JPH04114730U - Bow thruster control device - Google Patents

Bow thruster control device

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Publication number
JPH04114730U
JPH04114730U JP2535591U JP2535591U JPH04114730U JP H04114730 U JPH04114730 U JP H04114730U JP 2535591 U JP2535591 U JP 2535591U JP 2535591 U JP2535591 U JP 2535591U JP H04114730 U JPH04114730 U JP H04114730U
Authority
JP
Japan
Prior art keywords
bow thruster
blade angle
impeller
generator
control device
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
Application number
JP2535591U
Other languages
Japanese (ja)
Inventor
和夫 岩谷
Original Assignee
三菱重工業株式会社
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 三菱重工業株式会社 filed Critical 三菱重工業株式会社
Priority to JP2535591U priority Critical patent/JPH04114730U/en
Publication of JPH04114730U publication Critical patent/JPH04114730U/en
Pending legal-status Critical Current

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Abstract

(57)【要約】 【目的】 本考案は、操船に用いられるバウスラスタに
関し、特にバウスラスタの動力源としての発電機の過負
荷を防止できるようにしたバウスラスタ制御装置を提供
しようとするものである。 【構成】 本考案のバウスラスタ制御装置は、翼角調節
機構3を有する電動機駆動式インペラ5を装着されたバ
ウスラスタと、インペラ5を駆動する電動機4へ給電し
うる発電機1と、同発電機1の過負荷状態を検出しうる
過負荷検出回路2と、同過負荷検出回路2からの検出信
号に基づいて上記インペラ5の翼角を減少させるように
翼角調節機構3を制御しうるバウスラスタ制御回路6と
をそなえたことを特徴としている。これにより、バウス
ラスタのインペラ翼角の変位に伴う発電機の過負荷を防
止して、その他の負荷の選択遮断を抑制できるようにし
た。
(57) [Summary] [Purpose] The present invention relates to a bow thruster used for ship maneuvering, and specifically aims to provide a bow thruster control device that can prevent overloading of a generator serving as a power source for the bow thruster. [Structure] The bow thruster control device of the present invention includes a bow thruster equipped with an electric motor-driven impeller 5 having a blade angle adjustment mechanism 3, a generator 1 capable of supplying power to an electric motor 4 that drives the impeller 5, and the generator 1. an overload detection circuit 2 capable of detecting an overload state of the overload state; and a bow thruster control capable of controlling a blade angle adjustment mechanism 3 to reduce the blade angle of the impeller 5 based on a detection signal from the overload detection circuit 2. It is characterized by having a circuit 6. This prevents overloading of the generator due to changes in the bow thruster impeller blade angle, and suppresses selective interruption of other loads.

Description

【考案の詳細な説明】[Detailed explanation of the idea]

【0001】0001

【産業上の利用分野】[Industrial application field]

本考案は、操船に用いられるバウスラスタに関し、特にバウスラスタの動力源 としての発電機の過負荷を防止できるようにしたバウスラスタ制御装置に関する 。 The present invention relates to a bow thruster used for ship maneuvering, and in particular, the power source of the bow thruster. Regarding a bow thruster control device that can prevent overload of a generator. .

【0002】0002

【従来の技術】[Conventional technology]

従来のバウスラスタ制御装置では、図3に示すように、バウスラスタ使用時に は、バウスラスタのインペラを駆動する電動機Mの動力源としての複数の発電機 Gは並列運転状態にあり、その状態で支回路保護遮断器A、B、Cに接続された負 荷の総量が増加すると、発電機Gの過負荷検出器(OCR)が作動し、上記負荷 の総量が設定値を超えると、発電機Gの保護のため、遮断器Aまたは遮断器Bに 接続された船舶の推進に関係のない負荷を切離すべく、過負荷検出器OCRから の信号により遮断器Aまたは遮断器Bを開とし、負荷の遮断を行なっていた。 In the conventional bow thruster control device, as shown in Fig. 3, when using the bow thruster, is a plurality of generators as a power source for electric motor M that drives the impeller of the bow thruster. G is in a parallel operation state, and in that state, the negative When the total load increases, the overload detector (OCR) of generator G is activated and the load When the total amount exceeds the set value, circuit breaker A or circuit breaker B is activated to protect generator from the overload detector OCR in order to disconnect loads unrelated to the propulsion of the connected vessel. The signal was used to open circuit breaker A or circuit breaker B, thereby shedding the load.

【0003】0003

【考案が解決しようとする課題】[Problem that the idea aims to solve]

ところで、前述のような従来のバウスラスタ制御装置では、バウスラスタのイ ンペラの翼角変位による発電機Gの負荷変動と上記インペラの翼角制御回路との 電気的関連がなかったため、翼角が大となる方向に変化すると上記発電機に過負 荷が働き、すぐに、推進に関係のない負荷の選択遮断に結びついてしまうという 問題点がある。 By the way, in the conventional bow thruster control device as mentioned above, the bow thruster The relationship between the load fluctuation of the generator G due to the blade angle displacement of the impeller and the above impeller blade angle control circuit is as follows. Since there was no electrical connection, the generator would be overloaded if the blade angle increased. The load acts, which immediately leads to selective shedding of loads unrelated to propulsion. There is a problem.

【0004】 本考案は、このような問題点の解決をはかろうとするもので、発電機の過負荷 検出器からの信号の設定値を超える信号量にあわせてバウスラスタのインペラの 翼角を下げることにより発電機にかかる負荷を軽くできるようにした、バウスラ スタ制御装置を提供することを目的とする。0004 This invention attempts to solve these problems, and is designed to prevent overloading of generators. The impeller of the bow thruster is adjusted according to the signal amount exceeding the set value of the signal from the detector. A bow thruster that reduces the load on the generator by lowering the blade angle. The purpose of the present invention is to provide a star control device.

【0005】[0005]

【課題を解決するための手段】 上述の目的を達成するため、本考案のバウスラスタ制御装置は、翼角調節機構 を有する電動機駆動式インペラを装着されたバウスラスタと、上記インペラを駆 動する電動機へ給電しうる発電機と、同発電機の過負荷状態を検出しうる過負荷 検出回路と、同過負荷検出回路からの検出信号に基づいて上記インペラの翼角を 減少させるように上記翼角調節機構を制御しうるバウスラスタ制御回路とをそな えたことを特徴としている。[Means to solve the problem] In order to achieve the above object, the bow thruster control device of the present invention has a blade angle adjustment mechanism. A bow thruster equipped with an electric motor-driven impeller having a A generator that can supply power to a moving electric motor, and an overload that can detect the overload condition of the generator. The blade angle of the impeller is determined based on the detection circuit and the detection signal from the overload detection circuit. and a bow thruster control circuit that can control the blade angle adjustment mechanism to reduce the blade angle. It is characterized by the fact that

【0006】[0006]

【作用】[Effect]

上述の本考案のバウスラスタ制御装置では、バウスラスタのインペラの翼角変 位による負荷増加に伴う発電機の過負荷状態を検出して、その過負荷検出信号に 基づいて、上記インペラの翼角を減少させる作用が行なわれる。 In the bow thruster control device of the present invention described above, the blade angle change of the impeller of the bow thruster is Detects the overload condition of the generator due to the increase in load due to Based on this, an action is taken to reduce the blade angle of the impeller.

【0007】[0007]

【実施例】【Example】

以下、図面により本考案の一実施例としてのバウスラスタ制御装置について説 明すると、図1はその概略を示す系統図、図2はその制御の流れ図である。 Below, a bow thruster control device as an embodiment of the present invention will be explained with reference to the drawings. Specifically, FIG. 1 is a system diagram showing the outline thereof, and FIG. 2 is a flowchart of its control.

【0008】 図1に示すように、本実施例では、バウスラスタは翼角調節機構としての翼角 制御油圧装置3を有するインペラ5と同インペラを駆動する電動機4とで構成さ れている。そして、電動機4は発電機1から給電され、同発電機1の過負荷状態 を検出しうる過負荷検出回路(OCR:オーバーカレントリレー)2が主配電板 内の発電機1側に設けられている。[0008] As shown in Fig. 1, in this embodiment, the bow thruster is used as a blade angle adjustment mechanism. It is composed of an impeller 5 having a control hydraulic system 3 and an electric motor 4 that drives the impeller. It is. Then, the electric motor 4 is supplied with power from the generator 1, and the generator 1 is overloaded. Overload detection circuit (OCR: overcurrent relay) 2 that can detect It is provided on the generator 1 side inside.

【0009】 さらに、過負荷検出回路2からの検出信号に基づいてインペラ5の翼角を減少 させるように翼角制御油圧装置3を制御しうるバウスラスタ制御回路6がそなえ られている。[0009] Furthermore, the blade angle of the impeller 5 is decreased based on the detection signal from the overload detection circuit 2. A bow thruster control circuit 6 is provided that can control the blade angle control hydraulic system 3 to It is being

【0010】 このような構成により、図2に示す流れに従ってインペラ5の翼角制御が行な われる。すなわち、バウスラスタ運転時に、同バウスラスタのインペラ5の翼角 変位等により変動する発電機1の負荷を過負荷検出回路2にて検出し、その負荷 が設定電流値を超えると、過負荷検出回路2からの検出信号に基づきバウスラス タ制御回路6が働いて、その出力する制御信号により翼角制御油圧装置3がイン ペラ5の負荷を軽くするように翼角を減少させる作用を行なう。なお、過負荷検 出用の過電流設定器は可変とし、各船舶の状態により適宜設定可能とされる。0010 With this configuration, the blade angle of the impeller 5 is controlled according to the flow shown in FIG. be exposed. In other words, during bow thruster operation, the blade angle of the impeller 5 of the bow thruster The overload detection circuit 2 detects the load of the generator 1 that fluctuates due to displacement, etc. exceeds the set current value, the bow thrust is activated based on the detection signal from the overload detection circuit 2. The blade angle control hydraulic system 3 is activated by the control signal it outputs. The blade angle is reduced to reduce the load on the propeller 5. In addition, overload detection The overcurrent setting device for output is variable and can be set as appropriate depending on the condition of each ship.

【0011】 このようにして、バウスラスタのインペラ5の翼角の増大によって生じる発電 機1の過負荷の際に、その他の負荷の選択遮断を防ぎ、安全で快適な航海を続行 することができる。[0011] In this way, the power generation generated by increasing the blade angle of the impeller 5 of the bow thruster Prevents selective cutoff of other loads when aircraft 1 is overloaded, allowing safe and comfortable voyage to continue. can do.

【0012】0012

【考案の効果】[Effect of the idea]

以上詳述したように、本考案のバウスラスタ制御装置によれば、バウスラスタ のインペラの翼角の変位に伴う発電機の過負荷の際に、負荷選択遮断を防止でき るようになり、これにより安全で快適な航海を続行できる効果が得られる。 As detailed above, according to the bow thruster control device of the present invention, the bow thruster load selection can be prevented when the generator is overloaded due to the displacement of the impeller blade angle. This has the effect of allowing you to continue your voyage safely and comfortably.

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

【図1】本考案の一実施例としてのバウスラスタ制御装
置の概略を示す系統図である。
FIG. 1 is a system diagram schematically showing a bow thruster control device as an embodiment of the present invention.

【図2】図1に示すバウスラスタ制御装置の制御の流れ
図である。
FIG. 2 is a flowchart of control of the bow thruster control device shown in FIG. 1;

【図3】従来のバウスラスタ制御装置の回路図である。FIG. 3 is a circuit diagram of a conventional bow thruster control device.

【符号の説明】[Explanation of symbols]

1 発電機 2 過負荷検出回路 3 翼角制御油圧装置 4 電動機 5 インペラ 6 バウスラスタ制御回路 1 Generator 2 Overload detection circuit 3 Wing angle control hydraulic system 4 Electric motor 5 impeller 6 Bow thruster control circuit

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】 翼角調節機構を有する電動機駆動式イン
ペラを装着されたバウスラスタと、上記インペラを駆動
する電動機へ給電しうる発電機と、同発電機の過負荷状
態を検出しうる過負荷検出回路と、同過負荷検出回路か
らの検出信号に基づいて上記インペラの翼角を減少させ
るように上記翼角調節機構を制御しうるバウスラスタ制
御回路とをそなえたことを特徴とする、バウスラスタ制
御装置。
1. A bow thruster equipped with a motor-driven impeller having a blade angle adjustment mechanism, a generator that can supply power to the electric motor that drives the impeller, and an overload detector that can detect an overload state of the generator. and a bow thruster control circuit capable of controlling the blade angle adjustment mechanism to reduce the blade angle of the impeller based on a detection signal from the overload detection circuit. .
JP2535591U 1991-03-22 1991-03-22 Bow thruster control device Pending JPH04114730U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2535591U JPH04114730U (en) 1991-03-22 1991-03-22 Bow thruster control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2535591U JPH04114730U (en) 1991-03-22 1991-03-22 Bow thruster control device

Publications (1)

Publication Number Publication Date
JPH04114730U true JPH04114730U (en) 1992-10-09

Family

ID=31910104

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2535591U Pending JPH04114730U (en) 1991-03-22 1991-03-22 Bow thruster control device

Country Status (1)

Country Link
JP (1) JPH04114730U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020104612A (en) * 2018-12-26 2020-07-09 ナブテスコ株式会社 Control system of variable pitch propeller and control method of variable pitch propeller

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020104612A (en) * 2018-12-26 2020-07-09 ナブテスコ株式会社 Control system of variable pitch propeller and control method of variable pitch propeller

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