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JPS6250357B2 - - Google Patents
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JPS6250357B2 - - Google Patents

Info

Publication number
JPS6250357B2
JPS6250357B2 JP6219979A JP6219979A JPS6250357B2 JP S6250357 B2 JPS6250357 B2 JP S6250357B2 JP 6219979 A JP6219979 A JP 6219979A JP 6219979 A JP6219979 A JP 6219979A JP S6250357 B2 JPS6250357 B2 JP S6250357B2
Authority
JP
Japan
Prior art keywords
propeller
water
duct
waterway
speed
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
Application number
JP6219979A
Other languages
Japanese (ja)
Other versions
JPS55156795A (en
Inventor
Atsushi Ozaki
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shinmaywa Industries Ltd
Original Assignee
Shin Meiva Industry Ltd
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 Shin Meiva Industry Ltd filed Critical Shin Meiva Industry Ltd
Priority to JP6219979A priority Critical patent/JPS55156795A/en
Publication of JPS55156795A publication Critical patent/JPS55156795A/en
Publication of JPS6250357B2 publication Critical patent/JPS6250357B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H1/00Propulsive elements directly acting on water
    • B63H1/02Propulsive elements directly acting on water of rotary type
    • B63H1/12Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
    • B63H1/14Propellers
    • B63H1/18Propellers with means for diminishing cavitation, e.g. supercavitation
    • B63H2001/185Surfacing propellers, i.e. propellers specially adapted for operation at the water surface, with blades incompletely submerged, or piercing the water surface from above in the course of each revolution

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

【発明の詳細な説明】 この発明は高速船に用いられるプロペラ装置に
関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a propeller device used in a high-speed boat.

従来30kt位までの速力で使用される船舶におい
ては、断面が翼型や円弧型のスクリユープロペラ
を使用するのが普通であるが、約40kt以上の速力
になるとキヤビテーシヨンが発生して効率が著し
く悪化したり、潰食のためプロペラが損傷したり
するので、その防止手段としてスーパーキヤビテ
ーシヨンプロペラ、ウオータージエツト、サーフ
エスプロペラ等が研究され、一部実用化されてき
た。
Conventionally, ships operated at speeds of up to 30 kt usually use screw propellers with a wing-shaped or arc-shaped cross section, but when speeds exceed about 40 kt, cavitation occurs and efficiency is significantly reduced. This can lead to deterioration or damage to the propeller due to erosion, so as a means to prevent this, research has been conducted on supercavitation propellers, water jets, surf propellers, etc., and some of them have been put into practical use.

しかしながら、スーパーキヤビテーシヨンプロ
ペラは低中速における効率が悪く、キヤビテーシ
ヨンを発生し始める遷移速力(30〜40kt)におい
てはやはり潰食現象を起す欠点がある。またウオ
ータージエツトは近年改良が加えられて、例えば
インペラーの前にインデユーサーを設けて水圧を
高め、キヤビテーシヨンが発生する速力を高める
等の性能向上がみられるが、効率は最大60%程度
であり、また50kt以上ではやはりキヤビテーシヨ
ンが問題となる。
However, supercavitation propellers are inefficient at low to medium speeds and have the disadvantage of causing erosion at transition speeds (30 to 40kt) where cavitation begins to occur. In addition, improvements have been made to water jets in recent years, such as installing an inducer in front of the impeller to increase the water pressure and increase the speed at which cavitation occurs, but the efficiency is only about 60% at most. Also, cavitation becomes a problem at speeds over 50 kt.

これに対し、プロペラの上方を水面上に露出さ
せた状態で回転するいわゆるサーフエスプロペラ
は、キヤビテーシヨンを起していない“GAWN
の円弧翼型プロペラ性能曲線”に匹敵する70%以
上の効率が得られるが、プロペラの単位面積当り
の推力やトルクが小さく、この傾向は速力が小な
る程著しいので、速力が零付近ではプロペラが空
転して予定速力になかなか達しないおそれがあ
り、またプロペラが水面を間欠的に叩くので推力
やトルクの変動が非常に大きい欠点がある。
In contrast, the so-called surf-s propeller, which rotates with the upper part of the propeller exposed above the water surface, has a "GAWN" that does not cause cavitation.
However, the thrust and torque per unit area of the propeller are small, and this tendency becomes more pronounced as the speed decreases, so when the speed is near zero, the propeller There is a risk that the propeller will spin and not reach the planned speed, and the propeller will intermittently hit the water surface, resulting in large fluctuations in thrust and torque.

本発明の目的は従来の上記欠点を除去し、高速
において効率がよく、しかも副害の発生なしに良
好に作動するプロペラ装置を提供するにある。
SUMMARY OF THE INVENTION An object of the present invention is to eliminate the above-mentioned drawbacks of the conventional propeller system, and to provide a propeller device that is efficient at high speeds and operates well without causing side effects.

本発明は、前記のサーフエスプロペラの背面が
水面上より空気を吸い込み、背面に接して空気が
入つた空洞を形成するため、殆んどキヤビテーシ
ヨンの影響を受けないことに着目してなされたも
ので、その特徴は、前進状態においてはプロペラ
の後方を大気中に開放してプロペラ背面を空気を
吸い込み易い状態にするために、プロペラ前面に
プロペラの殆ど全体に水を当てるようなダクト又
は水路を船体に設け、プロペラ後流を水面上の大
気中に放出せしめた点にある。
The present invention was made based on the fact that the back surface of the Surf S propeller sucks air from above the water surface and forms a cavity filled with air in contact with the back surface, so it is hardly affected by cavitation. The feature is that in order to open the rear of the propeller to the atmosphere in the forward state and make it easier for the back of the propeller to suck in air, a duct or channel is installed in the front of the propeller to apply water to almost the entire propeller. It is installed on the ship's hull, and the propeller's wake is released into the atmosphere above the water surface.

以下本発明の実施例を図面を参照して説明す
る。
Embodiments of the present invention will be described below with reference to the drawings.

第1図は左方に航行する滑走艇の後部を示した
もので、船底1より下方に突出して設けた取水口
2から水をダクト3内に誘導し、その後端出口部
に軸受金具4により支持したプロペラ5を設け
る。6はプロペラ駆動軸である。ダクト3の内面
はプロペラ5の外周に近接させる。上記構造のV
型高速艇等が滑走すると、後方水面7は船尾にお
いてプロペラ5より低くなり、プロペラ5の後方
を大気中に完全に露出させる。その結果、プロペ
ラ5はダクト3から放出された周囲に自由表面を
有する水流の中で回転することになり、自由表面
よりプロペラ先端に空気が誘引され、第5図に示
すようにプロペラ5(羽根断面で示す)の背面5
aに空気が吸入されて空洞8を形成するので、サ
ーフエスプロペラと全く同様の性質をもつことに
なる。なお、自由表面に近い所で回転するプロペ
ラがよく空気を誘引することは周知の事実であ
る。これと共に、ダクト3内の水がプロペラ5の
前面全体に当るので推力やトルクがサーフエスプ
ロペラに較べて倍増し、しかもそれらが変動しな
いのである。更に、通常のスーパーキヤビテーシ
ヨン状態における空洞は真空に近い水の蒸気圧で
あるのに対し、空洞8の圧力は大気圧に近いの
で、これによる衝撃的圧力やこれに伴う潰食の発
生等はなく、キヤビテーシヨンの害を生じない。
Figure 1 shows the rear of a personal watercraft sailing to the left. Water is guided into a duct 3 from a water intake 2 protruding downward from the bottom 1, and a bearing fitting 4 is connected to the outlet at the rear end. A supported propeller 5 is provided. 6 is a propeller drive shaft. The inner surface of the duct 3 is brought close to the outer periphery of the propeller 5. V of the above structure
When a high-speed boat or the like is planing, the rear water surface 7 becomes lower than the propeller 5 at the stern, completely exposing the rear part of the propeller 5 to the atmosphere. As a result, the propeller 5 rotates in the water flow discharged from the duct 3 and having a free surface around it, and air is attracted from the free surface to the tip of the propeller, and as shown in FIG. (shown in cross section) back side 5
Since air is sucked into a to form a cavity 8, it has exactly the same properties as a Surf S propeller. It is a well-known fact that a propeller rotating close to a free surface often attracts air. At the same time, the water in the duct 3 hits the entire front surface of the propeller 5, so the thrust and torque are doubled compared to the Surf S propeller, and they do not fluctuate. Furthermore, while the cavity in a normal supercavitation state has a water vapor pressure close to a vacuum, the pressure in the cavity 8 is close to atmospheric pressure, so the impact pressure caused by this and the accompanying erosion occur. etc., and does not cause cavitation damage.

上記実施例における取水口2は船底下方に突出
したラム型式であるが、第2図に示す実施例は取
水口2aを船底1に下向けに開口させたフラツシ
型式であり、取水口2aの上壁下部を曲率小なる
凸面として船底面に滑らかに接続させると、停船
時はダクト3a及びプロペラ5が水没している
が、前進時は速度増加とともに船尾が上昇してコ
アンダー効果により水が効率よくダクト3a内に
誘引される。本実施例でもダクト3aの内面はプ
ロペラ外周に近接する。本実施例においては、プ
ロペラ5はダクト3aの後端より外に設置されて
おり、軸受金具4a内を通る駆動軸6aによりボ
ス9内のギヤボツクスを介して回転される。プロ
ペラ5は一部がダクト3aに入るように設けても
よい。
The water intake 2 in the above embodiment is of a ram type that protrudes below the bottom of the ship, but the embodiment shown in FIG. If the lower part of the wall is made into a convex surface with a small curvature and smoothly connected to the bottom of the ship, the duct 3a and propeller 5 are submerged in water when the ship is stationary, but when the ship is moving forward, the stern rises as the speed increases and water is efficiently drained due to the Coander effect. It is attracted into the duct 3a. In this embodiment as well, the inner surface of the duct 3a is close to the outer circumference of the propeller. In this embodiment, the propeller 5 is installed outside the rear end of the duct 3a, and is rotated via a gear box in a boss 9 by a drive shaft 6a passing through a bearing fitting 4a. The propeller 5 may be provided so that a portion thereof enters the duct 3a.

第3図a,bに示す他の実施例は、プロペラに
当る水流の上半分をプロペラ先端に近い自由水面
となるように船尾底部を後端10がほぼ半円にな
るように凹設した水路3bを設けたもので、水路
内面形状によるコアンダー効果については第2図
の実施例と同様であり、また水路内面はプロペラ
外周に近接しており、プロペラ5の背面上半部が
大気中に露出しており、プロペラ背面にサーフエ
スプロペラと同様に空気が誘引される。本実施例
においては、プロペラ5を支持するギヤボツクス
9b、軸受金具4b等をプロペラ5の後方に設
け、駆動軸6bを船外から船内に誘導している。
このようにするとプロペラ5の前方に構造物がな
いのでプロペラ性能を向上させることができる。
Another embodiment shown in FIGS. 3a and 3b is a channel in which the bottom of the stern is recessed so that the rear end 10 is approximately semicircular so that the upper half of the water flow that hits the propeller becomes a free water surface near the tip of the propeller. 3b, and the coander effect due to the inner surface shape of the waterway is similar to that of the embodiment shown in FIG. Air is attracted to the back of the propeller, similar to the Surf S propeller. In this embodiment, a gear box 9b, a bearing fitting 4b, etc. that support the propeller 5 are provided behind the propeller 5, and the drive shaft 6b is guided from outside the ship into the inside of the ship.
In this way, since there is no structure in front of the propeller 5, propeller performance can be improved.

第4図a,bに示す他の実施例は、船底1が船
の後端まで水平に延長する形において、後部船底
1cに後方が半円形をなす下面開放の成形部材1
1を固定して高速滑走時に後方水面を成形部材1
1の下部斜面11aによつて破線のように低下さ
せ、これによりプロペラ5の上半部を大気中に露
出させて第3図におけると同様の作用効果を得た
ものである。この構造は既存の舟艇にもそのまま
利用し得る便があり、適用範囲がきわめて広い利
点がある。
In another embodiment shown in FIGS. 4a and 4b, the bottom 1 extends horizontally to the rear end of the ship, and the rear bottom 1c has a molded member 1 with an open bottom and a semicircular shape at the rear.
1 is fixed and molds the rear water surface during high-speed skiing.
The propeller 5 is lowered as shown by the broken line by the lower slope 11a of the propeller 5, thereby exposing the upper half of the propeller 5 to the atmosphere to obtain the same effect as in FIG. This structure has the advantage of being able to be used as is on existing watercraft, and has an extremely wide range of applications.

次に本発明に使用されるプロペラの翼形につい
て説明する。
Next, the blade shape of the propeller used in the present invention will be explained.

第6図aはエーロフオイル型で、飛行機の空中
翼と同じものであり、効率がよいので中低速の船
に最も多用される翼型である。bは上下面が円弧
をなす円弧翼型で、中低速における性能はエーロ
フオイル型に劣るが、製作が容易で、キヤビテー
シヨンはエーロフオイル型よりも優れており、レ
ジヤーボートや特殊な高速船に使われる。
Figure 6a shows an airfoil type airfoil, which is the same as an airplane's airfoil, and is the airfoil type most commonly used for medium- and low-speed ships because of its high efficiency. Type b is an arcuate airfoil with the upper and lower surfaces forming arcs, and although its performance at medium and low speeds is inferior to the Aerofoil type, it is easier to manufacture and its cavitation is superior to the Aerofoil type, and is used in leisure boats and special high-speed boats.

第6図c,d,eはスーパーキヤビテーシヨン
の領域で使用される翼型(以下SC翼と称する)
であり、cは下面が平面の平面SC翼、dはTulin
−Burkart翼、eは5項翼の代表的な翼型であ
る。このほか図示しないが3項翼といわれるもの
もあり、これは翼下面がTulin−Burkart翼と5
項翼eとの中間の形状を有する。これらのTulin
−Burkart翼、3項翼、及び5項翼は高性能翼と
して知られており、高速水中翼船の翼やSCプロ
ペラとして使用されている。これに対し平面SC
翼は性能劣悪とされているが、円弧翼、平面SC
翼、Tulin−Burkart翼のプロペラをサーフエス
プロペラとして使用した実験成績では、Tulin−
Burkart翼が効率70〜75%、平面SC翼もこれとほ
ぼ同等の成績を示したのに対し、円弧翼のものは
効率60〜65%程度に止まるのと報告例もある。し
かしこれらの翼型のプロペラはいずれも本発明に
利用可能である。なお、プロペラ背面の通気を良
くするため、背面に段差を設けた第6図f、又は
背面外方に溝を設けたgの如きベンテドフオイル
型のプロペラも本発明に使用することができる。
Figure 6c, d, and e are airfoils used in the supercavitation area (hereinafter referred to as SC airfoils).
, c is a planar SC wing with a flat bottom surface, and d is Tulin
-Burkart wing, e is a typical airfoil shape of a 5-term wing. In addition, although not shown in the figure, there is also a type of wing called a trinomial wing, in which the lower surface of the wing is similar to the Tulin-Burkart wing.
It has a shape intermediate between that of the nuchal wing e. These Tulin
-Burkart blades, 3-term blades, and 5-term blades are known as high-performance blades and are used as high-speed hydrofoil blades and SC propellers. In contrast, the plane SC
Although the wings are said to have poor performance, arcuate wings and flat SC
In experimental results using a Tulin-Burkart wing propeller as a surf-s propeller, Tulin-
There are reports that Burkart blades have an efficiency of 70-75%, and flat SC blades have similar performance, while arc-shaped blades have an efficiency of only 60-65%. However, any of these airfoil type propellers can be used in the present invention. Incidentally, in order to improve ventilation on the back surface of the propeller, a bent oil type propeller as shown in FIG.

また前述の如き、サーフエスプロペラの速力零
付近における空転現象に対しては、プロペラを静
止状態において水没する位置に取付け、滑走状態
においてプロペラ後面が大気中に露出するよう水
路の後方出口の形状を選定することによつて解決
することができる。
In addition, as mentioned above, in order to prevent the spinning phenomenon of the Surf-S propeller near zero speed, the propeller is installed in a position where it is submerged in water when it is stationary, and the shape of the rear exit of the waterway is designed so that the rear surface of the propeller is exposed to the atmosphere when it is sliding. The problem can be solved by selecting

本発明は上記構成を有し、プロペラ後方を大気
中に解放し、且つプロペラ前面に水を当てさせる
ことにより、キヤビテーシヨンの発生を防止し、
しかも効率が良く、推力やトルクの変動がなく、
いかなる速力でも安定に作動し得る等のすぐれた
効果があり、構造もきわめて簡単で製作容易であ
り、使用するプロペラの翼型についても既存の水
中翼やSCプロペラの資料をそのまま活用し得る
ので直ちに実施可能である等の効果がある。
The present invention has the above configuration, and prevents the occurrence of cavitation by opening the rear of the propeller to the atmosphere and applying water to the front of the propeller.
Moreover, it is highly efficient, with no fluctuations in thrust or torque,
It has excellent effects such as being able to operate stably at any speed, and the structure is extremely simple and easy to manufacture.As for the blade shape of the propeller used, existing hydrofoils and SC propeller materials can be used as is, so it can be used immediately. It has the advantage of being possible to implement.

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

第1図,第2図,第3図a,第4図aは本発明
のそれぞれ異る実施例を示す部分断面立面図、第
3図b,第4図bはそれぞれ第3図a,第4図a
の実施例の側面図、第5図は本発明におけるプロ
ペラ背面の空洞発生説明図、第6図a〜gは本発
明に使用可能の各種のプロペラ翼型の断面図であ
る。 3,3a……ダクト、3b……水路、5……プ
ロペラ。
1, 2, 3a, and 4a are partially sectional elevational views showing different embodiments of the present invention, and FIGS. 3b and 4b are respectively 3a and 4b. Figure 4a
FIG. 5 is a diagram illustrating the generation of cavities on the back surface of the propeller in the present invention, and FIGS. 6 a to 6 g are sectional views of various propeller airfoils that can be used in the present invention. 3, 3a...Duct, 3b...Waterway, 5...Propeller.

Claims (1)

【特許請求の範囲】[Claims] 1 船体の後部船底に、前進時においてプロペラ
のほぼ全体に近い水面上露出部分に水が当る量の
水を吸引して船体後方の水面上の開放大気中に放
出し内面がプロペラ外周に近接したダクト又は水
路を設け、該ダクト又は水路の下部上壁を曲率小
なる凸面として船底面に滑らかに接続させ、該ダ
クト又は水路の出口部の水流中でプロペラを作動
させることを特徴とする通気型プロペラ装置。
1 At the rear bottom of the hull, when moving forward, water was sucked in an amount that hit almost the entire propeller exposed above the water surface, and was released into the open atmosphere above the water surface at the rear of the hull, so that the inner surface was close to the outer periphery of the propeller. A vented type characterized in that a duct or waterway is provided, the lower upper wall of the duct or waterway is a convex surface with a small curvature and smoothly connected to the bottom surface of the ship, and a propeller is operated in the water flow at the outlet of the duct or waterway. Propeller device.
JP6219979A 1979-05-22 1979-05-22 Ventilated propeller apparatus Granted JPS55156795A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6219979A JPS55156795A (en) 1979-05-22 1979-05-22 Ventilated propeller apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6219979A JPS55156795A (en) 1979-05-22 1979-05-22 Ventilated propeller apparatus

Publications (2)

Publication Number Publication Date
JPS55156795A JPS55156795A (en) 1980-12-06
JPS6250357B2 true JPS6250357B2 (en) 1987-10-23

Family

ID=13193230

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6219979A Granted JPS55156795A (en) 1979-05-22 1979-05-22 Ventilated propeller apparatus

Country Status (1)

Country Link
JP (1) JPS55156795A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0224290A (en) * 1988-07-13 1990-01-26 Nkk Corp Low resistance hydrofoil
JP2005030349A (en) * 2003-07-10 2005-02-03 Matsushita Electric Ind Co Ltd Multi-wing fan
JP2008180130A (en) * 2007-01-24 2008-08-07 Tokyo Electric Power Co Inc:The Axial water turbine and driving method thereof

Also Published As

Publication number Publication date
JPS55156795A (en) 1980-12-06

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