JPS59153689A - Boat propeller - Google Patents
Boat propellerInfo
- Publication number
- JPS59153689A JPS59153689A JP2668183A JP2668183A JPS59153689A JP S59153689 A JPS59153689 A JP S59153689A JP 2668183 A JP2668183 A JP 2668183A JP 2668183 A JP2668183 A JP 2668183A JP S59153689 A JPS59153689 A JP S59153689A
- Authority
- JP
- Japan
- Prior art keywords
- propeller
- vanes
- blade
- blades
- conditions
- 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
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
- B63H1/28—Other means for improving propeller efficiency
-
- 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
- B63H2001/145—Propellers comprising blades of two or more different types, e.g. different lengths
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)
Abstract
Description
【発明の詳細な説明】
この発明は、船舶の推進器として一般に使用されるスク
リュープロペラの改良に関し、旧来に存在する整数翼対
称プロペラでは、中間翼数に相当する諸能力(プロペラ
効率、プロペラの起振力)を発揮することが可能な舶用
プロペラを提供することを目的としたものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to the improvement of screw propellers that are generally used as propellers for ships. The purpose of this invention is to provide a marine propeller capable of exerting vibration excitation force.
船舶用推進器としては、一般にスクリュープロペラが多
く使用されており、現在、最も多く適用されているのが
4翼プロペラと6翼プロペラである。Generally, screw propellers are often used as marine propulsors, and currently, four-blade propellers and six-blade propellers are most commonly used.
ところが、前述の4翼お↓び6翼のプロペラは、容具の
諸条件、換言すれば、プロペラ翼径、ピッチ、面積比あ
るいはレーキ角度を全て同じ条件下に構成した「対称翼
型」プロペラである。However, the aforementioned 4-blade and 6-blade propellers are ``symmetrical blade type'' propellers configured under the same conditions for the container, in other words, the propeller blade diameter, pitch, area ratio, or rake angle. It is.
ところが、省エネルギ一対策が強く叫ばれている昨今で
は、この種プロペラにおいても、より 一層のプロペラ
効率の向上が希求されている。However, in recent years, there has been a strong demand for energy-saving measures, and even for this type of propeller, there is a desire to further improve propeller efficiency.
仁のプロペラ効率を向上させるため、前述の「対称翼型
プロさう」では、プロペラ翼の減少化あるいは翼面積比
の減少化の手段が施こされているが、プロペラ翼数を減
少させれば、プロペラの起振力「船尾付近の複雑に水流
の中でプロペラが回るため、プロペラの翼が流体から受
ける力はプロペラ−回転中に変動する。この変動力が船
体に伝わり、船体が振動することによって居住性の悪化
、船体部材の破損などの障害がおこる。このプロペラに
働く変動力をプロペラ起振力と呼ぶ。」が増加して船尾
の振動が船舶の安定性に対する問題を残している。この
ため、従来、一般商船では、この種問題の解決の一部と
して4翼プロペラあるいは6翼プロペラが多く適用され
ているが、石油資源の不足2価格の高騰などの社会的環
境の悪化にエリ、この種プロペラの設計全行なうに際し
ても省エネルギ一対策を施した種々のプロペラが提案さ
れ、また、実用に供されようとするが、その−例として
最近では翼数全減少させた「3翼の対称−7%llプロ
ペラ」が適用されつつある。In order to improve the efficiency of the propeller's propeller, the aforementioned ``symmetrical wing type propeller'' reduces the number of propeller blades or reduces the blade area ratio. For example, the vibrational force of the propeller is ``As the propeller rotates in the complicated water flow near the stern, the force that the propeller blades receive from the fluid fluctuates while the propeller rotates.'' This fluctuating force is transmitted to the hull, causing the hull to vibrate. This causes problems such as deterioration of habitability and damage to hull components.This fluctuating force acting on the propeller is called propeller excitation force.''As a result, vibrations at the stern of the ship continue to pose problems for the stability of the ship. There is. For this reason, in conventional commercial ships, four-blade propellers or six-blade propellers have often been applied as part of the solution to this type of problem. When designing this type of propeller, various propellers with energy-saving measures have been proposed and put into practical use.As an example, recently, a three-blade propeller with a completely reduced number of blades has been proposed. The symmetrical -7%ll propeller is being applied.
しかしながら、前述の「3翼対称型プロペラ」に於いて
も、予じめ設計された諸能力(プロペラ効率、プロペラ
起振力)の範噴のみしか能力が発揮できず、その中間的
翼数に相当するプロペラ効率は得られなかった。However, even with the above-mentioned "three-blade symmetrical propeller", the ability can only be demonstrated within the pre-designed range of various capacities (propeller efficiency, propeller excitation force), and the number of blades in between No comparable propeller efficiency was obtained.
本発明は、前述の諸事情に鑑み発明されたものであって
、現在実用に供されている2翼、4翼または6数のプロ
ペラにおける中間的翼数、換言すれば、2翼乃至3翼、
3翼乃至4翼などの中間翼数に対応するプロペラ効率な
らびにプロペラ起振力−2mることかできる舶用プロペ
ラであり、その特徴とするところは、複数翼のプロペラ
に於ける6翼のピッチ、径1面積比あるいはレーキ角度
の諸条件の一部または全部全相異する如く構成したとこ
ろに存在する。The present invention was invented in view of the above-mentioned circumstances, and is an intermediate number of blades among the two-blade, four-blade, or six-blade propellers currently in practical use, in other words, two to three blades. ,
It is a marine propeller that can achieve a propeller efficiency corresponding to an intermediate number of blades such as 3 or 4 blades, and a propeller excitation force of -2m. Its characteristics are the pitch of 6 blades in a multi-blade propeller, Some or all of the conditions of the diameter-to-area ratio or the rake angle are configured to be different.
以下、実施例の図面に基づき本発明全詳述するが、第1
図に示すグラフは、MAU型プロペラ設計図表から求め
た対称翼型プロペラの翼数全変化させた場合のプロペラ
効率の変化を示したものでらるQ
第1図から判明する通り、従来の3翼と6翼ならびに6
翼とが構成するプロペラ効率は同グラフη。 (鎖線)
の通り得られるので、現在多く使用されている4翼ある
いは6翼のプロペラにおける中間翼、例えば、4,5翼
に相当するプロペラ効率を得る場合には、その翼径、ピ
ッチ、面積比あるいはレーキ角度の一部または全部を異
なる条件にてプロペラ全設計すれば得られることが理解
できる。The present invention will be described in detail below based on drawings of embodiments.
The graph shown in the figure shows the change in propeller efficiency when the total number of blades is changed for a symmetrical blade type propeller obtained from the MAU type propeller design chart. wings and 6 wings and 6
The efficiency of the propeller made up of the blades is shown in the same graph η. (chain line)
Therefore, if you want to obtain propeller efficiency equivalent to the intermediate blade of the 4-blade or 6-blade propeller that is currently widely used, for example, 4 or 5 blades, the blade diameter, pitch, area ratio, or rake It can be understood that this can be achieved by designing the entire propeller under different conditions for part or all of the angle.
具体的には、第2図の実施例(プロペラの模型図〕に示
す通り、4枚のプロペラ翼A、B、C,Dを有する4翼
型プロペラにおいて、前記翼A翼とC翼、B翼とD翼と
全部々一対とするプロペラ翼の条件、即ち、翼径、免の
ピッチおよび翼の面積比ケ同じとする対称翼とする。Specifically, as shown in the embodiment (propeller model diagram) in FIG. 2, in a four-blade propeller having four propeller blades A, B, C, and D, the blades A, C, and B The conditions for the propeller blades in which the blades and the D blades are all paired are symmetrical blades, that is, the blade diameter, pitch, and area ratio of the blades are the same.
1!IJち、A翼とC翼の諸条件は同じ条件下とし、ま
た、Bj、lとDvgの諸条件は同じ条件とする他、A
、c3i;(どB、D翼とは、プロペラ翼の径、i°ラ
ッチ面積比の諸条件を、それぞれ約80%、約75チ、
約60%にしている。これによp、p、、 Cジエで
は全稚力の80%y<、B、D翼では全推力の20%全
出し、2,5翼に相当したプロペラ効率。1! The conditions for IJ, A wing and C wing are the same, and the conditions for Bj, l and Dvg are the same, and A
, c3i; (For B and D blades, the conditions of propeller blade diameter and i° latch area ratio are approximately 80%, approximately 75 inches,
It is set at about 60%. This results in a propeller efficiency equivalent to 80% of the total thrust for the p, p, and C wings, 20% of the total thrust for the B and D wings, and a propeller efficiency equivalent to 2.5 wings.
プロペラ起振力かえられる。Propeller excitation force can be changed.
さらに、径、ピッチ、面積比、レーキの組合せ全変更す
れば、任意の実数翼数に相当したプロペラが設計でき、
振動が問題とならないプロペラ起振力の限界で最高のプ
ロペラ効率のプロペラが実現できる。Furthermore, by changing the combination of diameter, pitch, area ratio, and rake, it is possible to design a propeller with any real number of blades.
A propeller with the highest propeller efficiency can be achieved at the limit of propeller excitation force where vibration is not a problem.
以上の実施例は、本発明の一実施例であり、各条件、プ
ロペラ翼叡は、適時、所望とする諸条件全設定すること
によシ目的に沿ったプロペラ効率及びプロペラの起振力
全勝ることができる。The above example is an example of the present invention, and each condition and propeller blade control can be set at the appropriate time to achieve propeller efficiency and propeller excitation force in accordance with the purpose. You can win.
以上のように、本発明は、舶用のプロペラにおける翼径
、ピッチ、面積比あるいはレーキ角度の各条件の一部ま
たは全部全相異する如く設定するように構成したので、
旧来のプロペラでは得られなかった中間翼の諸性能が得
られるものであって、船舶の省エネルギーの一部として
のプロペラとして極めて実用性の高い効果が得られるも
のである。As described above, the present invention is configured so that some or all of the conditions of the blade diameter, pitch, area ratio, or rake angle of a marine propeller are set to be different.
It is possible to obtain various performances of the intermediate blade that could not be obtained with conventional propellers, and it is highly practical as a propeller as part of energy saving for ships.
なお、第2図の実施例は本発明の一実施例であって、該
実施例に限定されるものではない。Note that the embodiment shown in FIG. 2 is one embodiment of the present invention, and the present invention is not limited to this embodiment.
第1図のグラフは、プロペラ翼数とプロペラ効率の変化
を示すグラフ、第2図は本発明のプロペラの一実施例を
示すfflW図である。
特許出朗人 株式会社神戸製鋼所The graph in FIG. 1 is a graph showing changes in the number of propeller blades and the propeller efficiency, and FIG. 2 is an fflW diagram showing one embodiment of the propeller of the present invention. Patent author Kobe Steel, Ltd.
Claims (1)
翼のピッチ、径1面積比あるいはレーキ角度の諸条件の
一部またけ全部を相異する条件となる如く構成したこと
全特徴とする舶用プロペラ。A marine propeller having a plurality of blades, characterized in that the propeller blades are configured such that some or all of the conditions of pitch, diameter/area ratio, or rake angle are different.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2668183A JPS59153689A (en) | 1983-02-18 | 1983-02-18 | Boat propeller |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2668183A JPS59153689A (en) | 1983-02-18 | 1983-02-18 | Boat propeller |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS59153689A true JPS59153689A (en) | 1984-09-01 |
Family
ID=12200135
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2668183A Pending JPS59153689A (en) | 1983-02-18 | 1983-02-18 | Boat propeller |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS59153689A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103158846A (en) * | 2011-12-09 | 2013-06-19 | 联合船舶设计发展中心 | Full-speed domain propeller unit |
-
1983
- 1983-02-18 JP JP2668183A patent/JPS59153689A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103158846A (en) * | 2011-12-09 | 2013-06-19 | 联合船舶设计发展中心 | Full-speed domain propeller unit |
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