JPH07251665A - Vehicle for flying body charging work - Google Patents

Vehicle for flying body charging work

Info

Publication number
JPH07251665A
JPH07251665A JP4373894A JP4373894A JPH07251665A JP H07251665 A JPH07251665 A JP H07251665A JP 4373894 A JP4373894 A JP 4373894A JP 4373894 A JP4373894 A JP 4373894A JP H07251665 A JPH07251665 A JP H07251665A
Authority
JP
Japan
Prior art keywords
vehicle
flying body
detector
signal
launcher
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.)
Withdrawn
Application number
JP4373894A
Other languages
Japanese (ja)
Inventor
Mitsuo Senda
光男 千田
Junichi Kono
順一 河野
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP4373894A priority Critical patent/JPH07251665A/en
Publication of JPH07251665A publication Critical patent/JPH07251665A/en
Withdrawn legal-status Critical Current

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  • Loading Or Unloading Of Vehicles (AREA)

Abstract

PURPOSE:To prevent a flying body from dropping down and a vehicle from tumbling by supervising the vehicle inclined by an inclination detector, in the vehicle wherein a mounting frame can be arranged in an optimum position for lifting the flying body by a position detector. CONSTITUTION:In a controller 20, in addition to a position detector 14 for detecting a position of a movable part of an arm 9 except an outrigger 15, receiving a signal from a position detector of a main beam 6 and a detection data from an inclination detector 18, a mounting frame 12 is arranged in an optimum position for lifting a flying body at its removing/charging time. That is, data from these detectors are fetched, to feed a differential amount operating signal to a hydraulic source unit 19, and to stop the body in a prescribed position. In the case of applying an interlock, a monitor signal is output to display a lock condition in the controller 20. Further at work suspension time, an interrupt signal from a available operating panel 21 is fetched, and a stop signal is output to the hydraulic source unit 19, to stop the movable part.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、車載型飛昇体発射機へ
運搬車両で移送された飛昇体を装填するために使用す
る、飛昇体装填作業用車両に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a vehicle for loading a flying object, which is used to load a flying object transferred by a transportation vehicle to an on-vehicle flying object launcher.

【0002】[0002]

【従来の技術】運搬車両で移送されてきた飛昇体を発射
機へ装填するには、従来、図5に示すように行われてい
た。図5(A)に示すように、発射機構を具えるコンテ
ナ01に収納された飛昇体を移送する運搬車両02が、
発射機03の近傍に到達すると、図5(B)に示すよう
に、重レッカクレーン04により、発射機03上の発射
済コンテナを取外し、その後に、飛昇体を収納したコン
テナ01を運搬車両02上から重レッカクレーン04で
吊上げて、発射機03上へ吊り降し、コンテナ01を発
射機03へ装着すると共に、発射機03から取外したコ
ンテナを、再び重レッカクレーン04で吊上げて運搬車
両02に積載し、撤去していた。
2. Description of the Related Art Conventionally, loading a flying object transferred by a transportation vehicle into a launcher has been performed as shown in FIG. As shown in FIG. 5 (A), a transport vehicle 02 that transfers a flying object housed in a container 01 equipped with a firing mechanism,
When reaching the vicinity of the launcher 03, as shown in FIG. 5 (B), the heavy-recker crane 04 removes the launched container on the launcher 03, and then the container 01 containing the flying object is transported by the transport vehicle 02. It is hoisted from above by a heavy recker crane 04, suspended on a launcher 03, the container 01 is mounted on the launcher 03, and the container removed from the launcher 03 is hoisted again by the heavy recker crane 04 to transport the vehicle 02. It was loaded on and removed.

【0003】この作業には、クレーン運転者、作業指揮
者、位置決め作業者等、複数の作業者を必要とし、ま
た、その作業は複数の作業者の声のかけ合いによる意志
伝達に頼っていた。このため、意志伝達の時間や、熟練
したクレーン運転者以外による重レッカクレーンの操作
時間の増加、又は重レッカクレーンの移動速度が遅いこ
となどにより、作業にかなり長い時間を必要としてい
た。また、クレーン運転者の運転ミス、または作業指揮
者からの意志伝達の不十分さ、又は判断ミス、等による
吊り上げられたコンテナ01付近にいる位置決め作業者
に、安全上の問題が生じる等の不具合があった。
This work requires a plurality of workers such as a crane driver, a work conductor, and a positioning worker, and the work relies on communication of intentions by talking with a plurality of workers. For this reason, a considerably long time is required for the work due to the time for transmitting the intention, the increase in the operation time of the heavy recker crane by a person other than a skilled crane driver, or the slow moving speed of the heavy recker crane. In addition, there is a problem such as a safety problem for the positioning operator near the suspended container 01 due to an operation error of the crane operator, insufficient communication from the work conductor, or a judgment error. was there.

【0004】[0004]

【発明が解決しようとする課題】本発明は、上述した、
従来の飛昇体の発射機への装填にあたり、不具合とされ
ていた、作業に多人数を要し、この多人数作業に伴う作
業時間の長期化、安全上の問題、又は機器・装置等の損
傷を回避するため、単独の作業者で飛昇体の発射機への
装填ができ、作業時間を短縮でき、さらには、危険な場
所から離れて作業ができ、安全上の問題がなく、作業を
確実に行えて、機器・装置を損なうことのない、飛昇体
装填作業用車両を提供することを課題とする。
The present invention has been described above.
It took many people to perform work, which had been considered a problem when loading a conventional flying object into a launcher.The work time was prolonged, safety problems, or damage to equipment or devices, etc. To avoid this, a single operator can load the flying object into the launcher, shorten the work time, and work away from a dangerous place, so that there is no safety problem and the work can be performed reliably. It is an object of the present invention to provide a vehicle for flying object loading work that can be performed at any time without damaging the equipment / device.

【0005】[0005]

【課題を解決するための手段】このため、本発明の飛昇
体装填作業用車両は、次の手段とした。 (1)車両上を車両走行方向にスライドして、車両走行
方向の位置調整ができるようにした台車上に、鉛直軸ま
わりに回動できる旋回台を設けた。 (2)旋回台上に、鉛直方向に伸縮できるメインビーム
を立設した。 (3)メインビームの側部に固着され、メインビームの
伸縮により上下動する外筒、および外筒の内部を摺動
し、先端に設けた飛昇体を載置する載架台を、水平方向
に移動させることのできる内筒からなるアームを設け
た。 (4)載架台の移動量を検出し、載置した飛昇体の位置
を検出できる位置検出器を設けた。 (5)車両の両側から外側へ張り出して設けられ、車両
にかかる荷重を肩代わりして保持するアウトリガを設け
た。 (6)車両の両側に設けられたアウトリガの高さを、そ
れぞれ検出して、その検出値から車両の傾きを検出し
て、車両の転倒を防止する傾斜検出器を設けた。
For this reason, the vehicle for loading a flying object according to the present invention has the following means. (1) A swivel base that is rotatable around a vertical axis is provided on a bogie that can be slid on the vehicle in the vehicle travel direction to adjust the position in the vehicle travel direction. (2) A main beam that can extend and contract in the vertical direction was erected on the swivel base. (3) The outer cylinder, which is fixed to the side of the main beam and moves up and down due to the expansion and contraction of the main beam, and the mounting table for sliding the inside of the outer cylinder and mounting the flying body at the tip, are set horizontally. An arm composed of an inner cylinder that can be moved is provided. (4) A position detector capable of detecting the amount of movement of the mounting table and detecting the position of the mounted flying body is provided. (5) Outriggers are provided that project outward from both sides of the vehicle and hold the load applied to the vehicle as a shoulder. (6) An inclination detector is provided to detect the height of the outriggers provided on both sides of the vehicle, detect the inclination of the vehicle from the detected values, and prevent the vehicle from falling.

【0006】[0006]

【作用】本発明の飛昇体装填作業用車両は、上述の手段
により、発射機に横付けした飛昇体装填作業用車両の両
側部にアウトリガを張り出し設置した後、台車、旋回
台、メインビームおよびアームを作動させて、発射機に
装填されている飛昇体の下部に載架台を誘導し、持上
げ、取外すことができる。
According to the vehicle for loading a flying object of the present invention, after the outriggers are installed on both sides of the vehicle for loading a flying object laterally attached to the launcher by the means described above, the bogie, the swivel base, the main beam and the arm are installed. Can be operated to guide the platform to the lower part of the flying body loaded in the launcher, lift it, and remove it.

【0007】その後、運搬車両で移送されて来た飛昇体
を、同様にして車両上から持上げ、台車、旋回台、メイ
ンビーム、およびアームの作動により、発射機へ正確に
取付け、装填することができる。この飛昇体の取外し、
装填時、位置検出器により、載架台を飛昇体の持上げに
最適な位置に配置することができるとともに、傾斜検出
器により、車両の傾きを常に監視できるので、飛昇体の
落下、又は車両の転倒を防止することができる。
After that, the flying object transferred by the transportation vehicle can be lifted from the vehicle in the same manner, and accurately mounted and loaded on the launcher by the operation of the carriage, the swivel base, the main beam, and the arm. it can. Remove this flying body,
During loading, the position detector allows the platform to be placed at the optimum position for lifting the flying object, and the inclination detector can constantly monitor the tilt of the vehicle, so the flying object falls or the vehicle falls. Can be prevented.

【0008】以上のことから、飛昇体の発射機への装填
が、単独の作業者で行うことができるとともに、作業時
間を大幅に短縮できる。また、安全上の問題点も解消で
き、機器、装置を不慮の事故により、損傷することもな
くなる。
As described above, the flying body can be loaded into the launcher by a single operator, and the working time can be greatly shortened. In addition, safety problems can be solved, and devices and devices are not damaged by an accident.

【0009】[0009]

【実施例】以下、本発明の飛昇体装填作業用車両の実施
例を、図面に基づき説明する。図1は、本発明の飛昇体
装填作業用車両の、一実施例を示す斜視図である。図に
おいて、1は本実施例を搭載する車両、2は車両1の荷
台の上に設置された固定板、3は固定板2上に敷設され
た軌道、4は軌道3上を車両走行方向にスライドする台
車、5は鉛直軸まわりに回動するように、台車4上に設
けられた旋回台、6は旋回台5上に下端が固着された固
定ビーム7と、油圧によって駆動され固定ビーム7と摺
動して鉛直軸方向に上下動する移動ビーム8からなるメ
インビーム、9は移動ビーム8に内側面が固着され、移
動ビーム8と共に上下動する外筒10と、油圧によって
駆動され、外筒10と摺動して水平方向に伸縮する内筒
11とからなるアーム、12は内筒11の先端に固着さ
れ、内部に飛昇体を収容するコンテナ25を載置するフ
ォーク13を、先端07に具える載架台、14は外筒1
0先端と、載架台12の後端を検出して、載架台12の
水平方向の移動量を検出する位置検出器である。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of a flying object loading work vehicle of the present invention will be described below with reference to the drawings. FIG. 1 is a perspective view showing an embodiment of a vehicle for loading a flying object of the present invention. In the figure, 1 is a vehicle equipped with the present embodiment, 2 is a fixed plate installed on the bed of the vehicle 1, 3 is a track laid on the fixed plate 2, and 4 is a track on the track 3 in the vehicle traveling direction. The sliding carriage 5 is a swivel provided on the carriage 4 so as to rotate about a vertical axis, and 6 is a fixed beam 7 whose lower end is fixed on the swivel 5 and a fixed beam 7 driven by hydraulic pressure. A main beam 9 composed of a moving beam 8 which slides and moves up and down in the vertical axis direction. An inner surface of the moving beam 8 is fixed to the moving beam 8, and an outer cylinder 10 which moves up and down together with the moving beam 8 is driven by hydraulic pressure to An arm 12 made up of an inner cylinder 11 that slides with the cylinder 10 and expands and contracts in the horizontal direction is fixed to the tip of the inner cylinder 11, and a fork 13 for mounting a container 25 containing a flying object therein is provided with a tip 07. A mounting stand equipped with 14 and an outer cylinder 1
It is a position detector that detects the 0 tip and the rear end of the mounting table 12 to detect the amount of horizontal movement of the mounting table 12.

【0010】なお、上記旋回台5、台車4およびメイン
ビーム6にも、図示はしてないが角度、および移動量を
それぞれ検出して、図示した位置検出器14からの情報
とともに、載架台12(上に載置されるコンテナ25,
25’)の三次元位置が検出できるようにしている。
Although not shown in the figure, the angle and the moving amount of each of the swivel base 5, the bogie 4 and the main beam 6 are respectively detected, and together with the information from the position detector 14 shown in the figure, the mounting base 12 is shown. (Container 25 placed on top,
25 ') three-dimensional position can be detected.

【0011】15は、車両1の前方および後方で、それ
ぞれ車両1の両側へ張り出して設けられたアウトリガ
で、車両1の両側から側方へ突出して設けられたビーム
の先端に、鉛直に固着されたシリンダ17と、シリンダ
17の内部を油圧で駆動されて上下動するロッド16と
からなる。また、18は各アウトリガ15の高さを検出
して、車両1の傾きを検出する傾斜検出器である。
Numeral 15 is an outrigger that is provided in front of and behind the vehicle 1 so as to project to both sides of the vehicle 1, and is vertically fixed to the tip of a beam provided to project laterally from both sides of the vehicle 1. And a rod 16 that is hydraulically driven inside the cylinder 17 and moves up and down. Reference numeral 18 denotes a tilt detector that detects the height of each outrigger 15 and detects the tilt of the vehicle 1.

【0012】また、19は車両1上に載置されて台車
4、旋回台5、メインビーム6、アーム9、およびアウ
トリガ15に高圧油を送り込み、これらの駆動を行うと
ともに、低圧油を回収するようにした油圧源ユニット、
20はコントローラ、21は手元操作盤である。
Further, 19 is mounted on the vehicle 1 and sends high-pressure oil to the carriage 4, the swivel 5, the main beam 6, the arm 9, and the outrigger 15 to drive them and collect the low-pressure oil. Hydraulic source unit,
Reference numeral 20 is a controller, and 21 is a hand operation panel.

【0013】本実施例は、上述のように構成されるの
で、図2に示すように、飛昇体を発射したコンテナ25
(以下空GMという)を、装填した発射機26の近傍
に、飛昇体22を収容したコンテナ25’(以下新GM
という)を、積載した運搬車両27が到着したら、発射
機26と運搬車両27の間に車両1を配置する。
Since this embodiment is constructed as described above, as shown in FIG.
A container 25 '(hereinafter referred to as a new GM) that accommodates the flying body 22 near the launcher 26 in which the empty GM is loaded.
When the loaded transportation vehicle 27 arrives, the vehicle 1 is arranged between the launcher 26 and the transportation vehicle 27.

【0014】次いで、図3のブロックに示すように、手
元操作盤21より、操作信号を油圧源ユニット19に送
り出すことにより、油圧源ユニット19は、油圧力によ
り駆動されるアーム9、メインビーム6、旋回台5、台
車4、およびアウトリガ15(これらを併せて、以下可
動部という)に高圧油を送り込み、伸縮および回転運動
をさせる。また、油圧源ユニット19は、手元操作盤2
1と、コントローラ20へ常にモニタ信号を返し、可動
部の状態をモニタすると共に、非常時には非常停止信号
を相手方とやりとりすることによって停止させる。
Next, as shown in the block of FIG. 3, an operation signal is sent from the hand operation panel 21 to the hydraulic pressure source unit 19, so that the hydraulic pressure source unit 19 is driven by hydraulic pressure to the arm 9 and the main beam 6. , High-pressure oil is sent to the swivel base 5, the bogie 4, and the outrigger 15 (these are collectively referred to as a movable part hereinafter) to expand and contract and rotate. In addition, the hydraulic power source unit 19 is the operation panel 2 at hand.
1, the monitor signal is constantly returned to the controller 20 to monitor the state of the movable portion, and in an emergency, the emergency stop signal is exchanged with the other party to stop the operation.

【0015】また、コントローラ20は、アウトリガ1
5を除く可動部の位置を検出する位置検出器14(前述
したように、アーム9の位置検出器14のみばかりでな
く、台車4、旋回台5、メインビーム9にも、それらの
移動量、角度を検出できる位置検出器を設けているが、
説明を簡単にするため、ここではアーム9の位置検出器
14のみを取上げた。)、傾斜検出器18からの検出デ
ータを取り込み、油圧源ユニット19へ差分の操作信号
を送り込み、所定の位置で停止させる。また、可動部が
最伸長時、最短縮時にインタロックがかかった際、イン
タロック信号を取り込み、モニタ信号を出して、ロック
がかかっている状態である事をコントローラ20に表示
するようにしている。
Further, the controller 20 includes an outrigger 1
The position detector 14 for detecting the positions of the movable parts other than 5 (as described above, not only the position detector 14 of the arm 9 but also the carriage 4, the swivel base 5, and the main beam 9 have their movement amounts, Although a position detector that can detect the angle is provided,
For simplicity of explanation, only the position detector 14 of the arm 9 is taken up here. ), The detection data from the inclination detector 18 is fetched, a differential operation signal is sent to the hydraulic power source unit 19, and it is stopped at a predetermined position. Further, when the movable portion is interlocked when it is extended or shortened most, an interlock signal is taken in and a monitor signal is output to display on the controller 20 that it is in a locked state. .

【0016】さらに、作業中断時には、手元操作盤21
よりの割込み信号を取り込み、油圧源ユニット19へ、
停止信号を出し可動部を停止させることも出来るように
した。
Further, when the work is interrupted, the hand operation panel 21
Take in the interrupt signal from the
It is also possible to issue a stop signal to stop the movable part.

【0017】次に、図4により本実施例を使用した飛昇
体の装填作業手順を示す。図4(A)は前述した図2の
平面図で、前述したように空GMを装填した発射機26
の近傍に、新GMを積載した運搬車両27が到着した
ら、運搬車両27を発射機26と平行に配置するととも
に、車両1を運搬車両27と発射機26との間に平行に
配置し、一方のアーム9のフォーク13が、空GMの支
持位置近傍を支持できる位置まで移動させ、次いでアウ
トリガを伸展させて、車両1を地上に固定する。なお、
運搬車両27と発射機26との間隔は、間に配置した車
両1のフォーク13の旋回範囲Rと干渉しない程度にし
ておく。
Next, FIG. 4 shows a procedure for loading a flying body using this embodiment. FIG. 4A is a plan view of FIG. 2 described above, and the launcher 26 loaded with the empty GM as described above.
When the transport vehicle 27 loaded with the new GM arrives in the vicinity of, the transport vehicle 27 is placed in parallel with the launcher 26, and the vehicle 1 is placed in parallel between the transport vehicle 27 and the launcher 26. The fork 13 of the arm 9 is moved to a position where it can support the vicinity of the support position of the empty GM, and then the outrigger is extended to fix the vehicle 1 to the ground. In addition,
The distance between the transport vehicle 27 and the launcher 26 is set so as not to interfere with the turning range R of the fork 13 of the vehicle 1 disposed therebetween.

【0018】次いで、旋回台5を旋回させてアーム9が
車両1の両側へ伸展できるようにし、メインビーム6を
伸展させる。この過程で、フォーク13と空GMの支持
位置とのずれは、台車4を使って微調整を行う。
Then, the swivel base 5 is swiveled so that the arms 9 can be extended to both sides of the vehicle 1 and the main beam 6 is extended. In this process, the displacement between the fork 13 and the supporting position of the empty GM is finely adjusted using the carriage 4.

【0019】次いで、図4(B)に示すように、フォー
ク13の位置が空GMの支持位置と一致したら、アーム
9を伸展させ、フォーク13を空GM25の支持位置に
挿入し、上昇させ、引込む。
Next, as shown in FIG. 4 (B), when the position of the fork 13 coincides with the supporting position of the empty GM, the arm 9 is extended, the fork 13 is inserted into the supporting position of the empty GM 25, and raised. Pull in.

【0020】この状態で、もう一方のフォーク13と、
新GM25’の支持位置との微調整を行った後、図4
(C)に示すように、アーム9を伸展させフォークを新
GM25’の支持位置へ挿入し、上昇させ、引込む
In this state, the other fork 13 and
After fine adjustment with the support position of the new GM25 ',
As shown in (C), the arm 9 is extended and the fork is inserted into the support position of the new GM 25 ', raised, and retracted.

【0021】次いで図4(D)に示すように、旋回台5
を回転させ、新GM25’を載置したフォーク13を発
射機26側に、空GM25を載置したフォーク13を運
搬車両27側に向ける。なお、R’はアーム9を縮退さ
せた状態でのフォーク13に載置された空GM25、新
GM25’の最大旋回範囲である。
Next, as shown in FIG. 4D, the swivel base 5
Is rotated so that the fork 13 on which the new GM 25 'is mounted faces the launcher 26 side, and the fork 13 on which the empty GM 25 is mounted faces the transport vehicle 27 side. Note that R'is the maximum turning range of the empty GM25 and the new GM25 'placed on the fork 13 with the arm 9 retracted.

【0022】次いで、図4(E)に示すように、アーム
9を、張出し、下降し、フォーク13に載架した新
GM25’を、発射機26に装填して、アーム9を引込
める。
Next, as shown in FIG. 4 (E), the arm 9 is extended and lowered, and the new GM 25 'mounted on the fork 13 is loaded into the launcher 26 and the arm 9 is retracted.

【0023】次いで、図4(F)に示すように、もう一
方のフォーク13に載架した空GM25を運搬車両25
に積載して、装填作業が終了する。
Next, as shown in FIG. 4 (F), the empty GM 25 mounted on the other fork 13 is transferred to the transport vehicle 25.
And the loading operation is completed.

【0024】[0024]

【発明の効果】以上、述べたように、本発明の飛昇体装
填作業用車両によれば、特許請求の範囲に示す構成によ
り、飛昇体の発射機への装填が単独の作業者で行うこと
ができるとともに、作業時間を大幅に短縮できる。
As described above, according to the vehicle for loading a flying vehicle of the present invention, the flying vehicle can be loaded into the launcher by a single operator, due to the structure described in the claims. In addition to being able to work, the working time can be greatly reduced.

【0025】また、安全上の問題点も解消でき、機器、
装置を不慮の事故により損傷することもなくなる。
In addition, the safety problem can be solved and the device,
The device is also protected from accidental damage.

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

【図1】本発明の飛昇体装填作業用車両の一実施例を示
す斜視図。
FIG. 1 is a perspective view showing an embodiment of a vehicle for loading a flying object according to the present invention.

【図2】図1に示す実施例を作業状態にしたレイアウト
を示す斜視図。
FIG. 2 is a perspective view showing a layout of the working example shown in FIG. 1 in a working state.

【図3】図1に示す実施例を作動させる、作動および制
御ブロック図。
3 is an operation and control block diagram for operating the embodiment shown in FIG. 1. FIG.

【図4】図1に示す実施例による飛昇体装填作業手順を
示す概要図。
FIG. 4 is a schematic diagram showing a flying body loading operation procedure according to the embodiment shown in FIG.

【図5】従来の飛昇体装填作業を示すシステムブロック
図。
FIG. 5 is a system block diagram showing a conventional flying object loading operation.

【符号の説明】[Explanation of symbols]

1 車両 2 固定板 3 軌道 4 台車 5 旋回台 6 メインビーム 7 固定ビーム 8 移動ビーム 9 アーム 10 外筒 11 内筒 12 載架台 13 フォーク 14 位置検出器 15 アウトリガ 16 ロッド 17 シリンダ 18 傾斜検出器 19 油圧源ユニット 20 コントローラ 21 手元操作盤 22 飛昇体 25 コンテナ 26 発射機 27 運搬車両 1 vehicle 2 fixed plate 3 orbit 4 bogie 5 swivel 6 main beam 7 fixed beam 8 moving beam 9 arm 10 outer cylinder 11 inner cylinder 12 mounting base 13 fork 14 position detector 15 outrigger 16 rod 17 cylinder 18 tilt detector 19 hydraulic Source unit 20 Controller 21 Hand operation panel 22 Flying body 25 Container 26 Launcher 27 Transport vehicle

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 車両上を車両走行方向にスライドする台
車上に設置され水平面内を回動する旋回台と、前記旋回
台上に立設され鉛直方向に伸縮するメインビームと、前
記メインビームの側部に固着された外筒および前記外筒
内を摺動し先端に固着した飛昇体を載置する載架台を水
平方向に移動させる内筒からなるアームと、前記載架台
の位置を検出する位置検出器と、前記車両の両側へ張り
出され荷重を支持するアウトリガと、前記アウトリガの
高さを検出し前記車両の傾きを検出する傾斜検出器とを
具えたことを特徴とする飛昇体装填作業用車両。
1. A swivel installed on a bogie that slides in a vehicle traveling direction on a vehicle and rotatable in a horizontal plane; a main beam standing upright on the swivel and extending and contracting in a vertical direction; An arm composed of an outer cylinder fixed to the side part and an inner cylinder that slides in the outer cylinder and horizontally moves a mounting table on which a flying body fixed to the tip is mounted, and the position of the mounting table described above are detected. A flying object loading, comprising: a position detector, an outrigger that extends to both sides of the vehicle and supports a load, and an inclination detector that detects a height of the outrigger and detects an inclination of the vehicle. Working vehicle.
JP4373894A 1994-03-15 1994-03-15 Vehicle for flying body charging work Withdrawn JPH07251665A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4373894A JPH07251665A (en) 1994-03-15 1994-03-15 Vehicle for flying body charging work

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4373894A JPH07251665A (en) 1994-03-15 1994-03-15 Vehicle for flying body charging work

Publications (1)

Publication Number Publication Date
JPH07251665A true JPH07251665A (en) 1995-10-03

Family

ID=12672127

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4373894A Withdrawn JPH07251665A (en) 1994-03-15 1994-03-15 Vehicle for flying body charging work

Country Status (1)

Country Link
JP (1) JPH07251665A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006037443A (en) * 2004-07-26 2006-02-09 Daikin Ind Ltd Multi-level parking device
CN104709728A (en) * 2015-04-08 2015-06-17 张永波 Full-automatic container loading equipment

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006037443A (en) * 2004-07-26 2006-02-09 Daikin Ind Ltd Multi-level parking device
CN104709728A (en) * 2015-04-08 2015-06-17 张永波 Full-automatic container loading equipment

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Effective date: 20010605