JP2535092B2 - Carrier - Google Patents

Carrier

Info

Publication number
JP2535092B2
JP2535092B2 JP2186821A JP18682190A JP2535092B2 JP 2535092 B2 JP2535092 B2 JP 2535092B2 JP 2186821 A JP2186821 A JP 2186821A JP 18682190 A JP18682190 A JP 18682190A JP 2535092 B2 JP2535092 B2 JP 2535092B2
Authority
JP
Japan
Prior art keywords
engine
traveling
steering
cylinder
machine body
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.)
Expired - Lifetime
Application number
JP2186821A
Other languages
Japanese (ja)
Other versions
JPH0478618A (en
Inventor
明 田中
謙三 古賀
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 JP2186821A priority Critical patent/JP2535092B2/en
Publication of JPH0478618A publication Critical patent/JPH0478618A/en
Application granted granted Critical
Publication of JP2535092B2 publication Critical patent/JP2535092B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Arrangement Of Transmissions (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、不整地走行装置を有した運搬車に関する。Description: [Industrial field of application] The present invention relates to a transport vehicle having an all-terrain traveling device.

〔従来の技術〕[Conventional technology]

上記運搬車において、従来、エンジンと運転部とを機
体横方向に並列配置し、これらエンジン及び運転部と荷
台とを機体前後方向に並列されて配置されていた。
In the above-mentioned transport vehicle, conventionally, the engine and the operating unit are arranged side by side in the lateral direction of the machine body, and the engine and the operating unit and the carrier are arranged side by side in the longitudinal direction of the machine body.

〔発明が解決しようとする課題〕[Problems to be Solved by the Invention]

従来、エンジンが機体側面視において走行装置より機
体前方や後方側に突出して位置すると共に、このことに
起因して、走行用ミッションも同様に位置し、殊に小型
運搬車の場合、荷台が空である時の前後の重量バランス
が悪くなり、機体が前後に傾斜した際の安定性が特に悪
くなりがちであった。
Conventionally, the engine is located so as to project to the front or rear of the machine from the traveling device in a side view of the machine, and due to this, the mission for traveling is also located, especially in the case of a small transport vehicle, the cargo bed is empty. The weight balance between the front and rear of the aircraft tended to be poor, and the stability when the aircraft leaned back and forth tended to be particularly poor.

本発明の目的は、全長や全高の増大を防止しながら、
積車時空車時のいずれにおいても前後の重量バランスが
良い状態にできる運搬車を提供することにある。
The object of the present invention is to prevent an increase in overall length and height,
An object of the present invention is to provide a transport vehicle that can maintain a good weight balance between the front and rear of the vehicle when the vehicle is loaded and unloaded.

〔課題を解決するための手段〕[Means for solving the problem]

本発明による運搬車にあっては、目的達成のために、
左右一対の不整地走行装置を有した走行機体に、運転部
と荷台とを機体前後方向に並列させて備えさせ、エンジ
ンを前記不整地走行装置の入力軸より前記荷台側に寄せ
て前記左右走行装置の間に配置すると共に、前記エンジ
ンの出力を前記不整地走行装置に伝達する走行用ミッシ
ョンを機体側面視で上端側ほど前記エンジン側に寄る傾
斜姿勢で前記エンジンと機体前後方向に並置し、前記荷
台の前記運転部側端部に前記エンジンの上部が入り込む
凹部を備えてある。その作用及び効果は次のとおりであ
る。
In the carrier according to the present invention, in order to achieve the purpose,
A traveling machine having a pair of left and right rough terrain traveling devices is provided with an operating unit and a loading platform in parallel in the longitudinal direction of the fuselage, and the engine is moved closer to the loading platform side from the input shaft of the rough terrain traveling device to run left and right. With the arrangement between the devices, the traveling mission for transmitting the output of the engine to the rough terrain traveling device is juxtaposed in the longitudinal direction of the engine with the engine in a tilted posture toward the engine side toward the upper end side in the side view of the vehicle body, A recess into which the upper portion of the engine is inserted is provided at an end of the cargo bed on the side of the operation unit. The action and effect are as follows.

〔作 用〕[Work]

エンジン、走行用ミッション及び荷台の前記配置構成
によれば、エンジン、走行用ミッション及び荷台夫々の
重心が機体側面視で走行装置の接地範囲内や、それに極
力近い箇所に位置して、車輌全体の重心が荷物重量が作
用してもしなくても接地範囲の極力中心側に位置するよ
うにできる。しかも、その割には、機体側面視におい
て、エンジンの下側部分と走行装置とが重なり、かつ、
エンジンの上側部分と荷台部分とが重なって、荷台が極
力低レベルに位置するように、かつ、運動部に極力接近
するようにできる。
According to the arrangement configuration of the engine, the traveling mission and the luggage carrier, the center of gravity of each of the engine, the traveling mission and the luggage carrier is located in the grounding range of the traveling device in a side view of the aircraft or at a position as close as possible to the grounding range of the entire vehicle. The center of gravity can be positioned as close to the center of the ground contact range as possible with or without the load weight. Moreover, the lower part of the engine and the traveling device overlap in the side view of the aircraft, and
The upper part of the engine and the bed part can be overlapped so that the bed is located at the lowest level and the moving part is brought as close as possible.

〔発明の効果〕〔The invention's effect〕

したがって積載荷物の有無にかかわらず、かつ、走行
地の前後傾斜や凹凸の有無にかかわらず、ピッチングし
にくい等安定して安全に走行できるようになった。
Therefore, regardless of whether or not there is a load, and whether or not the running ground is inclined forward or backward or whether or not there is unevenness, it is possible to travel stably and safely, such as with difficulty in pitching.

しかも、全高も全長も極力小であるようにコンパクト
に構成して操縦や格納がし易い有利なものにできた。
In addition, the overall height and overall length were made as small as possible to make it compact and easy to operate and store.

〔実施例〕〔Example〕

次に実施例を示す。 Next, examples will be shown.

第1図に示すように、運転部(1)を後端側に有した
クローラ式走行機体の前端側に、運転部(1)と機体前
後方向に並列するように配置した荷台(2)をダンプシ
リンダ(3)によって前端側の軸芯(X)周りで上下に
揺動操作できるように取付けて、荷台ダンプが可能な運
搬車を構成してある。
As shown in FIG. 1, on a front end side of a crawler type traveling machine body having a driving section (1) on a rear end side, a loading platform (2) arranged in parallel with the driving section (1) in the longitudinal direction of the machine body is provided. A dump truck (3) is mounted so as to be capable of swinging up and down around a front end side axis (X), thereby forming a transport vehicle capable of dumping a platform.

機体走行を可能にするに、第1図および第2図に示す
ように、機体側面視でエンジン(E)の重心が左右走行
装置(4),(4)の接地範囲内に位置するように、か
つ、エンジン(E)の下側部分が走行装置(4)と重な
るように左右走行装置(4),(4)の入力軸(4a)よ
り荷台側に寄せて左右走行装置(4),(4)の間に配
置したエンジン(E)を、左右走行装置(4),(4)
のトラックフレーム(4b),(4b)に架設のエンジン搭
載フレーム(5)に取付け、そして、エンジン(E)の
機体後方側に位置する走行用ミッション(M)を、上端
側ほどエンジン側に寄る傾斜姿勢でエンジン(E)と機
体前後方向に並列するようにして左右走行装置(4),
(4)に付設すると共に、第4図に示す伝動構造に基い
てエンジン(E)の回転出力を左右走行装置(4),
(4)に伝達するように構成してある。すなわち、エン
ジン(E)の回転出力を伝動ベルト(6)及び入力軸
(7)を介して油圧式無段変速ミッション部分(8)に
入力すると共に、この変速ミッション部分(8)の回転
出力を入力軸(9)を介して高低速2段換え可能なギア
式変速ミッション部分(10)に入力し、この変速ミッシ
ョン部分(10)の前進出力ギア(11)の回動力を一対の
操向クラッチ部材(12a),(12b)の一方を介して一方
の走行装置(4)の入力軸(4a)に、かつ、他方の操向
クラッチ部材(12b)を介して他方の走行装置(4)の
入力軸(4a)に夫々伝達するように、変速ミッション部
分(10)の一対の後進出力ギア(13a),(13b)の一方
の回動力を操向クラッチ部材(12a)を介して一方の走
行装置(4)の入力軸(4a)に、かつ、他方の後進出力
ギア(13b)の回動力を操向クラッチ部材(12b)を介し
て他方の走行装置(4)の入力軸(4a)に夫々伝達する
ように構成してある。
In order to enable the aircraft to travel, the center of gravity of the engine (E) should be located within the ground contact range of the left and right traveling devices (4) and (4) as shown in FIGS. 1 and 2. And, the left and right traveling devices (4) are moved closer to the cargo bed side from the input shaft (4a) of the left and right traveling devices (4) and (4) so that the lower part of the engine (E) overlaps with the traveling device (4). The engine (E) arranged between the (4) and the left and right traveling devices (4), (4)
Attached to the engine mounting frame (5) installed on the truck frames (4b) and (4b) of the vehicle, and the traveling mission (M) located on the rear side of the engine (E) is moved closer to the engine side toward the upper end side. The left and right traveling devices (4) are arranged in parallel with the engine (E) in the front-back direction of the body in an inclined posture.
In addition to being attached to (4), the rotational output of the engine (E) is based on the transmission structure shown in FIG.
It is configured to be transmitted to (4). That is, the rotation output of the engine (E) is input to the hydraulic continuously variable transmission portion (8) via the transmission belt (6) and the input shaft (7), and the rotation output of this transmission portion (8) is also input. It is input to a gear type transmission mission portion (10) capable of changing between high and low speed two stages via an input shaft (9), and the turning power of a forward output gear (11) of this transmission transmission portion (10) is paired with a steering clutch. One of the members (12a) and (12b) is connected to the input shaft (4a) of the one traveling device (4), and the other of the traveling device (4) is disposed via the other steering clutch member (12b). One of the traveling powers of one of the reverse output gears (13a) and (13b) of the speed change transmission part (10) is transmitted to the input shaft (4a) via the steering clutch member (12a) so as to be transmitted to the other. Rotation of the reverse output gear (13b) on the input shaft (4a) of the device (4) and on the other side The is arranged to respectively transmitted to the input shaft (4a) of the other of the traveling device through the steering clutch member (12b) (4).

ギア式変速ミッション部分(10)に、1つの逆転クラ
ッチ(14)及びブレーキ(15)を前記後進出力ギア(13
a)及び(13b)に作用するように付設してある。逆転ク
ラッチ部材(14)を逆転シリンダ(C1)により操作し、
走行ブレーキ(15)をブレーキシリンダ(C2)により操
作し、一対の操向クラッチ部材(12a),(12b)を一対
の走行シリンダ(C3),(C3)によって各別に操作する
ように構成するとともに、これらシリンダ(C1)ないし
(C3)を第3図に示す操作構造に基づいて1本の操向レ
バー(16)により操作し、左右走行装置(4),(4)
の各別な停止、制動及び逆転操作をして機体操向操作を
するように構成してある。
One reverse clutch (14) and brake (15) are attached to the reverse output gear (13) in the gear type transmission (10).
It is attached to act on a) and (13b). Operate the reverse rotation clutch member (14) with the reverse rotation cylinder (C 1 ),
The traveling brake (15) is operated by the brake cylinder (C 2 ), and the pair of steering clutch members (12 a) and (12 b) are operated separately by the pair of traveling cylinders (C 3 ), (C 3 ). With the construction, these cylinders (C 1 ) to (C 3 ) are operated by one steering lever (16) based on the operation structure shown in FIG. 3, and the left and right traveling devices (4), (4) are operated.
It is configured to perform the airframe steering operation by performing the respective stop, braking and reverse rotation operations.

すなわち、一対の操向シリンダ(C3),(C3)のため
の1つの制御弁(V)、逆転シリンダ(C1)とブレーキ
シリンダ(C2)を操作油路(17)に接続切換えするモー
ド切換え弁(18)、操作油路(17)のリリーフ圧を変更
して逆転シリンダ(C1)及びブレーキシリンダ(C2)の
切換え操作をする可変リリーフ弁(19)を操作ワイヤ等
で成る連係機構(20)により操向レバー(16)に連係さ
せてある。そして操向レバー(16)を機体横方向に揺動
操作して直進位置(S)に操作すると、制御弁(V)が
中立位置(N)になり、いずれもの操向シリンダ
(C3),(C3)が前進側になると共に逆転シリンダ
(C1)がクラッチ切り側でブレーキシリンダ(C2)がブ
レーキ切り側になる。操向レバー(16)を第1左旋回位
置(L1)または第1右旋回位置(R1)に操作すると、制
御弁(V)が旋回位置(A1)または(A2)になって一方
の操向シリンダ(C3)が前進側で他方の操向シリンダ
(C3)が後進側になり、可変リリーフ弁(19)が低圧で
逆転シリンダ(C1)及びブレーキシリンダ(C2)が切り
側になる。操向レバー(16)を第2左旋回位置(L2)ま
たは第2右旋回位置(R2)に操作すると、制御弁(V)
が旋回位置(A1)または(A2)になって一方の操向シリ
ンダ(C3)が前進側で他方の操向シリンダ(C3)が後進
側になり、可変リリーフ弁(19)が中圧でモード切換え
弁(18)がブレーキ位置(B)になって逆転シリンダ
(C1)が切り側でブレーキシリンダ(C2)が入り側にな
る。操向レバー(16)を第3左旋回位置(L3)または第
3右旋回位置(R3)に操作すると、制御弁(V)が旋回
位置(A1)または(A2)になって一方の操向シリンダ
(C3)が前進側で他方の操向シリンダ(C3)側が後進側
になり、可変リリーフ弁(19)が高圧でモード切換え
(18)が逆転位置(R)になってブレーキシリンダ
(C2)が切り側で逆転シリンダ(C1)が入り側になるの
である。
That is, one control valve (V) for the pair of steering cylinders (C 3 ) and (C 3 ), the reverse rotation cylinder (C 1 ) and the brake cylinder (C 2 ) are connected to the operation oil passage (17) and switched. The mode switching valve (18) and the variable relief valve (19) that changes the relief pressure of the operating oil passage (17) to switch between the reverse cylinder (C 1 ) and the brake cylinder (C 2 ) by operating wire etc. The steering mechanism (20) is linked to the steering lever (16). When the steering lever (16) is oscillated in the lateral direction of the body to move it to the straight-ahead position (S), the control valve (V) becomes the neutral position (N), and the steering cylinder (C 3 ), (C 3 ) is on the forward side, the reverse cylinder (C 1 ) is on the clutch disengagement side, and the brake cylinder (C 2 ) is on the brake disengagement side. When the steering lever (16) is operated to the first left turning position (L 1 ) or the first right turning position (R 1 ), the control valve (V) becomes the turning position (A 1 ) or (A 2 ). One steering cylinder (C 3 ) is on the forward side and the other steering cylinder (C 3 ) is on the reverse side, and the variable relief valve (19) is low pressure and the reverse cylinder (C 1 ) and brake cylinder (C 2) ) Is the cut side. When the steering lever (16) is operated to the second left turning position (L 2 ) or the second right turning position (R 2 ), the control valve (V)
Is in the swivel position (A 1 ) or (A 2 ) and one steering cylinder (C 3 ) is on the forward side and the other steering cylinder (C 3 ) is on the reverse side, and the variable relief valve (19) is At medium pressure, the mode switching valve (18) is in the brake position (B), the reverse cylinder (C 1 ) is on the open side, and the brake cylinder (C 2 ) is on the open side. When the steering lever (16) is moved to the 3rd left turning position (L 3 ) or 3rd right turning position (R 3 ), the control valve (V) becomes the turning position (A 1 ) or (A 2 ). One steering cylinder (C 3 ) is on the forward side and the other steering cylinder (C 3 ) is on the reverse side. The variable relief valve (19) is at high pressure and the mode switch (18) is in the reverse position (R). Then, the brake cylinder (C 2 ) is on the cutting side and the reverse cylinder (C 1 ) is on the entering side.

荷台(2)の後端部に、荷台(2)が下降走行位置に
在る状態でエンジン(E)の上側部分が入り込む凹部
(2a)を備えてある。すなわち、エンジン上側部の走行
機体から上方への突出にかかわらず、荷台(2)が極力
低レベルに、かつ、運転部(1)に接近して位置するよ
うにエンジン(E)と荷台(2)との干渉回避を前記凹
部(2a)により図ってある。
The rear end of the platform (2) is provided with a recess (2a) into which the upper part of the engine (E) enters when the platform (2) is in the lowered traveling position. That is, regardless of whether the upper part of the engine projects upward from the traveling body, the engine (E) and the carrier (2) are positioned so that the carrier (2) is located at a level as low as possible and close to the operating part (1). ), Interference is avoided by the recess (2a).

〔別実施例〕 第5図に示すように、運転部(1)を走行機体の前端
側で、荷台(2)を走行機体の後端側に配置して実施し
てもよい。したがって、荷台(2)の凹部(2a)を備え
る端部を運転部側端部と称する。
[Other Embodiments] As shown in FIG. 5, the operation unit (1) may be arranged on the front end side of the traveling machine body and the loading platform (2) may be arranged on the rear end side of the traveling machine body. Therefore, the end portion provided with the recessed portion (2a) of the loading platform (2) is referred to as the operation unit side end portion.

クローラ走行装置(4)に替え、3個以上のタイヤ車
輪が機体前後方向に並列する走行装置を採用して実施し
てもよい。したがって、これらを不整地走行装置(4)
と称する。
Instead of the crawler traveling device (4), a traveling device in which three or more tire wheels are arranged side by side in the machine longitudinal direction may be adopted. Therefore, these are used as the rough terrain traveling device (4).
Called.

尚、特許請求の範囲の項に図面との対照を便利にする
為に符号を記すが、該記入により本発明は添付図面の構
造に限定されるものではない。
It should be noted that reference numerals are added to the claims for convenience of comparison with the drawings, but the present invention is not limited to the structures of the accompanying drawings by the entry.

【図面の簡単な説明】[Brief description of drawings]

図面は本発明に係る運搬車の実施例を示し、第1図は運
搬車全体の一部切欠き側面図、第2図は運搬車全体の平
面図、第3図は油圧回路図、第4図は走行用ミッション
の概略図、第5図は別実施運搬車の一部切欠き側面図で
ある。 (1)……運転部、(2)……荷台、(2a)……凹部、
(4)……不整地走行装置、(4a)……入力軸、(E)
……エンジン、(M)……走行用ミッション。
The drawings show an embodiment of a carrier according to the present invention. Fig. 1 is a partially cutaway side view of the entire carrier, Fig. 2 is a plan view of the entire carrier, Fig. 3 is a hydraulic circuit diagram, and Fig. 4 FIG. 5 is a schematic view of a traveling mission, and FIG. 5 is a partially cutaway side view of a differently implemented transport vehicle. (1) …… Operating section, (2) …… Bag, (2a) …… Concave,
(4) …… Rough terrain traveling device, (4a) …… Input shaft, (E)
…… Engine, (M) …… Mission mission.

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】左右一対の不整地走行装置(4),(4)
を有した走行機体に、運転部(1)と荷台(2)とを機
体前後方向に並列させて備えさせ、エンジン(E)を前
記不整地走行装置(4),(4)の入力軸(4a)より前
記荷台側に寄せて前記左右走行装置(4),(4)の間
に配置すると共に、前記エンジン(E)の出力を前記不
整地走行装置(4),(4)に伝達する走行用ミッショ
ン(M)を機体側面視で上端側ほど前記エンジン(E)
側に寄る傾斜姿勢で前記エンジン(E)と機体前後方向
に並置し、前記荷台(2)の前記運転部側端部に前記エ
ンジン(E)の上部が入り込む凹部(2a)を備えてある
運搬車。
1. A pair of left and right rough terrain traveling devices (4), (4)
A traveling machine body having a driving section (1) and a loading platform (2) are provided in parallel with each other in the longitudinal direction of the machine body, and an engine (E) is provided with an input shaft () of the rough terrain traveling apparatuses (4) and (4). 4a) is arranged closer to the cargo bed side and arranged between the left and right traveling devices (4), (4), and transmits the output of the engine (E) to the rough terrain traveling devices (4), (4). The engine (E) is closer to the upper end of the traveling mission (M) in a side view of the machine body.
The engine (E) is juxtaposed in the longitudinal direction with the engine (E) in an inclined posture toward the side, and the cargo bed (2) is provided with a recessed portion (2a) into which the upper portion of the engine (E) is inserted at an end of the operating section side. car.
JP2186821A 1990-07-13 1990-07-13 Carrier Expired - Lifetime JP2535092B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2186821A JP2535092B2 (en) 1990-07-13 1990-07-13 Carrier

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2186821A JP2535092B2 (en) 1990-07-13 1990-07-13 Carrier

Publications (2)

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JPH0478618A JPH0478618A (en) 1992-03-12
JP2535092B2 true JP2535092B2 (en) 1996-09-18

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Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2579465Y2 (en) * 1992-03-19 1998-08-27 セイレイ工業株式会社 Mission arrangement for aerial work vehicles

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Publication number Publication date
JPH0478618A (en) 1992-03-12

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