JP2009293359A - Corotation preventing blade for ground improvement agitation device - Google Patents

Corotation preventing blade for ground improvement agitation device Download PDF

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Publication number
JP2009293359A
JP2009293359A JP2008169549A JP2008169549A JP2009293359A JP 2009293359 A JP2009293359 A JP 2009293359A JP 2008169549 A JP2008169549 A JP 2008169549A JP 2008169549 A JP2008169549 A JP 2008169549A JP 2009293359 A JP2009293359 A JP 2009293359A
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Prior art keywords
blade
ground improvement
trapezoidal
wing
blades
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JP2008169549A
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Japanese (ja)
Inventor
Yusei Kin
裕清 金
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SOIL TECHNO KK
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SOIL TECHNO KK
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Priority to JP2008169549A priority Critical patent/JP2009293359A/en
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  • Consolidation Of Soil By Introduction Of Solidifying Substances Into Soil (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To improve agitating capability without impairing corotation preventing function even when the hole wall of an excavated hole is soft, and to improve the accuracy of construction by suppressing wobbling by external force during excavation. <P>SOLUTION: The corotation preventing blade for a ground improvement agitation device comprises four orthogonal blades, each blade having a trapezoidal tip shape. <P>COPYRIGHT: (C)2010,JPO&INPIT

Description

この発明は掘削土と固化材を掘削・攪拌・混合する地盤改良工法で使用され、地盤改良攪拌装置の共回り防止翼に関するものである。  The present invention relates to a ground improvement method for excavating, stirring, and mixing excavated soil and solidified material, and relates to a co-rotation preventing blade of the ground improved stirring device.

従来から地盤改良攪拌装置の掘削軸に回転自在に外嵌し、該掘削軸の軸頭に配設した掘削翼の直径より大径な翼板を均等に配設した共回り防止構造が提供されているが、該共回り防止構造は2枚の共回り防止翼からなり、掘削孔の孔壁面が軟弱な時には、共に回る欠点を有していた。又掘削時の外力によってブレ出すと変心状態が増大され易く、動力損失や施工精度の低下を来す欠点も有していた。  Conventionally, there has been provided a co-rotation preventing structure in which a blade that is rotatably fitted to the excavation shaft of the ground improvement stirring device and that is larger than the diameter of the excavation blade disposed at the head of the excavation shaft is evenly disposed. However, the co-rotation prevention structure is composed of two co-rotation prevention blades, and has a drawback of rotating together when the hole wall surface of the excavation hole is soft. In addition, if the bulge is caused by external force at the time of excavation, the eccentric state is easily increased, and there is a disadvantage that power loss and construction accuracy are lowered.

特許文献1は、掘削土が掘削翼や掘削翼と共に回転する事態を防止する共回り防止装置であり現在一般的に使用されているが、掘削孔の孔壁面が軟弱な時には、共に回る事や掘削時の外力によってブレ出すと変心状態が増大され易く、動力損失や施工精度の低下を来す欠点を有している。
特開平11−107268
Patent Document 1 is a common rotation prevention device that prevents a situation in which excavated soil rotates together with excavated blades and excavated blades, and is currently generally used. However, when the hole wall surface of the excavated hole is soft, If it is blurred by an external force during excavation, the eccentricity is likely to increase, and there is a drawback that power loss and construction accuracy are reduced.
JP-A-11-107268

本発明の課題は、上記に鑑み、掘削孔の孔壁面が軟弱な時にも、共回り防止機能を損なうことなく、攪拌能力を向上させること、及び掘削時の外力によってのブレを抑え、施工の精度を向上させることである。  In view of the above, the object of the present invention is to improve the stirring ability without impairing the co-rotation prevention function even when the hole wall surface of the excavation hole is soft, and to suppress blurring due to external force during excavation. It is to improve accuracy.

本発明は、直交する4枚の翼からなりかつ翼の先端形状が台形であることを特徴する地盤改良攪拌装置の共回り防止翼である。  The present invention is a co-rotation preventing wing of a ground improvement agitating device comprising four blades orthogonal to each other and having a trapezoidal tip shape.

掘削翼の外端位置から共回り防止翼の外端まで広がる台形の翼板を取り付けることにより、従来の共回り防止構造の2枚の共回り防止翼に対して、孔壁面を抑える面積が増加し、抵抗が大きくなり共回り防止効果を向上することができる。  By attaching a trapezoidal blade that extends from the outer edge of the excavation blade to the outer edge of the anti-rotation blade, the area that suppresses the hole wall surface is increased compared to the two anti-rotation blades of the conventional anti-rotation structure. In addition, the resistance increases and the effect of preventing co-rotation can be improved.

共回り防止翼の外端が台形になった翼を直交する4枚の翼で均等に配設することにより、掘削時の土を切る回数が倍になり、従来の共回り防止構造の2枚の共回り防止翼にくらべ倍の攪拌効果が得られ、施工精度・品質向上の効果が得られる。  By arranging the trapezoidal wings with the trapezoidal outer wings with four wings that are orthogonal to each other, the number of times the soil is cut during excavation is doubled. Compared to the co-rotation prevention blade, the effect of stirring is doubled, and the effect of improving construction accuracy and quality is obtained.

共回り防止翼の外端が台形になった翼を直交する4枚の翼で均等に配設することにより、掘削時の外力によってのブレを、(共回り防止翼の外端が台形の翼板)の台形部分が掘削孔の孔壁面で抵抗し、縦方向・横方向共ブレを抑制し、攪拌能力・施工精度・品質の向上が図られる。  By arranging four trapezoidal blades with the trapezoidal outer edge of the co-rotation prevention wings evenly arranged, vibration due to external force during excavation can be prevented (the outer edge of the co-rotation prevention wing is trapezoidal) The trapezoidal part of the plate) resists at the hole wall surface of the excavation hole, suppresses both vertical and horizontal blurring, and improves the stirring ability, construction accuracy and quality.

本発明の実施形態を図1〜図8に示し、それに基づき本発明を説明する。本発明は図1(平面図)の様に、共回り防止翼の翼板3が直交する4枚の翼板で構成される。    Embodiments of the present invention are shown in FIGS. 1 to 8, and the present invention will be described based thereon. In the present invention, as shown in FIG. 1 (plan view), the blade plate 3 of the co-rotation preventing blade is constituted by four blade plates orthogonal to each other.

図2は翼板3が平行に掘削翼4の外端まで伸び、その外端から外側の台形抵抗板5の外端まで外側に広がり、台形を特長とする翼板を有する攪拌装置の正面図である。  FIG. 2 is a front view of a stirrer having blades characterized by a trapezoidal shape in which a blade plate 3 extends in parallel to the outer end of the excavating blade 4 and extends outward from the outer end to the outer end of the outer trapezoidal resistor plate 5. It is.

図3は共回り防止翼の正面図である。掘削翼4の外端まで伸び、その外端から外側の台形抵抗板5の外端まで外側に広がる角度は、40度〜60度の角度の範囲であるが、45度程度が望ましい。  FIG. 3 is a front view of the co-rotation preventing wing. The angle extending to the outer end of the excavating blade 4 and extending outward from the outer end to the outer end of the outer trapezoidal resistor plate 5 is in the range of 40 to 60 degrees, and is preferably about 45 degrees.

図4は、共回り防止翼の平面図である。直交する4枚の翼からなり、掘削翼1周における土を切る回数が4回となり、2枚翼に比べて倍の回数となり攪拌混合効率が高くなる。  FIG. 4 is a plan view of the co-rotation preventing wing. It consists of four blades orthogonal to each other, and the number of times of cutting the soil around the excavating blade is four times, which is twice as many as the two blades, and the stirring and mixing efficiency is increased.

図5は共回り防止翼の正面図で、孔壁面での抵抗する面積の増加部分を説明している。この増加部分は、掘削翼の外端から外側の台形抵抗板5の外端まで外側に広がる距離が大きい程抵抗が大きくなり、共回り防止効果が向上するが、通常は掘削翼径に関わらず、100mm程度でも十分である。    FIG. 5 is a front view of the co-rotation preventing wing and illustrates an increased portion of the resistance area on the hole wall surface. This increased portion increases the resistance as the distance extending from the outer end of the excavating blade to the outer end of the outer trapezoidal resistance plate 5 increases, and the corotation prevention effect is improved. Even about 100 mm is sufficient.

図6は共回り防止翼の平面図。掘削時の外力に対する台形抵抗板の抵抗を説明している。直交する4枚の翼とすることにより、縦方向・横方向の外力に対して抵抗する事ができる。    FIG. 6 is a plan view of the co-rotation preventing wing. It explains the resistance of the trapezoidal resistor plate to the external force during excavation. By using four orthogonal wings, it is possible to resist external forces in the vertical and horizontal directions.

図7は共回り防止翼の構成取付図を示し、形状と取り付け方を説明している。    FIG. 7 is a structural attachment diagram of the co-rotation preventing wing, and explains the shape and attachment method.

図8は共回り防止翼の正面図。板厚30mm程度、高さ150mm程度を説明。    FIG. 8 is a front view of the co-rotation preventing wing. Explains about 30mm thickness and 150mm height.

本発明に係る攪拌装置平面図。The stirring apparatus top view which concerns on this invention. 本発明に係る攪拌装置正面図。The stirring apparatus front view which concerns on this invention. 本発明に係る直交する4枚の翼からなりかつ翼の先端形状が台形であることを特徴とする共回り防止翼の正面図。The front view of the co-rotation prevention wing | blade which consists of four wing | blades orthogonal to the present invention, and the tip shape of a wing | blade is trapezoid. 本発明に係る直交する4枚の翼からなりかつ翼の先端形状が台形であることを特徴とする共回り防止翼の平面図(掘削翼1周における、土を切る回数の説明)。The top view of the co-rotation prevention wing | blade which consists of four orthogonal wing | blade which concerns on this invention, and the front-end | tip shape of a wing | blade is trapezoid (explanation of the frequency | count of cutting soil in 1 round of excavation blades). 本発明に係る共回り防止翼の正面図(設置面積増加部分説明)。The front view of the co-rotation prevention blade which concerns on this invention (installation area increase part description). 本発明に係る共回り防止翼の平面図(外力に対する抵抗の説明)。The top view of the co-rotation prevention wing | blade which concerns on this invention (explanation of resistance with respect to external force). 本発明に係る共回り防止翼の構成取付図(取り付け方法の説明)。FIG. 3 is a structural attachment diagram of the co-rotation preventing wing according to the present invention (explanation of the attachment method). 本発明に係る共回り防止翼の正面図(寸法・形状の説明)。The front view (description of a dimension and a shape) of the co-rotation prevention wing | blade which concerns on this invention.

符号の説明Explanation of symbols

1. 掘削軸
2. ボス
3. 共回り防止翼の翼板
4. 掘削翼
5. 共回り防止翼の台形抵抗板
1. Drilling shaft 2. Boss 3 3. Blades of co-rotation prevention wings 4. Excavator blade Trapezoidal resistance plate

Claims (1)

直交する4枚の翼からなりかつ翼の先端形状が台形であることを特徴する地盤改良攪拌装置の共回り防止翼。  An anti-spinning blade for a ground improvement stirrer comprising four blades orthogonal to each other and having a trapezoidal tip shape.
JP2008169549A 2008-06-02 2008-06-02 Corotation preventing blade for ground improvement agitation device Pending JP2009293359A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2008169549A JP2009293359A (en) 2008-06-02 2008-06-02 Corotation preventing blade for ground improvement agitation device

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Application Number Priority Date Filing Date Title
JP2008169549A JP2009293359A (en) 2008-06-02 2008-06-02 Corotation preventing blade for ground improvement agitation device

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JP2009293359A true JP2009293359A (en) 2009-12-17

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012241669A (en) * 2011-05-23 2012-12-10 Nippon Soken Inc Injector drive device
WO2018003889A1 (en) * 2016-06-28 2018-01-04 国立大学法人九州大学 Specific resistance detector using ground improvement blade

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012241669A (en) * 2011-05-23 2012-12-10 Nippon Soken Inc Injector drive device
WO2018003889A1 (en) * 2016-06-28 2018-01-04 国立大学法人九州大学 Specific resistance detector using ground improvement blade
JPWO2018003889A1 (en) * 2016-06-28 2019-04-18 国立大学法人九州大学 Resistivity detection device using ground improvement wing

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