JPS5985214A - Walking rice transplanter - Google Patents

Walking rice transplanter

Info

Publication number
JPS5985214A
JPS5985214A JP19545682A JP19545682A JPS5985214A JP S5985214 A JPS5985214 A JP S5985214A JP 19545682 A JP19545682 A JP 19545682A JP 19545682 A JP19545682 A JP 19545682A JP S5985214 A JPS5985214 A JP S5985214A
Authority
JP
Japan
Prior art keywords
coil spring
aircraft
operating
lever
operating tool
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
Application number
JP19545682A
Other languages
Japanese (ja)
Other versions
JPH0160209B2 (en
Inventor
守屋 利正
入江 滋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kubota Corp
Original Assignee
Kubota Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Kubota Corp filed Critical Kubota Corp
Priority to JP19545682A priority Critical patent/JPS5985214A/en
Publication of JPS5985214A publication Critical patent/JPS5985214A/en
Publication of JPH0160209B2 publication Critical patent/JPH0160209B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Transplanting Machines (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 本発明は、車輪を対機体駆動昇降させる操作部傾、コイ
ルスプリングで接地側に付勢された41号ff1lJ接
地フロートをその対1心多がほぼ一定に維持されるよう
に機械的に連動−rると共に、人為操作具を機械的に連
動し、前記コイルスプリングに対してそれがIIQ記フ
ロートに対して非作用状態にあるいは実質的に非作用状
態に9J換えられるように作用する牽制部材に、前記人
為操作具を機械的に連判した歩行4))、 1.114
i’i機に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention has a tilting operation part for raising and lowering the wheel by aircraft-based driving, and a No. 41 ff1lJ grounding float biased toward the grounding side by a coil spring, whose number of cores is maintained almost constant. The coil spring is mechanically interlocked so that it is mechanically interlocked, and the human operating tool is mechanically interlocked so that the coil spring is in a non-acting state or substantially in a non-acting state with respect to the float. Walking in which the human operating tool is mechanically connected to a restraining member that acts as follows 4)), 1.114
Regarding i'i machine.

上記歩行へ“シ1(1植!ハ、コイルスプリングな非作
用状態に1.?J換えることにより、接地フロートの揺
−J俣出による車輪の対機体自動昇降制御を敏感にして
機体をやや上昇姿勢側VC維持し、各整地フロートの泥
面に対する摺接抵抗を軽減した状態で軽く機体旋回でき
るようにしたものであるが、人為操作具と車輪昇II、
ト操作部及び牽り111部相とを連東;Jする圧、従来
、2本のりイヤーやロッド等により車輪Vf、降操作部
と牽il+11部相とを人為操作具に対して各別に連判
連結していた。
By changing 1.?J to the coil spring inactive state, the automatic lifting control of the wheels relative to the aircraft due to the swinging of the ground float will be made more sensitive to the aircraft, and the aircraft will be slightly lowered. This allows the aircraft to turn easily while maintaining the ascending attitude side VC and reducing the sliding resistance of each ground leveling float against the mud surface.
Conventionally, the wheel Vf, the lowering operation part and the traction 111 part are connected to the manual operation tool using two rope ears, rods, etc. It was connected.

しかしながら、人為操作具からの連動系か2系統となる
ために、構造が複雑になる欠点があった。
However, since there are two interlocking systems from the human operating tool, there is a drawback that the structure is complicated.

本発明の目的は、上述従来の実情に鑑みて、簡単かつ合
理的な改良により、人為操作具からの連III措造を簡
略化し、しかも、コイルスプリングの機N?、をより一
層lI!実にすると共に、操作構造をコンパクト化し得
るようにする点にある。
In view of the above-mentioned conventional situation, it is an object of the present invention to simplify the series III measures from the human operating tool by simple and rational improvements, and to solve the problem of coil spring machines. , even more! The object of the present invention is to make the operating structure more compact.

本発明の特徴構成け、旨記歩行型1)目′f1機におい
て、曲記人為操住1↓と操作部との連111’J部月金
1)11記コイルスプリング内に挿通し、01]記連動
部1’4 K曲記牽制部祠を取付けである串にある。
Features of the present invention: In the walking type 1) item 'f1 machine, the connection between the artificial control unit 1↓ and the operating section 111'J part 1) 11 is inserted into the coil spring, 01 ] Record interlocking part 1'4 K music restraining part shrine is attached to the skewer.

り才り、牽制部材−を人為操作具と操作部とのA uv
)部材に取付けるだけの簡単な喀良により5、連動部+
Aを兼用利用する状態で人為操作具からの連n(1,1
描造を一系統にすることができて、操作部及び牽制部材
に対する操作構造を大中に簡略化することができるに至
った。
The A uv between the human operating tool and the operating part is a check member.
) 5. Interlocking part +
When A is used for multiple purposes, the connection n (1, 1
The drawings can be made into one system, and the operation structure for the operation section and check member can be greatly simplified.

しかも、その連!IIIJ部相をコイルスプリング内に
挿辿するものであるから、連WJ部+、i を更に利用
してコイルスプリングの伸縮時の保形を図ることができ
て、コイルスプリングの付勢機能を良好に維持すること
ができ、さらに、コイルスプリング1j: l1lhの
箇所Kitけるに比して、コイルスプリングの専有スペ
ース看:も省くことができるに至り、全体として、製作
・組付は面並びに経済面に優れ、しかも、操作構造がコ
ンtXuクトであり、かつ、車輪の自前昇降制御性能に
優itた歩行型tlj t+T機を提供し得るに至った
。
Moreover, that series! Since the IIIJ part is inserted into the coil spring, the continuous WJ parts + and i can be further utilized to maintain the shape of the coil spring when it expands and contracts, improving the biasing function of the coil spring. In addition, compared to the coil spring 1j:l1lh part, the dedicated space for the coil spring can be saved, and overall, the manufacturing and assembly is much easier in both terms of production and economics. It has now been possible to provide a walking type tljt+T machine which has excellent performance, has a compact operating structure, and has excellent self-elevating and lowering control performance of its wheels.

次に本発明の′ノテ施例を例示図に、7i’=づいてt
tF述する。
Next, 7i' = t
tF will be described.

第1図に2ドずように、左右一対の推進七輪(八及び、
それとのta働により機体を対地支持する整地フロート
2)を備えた機体フレーム(3)に、萌部原切部(4)
、及び、左右一対の後方延出桿縦/翫ンドル(5)を設
けると共に、一定ストロークで一横往(Xi移切する傾
斜菌のせ台(61、及び、その苗σ)せ台161m左右
に・1νべて載欝された複数枚の7 ・7ト状苗県)の
夫々の下憎列から順次−株分づつの苗を取出し泥面に1
−ij付ける複数の1′I′1植付爪(71等諸装圓を
備えた苗植付装置(8)t%機体フレーノ・(3)の後
部に取付け、もって、機体の走行に伴ない順次複数条の
苗を植付ける歩行型出Ii1′(機をti’li成しで
ある。
As shown in Figure 1, there are a pair of propulsion seven wheels on the left and right (8 and 8).
A moebehara-kiri section (4) is attached to the fuselage frame (3) equipped with a ground leveling float 2) that supports the aircraft on the ground by its tacking action.
, and a pair of left and right rear-extending vertical/rod handles (5), and a tilted bacterial rack (61 and its seedlings σ) that moves horizontally (Xi) with a constant stroke (61 and its seedlings σ) on the left and right of the rack 161 m.・Sequentially take out one seedling from the bottom row of each of the 7-shaped seedlings placed on the ground and place them on the mud surface.
- ij attached to multiple 1'I'1 planting claws (71 etc. Seedling planting device (8) equipped with various mounting rounds) attached to the rear of the fuselage Freno (3), and with it, as the aircraft travels. This is a walking type method of planting multiple rows of seedlings in sequence.

前記左右一対の推進車輪(1)は、それらを取付けた左
右一対の車輪伝1リケース(9)ヲ油圧シリンダ(lO
)により左右一体内に機体横開き軸芯(P1周りで揺I
W)操作することにより対機体駆1111J昇N 4・
F作自rEに構成されており1走行状況に応じて機体の
対地+4さ葡久用できるように措成し7である。
The pair of left and right propulsion wheels (1) are connected to a hydraulic cylinder (lO
), the left and right sides of the aircraft are integrated into the horizontal opening axis (I swing around P1).
W) By operating the anti-aircraft drive 1111J Ascension N 4.
It is configured as F's own rE, and is designed to allow the aircraft to maintain +4 points above the ground depending on the driving situation.

+r+i l+I月′1仕に4’+’;i成されており
、(直イ鷲1作業時におい−U 、耕盤の凹凸に起因し
て1ijp′tV輪(1)の相対44.さが変化1−た
嚇合にも、その背反揺哨作用により機体−)及びに植伺
装置P’f +81 を略水平安勢に維持するべく構1
氏[7゛Cある。
+r+i l+I 4'+'; Even in the face of change 1-, the aircraft was able to maintain the aircraft (-) and the landing gear P'f +81 in a nearly horizontal position by its anti-rotation patrol function.
Mr. [There is 7゛C.

1111ル〜屯輔(1)の対(携体昇叶操(「構造&(
ついて以ト訂1!15する。
1111 le ~ Tunsuke (1) pair (portable body promotion ("Structure & (
Therefore, I am going to revise 1!15 below.

第2ト自イ)に示すように、機体フレーム(3)の前端
側左右中央箇所に、1個のセンサーフロート(11)を
、その曲端側横開き軸芯fQ)周りで揺初自在に連設す
ると共に、00記油圧シリンダ(10)操作用バルブ1
121に連動連結したL型4.+311J都桐(131
の揺…り端部とセンサーフロート曲の移’ ml、!部
とをロッド(141により連動連結しである。  イ:
[7て、■・型拙切部+4(131の揺1i1j+端部
の、L辺に梓当仔印する揺pg)接当部イ4’ 115
! @・イtしてL型揺胛部44 na+の揺n1り端
部並びにセンサーフ0−) 1111を下方側に付勢す
るコイルスプリング+lO1fr H’にけ、もって、
−ffイルスフリングl1lil G?:よ171=/
サーフ0−ト11211c %Z ’r、i7. m地
mf 1. ’lr、 +I与した状態で1iri付、
に行を行ない、刊盤深さの変illりに一弓因したセン
サーフロー11111の揺輯Iノ回出に寿、ついてパル
プ11z食自111jl操イt’: t、、つまD 1
1+Jt盤深さか深(なりスプリング叩に抗してヒンサ
ーフ[J−ト(111が上昇4:ij HIUr L/
た場合にC′」1、車輪(1)を対機体自d1.lJ”
F叶さぜ、かつ、耕盤19jさが浅くなりセンサーフロ
ート111)が下降lit? 1117 L、た場合に
は、屯M (11’e対卵町体自gp) J、 jjl
サセテJi’1(’J装闘t81 ′5C対地増υJ作
業高さに維持ずべく機体6.・自動昇降制御するように
構成しである。
As shown in Figure 2), one sensor float (11) is placed in the left and right center of the front end of the fuselage frame (3) so that it can swing freely around the horizontal opening axis fQ) on its curved end. 00 hydraulic cylinder (10) operating valve 1
L type 4. linked to 121. +311J Miyako Kiri (131
The rocking end and sensor float song transfer 'ml,! The parts are interlocked and connected by a rod (141).
[7, ■・Choosely cut part + 4 (shape 1i1j + end of 131, shank pg with azusa mark on the L side) Contact part a 4' 115
! At the end of the L-shaped swing part 44 na+ and the coil spring + lO1fr H' that biases the sensor f0-) 1111 downward,
-ffIlsfringl1lil G? :yo171=/
Surf 0-t 11211c %Z'r, i7. m ground mf 1. 'lr, with 1iri with +I applied,
11111, which was caused by the change in the depth of the printing board, and the pulp 11z food self 111jl operation t': t,, Tsuma D 1
1+Jt board depth or depth (Hinsurf against the spring strike [J-t (111 rises 4:ij HIUr L/
C'''1, the wheel (1) is placed against the aircraft itself d1. lJ”
F, and the tiller 19j becomes shallower and the sensor float 111) lowers. 1117 L, if tun M (11'e vs. Tamachi body gp) J, jjl
The aircraft is configured to automatically raise and lower to maintain the working height.

面、ロッド(14)の対し型4m fttg部材(13
1連結部に設けた長穴融通部(t4a)は、O’を付装
置(8)が対地適正4r業M1さKeyる時にセンサー
フロー) tillの揺利検出に基づくパルプ(121
自利操作に不感帯を股&Jるためのものであり、機体自
−り痒降制神のハ/ヂンクを防止−4″るように構成し
である。
face, rod (14) opposite type 4m fttg member (13
The elongated hole accommodating part (t4a) provided in the connecting part 1 connects the pulp (121
It is designed to cross a dead zone during self-advantageous maneuvers, and is designed to prevent the aircraft from becoming insensitive to its own operations.

’ijl +itj ハル)+1212 操作するに、
センサーフロー) tillの揺W月々出に基づいた自
制操作に優先して、操縦ハンドル(5)K設けた操作レ
バ−+171操作tてよV人為操作自在に構成されてお
り、次に、その人為操作溝造について第2図(イ)、(
ロ)、(’′9.に)により詳述する。
'ijl + itj hull) +1212 To operate,
In order to give priority to the self-control operation based on the monthly output of oscillations (sensor flow) till, the control handle (5) is configured to be able to be operated freely by man using the control lever (5) K and the control lever (171). Fig. 2 (A), (About the operation groove construction)
b) and (in ``9.'').

l’ifl filj L ;〜Q FITS ll+
、’J部+4’ 11!lに一体梱切自イEにjす3結
しグi ’T” −1,fllll 、5、前記揺剣接
当部桐(15)のスジリンク1l1il仕月3側端部と
を、揺…り接当部材1151側に連結1、 fr、 1
4 、ltZビンf1!11 (i; ’rアームIR
I tftl形成した長大(teq)に係合させ゛C連
110ノ連結すると共に、操作レバーf+71 トl1
ls 1lilJ l&当部tt Is;とを、ON記
コイJl/スプリング(161に種油ずる状態に配置さ
れたワイヤー■を介して連111J連結し、もって、操
作レバー(17)操作により下記(イ)、(ロ) 、 
fJ 、に)の4操作状彫を現出するべく構成しである
。
l'ifl filj L ;~Q FITS ll+
,'J part +4' 11! 5. Connect the threaded link 1l1il of the rocking sword contact part paulownia (15) to the end of the rocking sword 3 side. ...connected to the contact member 1151 side 1, fr, 1
4, ltZ bin f1!11 (i; 'r arm IR
I tftl is engaged with the formed elongate (teq) and connected to the C chain 110, and the operating lever f+71 to l1
ls 1lilJ l & this part tt Is; are connected to the ON-marked carp Jl/spring (161) via the wire ■ placed in a state where the seed oil is dripping, and then by operating the operating lever (17), the following (I) is connected. ),(B) ,
It is constructed to express the four operation shapes of fJ, ni).

(イ) 操作レバー(17iを自動制御位置+Alに操
作することにより、第2図(イ)に示す如(、ワイヤー
!211 を緩め、スプリング(161によるセンサー
フロー ート山)の゛ト方回付勢ヲ許容すると共に、パルプ11
21中立状1.・裸において係止ビン(19が長穴(i
sa)の略中間部に位11シ1するようにし、その長穴
(18A)のM!l! jf1作用をもってアーム(1
8)の揺利紮許容するこ♂によりスプリング1】6)付
勢状態のセンサーフD−1−Il+の揺i1(1月・々
出に基づくL型揺111J都祠(13Iの」−下揺りf
υを許1イして、パルプ(12Iを自111+H操作さ
せる前述機体自1i1J昇叶制御状誹。
(a) By operating the operation lever (17i) to the automatic control position +Al, loosen the wire !211 and rotate the spring (sensor float mountain by 161) as shown in Figure 2 (a). While allowing the bias, the pulp 11
21 neutral state 1.・When naked, the locking bottle (19 is a long hole (i)
11 shi 1 approximately in the middle of sa), and M! of that long hole (18A)! l! Arm (1
8) By allowing the oscillation of the spring 1] 6) The energized state of the sensor valve D-1-Il+'s oscillation i1 (L-type 111J Toshi (13I's) based on January 2011 - lower oscillation) f
υ is allowed and the pulp (12I is operated by 111+H).

(ロ)操作レバー171を旋回位「イ(*+に押作し、
かつその位11′1に片構成したレバー係止溝(21a
)に係[ヒ保持することにより、小2図(ロ)に示す如
く揺I切接当部月115)をスプリング11610伺勢
力に抗して中立状1氾の1.型部^Tり部(オ(131
から離間した揺WIJ位Klfに保↑vし、スプリング
161 Kよるセンサーフロートt+n +1勢作用を
解除して、センサーフロート曲の設定接地(Ii7車e
略0にすると共に、パルプ1121中立状p1子におい
て係止ビン(1!1が」・と穴(18りの中間部からや
や片寄った位置に位1r!するようにして、長大(18
a)の融通作用による前記り型揺動部材1131の上下
揺朝許谷状態ヲ維持し、もって、センサーフロー) 1
11+の上昇揺!II検出に基づ(パルプ113の車輪
対機体下降側への自制操作を敏感して機体及び植付装@
 (81’tやや上昇姿勢側に維持し、整地フロート(
2)の泥面に対する摺接抵抗を軽減した状態で機体旋回
を円滑に行なわせるための状態。
(b) Push the operation lever 171 to the turning position "A (*+),
And there is a lever locking groove (21a) formed in one piece at 11'1.
), by holding the oscillating I-cut abutment part 115) against the force of the spring 11610, as shown in Figure 2 (B), in the neutral state 1 flood. Mold part ^ T rib part (O (131
Hold Klf at the oscillation WIJ distance from ↑v, release the sensor float t + n + 1 force action by spring 161 K, and set the sensor float song to the ground (Ii7 car e
At the same time, make the pulp 1121 in the neutral state p1 so that the locking bottle (1!
The above-mentioned vertical swinging member 1131 is maintained in a vertically oscillating state by the accommodating action of a), thereby increasing the sensor flow) 1
11+ rising swing! Based on the II detection (sensitizing the self-control operation of the pulp 113 between the wheels and the lowering side of the fuselage, the fuselage and planting equipment @
(81't Maintain a slightly upward position and use the leveling float (
2) A condition that allows the aircraft to turn smoothly while reducing sliding resistance on muddy surfaces.

(ハ)操作レバー1171を固定位11. fNlに操
作し、かつその位IQのレバー係止ilt (21h)
 K−係止保持することにより、第2図(ハ)に示す如
く“、揺−接当部’F4’ 1151 fスプリング叩
に抗して中立状態のLハ゛シ拙if(り部材(131か
ら太きく 1lilI I/IJさぜると共に、パルプ
1121中)′L状鈎において係止ビン+191が長大
(18a)の端部に接当する位置に位置保持されるよう
にし、長大(18&)と係止ビン+19との係止作用よ
りL型部削部材口3の中立位置からの下+”f−揺!1
tlIヲ阻止して、パルプ(121の車輪対機体」−昇
側への操作を牽制し、路」二走行時管における機体の上
昇管5i′)を維持する状態。
(c) Move the operating lever 1171 to the fixed position 11. Operate to fNl and lock the lever to that extent IQ (21h)
As shown in FIG. 2(C), by holding the K-lock, the L-height in the neutral state resists the swinging force of the swinging abutting part 'F4' 1151f spring. While shaking the pulp 1121)', make sure that the L-shaped hook holds the locking bottle +191 in a position where it comes into contact with the end of the long piece (18a) and engages it with the long piece (18&). Due to the locking action with the locking pin +19, the L-shaped cutting member mouth 3 is lowered from the neutral position +"f-swing!1
A state in which the pulp (121 wheels to the fuselage) is restrained from moving to the ascending side, and the ascending pipe 5i' of the fuselage in the traveling pipe is maintained.

に)操作レバー(171をスプリングfJ1i1の付り
力に抗して上昇位IPt (11まで操作′ノーるこ七
に伴ない1、N12図に)に示す如く、係止ビン(19
1の長穴(tsa)端部に対する係止作)11をもって
L型揺動部材+13を強制的に上昇揺動させて、パルプ
112 f:車輪対機体下降側に操作し、路上走行等に
際して機体を強制上昇させる状態。
1) Move the operating lever (171) to the raised position IPt against the biasing force of spring fJ1i1 (operate up to 11).
1) Forcibly swing the L-shaped swinging member +13 up using the locking action on the end of the elongated hole (TSA) 11, and operate the pulp 112 f: toward the wheel-to-aircraft downward side to prevent the aircraft from moving on the road, etc. A state in which the value is forced to rise.

尚、前記操作レバー+171は、本機側から植付装置(
8)への動力伝1事を断続操作する植付クラッチ(図示
せず)にも連動されており、操作レバー(171を自1
制御位[IAIに操作することに伴ない植伺クラッチを
自!1lIJ的に入V操作し、かつ、操作レバー(1η
を他の操作位1i2 (14、fNl’ 、 (ulに
操作することに伴ない植伺りラッヂを・自動的に切り操
作できるようにし、走行状態に応じた機体の人為昇降操
作と植付装置#¥(8)の駆動操作とを一本の操作レバ
ー(171で同時に行なえるように構成しである。
In addition, the operation lever +171 can be used from the machine side to the planting device (
It is also linked to a planting clutch (not shown) that operates the power transmission 1 on and off to 8).
Control position [The clutch is automatically activated when operating the IAI! 1lIJ input V operation, and the operation lever (1η
When operating 1i2 (14, fNl', (ul), the planting latch can be automatically cut and operated, and the machine can be manually raised and lowered according to the driving condition and the planting device can be operated. It is configured so that the drive operation of #¥ (8) can be performed simultaneously with a single operating lever (171).

tた、1:1!中(271け、主クラツチレバ−Uと主
クラッチ外の操作部材(24a)とを連削連結するワイ
ヤーf21i1にJl’/ (XJけられたコイルスプ
リングであり、−1己クラツヂレバー4221 k明り
操作することに伴ない、第2図(ハ)に示す如く、アー
ノ・(8)σと1一端側係止部(18h) Kコイルス
プリングGel ’fir押圧接当させ、そのコイルス
プリング哨係止s (tsb)に対する抑圧接当作用、
及び、主クラツチレバ−(v9JF)操作に先行して行
逐われるoff記昇Plf!用操作レバー(171の固
定位置(閣への操作に伴ガう係止ピン(1g)と長穴(
18a)との係止作用、それら同作用(てよV主クラッ
チレバ−f22i切り操作時にtま、自動的Qてパルプ
(121の自動昇1・干操作を牽制し、例えば、苗補給
時においてセンサーノロ−) (Ill カ感用し、機
体が不測に自111J *、降することを(IYHi実
に防11・−「るように、しかも、苗補給高さ1+’j
節等のために主クラッチ(24i切り状態において機体
を上昇する必要がある場合には、コイルスプリング(2
71の旧勢力に抗した昇−ト用操作レバー07+操作に
よりtf!体を強制的に」1昇操作できるように構成し
である。
It was 1:1! It is a coil spring with Jl'/ Accordingly, as shown in Fig. 2 (c), Arno (8) σ and 1 one end side locking part (18h) K coil spring Gel 'fir are pressed into contact with each other, and the coil spring guard lock s ( suppressive abutment effect on tsb),
And, the OFF register Plf! is executed prior to main clutch lever (v9JF) operation. Fixed position of operation lever (171)
18a), and the same effect (when the V main clutch lever f22i is disconnected, the automatic Q clutch lever (121) is checked against the automatic raising and drying operations, for example, when replenishing seedlings. (IYHi actually prevents the aircraft from descending unexpectedly at 111J) (IYHi actually prevents 11.
If it is necessary to raise the aircraft with the main clutch (24i disconnected) due to knots, etc., use the coil spring
tf by operating the lift control lever 07+ against the old forces of 71! It is configured so that the body can be forcibly raised to 1.

以−ヒ、要するに、111記接坤11m市4jL定用コ
イルスプリング(16)のセンサフロート(111に対
する村上)作ntを操作レバー(171操作に伴ないイ
ト用状内と非作用状態とに切換えるようにイド用するI
n’t E+’・J接当用ち桐(15)金、FT1バ1
−己操作レバー(17)とパルプ1121 、:をj全
納連結するワイヤー(飛に直45”(的に成句けたこと
により、そのTツイヤ−(2nIi兼用利用する状Qす
でパルプ112及び拙nυ]接当部材1.Ijil K
対する操作レバー f171 カらノ連*’Itf’t
 m f−1系統1(1,、(−(7)連p+ tS;
造全簡略化するようKt71′I成」7である。
In short, the sensor float (Murakami for 111) of the 111 contact 11m city 4jL fixed coil spring (16) is switched between the operating state and the non-acting state according to the operation of the operating lever (171). I use it like this
n't E+'/J contact paulownia (15) gold, FT1 bar 1
- The self-operating lever (17) and the pulp 1121 are connected by a wire (directly 45") (by virtue of the fact that the T-wheel (2nIi) can be used for both the pulp 112 and the ] Contact member 1. Ijil K
Control lever for the f171 Karanoren*'Itf't
m f-1 lineage 1 (1,, (-(7) consecutive p+ tS;
Kt71'I is constructed to simplify the construction.

また、そのTツイヤ−卵を捨地回市消定用コイルスプリ
ング(旧に挿通間Fi したことにより、ワイヤーイ淵
によってコイルスプリング(16)の伸縮時の保形をl
d実にして、コイルスプリング(161の付勢4R能金
常に良好に維持するようにすると共に、コイルスゲリン
グ(16)の専有スペースを省e、6jt述連刺構・造
を簡略化したことと相俟って操作補遺を一層コンパクト
化するように構成しである。
In addition, the coil spring (16) for discarding waste land was inserted into the coil spring (formerly), so that the coil spring (16) retains its shape during expansion and contraction due to the wire edge.
d, the biasing 4R function of the coil spring (161) is always maintained in good condition, and the exclusive space of the coil spring (16) is saved. Together with this, the operating supplement is structured to be even more compact.

尚、スプリング(10の七ン刃−フロート山IVX対゛
Lる伺q、゛)作用を、ナ■作レバー(1’n 4・V
作に伴ない作用状1′11・j2非作用状7/!?に切
換えるように作用する部$4’ t:J、前記4111
1+1J接舊部i、4’ ++5+に代えて各種形状及
び各種作ptB拓造の部材を用いるこ々が可能であり、
千t1ら部(・]を総称して牽制部月(15:と称する
。
In addition, the action of the spring (10 seven blades - float mountain IVX vs.
Acting state 1'11・j2 Non-acting state 7/! ? The part that acts to switch to $4't:J, 4111 above
Instead of 1+1J joint part i, 4' ++5+, it is possible to use members of various shapes and various constructions of ptB construction,
The thousand T1 and others (・] are collectively referred to as (15:

す!に、操作レバー(171とパルプ(121とを連1
1すする連:11り部(](澗もτツイヤーに代えてロ
ッドやリンク′fI:、If1イル等各種の構成変更が
可能であり、才だそれに伴ないIK制部材(19の連初
部祠12111 K対する具体的取付は構造も各種の構
成変更が=1能である。
vinegar! , connect the operating lever (171 and pulp (121) in series.
1 Susuru part: 11 parts () (It is also possible to change the configuration of various things such as rods and links in place of τ gear, etc.). Regarding the specific installation of the shrine 12111K, various changes in the structure and configuration can be made.

本発明は、センサーノロートの1iii llσ月灸出
9で基づく中輪の対機体自Wす昇ト”を操作4’l’+
造定備えた各種型式の歩行型用植機を対硯とするもので
イ)る。
The present invention is based on the 1iii llσ moon moxibustion output 9 of the sensor nose.
A) It is a device that uses various types of walk-behind planting machines with built-in construction as a pair of inkstones.

【図面の簡単な説明】[Brief explanation of the drawing]

図面は本発明に係る歩行型用植磯の実施例を例示し7、
第1図は全体側flii図、第2図(イ)、 (ロ) 
。 (ハ)、 L−’、) tま、夫々中輪対機体昇151
!操作4119造の作動状だ1.示すlス1である。 
          ′(1)・・・・・−中輪、11
11・・・・接地ノロ−]・、(121・・ ・・操作
部、(J51・・・・・牽制部r4′、++6+・・・
・・コイルスプリング、0ト・・・・人為1・■作置、
C)Ill・・・・・連pf11部桐。 ?a ] 1 図口)         24
The drawings illustrate an embodiment of the walking-type floating rock according to the present invention7,
Figure 1 is the overall side flii diagram, Figure 2 (a), (b)
. (c), L-',) t, respectively, middle wheel vs. aircraft elevation 151
! Operation status of operation 4119 1. This is the number 1 shown below.
'(1)...--middle ring, 11
11...Grounding slope], (121...Operation section, (J51...Restraint section r4', ++6+...
...Coil spring, 0...Artificial 1.■Creation,
C) Ill...ren pf11 part paulownia. ? a] 1 figure opening) 24

Claims (1)

【特許請求の範囲】 中輪+11を対機体駆りジノ昇降させる操fP部112
1 K 。 コイルスプリング(161で接地側に付勢された揺動接
朋ノロ−) Ill ffiその対地姿勢がほぼ一定に
維持されるように機械的に連!IIQすると共に、人為
操作具(171を機械的に連VJ I、、前記コイルス
プリング(16)に対してそれが前記フロー) +11
に対して非ずi′:用状襲にあるいは実質的に非作用状
態に切]4えられるように作用する牽制部材051に、
前記人為操作具(171th1′ll&械的に連動した
歩行型田植機であって、前記人為操作具(171と操作
部+12との連+IJ部月(20)を1JfI記コイル
スプリング(161内に挿通し、F)II記連7jpJ
部利(2111に前記牽制部材咽を取付けである小を特
徴とする歩行型14植機。
[Claims] Operation fP unit 112 that raises and lowers the middle wheel +11 while driving against the aircraft.
1K. Coil spring (oscillating contact spring biased toward the ground side by 161) Ill ffi Mechanically connected so that its ground posture is maintained almost constant! IIQ and the human operating tool (171 mechanically connected VJ I, it is the flow for the coil spring (16)) +11
to the restraining member 051 that acts in such a way that it is turned into a non-acting state (i': switched to a non-operational or substantially inactive state),
The human operating tool (171th1'll & mechanically interlocked walking type rice transplanter, where the human operating tool (171 and the operating part + 12 connection + IJ part month (20) is inserted into the coil spring (161) F) II Journal 7jpJ
A walking type 14 transplanter characterized by a small size in which the restraining member throat is attached to Beri (2111).
JP19545682A 1982-11-08 1982-11-08 Walking rice transplanter Granted JPS5985214A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19545682A JPS5985214A (en) 1982-11-08 1982-11-08 Walking rice transplanter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19545682A JPS5985214A (en) 1982-11-08 1982-11-08 Walking rice transplanter

Publications (2)

Publication Number Publication Date
JPS5985214A true JPS5985214A (en) 1984-05-17
JPH0160209B2 JPH0160209B2 (en) 1989-12-21

Family

ID=16341365

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19545682A Granted JPS5985214A (en) 1982-11-08 1982-11-08 Walking rice transplanter

Country Status (1)

Country Link
JP (1) JPS5985214A (en)

Also Published As

Publication number Publication date
JPH0160209B2 (en) 1989-12-21

Similar Documents

Publication Publication Date Title
US3173632A (en) Landing gear for hovering type aircraft
US2249861A (en) Two way plow
US2616350A (en) Depth controller
US2437879A (en) Two-way plow
US2521895A (en) Earth boring attachment for tractors
US2872990A (en) Hitch
US2665622A (en) Tractor borne agricultural implement and hitch therefor
US1378196A (en) Tractor-plow
US3116939A (en) Load distributing laterally flexible hitch
US3205950A (en) Wheeled vehicles carrying tool bars for cultivation
US2923363A (en) Disc harrow
US3313094A (en) Mower mounting mechanism
JPS5988016A (en) Walking rice transplanter
JPH0117932Y2 (en)
US1352783A (en) Cultivator
JPS60188005A (en) Machine control device in rice transplanter
JPS6131615Y2 (en)
JPH0126645B2 (en)
SU1038423A1 (en) Levelling machine
JPS60244214A (en) rice transplanter
JPS6239623Y2 (en)
JPS5841123U (en) Riding rice transplanter
JPS6013303Y2 (en) Rice transplanter with automatic control device
JPS5814822Y2 (en) Walking device of rice transplanter
US1321937A (en) Traction-machine