JPH04128438A - Automatic trench excavator - Google Patents
Automatic trench excavatorInfo
- Publication number
- JPH04128438A JPH04128438A JP24855790A JP24855790A JPH04128438A JP H04128438 A JPH04128438 A JP H04128438A JP 24855790 A JP24855790 A JP 24855790A JP 24855790 A JP24855790 A JP 24855790A JP H04128438 A JPH04128438 A JP H04128438A
- Authority
- JP
- Japan
- Prior art keywords
- excavation
- guide material
- excavator
- ground
- camera
- 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.)
- Pending
Links
- 238000009412 basement excavation Methods 0.000 abstract description 52
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 230000003287 optical effect Effects 0.000 description 3
- 239000004020 conductor Substances 0.000 description 2
- 238000005553 drilling Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Landscapes
- Operation Control Of Excavators (AREA)
Abstract
Description
【発明の詳細な説明】
1産業上の利用分野1
この発明は自走式の溝掘り機に関するものであり、4j
fに、地上の誘導体に沿って走行する自動溝掘り機に関
するものである。[Detailed description of the invention] 1. Industrial application field 1. This invention relates to a self-propelled trench digging machine,
Part f relates to an automatic trenching machine that travels along a guide on the ground.
「従来の技術」
従来、此種自走式の溝掘り機は乗用型及び歩行J(II
ともに種々のものかある(特開昭L) 2− I L)
2601 ’、’公報、「f開明t) 2−8620
+) ’J公報等)。``Prior art'' Conventionally, this type of self-propelled trench digging machine has been used for riding type and walking type J(II).
There are various types of both (JP-A-Sho L) 2-IL)
2601', 'Publication, 'f Kaimei t) 2-8620
+) 'J Publication, etc.).
之等のt117i掘り機は乗用型及びノド打型ともに人
手による操作が必要であり、例えば家屋或は樹木等の周
囲を掘削する場合には、作業者が当1核lニジ、掘り機
を運転して掘削個所へ移動し、人手の操作によ−〕で掘
削装置を作動さUる。そして、所定の深さに達したとき
に掘削作業を停止1−シ、1−りひ2行6 i’l’/
J掘り機を運転して他の掘削個所へ移動する1、斯かる
操作を繰り返して一定周囲の掘削を行っている3、1]
発明が解決しようとする課題]
従来の満掘り機は、移動又は掘削の何れの作業のときて
あっても、その都度作業者によって操作しなくてはなら
ない。従って、家屋の周囲の掘削等、比較的簡易な掘削
作業でも人手を要し、作業効率か良好ではなかった。These T117i excavators, both the riding type and the throat type, require manual operation.For example, when excavating around a house or a tree, the operator must operate the excavator. Then move to the excavation location and operate the excavation equipment manually with -]. Then, when the predetermined depth is reached, the excavation work is stopped.
Operating the J excavator and moving to another excavation location 1, repeating such operations to excavate a certain surrounding area 3, 1]
Problems to be Solved by the Invention] Conventional full-digging machines must be operated by a worker each time they are moved or excavated. Therefore, even relatively simple excavation work, such as excavation around a house, requires manpower, and the work efficiency is not good.
そこで、一定周囲を自動走行1−1人丁、を労さずに所
定個所を自動的に掘削するために解決せられるべき技術
的課題か生じてくるのであり、本発明はこの課題を解決
することを1−1的とする。Therefore, a technical problem arises that needs to be solved in order to automatically excavate a predetermined location without the effort of one person to automatically travel around a certain area, and the present invention solves this problem. Let's call it 1-1.
[課題を解決するための手段11
この発明は+1記ト1的を達成するために提案IJ−ら
れたものであり、地上の誘”1体を読み取る手段と、誘
導体に沿って走行ずへ<1III記読み取り手段に連動
して制御される走行装置とを備え、誘導体の適宜個所に
設けた掘削部指示体を読み取ったときは、機体を停市し
て掘削装置を作動するような制御手段を設けたことを特
徴とする自動t1′l′)掘り機を提供Vんとするもの
である。[Means for Solving the Problems 11 This invention was proposed in order to achieve the above object, and it provides a means for reading an object on the ground without traveling along the guide. A traveling device controlled in conjunction with the reading means described in Section 1III, and a control means that stops the aircraft and operates the excavation device when the excavation section indicator provided at an appropriate location on the guide is read. An automatic t1'l') digging machine is provided.
1−作用1
自動溝掘り機を走行させて掘削を行う予定の行程上には
、予め地l−に誘導体を設けておく。次に、機体を走行
さU“ながら読み取り手段により地上の1透導体を検出
(7、該誘導体と機体とのずれを修正すべく走行装置を
操舵する。そして、読み取り手段の検出と走行装置の操
舵とを連動して制御を行い、地−にの誘導体に沿って機
体を走行させる。1-Function 1 A derivative is provided in the ground in advance on the route where the automatic trench excavator is scheduled to run and excavate. Next, while the aircraft is traveling, the reading means detects a transparent conductor on the ground (7, the traveling gear is steered to correct the deviation between the guiding body and the aircraft body. Then, the reading means detects and the traveling gear Control is performed in conjunction with steering, and the aircraft travels along a guide on the ground.
又、掘削予定個所には予め誘導体に沿って掘削部指示体
を設けてあり、前記読み取り手段によって地1−の掘削
部指示体を読み取ったときは、走行中の機体か停+l−
する。そして、掘削装置か作動して、掘削部指示体か設
i′Jられた個所を掘削する。Further, an excavation part indicator is provided in advance along the guide at the location where excavation is planned, and when the excavation part indicator on the ground 1- is read by the reading means, the moving aircraft is stopped or stopped.
do. Then, the excavation device is operated to excavate the location where the excavation section indicator is installed.
斯くの如く、地上の誘導体に沿つて走行及び掘削を繰り
返し、人手を労さすして自動的に掘削作業を行っていく
。In this way, the machine repeatedly travels and excavates along the guide on the ground, and the excavation work is performed automatically without any manual effort.
[実施例]
以ド、この発明の一実施例を別紙添イ:1図面に従って
詳述する0、第1図は歩行型の自動7+’/i掘り機(
1)の側面図であり、機体(2)の前部には油圧で操作
される掘削アー1− (3)が設けられ、その先端部に
ノ\ケツ1− (/l)を取り付けて掘削装置(5)が
構成されている、。[Embodiment] Hereinafter, an embodiment of the present invention will be described in detail according to the attached drawings.
1), in which a hydraulically operated excavator 1- (3) is installed at the front of the machine body (2), and a drill bit 1- (/l) is attached to the tip of the excavator 1- (3). A device (5) is configured.
機体(2)の左右下部には前輪(6)(6)と後輪(7
)(7)との間にクローラ(8)(8)が巻装され、エ
ンジン(9)の動力を左右のクローラ(8)(8)へ伝
動して走行装置(In)が構成されている。At the bottom left and right of the aircraft (2) are the front wheels (6) (6) and the rear wheels (7).
) (7), and crawlers (8) (8) are wound between them, and the power of the engine (9) is transmitted to the left and right crawlers (8) (8) to constitute a traveling device (In). .
機体(2)の」一部にはセンザア−1\(11)を固設
してあり、該センサアームQ +)は掘削アーム(3)
の」1方位置を前方に延設され、その前部は斜めF方に
屈曲している。該センサアーム(11)の先端部には、
後述する地上の誘導体を読み取る手段としてカメラ(1
多が設けられている。Sensor arm 1 (11) is fixed to a part of the fuselage (2), and the sensor arm Q +) is connected to the excavation arm (3).
The front part is bent diagonally in the F direction. At the tip of the sensor arm (11),
A camera (1
Many are provided.
そして、第2図に示したブロック図のように、ノノメラ
(1つは人力インタフェースを介してCP Uに接続さ
れ、又、11;1記掘削装置(5)及び走行装置(m)
は出力インタフェースを介してCPUに接続されている
。As shown in the block diagram shown in FIG.
is connected to the CPU via an output interface.
ここで、第3図に示すように、家屋(1■の周囲の所々
を掘削する場合について説明する。掘削を行うP 定の
行程−にには、−止めラインマーカ等により白色粉体の
白線を地上に敷設して誘導体(1/l)を設けておく。Here, as shown in Fig. 3, we will explain the case where excavation is carried out in various places around the house (1. is laid on the ground and a derivative (1/l) is provided.
そして、掘削個所には前記誘導体(Vl)−1−に掘削
部指示体(1つ(1つ−・・を設ける。この掘削部指示
体(1ツは、例えば丸印等の適宜形状でよい。。Then, at the excavation location, an excavation point indicator (one...) is provided on the derivative (Vl)-1-. ..
而して、第4図のフローチャー1・に従い、自動111
11)掘り機(1)の掘削作業の手順について説明する
3、先ず、1)11記カメラ(121により地1−に設
けられた白線の1透導体(14)を検出する(ステップ
団1 )。そして、モニタ画面内に写し出された誘導体
(目)の位置と、画面中央位置とのずれを算出する(ス
テップl112 )。Then, according to the flowchart 1 in Fig. 4, the automatic 111
11) Explaining the procedure of excavation work by the excavator (1) 3. First, 1) Detect the white line 1 transparent conductor (14) provided on the ground 1- by the camera 11 (121) (step group 1) Then, the deviation between the position of the guide (eye) projected on the monitor screen and the center position of the screen is calculated (step l112).
ここで、誘導体(N)のずれ方向を判断しくステラフ0
3L該誘導体(図)か画面中央位置より右側に(Y’f
ii′l: L、ているときは機体(2)か誘導体(X
)の左側へずれており、l’l’l i!己定走行装置
I(1)のサイトクラッチを断続操作して機体(2)を
右へ操舵しながら前進走行しくステップ+04)、機体
(2)を誘導体(Vl)ヒヘ戻す。これとは逆に、誘導
体(l/l)が画面中央位置34こり左側に位置してい
るときは機体(2)が誘導体(1/l)の右側へずれて
おり、然るときは、機体(2)を左へ操舵しなから前進
走行しくステップ106)、機体(2)を誘導体(1/
1)−1−へ戻す。又、誘導体(Z)が画面中央位置に
あるときは機体(2)のずれがなく、そのまま左右中央
位置で直進走行する(ステップ団5)3、このようにし
て、カメラ(1つにより地りの誘導体(l/l)を常時
検出しなから機体(2)とのずれを修正ずべく走行装置
(In)を制御し、誘導体(l/l)に沿って機体(2
)を走行させていく。そして、誘導体(x)−1:に設
けられた掘削部指示体(1ツをカメラ(17)が検出し
たときは(ステップ10?)、機体(2)の走行を停止
1ニジて掘削装置(5)を作動さけ、該掘削部指示体(
1ツか設けられた個所を掘削作業する(ステップ108
)。又、ステップ1[)7て掘削部指示体く1ツが検出
されないときはステップl旧へ戻る。斯かる動作を繰り
返し、第3図に示した誘導体(l/l)に沿って自動t
1も掘り機(1)をJjj(人走讐」さ已、掘削部指示
体く1つか設(Jられた所定の個所で停市しなから、家
屋(1→の周囲の掘削作業か人トを煩わずことなく自動
的に為される3゜方、上記動作とは異なり、ステップ団
1から107 に仝、る間は誘導体(→に沿−)で機体
<2)を走行さlると同時に一定の掘削深さて溝掘り作
業を行いながら進行17、ステップ1(17て掘削部指
示体(151を検出したときに機体(2)を停止1・し
、ステップ108でハ1(削指示個所でのル;削深さを
異にするような作業も可能である。Here, to determine the direction of deviation of the dielectric (N), use the steraf 0
3L The derivative (figure) is located to the right of the center of the screen (Y'f
ii'l: When L, the aircraft (2) or the derivative (X
) is shifted to the left of l'l'l i! The site clutch of the self-regulating traveling device I (1) is operated on and off to drive the aircraft (2) forward while steering it to the right (step +04), and the aircraft (2) is returned to the induction body (Vl). Conversely, when the guide (l/l) is located to the left of the screen center position 34, the aircraft (2) has shifted to the right of the guide (1/l); Step 106) to move the aircraft (2) forward without steering it to the left.
1) Return to -1-. Also, when the guide (Z) is at the center position of the screen, there is no deviation of the aircraft (2), and the aircraft (2) moves straight ahead at the left and right center position (step group 5) 3. In this way, the camera (1) The guide (l/l) of the aircraft (l/l) is constantly detected, and the traveling device (In) is controlled to correct the deviation from the aircraft (2), and the aircraft (2) moves along the guide (l/l).
). Then, when the camera (17) detects the excavation part indicator (1) provided on the derivative (x)-1 (step 10?), the machine (2) stops traveling and moves to the excavation device (1). 5), and avoid operating the excavation part indicator (
Excavating one or more provided locations (step 108)
). If the excavation section indicator is not detected in step 1 [)7, the process returns to step 1 (old). Repeat this operation and automatically tt along the derivative (l/l) shown in Figure 3.
The excavator (1) should be stopped at a predetermined place where the excavator (1) should be set up (Jjj (man running enemy)), and the excavation work around the house (1 Unlike the above-mentioned operation, the 3° direction is automatically performed without bothering with steps, and from step group 1 to step group 107, the aircraft is driven by the guide (along →). At the same time, while digging a trench to a certain depth, the machine (2) is stopped when the excavation part indicator (151) is detected in Step 1 (Step 1), and in Step 108, the excavation part indicator (151) is detected. It is also possible to perform work with different cutting depths at different locations.
ここて、第1図に示した)Jメラ(lのの前部側面に光
学式受光器(10を設け、第5図のブロック図に示すよ
うに入力インタフェースを介して光学式受光器(10を
CP Uへ接続し、前記カメラ(1乃と共に読み取り手
段を構成してもよい。そして、第6図に示rように、誘
導体(14)に沿って掘削個所に発光形の掘削部指示体
(r7)(r′7)・・・を設ける。この掘削部指示体
(r7)は発光形であればよく、例えばI用CI)等の
発光素子を使用する。Here, an optical receiver (10) is provided on the front side of the J-mera (l) shown in FIG. may be connected to the CPU and constitute a reading means together with the camera (1). Then, as shown in FIG. (r7) (r'7)... The excavation part indicator (r7) may be of a light-emitting type, and for example, a light-emitting element such as a CI for I is used.
1−記構成の自動溝掘り機(1)の掘削作業の手順は、
前述した第4図のフローチャー1・と全く同様であるが
、ステップH17−Cは掘削部指示体(r?)からの発
光ビートを11;I記光学式受光器(16)により検出
する3、以下、同様にして、機体(2)の走行を停+L
L−C掘削装置(5)を作動さけ、該掘削部指示体(
1力が設けられた個所を掘削作業する。斯かる動作を繰
り返し、第6図に示した家1z4 (1■の周囲の掘削
作業か自動的に為される。1- The procedure for excavation work using the automatic trench digging machine (1) configured as described below is as follows:
It is exactly the same as the flowchart 1 in FIG. 4 described above, but in step H17-C, the light emission beat from the excavation part indicator (r?) is detected by the optical receiver (16) 11; , and thereafter, in the same manner, stop the flight of the aircraft (2) +L
Avoid operating the L-C drilling rig (5), and press the excavation part indicator (
1. Excavate the area where the force is installed. By repeating this operation, the excavation work around the house 1z4 (1) shown in Figure 6 is automatically done.
更に、第1図に於て、機体(2)の前面F部にセンサア
ーム(ゆを突設し、下方に斜設された該センサ゛γ−A
(Iの先端部に超音波セン′す(1つ)等を設it、
第7図のブロック図に示すように入力インフッニスを介
して超音波センサ(19)をCPUへ接続し、掘削装置
(5)のバケツ;・(4)による掘削深さの検出手段を
構成してもよい。Furthermore, in FIG. 1, a sensor arm (Y) is provided protruding from the front F portion of the fuselage (2), and the sensor "γ-A" is provided diagonally downward.
(An ultrasonic sensor (one) etc. is installed at the tip of I,
As shown in the block diagram of Fig. 7, an ultrasonic sensor (19) is connected to the CPU via an input input, and a means for detecting the excavation depth by the bucket (4) of the excavation device (5) is configured. Good too.
上記構成の自動溝掘り機(+)の掘削作業の手順を第8
図に示すが、ステップ団8までは前述した第4図のフロ
ーチャー1・と全く同様であるが、ステップ1(18で
掘削作業を行いながら超音波センサ(+9)により掘削
深さを検出する(ステップ109)。そこで、掘削深さ
が予め設定しである所定値に達したか否かを判断しくス
テップll0L未だ所定値に達していないときはステッ
プ1[]8へ戻って掘削作業を継続する。そして、ステ
ップ1(18から111)のループで掘削深さか所定値
に達したときはステップ1]11へ戻り、lりびステッ
プ101からlIOまての動作を繰り返して掘削作業が
自動的に為されていくのである。The procedure for excavation work of the automatic trench digging machine (+) with the above configuration is explained in the 8th section.
As shown in the figure, steps up to step group 8 are exactly the same as the flowchart 1 in FIG. (Step 109). Then, it is determined whether the excavation depth has reached a predetermined value or not. If the excavation depth has not yet reached the predetermined value, the process returns to step 1[]8 to continue the excavation work. Then, when the excavation depth reaches a predetermined value in the loop of step 1 (from 18 to 111), return to step 1]11, repeat the operations from step 101 to step 10, and the excavation work is automatically started. It will be done to.
尚、この発明は、この発明の精神を逸脱しない限り種々
の改変を為す事ができ、そして、この発明が該改変せら
れたものに及ぶことは当然である。Note that this invention can be modified in various ways without departing from the spirit of the invention, and it goes without saying that this invention extends to such modifications.
し発明の効果1
この発明は上記一実施例に詳述したように、地上の誘導
体に沿って機体カイ1走しながら、掘削部指示体を設け
た所定個所で自動的に掘削作業が行われる。従って、r
・め誘導体及び掘削部指示体を所定位置に設けておけば
、それ以後の作業に人手を労すことかなく、一定周囲に
於ける掘削作業の自動化を図−)で作業効率の向1−に
寄与できる。Effects of the Invention 1 As detailed in the above-mentioned embodiment, the present invention is capable of automatically performing excavation work at a predetermined location provided with an excavation point indicator while the aircraft moves along a guide on the ground. . Therefore, r
・If the guide and the excavation point indicator are installed in the specified positions, the subsequent work will not require any manual effort, and the automation of excavation work in a certain area can be achieved, which will improve work efficiency. can contribute to
図は本発明の一実施例を示したものであり、第1図は自
動溝掘り機の側面図、第2図及び第5図及び第7図はブ
ロック図、第3図及び第6図は地−にに誘導体及び掘削
部指示体を設けた状態を示す平面図、第4図及び第8図
はフローチャー1・である。
(1)・・・・・・自動溝掘り機 (2)・・・・・
・機体(5)・・・・・・掘削装置 Qo)・・
・・・・走行装置(121・・・・・・カメラ
(VI)・・・・・・誘導体θつ(■・・・・・・掘
削部指示体 (10・・・・・・光学式受光器(+q)
・・・・・・超音波センサ
特許 出 願人 井関農機株式会社
同 株式会社 神戸製鋼所The figures show one embodiment of the present invention, in which Fig. 1 is a side view of an automatic trenching machine, Figs. 2, 5 and 7 are block diagrams, and Figs. 3 and 6 are block diagrams. Flowchart 1 is shown in FIGS. 4 and 8, which are plan views showing a state in which the guide body and the excavation part indicator are provided on the ground. (1)・・・Automatic trench digging machine (2)・・・・・・
・Aircraft (5)...Drilling equipment Qo)...
...Traveling device (121...Camera)
(VI)......Inductor θ (■...Excavation part indicator (10...Optical receiver (+q)
...Ultrasonic sensor patent Applicant: Iseki Agricultural Machinery Co., Ltd. Kobe Steel, Ltd.
Claims (1)
べく前記読み取り手段に連動して制御される走行装置と
を備え、誘導体の適宜個所に設けた掘削部指示体を読み
取ったときは、機体を停止して掘削装置を作動するよう
な制御手段を設けたことを特徴とする自動溝掘り機。It is equipped with a means for reading the guide on the ground, and a traveling device controlled in conjunction with the reading means so as to travel along the guide. An automatic trench digging machine characterized by being provided with a control means for stopping and operating the excavating device.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP24855790A JPH04128438A (en) | 1990-09-18 | 1990-09-18 | Automatic trench excavator |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP24855790A JPH04128438A (en) | 1990-09-18 | 1990-09-18 | Automatic trench excavator |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH04128438A true JPH04128438A (en) | 1992-04-28 |
Family
ID=17179934
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP24855790A Pending JPH04128438A (en) | 1990-09-18 | 1990-09-18 | Automatic trench excavator |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH04128438A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998011305A1 (en) * | 1996-09-13 | 1998-03-19 | Komatsu Ltd. | Automatic excavator, automatic excavation method and automatic loading method |
-
1990
- 1990-09-18 JP JP24855790A patent/JPH04128438A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998011305A1 (en) * | 1996-09-13 | 1998-03-19 | Komatsu Ltd. | Automatic excavator, automatic excavation method and automatic loading method |
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