JPH045599B2 - - Google Patents
Info
- Publication number
- JPH045599B2 JPH045599B2 JP6444883A JP6444883A JPH045599B2 JP H045599 B2 JPH045599 B2 JP H045599B2 JP 6444883 A JP6444883 A JP 6444883A JP 6444883 A JP6444883 A JP 6444883A JP H045599 B2 JPH045599 B2 JP H045599B2
- Authority
- JP
- Japan
- Prior art keywords
- fins
- support member
- rudder
- fin
- shaped
- 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
Links
- 230000000694 effects Effects 0.000 description 2
- 230000008602 contraction Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
Description
【発明の詳細な説明】
本発明は、舵に関するもので、詳しくは、両側
部にほぼ水平に張り出した翼形のフインを有する
船舶用の舵に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a rudder, and more particularly to a rudder for a ship having airfoil-shaped fins extending substantially horizontally on both sides.
従来のこの種の舵は、両側にほぼ水平に張り出
したフインを有するので、多くの利点を有し、と
くに、省エネルギー効果をもつものとされてい
た。しかし、前記フインの従来の取付け方法で
は、片持ち梁方式によるだけであつたので、該フ
インに大きな外力が作用すると、その取付け部に
過大な応力が発生した。すなわち、該フインが大
きな外力に耐えうるためには、該フインの張り出
し長さを短くしたり、あるいは厚さを増加して剛
性を保つなどの手段が必要であつた。しかし、張
り出しの短いフインや極端に分厚いフインでは、
性能が劣化するため、本来の省エネルギー効果を
発揮しきれない例が出てきた。 Conventional rudders of this type have fins that extend substantially horizontally on both sides, and thus have many advantages, particularly energy saving. However, since the conventional method for attaching the fins was only by a cantilever method, when a large external force was applied to the fins, excessive stress was generated at the attachment portion. That is, in order for the fins to withstand a large external force, it is necessary to take measures such as shortening the overhanging length of the fins or increasing the thickness to maintain rigidity. However, with short fins or extremely thick fins,
There have been cases where the original energy saving effect cannot be achieved due to performance deterioration.
本発明は、フインの張り出し長さを必要なだけ
長くし、かつ、充分に薄くして、フインの性能を
発揮させ、しかも、フインに大きな外力が作用し
ても、みだりに破損するおそれのないフイン付き
舶用舵を提供することを目的をするものである。 The present invention provides a fin in which the overhanging length of the fin is made as long as necessary, and the fin is made sufficiently thin so that the performance of the fin is exhibited, and there is no risk of undue damage even if a large external force is applied to the fin. The purpose of this invention is to provide a marine rudder with a built-in rudder.
このため、本発明の構成は、両側部にほぼ水平
に張り出した翼形のフインを有する船舶用の舵に
おいて、該フインの先端に固着されて該フインを
支持している支持部材を備えていることを特徴と
している。 For this reason, the structure of the present invention is a rudder for a ship having airfoil-shaped fins extending substantially horizontally on both sides, and includes a support member fixed to the tips of the fins to support the fins. It is characterized by
以下、本発明の実施態様について、図面を参照
しながら説明する。 Embodiments of the present invention will be described below with reference to the drawings.
第1図ないし第4図は本発明の第1実施例を示
したもので、第1図において、1は船体の船尾
部、2は舵(ここでは、舵本体2aと舵支持部材
2bとを含めて舵という。)、3は前記舵支持部材
2bの両側に片持ち梁方式に取付けられてほぼ水
平に張り出している翼形のフイン、4は該フイン
3の支持部材、5はプロペラ、6はその内側をプ
ロペラ後流が通過するプロペラ後流の及ぶ圏円で
ある。すなわち、この実施例では、プロペラ後流
の及ぶ圏円6まで、ほぼいつぱいにのばしたフイ
ン3の先端と舵支持部2bの上部とを、断面が翼
形になつているリング状の支持部材4で連結して
いる。 1 to 4 show a first embodiment of the present invention. In FIG. 1, 1 is the stern of the hull, and 2 is a rudder (here, a rudder main body 2a and a rudder support member 2b are shown). ), 3 is an airfoil-shaped fin attached in a cantilever manner to both sides of the rudder support member 2b and extends almost horizontally, 4 is a support member for the fin 3, 5 is a propeller, 6 is the circle within which the propeller wake passes. That is, in this embodiment, the tip of the fin 3 which is extended almost all the way to the circle 6 where the propeller wake reaches, and the upper part of the rudder support part 2b are connected by a ring-shaped support member having an airfoil-shaped cross section. Connected by 4.
したがつて、従来は片持ち梁であつたフイン3
を、ラーメン構造に変えたことにより、フイン3
の根元にかかるモーメントや剪断力を小さくする
ことができる。これにより、フイン3が薄くなる
ので、よりよい性能を発揮させることができる。
しかし、一方において、支持部材4の追加によ
り、摩擦抵抗や誘導抵抗が増加するが、これは、
リング状の前記支持部材4の断面を翼形にするこ
とで、かなり回避でき、全体として性能のよい省
エネルギー装置となる。 Therefore, the fin 3, which was conventionally cantilevered,
By changing the structure to a Ramen structure, Finn 3
It is possible to reduce the moment and shear force applied to the root of the tree. As a result, the fins 3 become thinner, so that better performance can be exhibited.
However, on the other hand, the addition of the support member 4 increases frictional resistance and induced resistance;
By making the cross section of the ring-shaped support member 4 airfoil-shaped, this can be avoided to a large extent, resulting in an energy-saving device with good overall performance.
さらに説明すると、第2図に示すように、フイ
ン3にかかる外力7を、支持部材4を通じて舵支
持部材2bの上部に分担させ、フイン3の付け根
のモーメントおよび剪断力を軽減させるのであ
る。またリング状の支持部材4の取付け位置は、
ほぼプロペラ後流の及ぶ圏円6に沿わせる。これ
は第3図に示すように、この付近の流れを有効利
用するためである。すなわち、流れは、ほぼプロ
ペラ後流の及ぶ圏円6を境にして内側で速く、外
側で遅い。そして流速の速いプロペラ後流の及ぶ
圏円6はプロペラ直径より少し縮む。ここに、第
4図に示すような翼形断面を有するリング状の支
持部材4を取付けることにより、流速の大なる内
側8が流速の小なる外側9に比較して、低圧とな
り、支持部材4に内向きの力10が生じ、この力
10はプロペラ5が回転することによつて発生す
る縮流11がつくる斜流のために、その向きが少
し前方に傾き、その前進方向成分がスラスト12
となる。このスラスト12で、支持部材4を付け
たことによる抵抗増加分を、かなり埋め合せする
ことができる。 To explain further, as shown in FIG. 2, the external force 7 applied to the fin 3 is distributed to the upper part of the rudder support member 2b through the support member 4, thereby reducing the moment and shearing force at the base of the fin 3. Furthermore, the mounting position of the ring-shaped support member 4 is as follows.
It is placed almost along the circle 6 covered by the propeller wake. This is to make effective use of the flow in this area, as shown in Figure 3. That is, the flow is fast on the inside and slow on the outside of the circle 6, which is the area covered by the propeller wake. The circle 6 covered by the wake of the propeller with a high flow velocity is slightly smaller than the diameter of the propeller. By attaching a ring-shaped support member 4 having an airfoil-shaped cross section as shown in FIG. An inward force 10 is generated, and this force 10 is slightly tilted forward due to the diagonal flow created by the contraction flow 11 generated by the rotation of the propeller 5, and its forward direction component becomes the thrust 12.
becomes. This thrust 12 can considerably compensate for the increase in resistance due to the attachment of the support member 4.
第5図は本発明の第2実施例を示したもので、
いわゆる逆G型の舵について示し、断面翼形のリ
ング状の支持部材4をフイン3の下側に取付けて
いる。すなわち、フイン3および支持部材4は、
ともに舵本体2aに取付けられている。 FIG. 5 shows a second embodiment of the present invention.
A so-called inverted G-type rudder is shown, and a ring-shaped support member 4 having an airfoil cross section is attached to the lower side of the fins 3. That is, the fins 3 and the support member 4 are
Both are attached to the rudder body 2a.
第6図は本発明の第3実施例を示したもので、
断面翼形の支持部材4は、リング状でなく、直線
状またはナツクル状になつている。 FIG. 6 shows a third embodiment of the present invention.
The support member 4, which has an airfoil cross-section, is not ring-shaped but straight or knuckle-shaped.
第7図は本発明の第4実施例を示したもので、
断面翼形の支持部材4を船体からとつている。 FIG. 7 shows a fourth embodiment of the present invention.
A support member 4 having an airfoil cross section is taken from the hull.
上述のように、本発明の舵は、両側部にほぼ水
平に張り出した翼形のフインの先端に固着されて
該フインを支持している支持部材を備えているか
ら、該支持部材により、フインにかかる外力が分
散して伝わり、したがつて、フインの張り出し長
さを必要なだけ長くし、かつ、充分に薄くしてフ
インの性能を発揮させることができるとともに、
フインを軽構造とすることができ、フイン本来の
省エネルギー効果の向上をはかることができる。 As described above, the rudder of the present invention includes a support member that is fixed to the tips of the airfoil-shaped fins extending substantially horizontally on both sides and supports the fins. The external force applied to the fins is transmitted in a dispersed manner, so that the overhanging length of the fins can be made as long as necessary and thin enough to exhibit the performance of the fins.
The fins can have a light structure, and the inherent energy saving effect of the fins can be improved.
図面は本発明の実施態様を示したもので、第1
図は第1実施例の斜視図、第2図は第1図の船体
の後部からみた拡大断面図、第3図は第2図のフ
イン位置の軸方向流速分布図、第4図は第2図の
フイン支持部材の作用の説明図、第5図は第2実
施例の斜視図、第6図は第3実施例の斜視図、第
7図は第4実施例の斜視図である。
1……船体の船尾部、2……舵、3……フイ
ン、4……フインの支持部材、5……プロペラ、
6……プロペラ後流の及ぶ圏円。
The drawings show embodiments of the present invention.
The figure is a perspective view of the first embodiment, Figure 2 is an enlarged cross-sectional view of the hull in Figure 1 seen from the rear, Figure 3 is an axial flow velocity distribution diagram at the fin position in Figure 2, and Figure 4 is the FIG. 5 is a perspective view of the second embodiment, FIG. 6 is a perspective view of the third embodiment, and FIG. 7 is a perspective view of the fourth embodiment. DESCRIPTION OF SYMBOLS 1... Stern part of the hull, 2... Rudder, 3... Fin, 4... Fin support member, 5... Propeller,
6...The circle covered by the propeller wake.
Claims (1)
を有する船舶用の舵において、該フインの先端に
固着されて該フインを支持している支持部材を備
えていることを特徴とする舵。1. A rudder for a ship having airfoil-shaped fins extending substantially horizontally on both sides, characterized by comprising a support member fixed to the tips of the fins to support the fins.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6444883A JPS59190095A (en) | 1983-04-14 | 1983-04-14 | rudder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6444883A JPS59190095A (en) | 1983-04-14 | 1983-04-14 | rudder |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59190095A JPS59190095A (en) | 1984-10-27 |
| JPH045599B2 true JPH045599B2 (en) | 1992-01-31 |
Family
ID=13258542
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6444883A Granted JPS59190095A (en) | 1983-04-14 | 1983-04-14 | rudder |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59190095A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0165793U (en) * | 1987-05-25 | 1989-04-27 | ||
| KR101225174B1 (en) * | 2010-09-15 | 2013-01-22 | 삼성중공업 주식회사 | Steering apparatus and ship including the same |
| KR101383687B1 (en) * | 2012-07-25 | 2014-04-09 | 대우조선해양 주식회사 | Vortex reducing module for rudder of vessel |
-
1983
- 1983-04-14 JP JP6444883A patent/JPS59190095A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59190095A (en) | 1984-10-27 |
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