JP2002285778A - Excavator - Google Patents
ExcavatorInfo
- Publication number
- JP2002285778A JP2002285778A JP2001088604A JP2001088604A JP2002285778A JP 2002285778 A JP2002285778 A JP 2002285778A JP 2001088604 A JP2001088604 A JP 2001088604A JP 2001088604 A JP2001088604 A JP 2001088604A JP 2002285778 A JP2002285778 A JP 2002285778A
- Authority
- JP
- Japan
- Prior art keywords
- groove
- bit device
- bit
- tip
- wing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000002093 peripheral effect Effects 0.000 claims description 41
- 238000005553 drilling Methods 0.000 claims description 12
- 238000009412 basement excavation Methods 0.000 claims description 8
- 238000000034 method Methods 0.000 claims description 2
- 230000008878 coupling Effects 0.000 claims 1
- 238000010168 coupling process Methods 0.000 claims 1
- 238000005859 coupling reaction Methods 0.000 claims 1
- 230000001105 regulatory effect Effects 0.000 abstract description 3
- 239000004927 clay Substances 0.000 description 14
- 239000004576 sand Substances 0.000 description 10
- 238000003780 insertion Methods 0.000 description 6
- 230000037431 insertion Effects 0.000 description 6
- 239000002689 soil Substances 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 230000000717 retained effect Effects 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000007664 blowing Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Landscapes
- Earth Drilling (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、水井戸,アンカー
工事,地辷り防止などで地中に埋設管を埋設する掘削に
用いる掘削装置に係わり、特にデバイスの先端に連結孔
を形成し、この連結孔内にビット装置の基端に設けた連
結軸を回動自在に連結し、前記デバイスに対して前記ビ
ット装置を回動して該ビット装置の穿孔径を拡大する掘
削装置に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an excavator used for excavating a buried pipe in the ground for water wells, anchor work, prevention of landslides, etc., and particularly to a connecting hole formed at a tip of a device. The present invention relates to an excavator in which a connection shaft provided at a base end of a bit device is rotatably connected within a connection hole, and the bit device is rotated with respect to the device so as to increase a hole diameter of the bit device. .
【0002】[0002]
【発明が解決しようとする課題】従来、鋼管などからな
る埋設管を埋め込むボーリングにおいては、埋設管の先
端に設けたビット装置に衝撃を与え回転しながら掘削を
行い、その掘削に伴って前記埋設管を継ぎ足して掘進す
るようにしており、その埋設管の地中への挿入を容易に
するため、前記埋設管より大径な穿孔径のビット装置が
使用される。Conventionally, in the case of boring for embedding a buried pipe made of a steel pipe or the like, excavation is performed while rotating by giving an impact to a bit device provided at the tip of the buried pipe. In order to facilitate the insertion of the buried pipe into the ground, a bit device having a larger diameter than the buried pipe is used.
【0003】例えば、特許公報第2710192号に
は、エアーハンマーの衝撃力及び回転力を受けるデバイ
スの先端に長さ方向の連結孔を成形し、この連結孔内に
ビット装置の長さ方向基端に設けた連結軸を回動自在に
挿入連結し、前記ビット装置に対して前記デバイスを円
周方向一側に所定角度回動して該ビット装置の穿孔径を
拡大し、前記デバイスの一側方向回転により前記ビット
装置を回転しながら穿孔する掘削装置において、前記デ
バイスに、放射方向に回動自在な複数の拡大翼を枢支し
た掘削装置が提案されている。この掘削装置では、ビッ
ト装置に対してデバイスを前進すると、ビット装置の保
持部が拡大翼に当接して該拡大翼が拡大する。これによ
り、ビット装置の穿孔径が拡大する。[0003] For example, in Japanese Patent Publication No. 2710192, a longitudinal connecting hole is formed at the tip of a device which receives the impact force and the rotational force of an air hammer, and the longitudinal end of the bit device is formed in the connecting hole. Is rotatably inserted and connected, and the device is rotated at a predetermined angle to one side in the circumferential direction with respect to the bit device to enlarge the perforation diameter of the bit device. In a drilling apparatus for drilling while rotating the bit device by directional rotation, there has been proposed a drilling apparatus in which the device pivotally supports a plurality of enlarged wings rotatable in a radial direction. In this excavator, when the device is advanced with respect to the bit device, the holding portion of the bit device contacts the enlarged wing, and the enlarged wing is enlarged. Thereby, the drilling diameter of the bit device is increased.
【0004】この拡大翼の取付構造について説明する
と、図13に示すように、拡大翼100を枢支するデバイ
ス101の先端面に円周等間隔で3個所の取付溝102を形成
するとともに、デバイス101の外周面から前記取付溝102
を貫通する軸孔103を形成している。また、前記拡大翼1
00の基部に貫通孔104を形成し、取付溝102に拡大翼100
の基部を挿入した状態でデバイス101の外側から軸孔103
と貫通孔104に軸105を貫通させることによって前記拡大
翼100をビット装置の中心に対して、放射方向に回動自
在に枢支している。このように、取付溝102と拡大翼100
に形成する軸105を貫通させて拡大翼100を枢支する構造
においては、軸105の脱落を防止する必要がある。この
ため、前記軸孔103の一端側に軸105の一端を位置決めす
る段部106で形成するとともに、軸孔103の他端側に挿入
孔108を形成し、この挿入孔108にロックピン107を圧入
して前記軸105の他端を係止している。このロックピン1
07は軸方向に割溝(図示しない)を有し、挿入孔108に
挿入した際の弾性復元力によって挿入孔108からの抜け
を防止するようにしている。[0004] The mounting structure of the enlarged wing will be described. As shown in FIG. 13, three mounting grooves 102 are formed at equal circumferential intervals on the distal end surface of a device 101 for pivotally supporting the enlarged wing 100. From the outer peripheral surface of 101, the mounting groove 102
Is formed. In addition, the expanding wing 1
00, a through hole 104 is formed at the base, and the enlarged wing 100 is formed in the mounting groove 102.
With the base of the device inserted, the shaft hole 103 is
The enlarged wing 100 is pivotally supported in the radial direction with respect to the center of the bit device by passing the shaft 105 through the through hole 104 and the shaft 105. Thus, the mounting groove 102 and the enlarged wing 100
It is necessary to prevent the shaft 105 from dropping off in a structure in which the shaft 105 is formed so as to pivotally support the enlarged wing 100. To this end, a step 106 for positioning one end of the shaft 105 is formed at one end of the shaft hole 103, and an insertion hole 108 is formed at the other end of the shaft hole 103, and a lock pin 107 is inserted into the insertion hole 108. The other end of the shaft 105 is press-fitted and locked. This lock pin 1
Reference numeral 07 has a split groove (not shown) in the axial direction, and prevents it from falling out of the insertion hole 108 by elastic restoring force when inserted into the insertion hole 108.
【0005】このように従来の掘削装置では、デバイス
101に拡大翼100を枢支するために、デバイス101に形成
する取付溝102を軸105を挿入する軸孔103を水平方向に
貫通形成することから、この軸孔103によって、デバイ
ス101の強度が低下し、拡大翼100の回転時において、こ
の拡大翼100を枢着する軸105に大きな力が加わった際、
軸孔103部分から亀裂が生じるなどして耐久性の低下が
懸念される。さらに、拡大翼100を枢着する軸105を挿入
孔108に挿入したロックピン107によって抜け止めする構
成のため、拡大翼100の回転時に軸105に大きな力が加わ
ると、ロックピン107が破損するなどして拡大翼100を枢
支する軸105が軸孔103から抜け落ちるといった問題があ
った。このように、拡大翼100を枢支する軸105が脱落す
ると、掘削が困難となり、一旦、作業を停止して、拡大
翼100の軸105を再度、ロックピン107で枢支するなど、
極めて煩雑なメンテナンス作業が必要であり、効率的な
掘削作業を行えないという問題もった。As described above, in the conventional drilling rig, the device
In order to pivotally support the enlarged wing 100 on the 101, a mounting groove 102 formed in the device 101 is formed through a shaft hole 103 for inserting the shaft 105 in a horizontal direction, so that the strength of the device 101 is increased by the shaft hole 103. When the expanding wing 100 rotates, when a large force is applied to the shaft 105 that pivots the expanding wing 100,
There is a concern that the durability may decrease due to cracks generated from the shaft hole 103 portion. Further, since the shaft 105 for pivotally attaching the enlarged wing 100 is prevented from coming off by the lock pin 107 inserted into the insertion hole 108, when a large force is applied to the shaft 105 during rotation of the enlarged wing 100, the lock pin 107 is damaged. For example, there is a problem that the shaft 105 pivotally supporting the enlarged wing 100 falls out of the shaft hole 103. In this way, when the shaft 105 pivotally supporting the enlarged wing 100 falls off, it becomes difficult to excavate, and once stopped, the shaft 105 of the enlarged wing 100 is pivoted again with the lock pin 107.
Extremely complicated maintenance work is required, and there is a problem that efficient excavation work cannot be performed.
【0006】また、この種の掘削装置では、図14に示
すように、前記デバイス101にエアハンマーに連通する
通路(図示せず)が形成され、この通路に連通する圧縮
空気路110がビット装置111に形成されている。そして、
この圧縮通路110の先端に複数の分岐通路110Aを連通さ
せ、これら各110Aをビット装置111の先端面に開口させ
ている。また、ビット装置111の先端面には前記各分岐
通路110Aの先端開口部に臨んで第1の溝部112を放射状
に形成し、これら第1の溝部112と連続するように、ビ
ット装置111の胴周面外側に第2の溝部113を縦設すると
ともに、デバイス101の外周には排出溝114(図13に示
す)が形成されている。そして、ビット装置111の先端
に開口する分岐通路110Aから圧縮空気を噴射すること
によって、ビット装置111で掘削した土砂などを第1の
溝部112から第2の溝部113に排出し、さらに、デバイス
101の排出溝114から地表へと排出するようにしている。In this type of excavator, as shown in FIG. 14, a passage (not shown) communicating with an air hammer is formed in the device 101, and a compressed air passage 110 communicating with this passage is provided in a bit device. 111 is formed. And
A plurality of branch passages 110 </ b> A are communicated with the tip of the compression passage 110, and each of the branch passages 110 </ b> A is opened on the tip surface of the bit device 111. A first groove 112 is formed radially on the distal end surface of the bit device 111 so as to face the distal end opening of each of the branch passages 110A, and the body of the bit device 111 is connected to the first groove 112. A second groove 113 is provided vertically outside the peripheral surface, and a discharge groove 114 (shown in FIG. 13) is formed on the outer periphery of the device 101. Then, by injecting compressed air from a branch passage 110A opening at the tip of the bit device 111, soil and the like excavated by the bit device 111 are discharged from the first groove portion 112 to the second groove portion 113.
The gas is discharged from the discharge groove 114 of the 101 to the ground surface.
【0007】ところで、前記ビット装置111の先端部は
テーパ面111Aと、このテーパ面と連続する胴周面111B
で構成され、胴周面111Bの先端面に第1の溝部112が形
成され、胴周面111Bの外周からテーパ面111Aのかけて
第2の溝部113が形成されているが、従来、図14に示す
ように、この種の掘削装置において、ビット装置111の
先端面に形成する第1の溝部112及び第2の溝部113の深
さSは比較的浅く形成され、また、ビット装置111の胴周
面111Bの長さLと、その胴周面111Bからテーパ面111A
にかけて形成される第2の溝部113の長さL1は比較的長
く形成されている。このため、掘削時において、特に、
シルト粘土質などの粘性を有する粘土層を掘削する場
合、ビット装置111の先端面に形成する第1の溝部112に
土砂が詰り易く、また、第2の溝部113の全長L1も長い
ことから、デバイス101の排出溝114に排出する途中の第
2の溝部113の部分においても泥や土砂が詰まり易い。
このため、掘削した土砂を効率的に排出することができ
ないという問題があった。Incidentally, the tip of the bit device 111 has a tapered surface 111A and a body peripheral surface 111B continuous with the tapered surface.
The first groove 112 is formed on the tip end surface of the body peripheral surface 111B, and the second groove 113 is formed from the outer periphery of the body peripheral surface 111B to the tapered surface 111A. As shown in FIG. 2, in this type of excavator, the depth S of the first groove 112 and the second groove 113 formed on the tip end surface of the bit device 111 is relatively small, and The length L of the peripheral surface 111B and the tapered surface 111A
The length L1 of the second groove 113 formed over is relatively long. For this reason, during excavation,
When excavating a clay layer having viscosity such as silt clay, the first groove 112 formed on the tip end surface of the bit device 111 is easily clogged with earth and sand, and the total length L1 of the second groove 113 is long. The portion of the second groove 113 that is being discharged to the discharge groove 114 of the device 101 is also likely to be clogged with mud or earth and sand.
For this reason, there was a problem that excavated earth and sand could not be efficiently discharged.
【0008】そこで本発明は、拡大翼の取付強度を高め
てデバイスに対する拡大翼の取付けを長期に渡って安定
的に維持できる掘削装置を提供することを目的とし、ま
た、掘削した土砂をスムーズに排出することができる掘
削装置を提供することを目的とする。SUMMARY OF THE INVENTION Accordingly, an object of the present invention is to provide an excavator capable of increasing the mounting strength of an expanding wing and maintaining the mounting of the expanding wing to a device stably for a long period of time. An object of the present invention is to provide a drilling device capable of discharging.
【0009】[0009]
【課題を解決するための手段】請求項1の発明の掘削装
置は、衝撃力及び回転力を受けるデバイスの先端に、ビ
ット装置を前進及び後退可能に設け、前記デバイスの先
端に、放射方向に回動可能な複数の拡大翼を枢支し、前
記デバイスの前記ビット装置に対する後退により前記拡
大翼を前記デバイス側に収納する取付溝を前記デバイス
に設け、前記デバイスの前記ビット装置に前進により前
記拡大翼を拡大し、埋設管の先端からビット装置の先端
及び前記拡大翼を突出して掘削を行う掘削装置におい
て、前記拡大翼の両側から突出する枢着軸を設け、この
枢着軸の両端部を枢着する左右一対の係合凹溝を前記取
付溝の対向する側壁面に形成するとともに、この係合凹
溝を前記デバイスの内面に開口させたものである。According to a first aspect of the present invention, there is provided an excavator, wherein a bit device is provided at a tip of a device which receives an impact force and a rotational force so as to be able to move forward and backward, and a tip of the device is radially provided at the tip of the device. The device is provided with a mounting groove for pivotally supporting a plurality of rotatable magnifying wings and receiving the magnifying wing on the device side by retreating the device with respect to the bit device, and advancing the bit device of the device to the bit device. In an excavator for enlarging an enlarged wing and excavating the tip of a bit device and the enlarged wing from the tip of a buried pipe to perform excavation, a pivot shaft protruding from both sides of the enlarged wing is provided, and both ends of the pivot shaft are provided. And a pair of left and right engaging concave grooves for pivotally connecting the mounting groove are formed on opposite side wall surfaces of the mounting groove, and the engaging concave grooves are opened on the inner surface of the device.
【0010】上記構成により、拡大翼の枢着軸を枢支す
る係合凹溝はデバイスの外面に開口することなく、デバ
イスの内側に凹設されているから、係合凹溝によってデ
バイスの強度を低下することはない。これにより、拡大
翼の回転時において、この拡大翼を枢着する枢着軸に大
きな力が加わったとしても、係合凹溝の部分から亀裂な
どが発生することもないため、耐久性を高めることがで
きる。また、拡大翼の組み付けは、単に拡大翼に設けた
枢着軸をデバイスの内側から係合凹溝に挿入して、係合
凹溝に沿わせてスライドさせるだけで簡単に拡大翼を枢
支することができるとともに、係合凹溝に枢着軸を嵌め
入れた状態でデバイスの内部にビット装置を組み付ける
ことによって、拡大翼はビット装置によって内側への移
動が規制され、係合凹溝に対して拡大翼が抜け止め保持
される。According to the above configuration, the engaging groove for pivotally supporting the pivot axis of the enlarged wing is not provided on the outer surface of the device but is formed inside the device. Does not decrease. As a result, even when a large force is applied to the pivot axis for pivotally attaching the enlarged wing during rotation of the enlarged wing, no crack or the like is generated from the engagement groove, thereby increasing the durability. be able to. To assemble the enlarged wing, simply insert the pivot shaft provided on the enlarged wing from the inside of the device into the engagement groove and slide along the engagement groove to easily pivot the enlarged wing. By mounting the bit device inside the device with the pivot shaft fitted in the engagement groove, the inward movement of the enlarged wing is regulated by the bit device, and the enlarged wing is inserted into the engagement groove. On the other hand, the expansion wing is retained and retained.
【0011】請求項2の発明の掘削装置は、前記請求項
1記載の掘削装置において、前記枢着軸の先端側を球面
状に形成し、この枢着軸と係合する前記係合凹溝の断面
形状をほぼ半円状に形成したものである。According to a second aspect of the present invention, there is provided the excavator according to the first aspect, wherein a tip side of the pivot shaft is formed in a spherical shape, and the engaging groove engages with the pivot shaft. Is formed in a substantially semicircular cross section.
【0012】上記構成により、枢着軸と係合凹溝とが滑
らかに嵌合し、拡大翼の動きもスムーズである。According to the above configuration, the pivot shaft and the engagement groove are fitted smoothly, and the movement of the enlarged wing is also smooth.
【0013】請求項3の発明の掘削装置は、衝撃力及び
回転力を受けるデバイスの先端に、ビット装置を前進及
び後退可能に設け、前記デバイスの先端に、放射方向に
回動可能な複数の拡大翼を枢支し、前記デバイスの前記
ビット装置に対する後退により前記拡大翼を前記デバイ
ス側に収納する取付溝を前記デバイスに設け、前記デバ
イスの前記ビット装置に前進により前記拡大翼を拡大
し、埋設管の先端からビット装置の先端及び前記拡大翼
を突出して掘削を行う掘削装置において、前記ビット装
置の基端に開口してビット装置の先端部まで圧縮空気を
通す圧縮空気通路を設けるとともに、その圧縮空気通路
の先端部から分岐して前記ビット装置の先端面に開口す
る複数の分岐通路を設け、かつ、前記ビット装置の先端
面に前記各分岐通路の開口部の周縁からそれぞれ前記ビ
ット装置の外周に向かって放射状に形成された第1の溝
部を設け、この第1の溝部と連通する第2の溝部を前記
ビット装置の胴周面外側に縦設するとともに、この第2
の溝部と対応して前記デバイスの外周に排出溝を形成し
たものである。According to a third aspect of the present invention, a bit device is provided at a tip of a device receiving an impact force and a rotational force so as to be able to move forward and backward, and a plurality of radially rotatable devices are provided at the tip of the device. Pivoting the expanding wing, providing a mounting groove in the device for receiving the expanding wing on the device side by retracting the device with respect to the bit device, expanding the expanding wing by advancing the bit device of the device, In a drilling device that excavates by projecting the tip of the bit device and the enlarged wing from the tip of the buried pipe, and providing a compressed air passage that opens to the base end of the bit device and allows compressed air to pass to the tip of the bit device, A plurality of branch passages branching from the distal end of the compressed air passage and opening to the distal end surface of the bit device are provided, and the branch passages are provided at the distal end surface of the bit device. First grooves are formed radially from the periphery of the opening toward the outer periphery of the bit device, and a second groove communicating with the first groove is provided vertically outside the body peripheral surface of the bit device. And this second
A discharge groove is formed on the outer periphery of the device in correspondence with the groove of (1).
【0014】上記構成により、分岐通路から圧縮空気を
吹き出すことによってビット装置で掘削した土砂や粘土
などがビット装置の先端面に形成する第1の溝部から第
2の溝部に排出され、さらに、デバイスの外周面に形成
する排出溝を経て地上に排出される。[0014] With the above structure, the earth and sand, clay and the like excavated by the bit device are discharged from the first groove portion formed in the tip end surface of the bit device to the second groove portion by blowing out the compressed air from the branch passage. Is discharged to the ground through a discharge groove formed on the outer peripheral surface of the.
【0015】請求項4の発明の掘削装置は、前記請求項
3記載の掘削装置において、前記第1の溝部の深さを前
記ビット装置の直径の7〜15%とするとともに、前記ビ
ット装置の胴周面の長さを30〜40mmに設定したもので
ある。According to a fourth aspect of the present invention, there is provided the excavator according to the third aspect, wherein the depth of the first groove portion is set to 7 to 15% of the diameter of the bit device, and the depth of the bit device is reduced. The length of the trunk surface is set to 30 to 40 mm.
【0016】上記構成により、シルト粘土質層など、粘
性が高い地層を掘削する場合、ビット装置の先端面に形
成する第1の溝部が深く、また、ビット装置の外周面に
形成する第2の溝部の全長が短いことから、ビット装置
で掘削したた土砂や粘土は第1、第2の溝部に土砂や粘
土などが詰まりにくい。これにより、ビット装置の先端
面に形成する第1の溝部から第2の溝部に排出され、さ
らに、デバイスの外周面に形成する排出溝を経てスムー
ズに地上へと排出される。According to the above configuration, when excavating a highly viscous layer such as a silt clayey layer, the first groove formed on the tip end surface of the bit device is deep and the second groove formed on the outer peripheral surface of the bit device. Since the total length of the groove is short, the soil and clay excavated by the bit device are unlikely to be clogged with the first and second grooves. As a result, the liquid is discharged from the first groove formed on the tip end surface of the bit device to the second groove, and further smoothly discharged to the ground via the discharge groove formed on the outer peripheral surface of the device.
【0017】[0017]
【発明の実施形態】以下、本発明の実施例を添付図面を
参照して説明する。図1ないし図12は本発明の一実施
例を示し、同図に示すように、鋼管などからなる埋設管
1の先端には、ビットケーシングパイプ2が溶着され、
このケーシングパイプ2は、内側の内周段部3を介して
先端に肉厚部4を有している。前記埋設管1内には、エ
アーハンマー5が挿入され、このエアーハンマー5には
デバイス6基端の筒部7が連結され、この筒部7の外周
にはスプライン溝8が一体に形成され、前記エアーハン
マー5の縦溝9に前記スプライン溝8が嵌合して該エア
ーハンマー5の回転が前記デバイス6に伝達されるよう
になっており、さらに、前記エアーハンマー5は圧縮空
気などを動力源とする図示しないハンマーピストンを内
蔵し、このハンマーピストンが前記筒部7を殴打して衝
撃力を伝達する。前記デバイス6の外周には、デバイス
6の軸方向に沿って掘削した土砂などを埋設管1上方に
排出する3本の排出溝10が等間隔に縦設されると共に、
前記ビットケーシングパイプ2の内周段部3に係合する
外周段部11が周設されている。前記デバイス6の先端側
には連結孔12が形成され、その連結孔12の内面に臨んで
回転伝達ピン13,13が横設され、この回転伝達ピン13,13
はデバイス6に上下に並んで穿設した取付孔14,14に着
脱自在に固定される。Embodiments of the present invention will be described below with reference to the accompanying drawings. FIGS. 1 to 12 show an embodiment of the present invention. As shown in FIG. 1, a bit casing pipe 2 is welded to the tip of a buried pipe 1 made of a steel pipe or the like.
The casing pipe 2 has a thick portion 4 at the tip via an inner inner peripheral step 3. An air hammer 5 is inserted into the buried pipe 1, and a cylinder 7 at the base end of the device 6 is connected to the air hammer 5, and a spline groove 8 is integrally formed on the outer periphery of the cylinder 7. The spline groove 8 is fitted into the vertical groove 9 of the air hammer 5 so that the rotation of the air hammer 5 is transmitted to the device 6, and the air hammer 5 is powered by compressed air or the like. A hammer piston (not shown) serving as a source is built in, and the hammer piston strikes the cylindrical portion 7 to transmit an impact force. On the outer periphery of the device 6, three discharge grooves 10 for discharging earth and sand excavated along the axial direction of the device 6 above the buried pipe 1 are vertically provided at equal intervals,
An outer peripheral step portion 11 which engages with the inner peripheral step portion 3 of the bit casing pipe 2 is provided around. A connection hole 12 is formed on the distal end side of the device 6, and rotation transmitting pins 13, 13 are laterally provided facing the inner surface of the connection hole 12.
Are removably fixed to mounting holes 14, 14 pierced vertically in the device 6.
【0018】前記連結孔12には、ビット装置15基端の連
結軸16が回動かつ上下スライド可能に挿入され、この連
結軸16の外周には前記回転伝達ピン13,13に係合し前記
ビット装置15を所定角度回転可能とする係合溝17,17が
上下に並んで形成されている。この係合溝17,17は、前
記回転伝達ピン13が前記連結軸16の外周に沿って略90
度回動可能に形成され、その円周方向一側には、回転伝
達ピン13を介して、デバイス6の一側方向Rの回転をビ
ット装置15に伝達する伝達係合部たる一側係合面18と、
他側方向の回転をビット装置15に伝達する他側係合部た
る他側係合面19とが形成され、その係合溝17は、前記伝
達ピン13の直径よりやや大きく形成され、かつ先端側の
係合溝17の他端側係合面19の上方には、該他側係合面19
に連続して、前記回転伝達ピン13に係合し前記ビット装
置15を長さ方向に前後及び後退可能な平坦面を有するス
ライド溝部20が形成されている。A connecting shaft 16 at the base end of the bit device 15 is rotatably and vertically slidably inserted into the connecting hole 12, and the outer periphery of the connecting shaft 16 is engaged with the rotation transmitting pins 13 Engaging grooves 17, 17 that allow the bit device 15 to rotate by a predetermined angle are formed vertically. The engagement grooves 17, 17 are provided so that the rotation transmitting pin 13 is substantially 90
One side engagement, which is a transmission engagement portion that transmits rotation of the device 6 in one direction R to the bit device 15 via the rotation transmission pin 13 on one side in the circumferential direction. Face 18 and
The other-side engaging surface 19, which is the other-side engaging portion for transmitting the rotation in the other direction to the bit device 15, is formed, and the engaging groove 17 is formed slightly larger than the diameter of the transmitting pin 13, and The other-side engaging surface 19 is provided above the other-side engaging surface 19 of the side engaging groove 17.
A sliding groove 20 having a flat surface that engages with the rotation transmitting pin 13 and that allows the bit device 15 to move back and forth and back in the longitudinal direction is formed.
【0019】前記デバイス6の先端には、図5に示すよ
うに、円周等間隔で3箇所の取付溝21がデバイス6の先
端面に開口するようにして形成され、この各取付溝21に
枢着軸22を介して拡大翼23が枢支されている。前記枢着
軸22は前記拡大翼23の基部側に位置して水平方向に貫通
し、その枢着軸22の両端が拡大翼23の両側面から突出し
ている。該拡大翼23から突出する枢着軸22の両端部分は
滑らかな球面部22Aとなっている。また、前記各取付溝
21の対向する両側壁面にはそれぞれ前記枢着軸22を枢支
する左右一対の係合凹溝24が形成されている。この係合
凹溝24は、前記デバイス6の内面に開口している。ま
た、前記枢着軸22の断面形状は、前記枢着軸22の両端先
端部分と嵌合するように半円形状に形成されている。そ
して、前記拡大翼23に装着した枢着軸22の両端を前記デ
バイス6の内側から前記係合凹溝24に挿入することによ
って軸支する。こうして拡大翼23はビット装置15の中心
軸に対して、放射方向に回動自在に取付けられている。
前記拡大翼23の基端には、該拡大翼23の拡大状態で、前
記取付溝21の傾斜した内端面21Aに当接する平坦状の肩
面23Aが形成されており、この肩面23Aに連続して前記
枢着軸22を中心とした湾曲面25が形成されている。ま
た、前記拡大翼23の先端側には、左右に幅広部26,26が
設けられ、この幅広部26,26の左右基端側には、傾斜面2
7,27がそれぞれ設けられている。前記取付溝21の先端側
には、基端側より幅広で前記幅広部26の基端側が収納可
能な幅広溝部28が形成されており、この幅広溝部28に
は、拡大翼23の拡大状態で、前記傾斜面27が当接する受
面29が設けられている。At the distal end of the device 6, as shown in FIG. 5, three mounting grooves 21 are formed at equal intervals on the circumference so as to open on the distal end surface of the device 6. An enlarged wing 23 is pivotally supported via a pivot shaft 22. The pivot shaft 22 is located on the base side of the enlarged wing 23 and penetrates in the horizontal direction. Both ends of the pivot shaft 22 project from both side surfaces of the enlarged wing 23. Both ends of the pivot shaft 22 protruding from the enlarged wing 23 are formed as smooth spherical portions 22A. In addition, each of the mounting grooves
A pair of left and right engaging concave grooves 24 for pivotally supporting the pivot shaft 22 are formed on opposite side wall surfaces of the pair 21 respectively. The engagement groove 24 is open on the inner surface of the device 6. Further, the cross-sectional shape of the pivot shaft 22 is formed in a semicircular shape so as to be fitted to both ends of the pivot shaft 22. Then, both ends of the pivot shaft 22 attached to the enlarged wing 23 are inserted into the engagement groove 24 from inside the device 6 to support the shaft. In this way, the expanding wing 23 is mounted to be rotatable in the radial direction with respect to the center axis of the bit device 15.
At the base end of the enlarged wing 23, a flat shoulder surface 23A that is in contact with the inclined inner end surface 21A of the mounting groove 21 in an enlarged state of the enlarged wing 23 is formed, and is continuous with the shoulder surface 23A. Thus, a curved surface 25 centering on the pivot shaft 22 is formed. Also, wide portions 26, 26 are provided on the left and right sides on the distal end side of the enlarged wing 23, and the inclined surfaces 2 are provided on the left and right base end sides of the wide portions 26, 26.
7,27 are provided respectively. On the distal end side of the mounting groove 21, a wide groove portion 28 wider than the base end side and capable of storing the base end side of the wide portion 26 is formed, and in the wide groove portion 28, the enlarged wing 23 is in an expanded state. A receiving surface 29 with which the inclined surface 27 contacts is provided.
【0020】さらに、ビット装置15の連結軸16の先端側
に縮小状態で前記拡大翼23が沿い前記埋設管1及びビッ
トケーシングパイプ2内を挿通可能となっている。前記
ビット装置15の先端にテーパ面32と、このテーパ面32と
連続する胴周面32Aとを形成、前記テーパ面32を前記拡
大翼23の内側面23Bに当接することによって該拡大翼23
を拡大状態で保持する。また、前記拡大翼23及びビット
装置15の先端面には超硬合金からなる複数のチップ33が
設けられており、前記拡大翼23の先端面は略く字型をな
し、その外側中央と内側左右に前記チップ33が設けら
れ、該拡大翼23の回転方向先端側には、アーク溶接など
により、前記拡大翼23より硬質な硬質肉盛部34が設けら
れている。Further, the expanding wing 23 extends along the distal end side of the connecting shaft 16 of the bit device 15 in a contracted state, and can be inserted through the buried pipe 1 and the bit casing pipe 2. A tapered surface 32 and a body peripheral surface 32A continuous with the tapered surface 32 are formed at the tip of the bit device 15, and the tapered surface 32 is brought into contact with an inner side surface 23B of the enlarged wing 23 so that the enlarged blade 23
Is held in an enlarged state. Further, a plurality of chips 33 made of cemented carbide are provided on the distal end surfaces of the enlarged wing 23 and the bit device 15, and the distal end surface of the enlarged wing 23 has a substantially rectangular shape, and has an outer center and an inner side. The tip 33 is provided on the left and right, and a hard overlay portion 34 that is harder than the enlarged wing 23 is provided on the tip side in the rotation direction of the enlarged wing 23 by arc welding or the like.
【0021】前記デバイス6にはエアハンマー5に連通
する通路41が形成され、この通路41に連通する圧縮空気
路42がビット装置15に形成され、この圧縮通路42の先端
に連通する3つの分岐通路42A,42A,42Aが前記ビット
装置15の胴周面32Aの先端面に開口している。そして、
各分岐通路42Aの開口部に臨んで3本の第1の溝部43,4
3,43が、前記胴周面32Aの先端面の中心から胴周面32
Aの外周縁に向かって放射状に形成されている。また、
これら第1の溝部43,43,43と連続するように、胴周面3
2Aの外周面に第2の溝部45,45,45が円周等間隔に形
成され、さらに、この第2の溝部45,45,45に前記デバ
イス6の外周面に形成する排出溝10が連設されている。
なお、本実施例では、ビット装置15の直径Dが137m
m、胴周面32Aの長さL、すなわち、ビット装置15の先
端面からテーパ面32までの長さはほぼ37mmで、胴周面
32Aからテーパ面32にかけて形成される第2の溝部45の
長さL1を47mmに設定している。一方、胴周面32Aの
先端面に形成する第1の溝部43の深さSと胴周面32Aの
外周面に形成する第2の溝部45の深さS1はビット装置
15の直径Dの7〜15%、すなわち、ほぼ9.6〜20.5m
m、本実施例においては17.5mmとしている。In the device 6, a passage 41 communicating with the air hammer 5 is formed. A compressed air passage 42 communicating with the passage 41 is formed in the bit device 15, and three branches communicating with the tip of the compression passage 42. The passages 42A, 42A, 42A are open at the tip end of the body peripheral surface 32A of the bit device 15. And
Three first grooves 43, 4 facing the opening of each branch passage 42A
3 and 43 are from the center of the front end surface of the body peripheral surface 32A to the body peripheral surface 32A.
A is formed radially toward the outer peripheral edge of A. Also,
The trunk peripheral surface 3 is connected to these first grooves 43, 43, 43 so as to be continuous.
Second grooves 45, 45, 45 are formed on the outer peripheral surface of 2A at equal circumferential intervals, and a discharge groove 10 formed on the outer peripheral surface of the device 6 is connected to the second grooves 45, 45, 45. Has been established.
In this embodiment, the diameter D of the bit device 15 is 137 m.
m, the length L of the trunk surface 32A, that is, the length from the tip end surface of the bit device 15 to the tapered surface 32 is approximately 37 mm,
The length L1 of the second groove 45 formed from 32A to the tapered surface 32 is set to 47 mm. On the other hand, the depth S1 of the first groove 43 formed on the tip end surface of the body peripheral surface 32A and the depth S1 of the second groove 45 formed on the outer peripheral surface of the body peripheral surface 32A are determined by the bit device.
7 to 15% of the diameter D of 15, ie, approximately 9.6 to 20.5 m
m, 17.5 mm in this embodiment.
【0022】さらに、前記デバイス6には、後向きに圧
縮空気を噴射する2の圧縮空気路50が3箇所形成され、
この圧縮空気路50は、前記通路41に連通して前記排出溝
10の間において前記デバイス6の肩面6Aに開口する。Further, the device 6 is provided with two compressed air passages 50 for injecting compressed air backward, at three places.
The compressed air passage 50 communicates with the passage 41 and is connected to the discharge groove.
Between 10 the openings are made in the shoulder 6A of the device 6.
【0023】次ぎに上記掘削装置の使用方法につき説明
すると、図8に示すように、拡大翼23に枢着軸22を貫通
させた後、その枢着軸22の両端をデバイス6の内側から
取付溝21に形成する係合凹溝24に挿入する。この後、拡
大翼23を係合凹溝24に沿わせてスライドさせることによ
って、枢着軸22が係合凹溝24の端面に突き当てる。これ
により拡大翼23が取付溝21に軸支され、こうして拡大翼
23はビット装置15の中心軸に対して、放射方向に回動自
在に取付けられている。この時、拡大翼23の枢着軸22
は、デバイス6の内側に開口した係合凹溝24に沿ってス
ライド自在に保持されているに過ぎないが、図2に示す
ように、取付溝21に拡大翼23を軸支した状態で埋設管1
内に挿入したビット装置15を回転伝達ピン13によってス
ライド溝部20の上端に係止することによって、拡大翼23
は、その内側に位置するビット装置15により内側への移
動が規制させる。すなわち、ビット装置15はデバイス6
に吊り下げられた状態となり、拡大翼23は連結軸16に沿
って吊り下げられた状態で埋設管1内を移動可能とな
る。そしてビット装置15を一側方向Rに回転させ衝撃を
加えながら接地すると、ビット装置15の先端のチップ33
により掘削が開始され、この掘削によってビット装置15
と拡大翼23とがビットケーシングパイプ2の先端より押
し出され、接地したビット装置15に対してデバイス6が
前進すると、回転伝達ピン13がスライド溝部20の前端に
前進する。この前進により連結軸16が連結孔13内を後退
し、図4に示すようにビット装置15のテーパ面32が拡大
翼23の内側面23Bに当接して該拡大翼23が拡大状態に保
持され、かつ拡大翼23の肩面23Aが内端面21Aに当接し
て位置決めされ、ビット装置15の穿孔径Pが拡大する。
同時にデバイス6の回転により回転伝達ピン13,13が係
合溝17,17の一側方向Rに回転して一側係合面18,18に
係合し、デバイス6の一側方向Rの回転がビット装置15
に伝達される。さらにこの状態でデバイス6の外周段部
11がビットケーシングパイプ2の内周段部3に当接し、
エアーハンマー5からの衝撃がビットケーシングパイプ
2へも伝達される。このようにして、拡大翼23を拡大し
た状態で、例えばビット装置15を1分間に1100回打
撃し、かつ1分間に20回転させるとともに、ビット装
置15の先端に形成する分岐通路42A,42A,42Aから圧縮
空気を噴射して掘削を行う。そして所定深さの掘削が終
了したら、デバイス6を他側方向に回転する。この回転
により回転伝達ピン13,13がスライド溝部20側に移動
し、デバイス6を上方に引き上げると、スライド溝部20
に沿って回転伝達ピン13,13が移動し、拡大翼23が縮小
しながらビットケーシングパイプ2内に収納され、ビッ
ト装置15が埋設管1内を移動可能となって、これを地上
に引き上げることができる。Next, a method of using the above-mentioned excavator will be described. As shown in FIG. 8, after the pivot shaft 22 is passed through the enlarged wing 23, both ends of the pivot shaft 22 are attached from the inside of the device 6. It is inserted into the engagement groove 24 formed in the groove 21. Thereafter, the enlarged wing 23 is slid along the engagement groove 24 so that the pivot shaft 22 abuts against the end face of the engagement groove 24. As a result, the enlarged wing 23 is supported by the mounting groove 21, and
Reference numeral 23 is attached to the center axis of the bit device 15 so as to be rotatable in the radial direction. At this time, the pivot 22
Is merely slidably held along an engagement concave groove 24 opened inside the device 6, but is buried in a state in which the enlarged wing 23 is pivotally supported in the mounting groove 21 as shown in FIG. Tube 1
By locking the bit device 15 inserted into the upper end of the slide groove portion 20 by the rotation transmitting pin 13,
Is restricted from moving inward by the bit device 15 located inside. That is, the bit device 15 is the device 6
And the enlarged wings 23 can move inside the buried pipe 1 while being suspended along the connecting shaft 16. Then, when the bit device 15 is rotated in one direction R and grounded while applying an impact, the tip 33 at the tip of the bit device 15 is turned on.
Drilling is started by this
When the device 6 advances from the tip of the bit casing pipe 2 and the device 6 advances with respect to the grounded bit device 15, the rotation transmitting pin 13 advances to the front end of the slide groove 20. By this advance, the connecting shaft 16 retreats in the connecting hole 13, and as shown in FIG. 4, the tapered surface 32 of the bit device 15 contacts the inner side surface 23B of the expanding wing 23, and the expanding wing 23 is held in the expanded state. In addition, the shoulder surface 23A of the enlarged wing 23 is positioned in contact with the inner end surface 21A, and the drilling diameter P of the bit device 15 is enlarged.
At the same time, the rotation of the device 6 causes the rotation transmitting pins 13, 13 to rotate in one direction R of the engagement grooves 17, 17 to engage with the one-side engagement surfaces 18, 18, and to rotate in one direction R of the device 6. Is a bit device 15
Is transmitted to In this state, the outer peripheral step of the device 6
11 contacts the inner peripheral step 3 of the bit casing pipe 2,
The impact from the air hammer 5 is also transmitted to the bit casing pipe 2. In this way, with the expanding wing 23 expanded, for example, the bit device 15 is blown 1100 times per minute and rotated 20 times per minute, and the branch passages 42A, 42A, Excavation is performed by injecting compressed air from 42A. When the excavation at the predetermined depth is completed, the device 6 is rotated in the other direction. By this rotation, the rotation transmitting pins 13, 13 move to the slide groove 20 side, and when the device 6 is pulled up, the slide groove 20
The rotation transmission pins 13 and 13 move along, and the expanding wings 23 are stored in the bit casing pipe 2 while contracting, and the bit device 15 becomes movable in the buried pipe 1 and is raised to the ground. Can be.
【0024】このような拡孔する装置を用いて例えば、
シルト粘土質などの粘性を高い層を掘削する場合、ビッ
ト装置15の先端面に形成する第1の溝部43,43,43及び
ビット装置15の外周に形成する第2の溝部45,45,45が
深さが浅い場合、掘削した粘土が、まず、ビット装置15
の先端面に形成する第1の溝部43,43,43の部分で詰っ
てしまい、いくらビット装置15の先端に形成する分岐通
路42A,42A,42Aから圧縮空気を噴射しても、掘削した
粘土層を第2の溝部45,45,45側へ排出することが困難
である。また、第2の溝部45,45,45の全長、すなわ
ち、ビット装置15の胴周面32Aの長さLが長い場合に
は、前記ビット装置15の先端面に形成する第1の溝部4
3,43,43の部分で粘土が詰らなくとも、前記ビット装置
15の外周面に形成する第2の溝部45,45,45の部分で詰
まってしまい、デバイス6の排出溝10側へと排出するこ
とができない。しかし、本実施例では、ビット装置15の
先端面に形成する第1の溝部43とビット装置15の胴周面
32Aの外周面に形成する第2の溝部45の深さS,S1が1
7.5mmと深く設定されるとともに、ビット装置15の胴
周面32Aの長さLを30〜40mm、本実施例ではほぼ37m
mであり、該胴周面32Aからテーパ面32にかけて形成さ
れる第2の溝部45の長さL1を47mmと通常の掘削装置
に比べて短く形成することによって、これらビット装置
15に形成する第1の溝部43及び第2の溝部45の部分での
粘土や土砂などの詰りを抑制することができる。このた
め、ビット装置15に形成する第1の溝部43に開口する分
岐通路42A,42A,42Aからの圧縮空気によって、掘削し
た土砂や粘土を第1の溝部43から第2の溝部45からデバ
イス6の排出溝10へと確実に排出することができるた
め、排出溝10からスムーズに地上へと排出することがで
きる。Using such a device for expanding holes, for example,
When excavating a highly viscous layer such as silt clay, a first groove 43, 43, 43 formed on the tip end surface of the bit device 15 and a second groove 45, 45, 45 formed on the outer periphery of the bit device 15 are formed. If the depth is shallow, the excavated clay
No matter how much compressed air is injected from the branch passages 42A, 42A, 42A formed at the tip of the bit device 15, the excavated It is difficult to discharge the layer to the second groove portions 45, 45, 45 side. When the total length of the second grooves 45, 45, 45, that is, the length L of the body peripheral surface 32A of the bit device 15, is long, the first groove 4 formed on the distal end surface of the bit device 15 is formed.
Even if the clay is not clogged in the portion of 3, 43, 43, the bit device
The second groove portions 45, 45, 45 formed on the outer peripheral surface of the device 15 are clogged at the portion, and cannot be discharged to the discharge groove 10 side of the device 6. However, in this embodiment, the first groove 43 formed on the tip end surface of the bit device 15 is
The depth S, S1 of the second groove 45 formed on the outer peripheral surface of 32A is 1
The length L is set to 7.5 mm, and the length L of the body peripheral surface 32A of the bit device 15 is set to 30 to 40 mm.
m, and the length L1 of the second groove 45 formed from the trunk peripheral surface 32A to the tapered surface 32 is made 47 mm, which is shorter than that of a normal excavator.
Clogging of clay, earth and sand, etc. in the first groove portion 43 and the second groove portion 45 formed in 15 can be suppressed. For this reason, the excavated earth and sand or clay is transferred from the first groove 43 to the second groove 45 by the compressed air from the branch passages 42A, 42A, 42A opened to the first groove 43 formed in the bit device 15. Can be surely discharged to the discharge groove 10, and thus can be smoothly discharged from the discharge groove 10 to the ground.
【0025】以上のように、本実施例では、拡大翼23に
貫通させた枢着軸22を係合凹溝24の取付溝21の両側面に
形成した係合凹溝24にスライドさせてデバイス6に拡大
翼23を枢支することから、係合凹溝24によってデバイス
6の強度を低下する虞れはない。このため、拡大翼23の
回転時において、この拡大翼23を枢着する枢着軸22に大
きな力が加わったとしても、係合凹溝24の部分から亀裂
が発生することもない。また、拡大翼23の組み付けは、
単に拡大翼23に装着する枢着軸22を取付溝23に形成する
係合凹溝24にデバイス6の内側から挿入して、拡大翼23
を係合凹溝24に沿わせて奥側(デバイス6の外方側)に
スライドさせるだけで枢着軸22を抜け止めするための、
ロックピンなども不要であるため、拡大翼23の組み付け
作業も容易である。なお、この状態のままでは、拡大翼
23の枢着軸22は係合凹溝24に対して位置決めされていな
いが、取付溝23に拡大翼23を取り付けた状態で、その拡
大翼23の内面側に回転伝達ピン13よってビット装置15を
組み付けると、拡大翼23はビット装置15によって内側へ
の移動が規制されるため、係合凹溝24に対して枢着軸22
が抜け止めされる。これにより、デバイス6に対して拡
大翼23が抜け止め保持される。また、拡大翼23を枢着す
る枢着軸22の両端に球面部22Aが形成され、これを軸支
する係合凹溝24の断面形状を、前記球面部22Aと嵌合す
るように半円状に形成したことにより、枢着軸22と係合
凹溝24とが滑らかに嵌合することから、ビット装置15と
連動する拡大翼23の動きもスムーズである。As described above, in the present embodiment, the pivot shaft 22 penetrated by the enlarged wing 23 is slid into the engagement grooves 24 formed on both sides of the mounting groove 21 of the engagement groove 24 so that the device is Since the enlarged wing 23 is pivotally supported on the device 6, there is no possibility that the strength of the device 6 is reduced by the engagement groove 24. Therefore, even when a large force is applied to the pivot shaft 22 for pivotally attaching the enlarged wing 23 during rotation of the enlarged wing 23, no crack is generated from the engagement groove 24. Also, assembling of the enlarged wings 23,
Simply insert the pivot 22 attached to the enlarged wing 23 into the engagement groove 24 formed in the mounting groove 23 from inside the device 6, and
In order to prevent the pivot shaft 22 from slipping off by merely sliding the inner side along the engaging groove 24 (outward of the device 6).
Since a lock pin or the like is not required, the assembling work of the enlarged wing 23 is also easy. In this state, the expanded wing
Although the pivot shaft 22 of 23 is not positioned with respect to the engaging groove 24, the bit device 15 is mounted on the inner surface side of the enlarged wing 23 by the rotation transmitting pin 13 with the enlarged wing 23 attached to the mounting groove 23. When the wing 23 is assembled, the inward movement of the expanding wing 23 is regulated by the bit device 15, so that the pivot shaft 22 is
Is stopped. As a result, the enlarged wing 23 is retained and held against the device 6. Further, spherical portions 22A are formed at both ends of a pivot shaft 22 for pivotally mounting the enlarged wings 23, and the cross-sectional shape of the engaging concave groove 24 which supports the spherical portions 22A is semicircular so as to fit with the spherical portion 22A. With this configuration, the pivot shaft 22 and the engaging groove 24 fit smoothly, so that the movement of the expanding wing 23 interlocked with the bit device 15 is also smooth.
【0026】また、本実施例では、ビット装置15の圧縮
空気路42に連通する3つの分岐通路42A,42A,42Aを前
記ビット装置15の先端面に開口させ、その分岐通路42A
の開口部に臨む3本の第1の溝部43,43,43の深さS
と、ビット装置15の胴周面32Aの外周面に形成する第2
の溝部45の深さS1をビット装置15の直径Dの7〜15
%、ビット装置15の直径が137mmに形成した本実施例
においては17.5mmと深く設定するとともに、ビット装
置15の胴周面32Aの長さLを30〜40mm、本実施例では
ほぼ37mmと短く形成することによって、第1の溝部4
3,43,43に連通する第2の溝部45,45,45の長さL1を4
7mmと短く形成することにより、シルト粘土質などの
粘性を高い層を掘削する場合であっても、ビット装置15
に形成する第1の溝部43及び第2の溝部45の部分で粘土
や土砂などが詰りにくいことから、ビット装置15で掘削
した粘土や土砂を第1の溝部43から第2の溝部45及びデ
バイス6の排出溝10に沿ってスムーズに地上へと排出す
ることができる。In this embodiment, three branch passages 42A, 42A, 42A communicating with the compressed air passage 42 of the bit device 15 are opened at the tip end surface of the bit device 15, and the branch passage 42A is provided.
Depth S of three first grooves 43, 43, 43 facing the opening of
And a second formed on the outer peripheral surface of the body peripheral surface 32A of the bit device 15.
The depth S1 of the groove 45 is 7 to 15 of the diameter D of the bit device 15.
%, In the present embodiment in which the diameter of the bit device 15 is formed to be 137 mm, the depth L is set to 17.5 mm, and the length L of the body peripheral surface 32A of the bit device 15 is 30 to 40 mm, which is as short as approximately 37 mm in the present embodiment. By forming the first groove 4
The length L1 of the second grooves 45, 45, 45 communicating with 3, 43, 43 is set to 4
By forming it as short as 7 mm, even when excavating a highly viscous layer such as silt clay,
Clay and earth and sand are hardly clogged in the portion of the first groove 43 and the second groove 45 which are formed in the first groove 43, and the clay and earth and sand excavated by the bit device 15 are removed from the first groove 43 and the second groove 45 and the device. 6 can be smoothly discharged to the ground along the discharge groove 10.
【0027】以上、本発明の一実施例について詳述した
が、本発明は前記実施例に限定されるものではなく、本
発明の要旨の範囲内で種々の変形実施例は可能である。
例えば、本実施例では、枢着軸の両端を円球状に形成し
た例を示したが、必ずしも円球状に形成する必要はな
い。また、ビット装置の先端面に形成する第1、第2の
溝部の形状や数なども適宜選定すればよいものである。
さらに、本発明の装置は横方向への掘削にも用いること
が可能であり、また、エアハンマーも各種のタイプのも
のを用いることができる。As described above, one embodiment of the present invention has been described in detail. However, the present invention is not limited to the above-described embodiment, and various modified embodiments are possible within the scope of the present invention.
For example, in this embodiment, an example is shown in which both ends of the pivot shaft are formed in spherical shapes, but it is not always necessary to form them in spherical shapes. The shape and number of the first and second grooves formed on the tip end surface of the bit device may be appropriately selected.
Further, the device of the present invention can be used for excavation in a lateral direction, and various types of air hammers can be used.
【0028】[0028]
【発明の効果】請求項1の発明の掘削装置によれば、衝
撃力及び回転力を受けるデバイスの先端に、ビット装置
を前進及び後退可能に設け、前記デバイスの先端に、放
射方向に回動可能な複数の拡大翼を枢支し、前記デバイ
スの前記ビット装置に対する後退により前記拡大翼を前
記デバイス側に収納する取付溝を前記デバイスに設け、
前記デバイスの前記ビット装置に前進により前記拡大翼
を拡大し、埋設管の先端からビット装置の先端及び前記
拡大翼を突出して掘削を行う掘削装置において、前記拡
大翼の両側から突出する枢着軸を設け、この枢着軸の両
端部を枢着する左右一対の係合凹溝を前記取付溝の対向
する側壁面に形成するとともに、この係合凹溝を前記デ
バイスの内面に開口させたものであるから、拡大翼の回
転時において、この拡大翼を枢着する枢着軸に大きな力
が加わったとしても、係合凹溝の部分から亀裂が発生す
ることもないため、耐久性を高めることができるととも
に、拡大翼の組み付け作業を簡略化することができる。
また、デバイスに組み付けた拡大翼は、その内側に組み
付けたビット装置によって、抜け止めされることから、
拡大翼を長期に渡って安定的に枢支することが可能であ
り、メンテナンス作業も不要である。According to the first aspect of the present invention, a bit device is provided at the tip of a device that receives an impact force and a rotational force so as to be able to move forward and backward, and the tip of the device is pivoted in a radial direction. A mounting groove for pivotally supporting a plurality of possible expansion wings and receiving the expansion wing on the device side by retreating the device with respect to the bit device;
In a drilling device for expanding the enlarged wing by advancing the bit device of the device and projecting the tip of the bit device and the enlarged wing from the tip of a buried pipe to excavate, a pivot shaft protruding from both sides of the enlarged wing. And a pair of left and right engagement grooves for pivotally connecting both ends of the pivot shaft are formed on opposing side walls of the mounting groove, and the engagement grooves are opened on the inner surface of the device. Therefore, even when a large force is applied to the pivot shaft that pivotally connects the enlarged wing during rotation of the enlarged wing, no crack is generated from the engagement groove, so that the durability is improved. And the assembling work of the enlarged wing can be simplified.
Also, since the expanding wing assembled to the device is prevented from falling off by the bit device assembled inside,
The extended wing can be pivoted stably for a long time, and no maintenance work is required.
【0029】請求項2の発明の掘削装置によれば、前記
請求項1記載の掘削装置において、前記枢着軸の先端側
を球面状に形成し、この枢着軸と係合する前記係合凹溝
の断面形状をほぼ半円状に形成したものであるから、枢
着軸と係合凹溝とが滑らかに嵌合し、拡大翼の動きもス
ムーズである。According to a second aspect of the present invention, in the excavating apparatus according to the first aspect, the distal end side of the pivot shaft is formed in a spherical shape, and the engaging portion engages with the pivot shaft. Since the cross-sectional shape of the concave groove is substantially semicircular, the pivot shaft and the engaging concave groove fit smoothly, and the movement of the enlarged wing is also smooth.
【0030】請求項3の発明の掘削装置によれば、衝撃
力及び回転力を受けるデバイスの先端に、ビット装置を
前進及び後退可能に設け、前記デバイスの先端に、放射
方向に回動可能な複数の拡大翼を枢支し、前記デバイス
の前記ビット装置に対する後退により前記拡大翼を前記
デバイス側に収納する取付溝を前記デバイスに設け、前
記デバイスの前記ビット装置に前進により前記拡大翼を
拡大し、埋設管の先端からビット装置の先端及び前記拡
大翼を突出して掘削を行う掘削装置において、前記ビッ
ト装置の基端に開口してビット装置の先端部まで圧縮空
気を通す圧縮空気通路を設けるとともに、その圧縮空気
通路の先端部から分岐して前記ビット装置の先端面に開
口する複数の分岐通路を設け、かつ、前記ビット装置の
先端面に前記各分岐通路の開口部の周縁からそれぞれ前
記ビット装置の外周に向かって放射状に形成された第1
の溝部を設け、この第1の溝部と連通する第2の溝部を
前記ビット装置の胴周面外側に縦設するとともに、この
第2の溝部と対応して前記デバイスの外周に排出溝を形
成したものであるから、第1の溝部から圧縮空気を吹き
出すことによってビット装置で掘削した土砂が第1の溝
部からる第2の溝部に送られ、さらに、デバイスの外周
面に形成する排出溝から地上にスムーズに排出される。According to the third aspect of the present invention, the bit device is provided at the tip of the device receiving the impact force and the rotational force so as to be able to move forward and backward, and the tip of the device is rotatable in the radial direction. A mounting groove is provided in the device for pivotally supporting a plurality of enlarged wings and retracting the enlarged wing on the device side by retreating the device with respect to the bit device, and expanding the enlarged wing by advancing the bit device of the device. In a drilling device for excavating by projecting the tip of the bit device and the enlarged wing from the tip of the buried pipe, a compressed air passage is provided at the base end of the bit device and through which compressed air passes to the tip of the bit device. A plurality of branch passages that branch off from the distal end portion of the compressed air passage and open to the distal end surface of the bit device; The formed radially toward the outer periphery of each of the bit device from the peripheral edge of the opening of the passage 1
And a second groove communicating with the first groove is vertically provided on the outer peripheral surface of the body of the bit device, and a discharge groove is formed on the outer periphery of the device corresponding to the second groove. Since the compressed air is blown out from the first groove, the earth and sand excavated by the bit device is sent to the second groove formed from the first groove, and further discharged from the discharge groove formed on the outer peripheral surface of the device. Discharged smoothly to the ground.
【0031】請求項4の発明の掘削装置によれば、前記
請求項3記載の掘削装置において、前記第1の溝部の深
さを前記ビット装置の直径の7〜15%とするとともに、
前記ビット装置の胴周面の長さを30〜40mmに設定した
ものであるから、シルト粘土質層など、粘性が高い地層
を掘削する場合であっても、第1、第2の溝部の部分で
土砂や粘土などが詰まりにくく、掘削した土砂や粘土を
確実に排出することができる。According to a fourth aspect of the present invention, in the excavator of the third aspect, the depth of the first groove is set to 7 to 15% of the diameter of the bit device.
Since the length of the body peripheral surface of the bit device is set to 30 to 40 mm, even when excavating a highly viscous stratum such as a silt clayey layer, the first and second groove portions are formed. The soil and clay are hardly clogged, and the excavated soil and clay can be reliably discharged.
【図1】本発明の一実施例を示すデバイスとビット装置
の分解斜視図である。FIG. 1 is an exploded perspective view of a device and a bit device according to an embodiment of the present invention.
【図2】本発明の一実施例を示す断面図である。FIG. 2 is a sectional view showing one embodiment of the present invention.
【図3】本発明の一実施例を示す要部の断面図である。FIG. 3 is a sectional view of a main part showing one embodiment of the present invention.
【図4】本発明の一実施例を示す拡大翼を拡大した状態
の断面図である。FIG. 4 is an enlarged sectional view of an enlarged wing showing one embodiment of the present invention.
【図5】本発明の一実施例を示す拡大翼の取付状態を示
す要部の断面図である。FIG. 5 is a sectional view of a main part showing an attached state of an enlarged wing showing one embodiment of the present invention.
【図6】本発明の一実施例を示す拡大翼の平面図であ
る。FIG. 6 is a plan view of an enlarged wing showing one embodiment of the present invention.
【図7】本発明の一実施例を示す拡大翼を先端側から見
た正面図である。FIG. 7 is a front view of the enlarged wing, showing one embodiment of the present invention, as viewed from the tip side.
【図8】本発明の一実施例を示す拡大翼回りの断面図で
ある。FIG. 8 is a sectional view around an enlarged wing showing one embodiment of the present invention.
【図9】本発明の一実施例を示す拡大翼回りの断面図で
あり、拡大翼を拡大した状態を示す。FIG. 9 is a cross-sectional view around an enlarged wing showing one embodiment of the present invention, showing a state where the enlarged wing is enlarged.
【図10】本発明の一実施例を示すビット装置先端側の
圧縮空気路を示す示す断面図である。FIG. 10 is a cross-sectional view showing a compressed air passage on the tip end side of a bit device according to an embodiment of the present invention.
【図11】本発明の一実施例を示すビット装置の平面図
である。FIG. 11 is a plan view of a bit device showing one embodiment of the present invention.
【図12】本発明の一実施例を示すビット装置基端側の
圧縮空気路を示す示す断面図である。FIG. 12 is a sectional view showing a compressed air passage on the base end side of the bit device according to the embodiment of the present invention.
【図13】従来例を示す拡大翼の取付状態を示す要部の
断面図である。FIG. 13 is a cross-sectional view of a main part showing an attached state of an enlarged wing showing a conventional example.
【図14】従来例を示すビット装置先端側の圧縮空気路
を示す示す断面図である。FIG. 14 is a cross-sectional view showing a compressed air passage at the tip end side of a bit device showing a conventional example.
6 デバイス 10 排出溝 15 ビット装置 21 取付溝 22 枢着軸 24 枢着溝 22A 球面部 23 拡大翼 24 係合凹溝 32 テーパ面 32A 胴周面 42 圧縮空気路 42A 分岐通路 43 第1の溝部 45 第2の溝部 D ビットの直径 L ビットの胴周面の長さ 6 Device 10 Discharge groove 15 Bit device 21 Mounting groove 22 Pivot shaft 24 Pivot groove 22A Spherical portion 23 Enlarged wing 24 Engagement groove 32 Tapered surface 32A Body peripheral surface 42 Compressed air path 42A Branch passage 43 First groove 45 The second groove D The diameter of the bit L The length of the circumferential surface of the bit
───────────────────────────────────────────────────── フロントページの続き (72)発明者 加藤 富夫 新潟県新津市大字中村285番地3 有限会 社ウエルマン内 (72)発明者 田中 秀穂 新潟県新津市大字中村285番地3 有限会 社ウエルマン内 (72)発明者 松田 広希 新潟県新津市大字中村285番地3 有限会 社ウエルマン内 Fターム(参考) 2D029 DE01 EB01 PA02 PB02 PB03 PB05 ──────────────────────────────────────────────────続 き Continued on the front page (72) Inventor Tomio Kato 285-3 Nakamura, Oaza, Niitsu, Niigata Prefecture Inside Wellman Co., Ltd. 72) Inventor Hiroki Matsuda 285, Nakamura, Niitsu-shi, Niigata F-term in Welmann Co., Ltd. (Reference) 2D029 DE01 EB01 PA02 PB02 PB03 PB05
Claims (4)
端に、ビット装置を前進及び後退可能に設け、前記デバ
イスの先端に、放射方向に回動可能な複数の拡大翼を枢
支し、前記デバイスの前記ビット装置に対する後退によ
り前記拡大翼を前記デバイス側に収納する取付溝を前記
デバイスに設け、前記デバイスの前記ビット装置に前進
により前記拡大翼を拡大し、埋設管の先端からビット装
置の先端及び前記拡大翼を突出して掘削を行う掘削装置
において、前記拡大翼の両側から突出する枢着軸を設
け、この枢着軸の両端部を枢着する左右一対の係合凹溝
を前記取付溝の対向する側壁面に形成するとともに、こ
の係合凹溝を前記デバイスの内面に開口させたことを特
徴とする掘削装置。1. A bit device is provided at a tip of a device receiving an impact force and a rotational force so as to be able to move forward and backward, and a plurality of radially rotatable magnifying wings is pivotally supported at the tip of the device. A mounting groove for accommodating the expanding wing on the device side is provided in the device by retracting the device with respect to the bit device, and the expanding wing is expanded by advancing the bit device of the device, and the bit device is inserted from the tip of the buried pipe. In an excavating device for excavating the tip and the enlarged wing, a pivot shaft is provided to project from both sides of the enlarged wing, and a pair of right and left engagement grooves for pivotally coupling both ends of the pivot shaft is provided. An excavator, wherein the excavation groove is formed on an opposing side wall surface of the groove, and the engagement groove is opened on an inner surface of the device.
この枢着軸と係合する前記係合凹溝の断面形状をほぼ半
円状に形成したことを特徴とする請求項1記載の掘削装
置。2. A front end side of the pivot shaft is formed in a spherical shape,
2. The excavator according to claim 1, wherein the cross-sectional shape of the engaging groove engaged with the pivot shaft is substantially semicircular.
端に、ビット装置を前進及び後退可能に設け、前記デバ
イスの先端に、放射方向に回動可能な複数の拡大翼を枢
支し、前記デバイスの前記ビット装置に対する後退によ
り前記拡大翼を前記デバイス側に収納する取付溝を前記
デバイスに設け、前記デバイスの前記ビット装置に前進
により前記拡大翼を拡大し、埋設管の先端からビット装
置の先端及び前記拡大翼を突出して掘削を行う掘削装置
において、前記ビット装置の基端に開口してビット装置
の先端部まで圧縮空気を通す圧縮空気通路を設けるとと
もに、その圧縮空気通路の先端部から分岐して前記ビッ
ト装置の先端面に開口する複数の分岐通路を設け、か
つ、前記ビット装置の先端面に前記各分岐通路の開口部
の周縁からそれぞれ前記ビット装置の外周に向かって放
射状に形成された第1の溝部を設け、この第1の溝部と
連通する第2の溝部を前記ビット装置の胴周面外側に縦
設するとともに、この第2の溝部と対応して前記デバイ
スの外周に排出溝を形成したことを特徴とする掘削装
置。3. A bit device is provided at a tip of a device receiving an impact force and a rotational force so as to be able to move forward and backward, and a plurality of radially rotatable expanding wings are pivotally supported at the tip of the device. A mounting groove for accommodating the expanding wing on the device side is provided in the device by retracting the device with respect to the bit device, and the expanding wing is expanded by advancing the bit device of the device, and the bit device is inserted from the tip of the buried pipe. In a drilling device that excavates by extruding the tip and the expanding wing, a compressed air passage that opens to the base end of the bit device and allows compressed air to pass to the distal end of the bit device is provided, and from the distal end of the compressed air passage. A plurality of branch passages that are branched and open at the distal end surface of the bit device are provided, and the distal end surface of the bit device is forwardly provided from the periphery of the opening of each branch passage. A first groove portion is formed radially toward the outer periphery of the bit device, and a second groove portion communicating with the first groove portion is vertically provided outside the body peripheral surface of the bit device. An excavator, wherein a discharge groove is formed on an outer periphery of the device corresponding to the groove of (1).
の直径の7〜15%とするとともに、前記ビット装置の胴
周面の長さを30〜40mmに設定したことを特徴とする請
求項3記載の掘削装置。4. The method according to claim 1, wherein the depth of the first groove portion is set to 7 to 15% of the diameter of the bit device, and the length of the body peripheral surface of the bit device is set to 30 to 40 mm. An excavator according to claim 3.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2001088604A JP3706039B2 (en) | 2001-03-26 | 2001-03-26 | Drilling rig |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2001088604A JP3706039B2 (en) | 2001-03-26 | 2001-03-26 | Drilling rig |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2002285778A true JP2002285778A (en) | 2002-10-03 |
| JP3706039B2 JP3706039B2 (en) | 2005-10-12 |
Family
ID=18943674
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2001088604A Expired - Lifetime JP3706039B2 (en) | 2001-03-26 | 2001-03-26 | Drilling rig |
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| Country | Link |
|---|---|
| JP (1) | JP3706039B2 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006025713A1 (en) * | 2004-09-03 | 2006-03-09 | Byung-Duk Lim | A drilling apparatus having in-line extending wings and driving method thereof |
| KR101229209B1 (en) | 2012-08-13 | 2013-02-01 | 이수영 | Hammer bit |
| KR101523298B1 (en) * | 2013-05-23 | 2015-05-28 | (주)씨엔피텍 | Drilling bit |
| WO2017116001A1 (en) * | 2015-12-29 | 2017-07-06 | 동림산업 주식회사 | Head-enhanced drill bit |
| US11959336B2 (en) | 2017-07-24 | 2024-04-16 | Luc Charland | Drilling system and method of using same |
-
2001
- 2001-03-26 JP JP2001088604A patent/JP3706039B2/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006025713A1 (en) * | 2004-09-03 | 2006-03-09 | Byung-Duk Lim | A drilling apparatus having in-line extending wings and driving method thereof |
| AU2005280737B2 (en) * | 2004-09-03 | 2011-01-27 | Everdigm Rock Tools Group | A drilling apparatus having in-line extending wings and driving method thereof |
| KR101229209B1 (en) | 2012-08-13 | 2013-02-01 | 이수영 | Hammer bit |
| WO2014027819A1 (en) * | 2012-08-13 | 2014-02-20 | Lee Kwang Ik | Hammer bit and ground perforation method using same |
| KR101523298B1 (en) * | 2013-05-23 | 2015-05-28 | (주)씨엔피텍 | Drilling bit |
| WO2017116001A1 (en) * | 2015-12-29 | 2017-07-06 | 동림산업 주식회사 | Head-enhanced drill bit |
| US11959336B2 (en) | 2017-07-24 | 2024-04-16 | Luc Charland | Drilling system and method of using same |
| EP3658741B1 (en) * | 2017-07-24 | 2026-01-21 | Luc Charland | Drilling system and method of using same |
Also Published As
| Publication number | Publication date |
|---|---|
| JP3706039B2 (en) | 2005-10-12 |
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