JP2006123849A - Rudder device for ship - Google Patents
Rudder device for ship Download PDFInfo
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- JP2006123849A JP2006123849A JP2004317729A JP2004317729A JP2006123849A JP 2006123849 A JP2006123849 A JP 2006123849A JP 2004317729 A JP2004317729 A JP 2004317729A JP 2004317729 A JP2004317729 A JP 2004317729A JP 2006123849 A JP2006123849 A JP 2006123849A
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- rudder
- propeller
- fin
- blade
- fins
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T70/00—Maritime or waterways transport
- Y02T70/50—Measures to reduce greenhouse gas emissions related to the propulsion system
Abstract
Description
この発明は、船舶用舵装置に関し、プロペラ回転流のエネルギー回収およびプロペラ面流場の改善を図り、伴流率および推進器効率比の改善を図るようにしたものである。 The present invention relates to a marine rudder device, and aims to improve energy recovery of propeller rotating flow and improvement of propeller surface flow field, thereby improving wake ratio and propulsion device efficiency ratio.
船舶の推進性能の向上を目的として、プロペラの回転によって生じる流れ(プロペラ後流)のエネルギーを回収するために、舵板や舵柱にフィンを設けた船舶用舵装置が従来から種々提案されている。 For the purpose of improving the propulsion performance of a ship, various ship rudder devices having fins on a rudder plate and a rudder column have been proposed in order to recover energy of a flow (propeller wake) generated by propeller rotation. Yes.
例えば特許文献1に開示された舵では、図5に示すように、プロペラ1の後方に配設される舵2の上下方向長さの中央付近における両側面にそれぞれヒレ3を備え、プロペラ1の回転にともないそのプロペラ翼が上昇する側におけるヒレ3が正の迎え角を有するとともに、そのプロペラ翼が下降する側におけるヒレ3が負の迎え角を有するようになっている。 For example, in the rudder disclosed in Patent Document 1, as shown in FIG. 5, fins 3 are provided on both side surfaces in the vicinity of the center of the vertical length of the rudder 2 disposed behind the propeller 1. The fin 3 on the side where the propeller blade rises with rotation has a positive angle of attack, and the fin 3 on the side where the propeller blade descends has a negative angle of attack.
また、特許文献2に開示された船舶の推進性能向上装置では、図6に示すように、プロペラ1後方の舵2のほぼプロペラ軸心線上に小型のバルブ4を設けるとともに、このバルブ4に翼断面を持つ左右1対のフィン5を設けるようにしており、これにより、構成の簡素化を図るとともに、中・高速船のような船尾の流れの速い船でも、負荷抵抗の増加よりも推進効率の改善が大きくなるようにしている。 Further, in the ship propulsion performance improving device disclosed in Patent Document 2, as shown in FIG. 6, a small valve 4 is provided substantially on the propeller axis of the rudder 2 behind the propeller 1, and a wing is provided on the valve 4. A pair of left and right fins 5 having a cross-section are provided, thereby simplifying the configuration, and propulsion efficiency even with a fast stern flow such as a medium or high speed ship rather than an increase in load resistance. The improvement is getting bigger.
さらに、特許文献3の船舶用舵、特許文献4の舵、特許文献5の船の舵装置などにフィンを設けた船舶用の舵に関する技術が提案されている。
ところが、特許文献1〜5のいずれの船舶用の舵装置などに関する提案でも、舵やボスに設けたフィン又はヒレによってプロペラ後流のエネルギーを揚力として回収し、揚力の船進行方向成分を推力として船舶の推力向上に寄与させ、全体として省エネルギー、燃費の向上を図るものであるが、これら従来のフィン又はヒレを有する船舶用の舵装置についてさらなる実験・検討を重ねた結果、プロペラ回転流のエネルギー回収を主目的としているため、プロペラ面流場の改善が十分でなく、伴流率および推進器効率比に改善の余地があることが分かった。 However, in any proposal related to the rudder device for ships of Patent Documents 1 to 5, the energy behind the propeller is recovered as lift by the fins or fins provided on the rudder and boss, and the ship traveling direction component of lift is used as the thrust. It contributes to improving the thrust of the ship, and as a whole, energy saving and fuel efficiency are improved. As a result of further experiments and examinations on these conventional rudder devices with fins or fins, the energy of the propeller rotating flow Since recovery is the main purpose, it was found that the propeller surface flow field was not sufficiently improved, and there was room for improvement in the wake ratio and propulsion unit efficiency ratio.
この発明は、かかる従来技術の課題に鑑みてなされたもので、プロペラ面流場の改善により伴流率および推進器効率比を改善することができる船舶用舵装置を提供しようとするものである。 This invention is made in view of the subject of this prior art, and intends to provide the ship rudder apparatus which can improve a wake rate and a propulsion device efficiency ratio by the improvement of a propeller surface flow field. .
上記従来技術が有する課題を解決するため、この発明の請求項1記載の船舶用舵装置は、船体に舵板を回動可能に支持するプロペラ後方のラダーホーン又は舵板の両側に、フィンを設けた船舶用舵装置であって、前記フィンを前進翼とするとともに、前記フィンの翼厚弦長比を翼根部で15〜40%、翼端部で5〜20%としたことを特徴とするものである。 In order to solve the above-described problems of the prior art, a marine rudder device according to claim 1 of the present invention has fins on both sides of a rudder horn or a rudder plate behind a propeller that rotatably supports a rudder plate on a hull. A marine rudder device provided, wherein the fin is a forward wing, and a blade thickness chord ratio of the fin is 15 to 40% at a blade root and 5 to 20% at a blade tip. To do.
この船舶用舵装置によれば、フィンを前進翼とすることでプロペラにフィンの前縁を近づけるようにするとともに、フィンを厚翼としており、これらによりプロペラ面での流れを遅くすることでプロペラ面流場の改善による伴流率および推進器効率比を改善できるようになる。 According to this marine rudder device, the fins are made forward blades to bring the front edge of the fins closer to the propellers, and the fins are thick wings, thereby slowing the flow on the propeller surface, thereby propellers. The wake ratio and propulsion efficiency ratio can be improved by improving the surface flow field.
また、この発明の船舶用舵装置では、前記フィンを、前記プロペラ軸心高さよりプロペラ半径の70%以内の上方に設けるようにしたり、前記フィンの翼幅を、前記プロペラ半径の50〜100%としたり、さらに、前記フィンの翼端の翼弦長を、翼根の40〜90%とするようにしても良い。 In the marine rudder device of the present invention, the fin is provided above 70% of the propeller radius from the propeller shaft center height, or the wing width of the fin is 50 to 100% of the propeller radius. Further, the chord length of the fin blade tip may be 40 to 90% of the blade root.
ここで、前進翼とは、翼根部の翼弦長の中点と、翼端部の翼弦長の中点を結ぶ線が水平面上において舵中心線となす角が90度(直角)以下である平面形状を有する翼をいう(図4参照)。 Here, the forward wing means that the angle between the midpoint of the chord length of the wing root and the midpoint of the chord length of the wing tip and the rudder center line on the horizontal plane is 90 degrees (right angle) or less. It refers to a wing having a certain planar shape (see FIG. 4).
この発明の請求項1記載の船舶用舵装置によれば、ラダーホーン又は舵板の両側に設けるフィンを前進翼とすることでプロペラにフィンの前縁を近づけるようにするとともに、フィンを厚翼としており、これらによりプロペラ面での流れを遅くすることができ、プロペラ面流場の改善による伴流率および推進器効率比を改善することができる。 According to the marine rudder device of the first aspect of the present invention, the fins provided on both sides of the rudder horn or the rudder plate are made to be forward wings so that the front edge of the fins can be brought close to the propeller, and the fins are thick wings. Thus, the flow on the propeller surface can be slowed down, and the wake ratio and the propulsion device efficiency ratio can be improved by improving the propeller surface flow field.
また、この発明の請求項2〜4記載の船舶用舵装置によれば、フィンの取り付け高さ、フィンの翼幅、フィン翼端の翼弦長を所定の範囲とすることで、フィンを有効に機能させてプロペラ面での流れを遅くすることができ、プロペラ面流場の改善による伴流率および推進器効率比を改善することができる。 Further, according to the marine rudder device according to claims 2 to 4 of the present invention, the fins are effective by setting the fin mounting height, the fin wing width, and the chord length of the fin wing tip within a predetermined range. It is possible to slow down the flow on the propeller surface and improve the wake ratio and the propulsion unit efficiency ratio by improving the propeller surface flow field.
さらに、これら各請求項記載の構成を複数組み合わせた船舶用舵装置によれば、それぞれの作用効果を組み合わせて発揮させることができる。 Furthermore, according to the marine vessel rudder apparatus combining a plurality of configurations described in the respective claims, the respective operational effects can be exhibited in combination.
以下、この発明の一実施の形態について、図面に基づき詳細に説明する。
図1および図2は、この発明の船舶舵装置の一実施の形態にかかり、図1は概略正面図および拡大A−A断面図、図2はフィン形状を定義するための説明正面図および部分拡大平面図である。
Hereinafter, an embodiment of the present invention will be described in detail with reference to the drawings.
1 and 2 relate to an embodiment of a ship rudder device according to the present invention, FIG. 1 is a schematic front view and an enlarged AA sectional view, and FIG. 2 is an explanatory front view and part for defining a fin shape. It is an enlarged plan view.
この船舶用舵装置10では、船体に舵板11を回動可能に支持するプロペラ12後方のラダーホーン13の両側にフィン14を設け、このフィン14を前進翼とするとともに、従来に比べ翼厚を厚くしてあり、これらによって、プロペラ面での流れを遅くするようにし、プロペラ面流場の改善による伴流率および推進器効率比の改善を図るようにしている。 In this marine vessel rudder device 10, fins 14 are provided on both sides of a rudder horn 13 behind a propeller 12 that rotatably supports a rudder plate 11 on a hull, and the fins 14 serve as forward wings. Thus, the flow on the propeller surface is slowed down, and the wake ratio and the propulsion efficiency ratio are improved by improving the propeller surface flow field.
なお、このフィン14は、ラダーホーンの両側に限らず、舵板11の両側に設けるようにしても良い。
この船舶用舵装置10では、ラダーホーン13の両側に水平に突き出して設けるフィン14が前進翼、すなわち後退角が0度とされ、前縁が船首尾方向と直交するように形成してある。
The fins 14 may be provided not only on both sides of the ladder horn but also on both sides of the rudder plate 11.
In this marine vessel rudder device 10, fins 14 provided so as to protrude horizontally on both sides of the ladder horn 13 are formed so that the forward wing, that is, the receding angle is 0 degree, and the leading edge is orthogonal to the bow-stern direction.
このようなフィン14を後退角が0度の前進翼とすることで、フィン14をプロペラ12に近づけることができ、プロペラ面の流れを遅くするとともに、プロペラ面での流れが均一化される。
また、この船舶用舵装置10では、フィン14の翼厚を従来に比べ厚くしてあり、翼厚弦長比を翼根部で15〜40%、翼端部で5〜20%としてある。
By using such a fin 14 as an advancing wing having a receding angle of 0 degrees, the fin 14 can be brought closer to the propeller 12, the flow of the propeller surface is slowed, and the flow on the propeller surface is made uniform.
Moreover, in this marine vessel rudder apparatus 10, the blade thickness of the fin 14 is made thicker than before, and the blade thickness chord length ratio is 15-40% at the blade root and 5-20% at the blade tip.
従来のフィンでは、翼根部で翼厚弦長比で10%程度であり、このフィン14では2倍以上4倍程度としてあり、好ましくは翼根部で3〜4倍とすることで、一層顕著な効果を得ることができる。 In the conventional fin, the blade thickness chord length ratio is about 10% at the blade root, and the fin 14 is about 2 to 4 times, preferably 3 to 4 times at the blade root. An effect can be obtained.
このようにフィン14の翼厚を厚くすることでフィン14の排除効果によりプロペラ面の速い流れが遅くなってプロペラ面で流れが均一化され、これにより伴流率および推進器効率比が改善される。 By increasing the blade thickness of the fins 14 in this way, the fast flow of the propeller surface is slowed by the effect of eliminating the fins 14 and the flow is made uniform on the propeller surface, thereby improving the wake ratio and the thruster efficiency ratio. The
このフィンの厚翼による伴流率および推進器効率比の改善について、翼根部の翼厚弦長比を30%とした厚翼の場合と、翼根部の翼厚弦長比を10%とした薄翼の場合について試験を行った結果を図3に示した。 Regarding the improvement of the wake ratio and thruster efficiency ratio of this fin with thick blades, the blade thickness chord length ratio of the blade root portion is set to 30% and the blade thickness chord length ratio of the blade root portion is set to 10%. The results of testing for thin blades are shown in FIG.
同図は、ラダーホーンにフィンを装着しない場合に対する改善率を示したものであり、翼厚比を増すことで、薄翼に比べ、伴流率の改善は著しく、推進器効率比も改善され、所要馬力では3%ほど改善されることが分かる。 This figure shows the improvement rate compared to the case where no fin is attached to the ladder horn. By increasing the blade thickness ratio, the wake ratio is significantly improved and the propulsion unit efficiency ratio is also improved compared to the thin blade. It can be seen that the required horsepower is improved by about 3%.
このようなフィン14は、プロペラ12の軸心高さからプロペラ半径の0〜70%上方に取り付けることが好ましい。これらの範囲を越えた位置では、フィン14を設置することによる顕著な効果を得ることができなくなるからである。 Such a fin 14 is preferably attached at 0 to 70% above the propeller radius from the axial center height of the propeller 12. This is because a remarkable effect due to the installation of the fins 14 cannot be obtained at positions exceeding these ranges.
また、フィン14の翼幅は、プロペラ12の半径の50〜100%とすることが好ましい。50%より狭い翼幅では、フィン14による効果を得ることができず、100%を越えた広い翼幅としても得られる効果の増大は望めず、製作コストの増大などの問題が生じる。 Further, the blade width of the fin 14 is preferably 50 to 100% of the radius of the propeller 12. If the blade width is less than 50%, the effect of the fins 14 cannot be obtained, and an increase in the effect obtained even with a wide blade width exceeding 100% cannot be expected, causing problems such as an increase in manufacturing cost.
さらに、フィン14の翼端の翼弦長を、翼根の40〜90%とすることが好ましい。フィン14は前進翼であればよく、後縁については後退角を設けても良く、これにより翼端の翼弦長を翼根の40〜90%の範囲とする。40%より小さくすると、翼端でのフィンの効果が不十分となる。 Furthermore, it is preferable that the chord length of the blade tip of the fin 14 is 40 to 90% of the blade root. The fins 14 may be forward wings and may be provided with a receding angle at the trailing edge, so that the chord length of the wing tip is in the range of 40 to 90% of the blade root. If it is smaller than 40%, the fin effect at the blade tip becomes insufficient.
以上、詳細に説明したように、この船舶用舵装置10によれば、フィン14を前進翼とすることで、プロペラ12にフィン14の前縁を近づけるとともに、フィン14の翼厚弦長比を、翼根部で15〜40%、翼端部で5〜20%として従来に比べて厚翼としたので、これらによりプロペラ面での流れを遅くすることができ、プロペラ面流場の改善による伴流率および推進器効率比を改善することができる。 As described above in detail, according to this boat rudder device 10, by using the fin 14 as a forward wing, the front edge of the fin 14 is brought closer to the propeller 12, and the blade chord length ratio of the fin 14 is increased. Since the blade root is 15-40% at the blade root and 5-20% at the blade tip compared to the conventional blade, the flow on the propeller surface can be slowed down, and the propeller surface flow field is improved. The flow rate and propulsion efficiency ratio can be improved.
10 船舶用舵装置
11 舵板
12 プロペラ
13 ラダーホーン
14 フィン
DESCRIPTION OF SYMBOLS 10 Boat rudder 11 Rudder board 12 Propeller 13 Ladder horn 14 Fin
Claims (4)
前記フィンを前進翼とするとともに、前記フィンの翼厚弦長比を翼根部で15〜40%、翼端部で5〜20%としたことを特徴とする船舶用舵装置。 A rudder horn behind a propeller that rotatably supports a rudder plate on a hull or a rudder device for a ship provided with fins on both sides of a rudder plate,
A marine rudder apparatus, wherein the fin is a forward wing, and the blade thickness chord ratio of the fin is 15 to 40% at the blade root and 5 to 20% at the blade tip.
4. The marine rudder device according to claim 1, wherein a chord length of a wing tip of the fin is 40 to 90% of a blade root.
Priority Applications (1)
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JP2004317729A JP2006123849A (en) | 2004-11-01 | 2004-11-01 | Rudder device for ship |
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JP2004317729A JP2006123849A (en) | 2004-11-01 | 2004-11-01 | Rudder device for ship |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101381516B1 (en) * | 2012-05-15 | 2014-04-10 | 현대중공업 주식회사 | A rudder for ship |
KR101381464B1 (en) * | 2012-05-15 | 2014-04-10 | 현대중공업 주식회사 | A rudder for ship |
KR101402529B1 (en) * | 2012-07-27 | 2014-06-19 | 현대중공업 주식회사 | A rudder for ship |
CN105197220A (en) * | 2015-10-09 | 2015-12-30 | 上海船舶研究设计院 | Shilling rudder used for icebreaker |
KR20170112880A (en) * | 2016-03-24 | 2017-10-12 | 재팬 마린 유나이티드 코포레이션 | Rudder for ship |
CN111907683A (en) * | 2019-05-10 | 2020-11-10 | 三菱重工业株式会社 | Rudder and ship provided with same |
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JPH0263295A (en) * | 1988-08-29 | 1990-03-02 | Sony Corp | White balance adjustment circuit |
JPH04314689A (en) * | 1991-04-12 | 1992-11-05 | Hitachi Zosen Corp | Rudder |
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2004
- 2004-11-01 JP JP2004317729A patent/JP2006123849A/en active Pending
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Publication number | Priority date | Publication date | Assignee | Title |
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JPH0263295A (en) * | 1988-08-29 | 1990-03-02 | Sony Corp | White balance adjustment circuit |
JPH04314689A (en) * | 1991-04-12 | 1992-11-05 | Hitachi Zosen Corp | Rudder |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101381516B1 (en) * | 2012-05-15 | 2014-04-10 | 현대중공업 주식회사 | A rudder for ship |
KR101381464B1 (en) * | 2012-05-15 | 2014-04-10 | 현대중공업 주식회사 | A rudder for ship |
KR101402529B1 (en) * | 2012-07-27 | 2014-06-19 | 현대중공업 주식회사 | A rudder for ship |
CN105197220A (en) * | 2015-10-09 | 2015-12-30 | 上海船舶研究设计院 | Shilling rudder used for icebreaker |
KR20170112880A (en) * | 2016-03-24 | 2017-10-12 | 재팬 마린 유나이티드 코포레이션 | Rudder for ship |
CN111907683A (en) * | 2019-05-10 | 2020-11-10 | 三菱重工业株式会社 | Rudder and ship provided with same |
JP2020185810A (en) * | 2019-05-10 | 2020-11-19 | 三菱重工業株式会社 | Rudder and ship with it |
CN111907683B (en) * | 2019-05-10 | 2022-11-04 | 三菱重工业株式会社 | Rudder and ship provided with same |
JP7237718B2 (en) | 2019-05-10 | 2023-03-13 | 三菱重工業株式会社 | Rudders and ships equipped with them |
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