JPH0218277B2 - - Google Patents
Info
- Publication number
- JPH0218277B2 JPH0218277B2 JP57052657A JP5265782A JPH0218277B2 JP H0218277 B2 JPH0218277 B2 JP H0218277B2 JP 57052657 A JP57052657 A JP 57052657A JP 5265782 A JP5265782 A JP 5265782A JP H0218277 B2 JPH0218277 B2 JP H0218277B2
- Authority
- JP
- Japan
- Prior art keywords
- propeller
- propeller blade
- annular recess
- communication
- recess
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H1/00—Propulsive elements directly acting on water
- B63H1/02—Propulsive elements directly acting on water of rotary type
- B63H1/12—Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
- B63H1/14—Propellers
- B63H1/18—Propellers with means for diminishing cavitation, e.g. supercavitation
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Hydraulic Turbines (AREA)
Description
【発明の詳細な説明】 本発明は船舶の推進装置に関する。[Detailed description of the invention] The present invention relates to a propulsion device for a ship.
プロペラが船後伴流中で回転すると、プロペラ
面内の伴流分布(1−w)は円周方向で変化す
る。即ち、第1図aに示すように、プロペラ翼が
円周方向0゜(トツプ)付所を通過する際は小さく
なり、また180゜(ボトム)付近を通過する際は大
きくなる。なお第1図bはプロペラ翼の回転角度
位置を示すものである。従つて、プロペラ翼が0゜
付近を通過する際に伴流が不均一となり、プロペ
ラ翼の圧力面と背面との圧力差が激しく変動し
て、船体振動及びキヤビテーシヨン発生の原因と
なつていた。 When the propeller rotates in the wake after the ship, the wake distribution (1-w) in the plane of the propeller changes in the circumferential direction. That is, as shown in FIG. 1a, when the propeller blade passes through a point at 0° (top) in the circumferential direction, it becomes smaller, and when it passes around 180° (bottom) in the circumferential direction, it becomes larger. Note that FIG. 1b shows the rotation angle position of the propeller blades. Therefore, when the propeller blade passes around 0°, the wake becomes non-uniform, and the pressure difference between the pressure surface and the back surface of the propeller blade fluctuates drastically, causing hull vibration and cavitation.
そこで、本発明は伴流の変化によるプロペラ翼
の圧力面と背面との圧力差を緩和させ得る船舶の
推進装置を提供することを目的とする。 SUMMARY OF THE INVENTION Therefore, an object of the present invention is to provide a propulsion device for a ship that can alleviate the pressure difference between the pressure surface and the back surface of a propeller blade due to a change in wake.
即ち、本発明はプロペラ軸周囲の船尾非回転部
に対応するプロペラボス部の船首側の外周部に環
状凹部を形成し、各プロペラ翼に、一端がプロペ
ラ翼圧力面に開口すると共に他端が上記環状凹部
に開口する第1連通路と、一端がプロペラ翼背面
に開口すると共に他端が上記環状凹部に開口する
第2連通路とを穿設し、上記環状凹部に位置させ
られて上記第1連通路と第2連通路の他端開口同
士を所定範囲で互いに連通させる連通凹部を有す
る制御リングを船尾非回転部に固定し、且つ上記
制御リングの連通凹部を伴流分布に応じて制御リ
ング上端部のトツプ部分が開口面が広いほぼ三日
月形状にしたことを特徴とするものである。 That is, in the present invention, an annular recess is formed on the outer periphery of the bow side of the propeller boss portion corresponding to the non-rotating portion of the stern around the propeller shaft, and one end of each propeller blade is opened to the propeller blade pressure surface, and the other end is opened to the propeller blade pressure surface. A first communication passage that opens into the annular recess, and a second communication passage that has one end opening at the back surface of the propeller blade and the other end opening into the annular recess, and the second communication passage is located in the annular recess. A control ring having a communication recess that allows the openings at the other ends of the first communication passage and the second communication passage to communicate with each other within a predetermined range is fixed to the stern non-rotating part, and the communication recess of the control ring is controlled according to the wake distribution. The top of the ring is characterized by a nearly crescent-shaped top with a wide opening.
上記構成によると、伴流によるプロペラ翼圧力
面と背面との圧力差を緩和することができるの
で、プロペラに起因する船体振動及びプロペラに
発生するキヤビテーシヨンを減少させることがで
き、従つてプロペラ効率を向上させることができ
る。 According to the above configuration, the pressure difference between the propeller blade pressure surface and the back surface caused by the wake can be alleviated, so it is possible to reduce the hull vibration caused by the propeller and the cavitation generated in the propeller, thereby increasing the propeller efficiency. can be improved.
以下本発明の一実施例を第2図及び第3図に基
づき説明する。1は船舶におけるプロペラで、プ
ロペラボス部2の船首側部分で且つプロペラ軸3
外周部には、環状凹部4が形成されている。各プ
ロペラ翼5には、一端がプロペラ翼圧力面5aに
開口すると共に他端が環状凹部4に開口する第1
連通路6と、一端がプロペラ翼背面5bに開口す
ると共に他端が環状凹部4に開口する第2連通路
7とが穿設されている。なお、上記連通路6,7
環状凹部4側の開口位置はそれぞれのプロペラ翼
5の取付位置に対応させられている。そして、上
記第1連通路6と第2連通路7の環状凹部4側の
開口同士を所定範囲で互いに連通させる連通凹部
8aを有する制御リング8が、環状凹部4内に位
置させられると共に船尾非回転部9が(例えばス
タンチユーブ)に固定させられている。ところ
で、上記制御リング8の連通凹部8aは、伴流分
布(第1図aに示す)の小さいところにおいて、
プロペラ翼5の圧力面5aと背面5bとを連通さ
せてその圧力変動を緩和させるためのもので、従
つて伴流分布に応じてその形状が決定される。例
えば、第1図aに示す伴流分布に従うと、連通凹
部8aは第3図に示すように、トツプ(0゜付近)
部分では広く、真横(90゜、270゜付近)部分では
連通部開口面積が半分程度となるように順次狭め
られ、またボトム(180゜付近)部分では連通部開
口が閉鎖状態となるようにされる。従つて、ほぼ
三日月形状となる。なお上記制御リング8は船体
の伴流分布に応じて所定の連通凹部8aを有する
ものに取替えることができる。 An embodiment of the present invention will be described below with reference to FIGS. 2 and 3. Reference numeral 1 denotes a propeller for a ship, which is a bow side portion of a propeller boss portion 2 and a propeller shaft 3.
An annular recess 4 is formed on the outer periphery. Each propeller blade 5 has a first opening having one end opening to the propeller blade pressure surface 5a and the other end opening to the annular recess 4.
A communication passage 6 and a second communication passage 7 having one end open to the propeller blade back surface 5b and the other end opening to the annular recess 4 are bored. In addition, the above-mentioned communication paths 6, 7
The opening position on the annular recess 4 side corresponds to the mounting position of each propeller blade 5. A control ring 8 having a communication recess 8a that allows the openings of the first communication path 6 and the second communication path 7 on the annular recess 4 side to communicate with each other within a predetermined range is located within the annular recess 4 and is located at the stern. A rotating part 9 is fixed to a stand tube, for example. By the way, the communication recess 8a of the control ring 8 has a small wake distribution (shown in FIG. 1a) where the wake distribution is small.
This is for communicating the pressure surface 5a and the back surface 5b of the propeller blade 5 to alleviate pressure fluctuations, and therefore, its shape is determined according to the wake distribution. For example, according to the wake distribution shown in FIG. 1a, the communicating recess 8a is located at the top (near 0°)
It is wide at the part, and gradually narrows so that the opening area of the communication part is about half at the side part (around 90°, 270°), and the opening area of the communication part is closed at the bottom part (around 180°). Ru. Therefore, it has an almost crescent shape. Note that the control ring 8 can be replaced with one having a predetermined communication recess 8a depending on the wake distribution of the hull.
以上のように、本発明の船舶の推進装置によれ
ば、プロペラ翼圧力面に開口する第1の連通路
と、プロペラ翼背面に開口する第2の連通路を、
船尾非回転部に固定されかつ環状凹部内に位置す
る制御リングに伴流分布を対応して形成された三
日月形状の連通凹部を介して、プロペラ翼の回転
に伴つて連通するようにしたので、伴流によるプ
ロペラ翼圧力面と背面との圧力差を伴流分布の小
さく圧力差の大きいプロペラ翼トツプ位置を中心
として緩和することができ、プロペラに起因する
船体振動及びプロペラに発生するキヤビテーシヨ
ンを減少させることができ、従つてプロペラ効率
を向上させることができる。また、従来のプロペ
ラ翼面に孔を貫設し、プロペラ翼圧力面と背面と
の圧力差を全ての回転位置で緩和するものに比較
して、伴流分布に応じてその圧力差が大きくかつ
変動の激しい部分を中心に圧力を緩和することが
でき、プロペラ効率を低下させることなく効率的
な圧力緩和が可能である。さらに、従来のプロペ
ラ翼面のキヤビテイシヨン発生予想位置に水を噴
出させてキヤビテイシヨンを防止するものに比較
して、非常に簡単な構成で、伴流分布に応じてプ
ロペラ翼圧力面と背面との圧力差を利用して、そ
の圧力差を効果的に緩和できる。 As described above, according to the marine vessel propulsion device of the present invention, the first communication path that opens to the pressure surface of the propeller blade and the second communication path that opens to the back surface of the propeller blade.
The control ring is fixed to the non-rotating part of the stern and is located in the annular recess, and the control ring is connected to the control ring as the propeller blade rotates through the crescent-shaped communication recess formed in correspondence with the wake distribution. The pressure difference between the propeller blade pressure surface and the back surface caused by the wake can be alleviated centering on the propeller blade top position where the wake distribution is small and the pressure difference is large, reducing hull vibration caused by the propeller and cavitation occurring in the propeller. Therefore, the propeller efficiency can be improved. In addition, compared to conventional propeller blades that have holes penetrating through them to alleviate the pressure difference between the propeller blade pressure surface and the back surface at all rotational positions, the pressure difference is large depending on the wake distribution. It is possible to relieve pressure mainly in areas with severe fluctuations, and efficient pressure relief is possible without reducing propeller efficiency. Furthermore, compared to the conventional method that prevents cavitation by jetting water at the predicted position of cavitation on the propeller blade surface, the structure is very simple, and the pressure between the propeller blade pressure surface and the back surface is adjusted according to the wake distribution. By using the difference, the pressure difference can be effectively alleviated.
第1図aはプロペラ回転角と伴流分布との関係
を示すグラフ、第1図bはプロペラ回転角位置を
示す図、第2図は本発明の一実施例の一部切欠側
面図、第3図は第2図の−矢視断面図であ
る。
1……プロペラ、2……プロペラボス部、3…
…プロペラ軸、4……環状凹部、5……プロペラ
翼、5a……圧力面、5b……背面、6……第1
連通路、7……第2連通路、8……制御リング、
8a……連通凹部、9……船尾非回転部。
FIG. 1a is a graph showing the relationship between propeller rotation angle and wake distribution, FIG. 1b is a diagram showing the propeller rotation angle position, and FIG. 3 is a sectional view taken along the - arrow in FIG. 2. 1... propeller, 2... propeller boss section, 3...
...propeller shaft, 4 ... annular recess, 5 ... propeller blade, 5a ... pressure surface, 5b ... back surface, 6 ... first
Communication path, 7...Second communication path, 8...Control ring,
8a...Communication recess, 9...Stern non-rotating part.
Claims (1)
ロペラボス部の船首側の外周部に環状凹部を形成
し、各プロペラ翼に、一端がプロペラ翼圧力面に
開口すると共に他端が上記環状凹部に開口する第
1連通路と、一端がプロペラ翼背面に開口すると
共に他端が上記環状凹部に開口する第2連通路と
を穿設し、上記環状凹部に位置させられて上記第
1連通路と第2連通路の他端開口同士を所定範囲
で互いに連通させる連通凹部を有する制御リング
を船尾非回転部に固定し、且つ上記制御リングの
連通凹部を伴流分布に応じて制御リング上端部の
トツプ部分に開口面が広いほぼ三日月形状にした
ことを特徴とする船舶の推進装置。1. An annular recess is formed on the outer periphery of the bow side of the propeller boss portion corresponding to the stern non-rotating portion around the propeller shaft, and one end of each propeller blade opens to the propeller blade pressure surface, and the other end opens to the annular recess. A first communicating passage that opens, and a second communicating passage that has one end opening at the back surface of the propeller blade and the other end opening into the annular recess, and is located in the annular recess and connects to the first communicating passage. A control ring having a communication recess that allows the openings at the other ends of the second communication passages to communicate with each other within a predetermined range is fixed to the non-rotating part of the stern, and the communication recess of the control ring is connected to the upper end of the control ring according to the wake distribution. A propulsion device for a ship characterized by a nearly crescent-shaped top with a wide opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5265782A JPS58170692A (en) | 1982-03-30 | 1982-03-30 | Ship propulsion system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5265782A JPS58170692A (en) | 1982-03-30 | 1982-03-30 | Ship propulsion system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS58170692A JPS58170692A (en) | 1983-10-07 |
| JPH0218277B2 true JPH0218277B2 (en) | 1990-04-25 |
Family
ID=12920927
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5265782A Granted JPS58170692A (en) | 1982-03-30 | 1982-03-30 | Ship propulsion system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58170692A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH042465U (en) * | 1990-04-19 | 1992-01-10 |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5134200A (en) * | 1974-09-17 | 1976-03-23 | Kanebo Ltd | Isokinorinjudotai no goseiho |
| JPS53110699U (en) * | 1977-02-10 | 1978-09-04 |
-
1982
- 1982-03-30 JP JP5265782A patent/JPS58170692A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH042465U (en) * | 1990-04-19 | 1992-01-10 |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS58170692A (en) | 1983-10-07 |
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