大翼50が地盤(壁面)に貫入埋設され、拡大翼50により地盤支持力を増強させることができる。 Then, when the rotary embedded tip enlarged wing pile 1 is buried to the desired ground (supporting layer), this time, the rotary embedded tip enlarged wing pile 1 is moved in the opposite direction around the axis by a rotary drive device provided in the construction machine. By rotating B, that is, counterclockwise, the expanding wing 50 protrudes from the pile 1 diameter. That is, the expanding wings 50 are penetrated and buried in the ground (wall surface), and the supporting force of the ground can be enhanced by the expanding wings 50 .

軸回りの反対方向をなす逆転方向Bの回転によって、抵抗(応力)が掛かり、拡大翼50が、花びらが開くように外側に広がるように動いて拡大状態となる。具体的には、第一の拡大翼51に備えた第一の推進翼61の第二作用面61b(逆転方向側61rから徐々に)、第二の拡大翼52に備えた第二の推進翼62の第二作用面62b(逆転方向側62rから徐々に)、第三の拡大翼53に備えた第三の推進翼63の第二作用面63b(逆転方向側63rから徐々に)、第四の拡大翼54に備えた第四の推進翼64の第二作用面64b(逆転方向側64rから徐々に)に抵抗(応力)が掛かり、これにより第一の拡大翼51乃至第四の拡大翼54が回転埋設先端拡大翼杭1の外径1оから杭1の径方向外方に突出する。すなわち、拡大翼50は、縮小状態で地中に貫入するが、この縮小状態から地盤支持力を増強する拡大状態となる。 Rotation in the reverse direction B, which is the opposite direction about the axis, causes resistance (stress) to be applied, and the spreader wings 50 move to spread outward to open the petals and enter the spread state. Specifically, the second action surface 61b (gradually from the reverse direction side 61r) of the first propelling blade 61 provided on the first expanding blade 51, the second propelling blade provided on the second expanding blade 52 62 (gradually from the reverse direction side 62r), the second action surface 63b (gradually from the reverse direction side 63r) of the third propeller blade 63 provided in the third expansion wing 53, the fourth Resistance (stress) is applied to the second action surface 64b (gradually from the reverse direction side 64r) of the fourth propelling wing 64 provided in the expanding wing 54 of the above, and as a result, the first expanding wing 51 to the fourth expanding wing 54 protrudes outward in the radial direction of the pile 1 from the outer diameter 1? In other words, the expansion wing 50 penetrates into the ground in a contracted state, and from this contracted state, expands to increase the ground bearing force.

このように回転駆動装置により回転埋設先端拡大翼杭1を逆転方向Bに回転させることによって拡大翼50が突出し、拡大翼50が地盤壁面に貫入埋設されたら、施工機械に設けられる回転駆動装置から回転埋設先端拡大翼杭1を取り外して施工を完了する。 By rotating the rotary-buried tip expanding wing pile 1 in the reverse direction B in this way, the expanding wing 50 protrudes, and when the expanding wing 50 is penetrated and embedded in the ground wall surface, the rotating drive device provided in the construction machine rotates. The rotary buried tip enlarged wing pile 1 is removed to complete the construction.

本発明の回転埋設先端拡大翼杭1は、打込み工法ではなく回転貫入工法で用いられる杭1であるため、施工時においては、振動、騒音がない。また、埋め立てられ地下水を多く含む地盤、飽和した緩い砂地盤等の軟弱地盤においても施工が可能である。よって、建築土木の基礎工事の分野において多岐にわたって使用することができる。 Since the rotating embedded tip enlarged wing pile 1 of the present invention is a pile 1 used in a rotary penetration method rather than a driving method, there is no vibration or noise during construction. In addition, construction is possible even in soft ground such as reclaimed ground containing a lot of groundwater and saturated loose sandy ground. Therefore, it can be used in a wide variety of fields in the field of foundation work for construction and civil engineering.

円筒杭本体10の外周15の面に摩擦力(外周面摩擦力)が働き、また、回転埋設先端拡大翼杭1の先端側Xに先端支持力が働き、極めて簡単な作業によって回転埋設先端拡大翼杭1を地盤に強固に立てることができる。 A frictional force (outer peripheral surface frictional force) acts on the surface of the outer periphery 15 of the cylindrical pile body 10, and a tip supporting force acts on the tip end side X of the rotary embedded tip enlarged wing pile 1, and the rotary embedded tip can be expanded by a very simple operation. The wing pile 1 can be firmly erected on the ground.

本発明の回転埋設先端拡大翼杭1は、地盤を掘削する部位が円筒杭本体10の外周15の面から径方向外方(外径1о)に突出しない状態で回転され、筒状掘削刃30にて地中が掘削されて、回転埋設先端拡大翼杭1が外径1оの範囲内で地中に貫入されるようになっている。したがって、地中への貫入時に、円筒杭本体10の周囲の掘削土が、杭1本体の外周3面からの突出部位にてほぐされたり、かき乱されたりするようなことがなく、地中に貫入された状態下で、円筒杭本体10の外周面摩擦力が十分な大きさにおいて効果的に確保され得る。 The rotating embedded tip enlarged wing pile 1 of the present invention is rotated in a state in which the site for excavating the ground does not protrude radially outward (outer diameter 1 ) from the surface of the outer circumference 15 of the cylindrical pile body 10, and the cylindrical excavating edge 30 The ground is excavated at , and the rotating buried tip enlarged wing pile 1 is penetrated into the ground within the range of the outer diameter 1'. Therefore, when the soil is penetrated into the ground, the excavated soil around the cylindrical pile body 10 is not loosened or disturbed by the protruding portions from the three outer peripheral surfaces of the pile 1 body, and the soil is not disturbed. Under the penetrating state, the outer peripheral surface frictional force of the cylindrical pile body 10 can be effectively secured with a sufficient magnitude.

掘削された箇所においては、杭1本来の原形を維持することができ、杭1の施工効率、支持力を大幅に向上させることができる。 At the excavated location, the original shape of the pile 1 can be maintained, and the construction efficiency and bearing capacity of the pile 1 can be greatly improved.

また、回転埋設先端拡大翼杭1の先端側Xに立設された筒状掘削刃30の空洞39と円筒杭本体10の空洞13が連通しているため、掘削土が円筒杭本体10の内部に入り込むことによって円筒杭本体10の内周面摩擦力も効果的に確保され得る。 In addition, since the cavity 39 of the cylindrical excavation blade 30 erected on the tip end side X of the rotary buried tip enlarged wing pile 1 and the cavity 13 of the cylindrical pile body 10 are in communication, the excavated soil is placed inside the cylindrical pile body 10. Frictional force on the inner peripheral surface of the cylindrical pile main body 10 can be effectively ensured by entering.

回転埋設先端拡大翼杭1の十分な安定化を図ることができ、安全、安心面においても良好な杭1を提供できる。先端支持力、周面摩擦力、水平垂直力が革新的な発明であるため、杭業界において大きな前進である。 It is possible to sufficiently stabilize the rotary-buried tip enlarged wing pile 1, and to provide a favorable pile 1 in terms of safety and security. It is a big step forward in the pile industry because tip bearing force, circumferential friction force and horizontal vertical force are innovative inventions.

以上、各実施形態に基づき本発明を説明したが、本発明は上記実施形態に限定されるものではなく、本発明の趣旨を逸脱しない範囲で、変更を加えてもよいし、各実施形態に記載の技術、又は、その他の公知や周知の技術を組み合わせるようにしてもよい。また、本発明と同様の効果を奏することができれば、設計等に応じて種々の変更、別の形態がとられてもよい。 The present invention has been described above based on each embodiment, but the present invention is not limited to the above embodiments, and modifications may be made to each embodiment without departing from the scope of the present invention. You may make it combine the described technique or other well-known or well-known technique. Further, various modifications and other forms may be adopted depending on the design, etc., as long as the same effect as the present invention can be obtained.

各図において各実施形態を図示したが、図を分かりやすくする等のために、一部構成を省略、簡略化した部分があるため、本発明は図示した実施形態に限定されるものではない。また、一部透視した部分もある。 Although each drawing illustrates each embodiment, the present invention is not limited to the illustrated embodiments because some configurations are omitted and simplified for the sake of clarity of the drawings. In addition, there is also a partially see-through portion.

1:回転埋設先端拡大翼杭
1о:外径
3:外周面
5:先端
10:円筒杭本体
10о:外径
11:先端面
12:突環状部
13:空洞
15;外周
20:先端板
20i:内径
20о:外径
21:表面
22:穴
30:筒状掘削刃
30i:内径
30о:外径
31:本体
33:刃部
35:外周
37:山刃部
38:谷刃部
39:空洞
40:回動連結具
41:リブ
46:リブ
48:支軸
49:ベース
50:拡大翼
50a:表面
50f:正転方向側
50r:逆転方向側
50t:上端
50x:下端
50z:折曲部
51:第一の拡大翼
51a:表面
51b:裏面
51f:正転方向側
51r:逆転方向側
51t:上端
52:第二の拡大翼
52a:表面
52b:裏面
52f:正転方向側
52r:逆転方向側
52t:上端
53:第三の拡大翼
53a:表面
53b:裏面
53f:正転方向側
53r:逆転方向側
53t:上端
54:第四の拡大翼
54a:表面
54b:裏面
54f:正転方向側
54r:逆転方向側
54t:上端
60:推進翼
60a:第一作用面
60b:第二作用面
60f:正転方向側
60r:逆転方向側
61:第一の推進翼
61a:第一作用面
61b:第二作用面
61f:正転方向側
61r:逆転方向側
62:第二の推進翼
62a:第一作用面
62b:第二作用面
62f:正転方向側
62r:逆転方向側
63:第三の推進翼
63a:第一作用面
63b:第二作用面
63f:正転方向側
63r:逆転方向側
64:第四の推進翼
64a:第一作用面
64b:第二作用面
64f:正転方向側
64r:逆転方向側
OD:外径方向
AX:軸心方向
A:正転方向
B:逆転方向
C1:仮想線
C2:仮想線
X:先端側
Y:後端側

1: Rotary-buried tip enlarged wing pile 1: Outer diameter 3: Outer peripheral surface 5: Tip 10: Cylindrical pile body 10: Outer diameter 11: Tip surface 12: Protruding annular part 13: Cavity 15: Outer periphery 20: Tip plate 20i: Inner diameter 20: Outer diameter 21: Surface 22: Hole 30: Cylindrical excavating blade 30i: Inner diameter 30: Outer diameter 31: Main body 33: Blade portion 35: Periphery 37: Mountain blade portion 38: Valley blade portion 39: Cavity 40: Rotation Connector 41: Rib 46: Rib 48: Support shaft 49: Base 50: Enlarging wing 50a: Surface 50f: Forward direction side 50r: Reverse direction side 50t: Upper end 50x: Lower end 50z: Bending portion 51: First expansion Wing 51a: front surface 51b: back surface 51f: forward rotation direction side 51r: reverse rotation direction side 51t: upper end 52: second enlarged wing 52a: front surface 52b: back surface 52f: forward rotation direction side 52r: reverse rotation direction side 52t: upper end 53: Third enlarging wing 53a: Front surface 53b: Back surface 53f: Forward direction side 53r: Reverse direction side 53t: Upper end 54: Fourth enlarging wing 54a: Front surface 54b: Back surface 54f: Forward direction side 54r: Reverse direction side 54t : upper end 60: propeller blade 60a: first action surface 60b: second action surface 60f: forward direction side 60r: reverse direction side 61: first propeller blade 61a: first action surface 61b: second action surface 61f: Forward direction side 61r: Reverse direction side 62: Second propeller blade 62a: First action surface 62b: Second action surface 62f: Forward direction side 62r: Reverse direction side 63: Third propeller blade 63a: First Working surface 63b: Second working surface 63f: Forward direction side 63r: Reverse direction side 64: Fourth propeller blade 64a: First working surface 64b: Second working surface 64f: Forward direction side 64r: Reverse direction side OD : Outer diameter direction AX: Axial direction A: Forward rotation direction B: Reverse rotation direction C1: Imaginary line C2: Imaginary line X: Front end side Y: Rear end side

Claims (3)

正転方向の回転によって地盤に貫入される回転埋設先端拡大翼杭であって、
円筒杭本体と、
前記円筒杭本体の先端側軸心に立設する筒状掘削刃と、
前記筒状掘削刃の外周に沿って回動連結具を介して回動自在に配設する複数の拡大翼と、を備え、
各前記拡大翼の表面には、正転方向側を下に傾斜する推進翼が突設され、
各前記拡大翼は、正転方向側の一部が他の前記拡大翼の逆転方向側の一部で被覆され、
正転方向に回転する状態では、各前記拡大翼の全てが前記回転埋設先端拡大翼杭の外径内に収容され、
逆転方向に回転する状態では、各前記拡大翼の一部が前記回転埋設先端拡大翼杭の外径外に突出されることを特徴とした回転埋設先端拡大翼杭。
A rotating embedded tip enlarged wing pile penetrating into the ground by rotating in the normal direction,
a cylindrical pile body;
a cylindrical excavating blade erected at the tip-side axial center of the cylindrical pile body;
a plurality of enlarging wings rotatably arranged along the outer circumference of the cylindrical digging blade via a rotatable connector,
A propulsion wing inclined downward on the forward rotation direction side protrudes from the surface of each of the expansion wings,
a part of each of the expansion wings on the forward rotation direction side is covered with a part of the other expansion wings on the reverse rotation direction side;
When rotating in the normal direction, all of the expansion wings are accommodated within the outer diameter of the rotary embedded tip expansion wing pile,
A rotary embedded tip enlarged wing pile characterized in that a part of each of the enlarged wings protrudes outside the outer diameter of the rotary embedded tip enlarged wing pile when rotated in a reverse direction.
前記回転埋設先端拡大翼杭の先端側又は前記拡大翼の表面にストッパーを備えたことを特徴とする、請求項1に記載の回転埋設先端拡大翼杭。
2. The rotary embedded tip enlarged wing pile according to claim 1, wherein a stopper is provided on the tip side of said rotary embedded tip enlarged wing pile or on the surface of said enlarged wing.
前記拡大翼の逆転方向側の一部を外側に折曲げた折曲部としたことを特徴とする、請求項1又は請求項2に記載の回転埋設先端拡大翼杭。

3. The rotary-embedded tip expansion wing pile according to claim 1, wherein a portion of the expansion wing on the reverse direction side is bent outward to form a bent portion.

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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4812807B1 (en) * 1968-02-27 1973-04-23
JPS62228519A (en) * 1986-03-29 1987-10-07 Yukio Matsumoto Pit wall compression-preboring work and excavator therefor
JPS63184614A (en) * 1987-01-28 1988-07-30 Giken Seisakusho:Kk Method and apparatus for penetration of steel tubular pile
JP2005336761A (en) * 2004-05-25 2005-12-08 Takumi Juki:Kk Rotatably penetrating expanded wing pile
JP2005350914A (en) * 2004-06-09 2005-12-22 Daido Concrete Co Ltd Burial method of hollow pile and excavator used therefor
JP2006241919A (en) * 2005-03-07 2006-09-14 Haseko Corp Pile construction machine and pile construction method
JP2016075139A (en) * 2014-10-06 2016-05-12 千代田工営株式会社 Rotary penetration pile, and construction method for consolidated foundation using the rotary penetration pile
JP2019049174A (en) * 2017-09-11 2019-03-28 有限会社松村精機 Foundation pile

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4812807B1 (en) * 1968-02-27 1973-04-23
JPS62228519A (en) * 1986-03-29 1987-10-07 Yukio Matsumoto Pit wall compression-preboring work and excavator therefor
JPS63184614A (en) * 1987-01-28 1988-07-30 Giken Seisakusho:Kk Method and apparatus for penetration of steel tubular pile
JP2005336761A (en) * 2004-05-25 2005-12-08 Takumi Juki:Kk Rotatably penetrating expanded wing pile
JP2005350914A (en) * 2004-06-09 2005-12-22 Daido Concrete Co Ltd Burial method of hollow pile and excavator used therefor
JP2006241919A (en) * 2005-03-07 2006-09-14 Haseko Corp Pile construction machine and pile construction method
JP2016075139A (en) * 2014-10-06 2016-05-12 千代田工営株式会社 Rotary penetration pile, and construction method for consolidated foundation using the rotary penetration pile
JP2019049174A (en) * 2017-09-11 2019-03-28 有限会社松村精機 Foundation pile

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