JPS62149598A - Marine counter propeller - Google Patents

Marine counter propeller

Info

Publication number
JPS62149598A
JPS62149598A JP29158685A JP29158685A JPS62149598A JP S62149598 A JPS62149598 A JP S62149598A JP 29158685 A JP29158685 A JP 29158685A JP 29158685 A JP29158685 A JP 29158685A JP S62149598 A JPS62149598 A JP S62149598A
Authority
JP
Japan
Prior art keywords
propeller
front propeller
diameter
axis
rear propeller
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.)
Granted
Application number
JP29158685A
Other languages
Japanese (ja)
Other versions
JPH0659871B2 (en
Inventor
Shigeki Nishiyama
茂樹 西山
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.)
IHI Corp
Original Assignee
IHI Corp
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 IHI Corp filed Critical IHI Corp
Priority to JP29158685A priority Critical patent/JPH0659871B2/en
Publication of JPS62149598A publication Critical patent/JPS62149598A/en
Publication of JPH0659871B2 publication Critical patent/JPH0659871B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Abstract

PURPOSE:To avoid tip vortex cavitation by inclining the wing tip part of a front propeller toward the rear stream side in order to incline the whole rear propeller toward the upper stream side. CONSTITUTION:A front propeller 6 and a rear propeller 8 are placed onto one rotary axis in order to be revolved in the opposit direction to each other. And, the part extending from a root part 7 by 0.8 length of the radius of the front propeller 6 is arranged at a right angle to the rotary axis and the part extending up to a wind tip therefrom is inclined rearward. Also, the whole rear propeller 8 is inclined forward rather than the surface vertical to the rotary axis. And, the diameter of the rear propeller projected or the surface vertical to the rotary axis is made to be smaller than that of the front propeller projected to the surface vertical to the rotary axis, and made to be greater than 0.9.

Description

【発明の詳細な説明】 [産業上の利用分野」 本発明は、前側プロペラと後側プロペラとを1つの回転
軸線上に並べ、前側プロペラと後側プロペラとを互に反
対方向に回転させて船舶を推進させるようにした舶用二
重反転プロペラに関するものである。
[Detailed Description of the Invention] [Industrial Application Field] The present invention provides a system in which a front propeller and a rear propeller are arranged on one rotational axis, and the front propeller and the rear propeller are rotated in opposite directions. This invention relates to a contra-rotating propeller for ships that propels ships.

[従来の技術] 従来の舶用二重反転プロペラを第3図について説明する
と、船体aには、前側プロペラbと後側プロペラCとが
1つの回転軸線d 」ニに並べられて取イ」けられてい
る。前側ブ[1ペラbは右ピッヂの普通型プロペラで右
回転し、後側プロペラCは左ピッチの普通型ブl]ペラ
で左回転し、船体aを推進するようになっている。
[Prior Art] A conventional marine counter-rotating propeller is explained with reference to FIG. It is being The front propeller [1 propeller B is a normal propeller with a right pitch and rotates clockwise, and the rear propeller C is a normal propeller with a left pitch and rotates counterclockwise to propel the hull a.

[発明が解決しようとする問題点] このような舶用二組反転プロペラでは、作動荷重が比較
的高い場合に前側プロペラbの翼端eから発生して流出
するチップポルデックスキ!?ビテーションfが後側プ
ロペラCの直径をあらかじめ前側プロペラ6の直径より
も10%程度小さくしておいても後側プロペラCに干渉
する。
[Problems to be Solved by the Invention] In such a two-set reversing marine propeller, when the operating load is relatively high, a chip pordex occurs and flows out from the blade tip e of the front propeller b. ? The biting f interferes with the rear propeller C even if the diameter of the rear propeller C is made approximately 10% smaller than the diameter of the front propeller 6 in advance.

前側プ[コペラbと後側プ(コペラCとの干渉ににつで
チップ小ルテツクスキX7ビテーシヨンfか後側プロペ
ラCの萱に当り、長時間作動では後側プロペラにキャビ
テーションエ[1−ジョンを発生させる恐れが必る9、
この対策の1つとして。
Due to the interference between the front propeller B and the rear propeller C, the small tip ski There is a risk that it will occur9.
As one of these measures.

後側プロペラCの直径をざらに小さくすることも考えら
れるが、船舶の11f−l装置全体として性能低下をぎ
たづため、1q策でない。
Although it is conceivable to roughly reduce the diameter of the rear propeller C, this is not a 1q measure because it would lead to a decline in the performance of the entire 11f-l device of the ship.

本発明は、このようなチップポルテックスキャビテーシ
ョン[を回避できるようにして、舶用二重反転プロペラ
の性能を向上さuようとするものである。
The present invention aims to improve the performance of a marine counter-rotating propeller by making it possible to avoid such tip portex cavitation.

[問題点を解決するための手段] 本発明は、前側プロペラと後側プロペラとを1つの回転
軸線上に並べ、前側プロペラと後側プロペラとを互に反
対方向に回転させる舶用二手反転プロペラにおいて、前
側プロペラの翼根部から半径のほぼO18までの長さの
部分を回転軸線に対して直角とし、前側プロペラの半径
のほぼ0,8の長さの位置から翼端までの部分を後方(
後流側)に傾斜させ、後側プロペラ金体を回転軸線に直
角の面よりら前方(上流側)に傾斜ざV、回転軸線に直
角の而に投影した後側プロペラの直径を、回転軸線に直
角の而に投影した前側プロペラの直径より小さく、かつ
、0.9よりも大ぎな寸法にした舶用二重反転プロペラ
としたものでおる。
[Means for Solving the Problems] The present invention provides a two-handed reversible marine propeller in which a front propeller and a rear propeller are arranged on one rotational axis, and the front propeller and the rear propeller rotate in opposite directions. , the length from the blade root of the front propeller to approximately O18 of the radius is perpendicular to the axis of rotation, and the portion from the length of approximately 0.8 of the radius of the front propeller to the blade tip is the rear (
The diameter of the rear propeller is the diameter of the rear propeller when the rear propeller body is tilted forward (upstream) from a plane perpendicular to the axis of rotation, and the diameter of the rear propeller is projected at right angles to the axis of rotation. This is a contra-rotating marine propeller whose dimensions are smaller than the diameter of the front propeller projected perpendicularly to and larger than 0.9.

[作  用] 前側プロペラと後側プロペラとが接近して設けられ、こ
れらのプ1コペラか高荷重度で作動している場合でも、
後側プロペラは、前側プロペラから流出するチップポル
テックスキャビテーションを回避することができる。
[Function] Even if the front propeller and the rear propeller are installed close to each other and these two propellers are operating under high load,
The rear propeller can avoid tip portex cavitation flowing out from the front propeller.

[実 施 例] 以下、本発明の一実施例を、図面を参照して説明する。[Example] Hereinafter, one embodiment of the present invention will be described with reference to the drawings.

第1図において、1は前側プロペラ回転軸、2は後側プ
ロペラ回転軸であって、これらの回転軸は図示しない船
体の船尾にd3いて、1つの回転軸線3上に同心に配設
されている。前側プロペラ回転l1111にはボス4が
取付けられており、後側プロペラ回転1N12はボス5
が取付けられていて、ボス4には前側プロペラ6の翼根
部7が固着されており、ボス5には後側プロペラ8の翼
根部9が固着され、前側プロペラ6と後側プロペラ8と
は1つの回転軸線3上に並んでいる。
In FIG. 1, 1 is a front propeller rotation shaft, and 2 is a rear propeller rotation shaft. There is. Boss 4 is attached to front propeller rotation 1111, and boss 5 is attached to rear propeller rotation 1N12.
is attached, the blade root 7 of the front propeller 6 is fixed to the boss 4, the blade root 9 of the rear propeller 8 is fixed to the boss 5, and the front propeller 6 and the rear propeller 8 are connected to one another. They are lined up on two rotational axes 3.

そして前側プロペラ6と後側プロペラ8とは互に反対方
向に回転し、図示しない船体を推進させるようになって
いる。
The front propeller 6 and the rear propeller 8 rotate in opposite directions to propel the hull (not shown).

前側プロペラ6は、翼根部7から半径Rのほぼ0.8R
までの艮ざの部分を回転軸線3に対して直角の方向(零
レーキ角)とし、前側ブ1コペラ6の半径のほぼ0,8
Rの長さの位置から翼端10までの部分を、回転軸線3
に対して直角な而に対し角度θbで後方(後流側)に傾
斜さμている。
The front propeller 6 has a radius R of approximately 0.8R from the blade root 7.
The direction of the rake up to is perpendicular to the axis of rotation 3 (zero rake angle), and the radius of the front blade 1 is approximately 0.8 of the radius of the copella 6.
The part from the length position of R to the blade tip 10 is the rotation axis 3
Although it is perpendicular to , it is inclined backward (to the downstream side) at an angle θb.

後側プロペラ8は、回転軸線3に直角な面に対し角度0
1て前方(上流側)に全体を傾斜さUている。そして前
側ブ1コペラ6が回転軸線3に直角な面に投影した面側
ブl]ベラ6の直径を第2図に示すJ:うにDFとした
とき、後側プロペラ8が回転軸線3に直角な面に投影し
た後側プロペラ8の直径り八は、019DF<D八<D
F−どなるように、前側プロペラ6の直径DFの0.9
よりも大きいが、前側プロペラの直径D=よりも小ざな
範囲の寸法にしている。
The rear propeller 8 is at an angle of 0 with respect to a plane perpendicular to the rotation axis 3.
The entire structure is tilted forward (upstream). When the diameter of the front propeller 1 and propeller 6 is projected onto a plane perpendicular to the rotational axis 3 and the diameter of the propeller 6 is J: DF shown in FIG. 2, the rear propeller 8 is perpendicular to the rotational axis 3. The diameter of the rear propeller 8 projected onto the plane is 019DF<D8<D
F - 0.9 of the diameter DF of the front propeller 6
It is larger than the diameter D of the front propeller, but the size is within a smaller range than the diameter D= of the front propeller.

後側プロペラ8の直径DAは前側プロペラ6の直径D=
よりわずかに小さい程度なので、前側プロペラ6のlG
m10と、後側プロペラ8の翼端11とは接近すること
になるが、本舶用二重反転プロペラでは前側プロペラ6
および後側プロペラ8が高荷重度で作動している場合で
も、前側プロペラ6の翼Minから流出するチップポル
テックスキャビテーションを回避することができる。1 前側プロペラ6と後側プロペラ8とは互に反対方向に回
転するので、プロペラ後方のスリラプス1〜リーム中の
回転方向の速度成分が回転軸線3方向に変換できるうえ
、後側プロペラ8の直径DAも従来の二組反転プロペラ
における後側プロペラの直径より大きくてきるので、従
来」:りも低荷重度の作動かできることになる。
The diameter DA of the rear propeller 8 is the diameter D of the front propeller 6 =
Since it is slightly smaller than the lG of the front propeller 6
m10 and the blade tip 11 of the rear propeller 8 will be close to each other, but in this counter-rotating marine propeller, the front propeller 6
Even when the rear propeller 8 is operating at a high load level, tip portex cavitation flowing out from the blade Min of the front propeller 6 can be avoided. 1 Since the front propeller 6 and the rear propeller 8 rotate in opposite directions, the speed component in the rotational direction during the thrilapse 1 to ream behind the propeller can be converted to the rotational axis 3 direction, and the diameter of the rear propeller 8 Since the DA is also larger than the diameter of the rear propeller in a conventional two-set reversing propeller, it is possible to operate with a lower load than the conventional one.

[発明の効果] 結局、本発明によって、高いプロペラ弔独効率がjqら
れる上、前側プロペラから流出し後側プロペラにエロー
ジョンをもたらすチップ小ルテックスキ1?ビテーショ
ンを回避できる。
[Effects of the Invention] In the end, the present invention not only provides high propeller recovery efficiency, but also reduces the possibility of small chips flowing out of the front propeller and causing erosion to the rear propeller. Biting can be avoided.

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

第1図は本発明の一実施例の側面図、第2図は第1図の
■−■矢視図、第3図は従来の舶用二手反転プロペラの
側面図である。 3は回転軸線、6は前側プロペラ、7,9は究根部、8
は後側プロペラ、1o、 iiは翼端を示覆。
FIG. 1 is a side view of an embodiment of the present invention, FIG. 2 is a view taken along the line ■--■ in FIG. 1, and FIG. 3 is a side view of a conventional marine two-handed reversible propeller. 3 is the rotation axis, 6 is the front propeller, 7 and 9 are the root parts, 8
is the rear propeller, 1o and ii are the wing tips.

Claims (1)

【特許請求の範囲】[Claims] 1)前側プロペラと後側プロペラとを1つの回転軸線上
に並べ、前側プロペラと後側プロペラとを互に反対方向
に回転させる舶用二重反転プロペラにおいて、前側プロ
ペラの翼根部から半径のほぼ0.8までの長さの部分を
回転軸線に対して直角(零レーキ角)とし、その翼半径
のほぼ0.8の長さの位置から翼端までの部分を後流側
に傾斜させ、また、後側プロペラ全体を回転軸線に直角
の面よりも上流側に傾斜させ、回転軸線に直角の面に投
影した後側プロペラの直径を、回転軸線に直角の面に投
影した前側プロペラの直径より小さく、かつ、0.9よ
りも大きな寸法にしたことを特徴とする舶用二重反転プ
ロペラ。
1) In a contra-rotating marine propeller in which the front propeller and the rear propeller are arranged on one rotational axis and rotate in opposite directions, the radius from the blade root of the front propeller is approximately 0. The length up to 0.8 is perpendicular to the rotation axis (zero rake angle), and the part from approximately 0.8 of the blade radius to the blade tip is tilted to the wake side, and , the entire rear propeller is tilted upstream from the plane perpendicular to the axis of rotation, and the diameter of the rear propeller projected onto the plane perpendicular to the axis of rotation is greater than the diameter of the front propeller projected onto the plane perpendicular to the axis of rotation. A counter-rotating marine propeller characterized by being small and having dimensions larger than 0.9.
JP29158685A 1985-12-23 1985-12-23 Marine counter-rotating propeller Expired - Lifetime JPH0659871B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP29158685A JPH0659871B2 (en) 1985-12-23 1985-12-23 Marine counter-rotating propeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP29158685A JPH0659871B2 (en) 1985-12-23 1985-12-23 Marine counter-rotating propeller

Publications (2)

Publication Number Publication Date
JPS62149598A true JPS62149598A (en) 1987-07-03
JPH0659871B2 JPH0659871B2 (en) 1994-08-10

Family

ID=17770852

Family Applications (1)

Application Number Title Priority Date Filing Date
JP29158685A Expired - Lifetime JPH0659871B2 (en) 1985-12-23 1985-12-23 Marine counter-rotating propeller

Country Status (1)

Country Link
JP (1) JPH0659871B2 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6428094A (en) * 1987-07-22 1989-01-30 Kawasaki Heavy Ind Ltd Propelling device for ship
US5190441A (en) * 1990-08-13 1993-03-02 General Electric Company Noise reduction in aircraft propellers
JP2012096767A (en) * 2010-11-05 2012-05-24 Niigata Power Systems Co Ltd Marine propulsion device
EP2631168A4 (en) * 2010-10-19 2017-09-20 Mitsubishi Heavy Industries, Ltd. Propulsion device and ship using same
US10414486B2 (en) 2015-11-30 2019-09-17 General Electric Company Airfoil for a rotary machine including a propellor assembly

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5690564B2 (en) * 2010-11-25 2015-03-25 ジャパンマリンユナイテッド株式会社 Counter-rotating propeller and ship
EP2944560A1 (en) * 2014-05-14 2015-11-18 ABB Oy Propulsion unit

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6428094A (en) * 1987-07-22 1989-01-30 Kawasaki Heavy Ind Ltd Propelling device for ship
US5190441A (en) * 1990-08-13 1993-03-02 General Electric Company Noise reduction in aircraft propellers
EP2631168A4 (en) * 2010-10-19 2017-09-20 Mitsubishi Heavy Industries, Ltd. Propulsion device and ship using same
JP2012096767A (en) * 2010-11-05 2012-05-24 Niigata Power Systems Co Ltd Marine propulsion device
US10414486B2 (en) 2015-11-30 2019-09-17 General Electric Company Airfoil for a rotary machine including a propellor assembly
US11136109B2 (en) 2015-11-30 2021-10-05 General Electric Company Airfoil for a rotary machine including a propellor assembly

Also Published As

Publication number Publication date
JPH0659871B2 (en) 1994-08-10

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