JPS623357Y2 - - Google Patents

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Publication number
JPS623357Y2
JPS623357Y2 JP3206981U JP3206981U JPS623357Y2 JP S623357 Y2 JPS623357 Y2 JP S623357Y2 JP 3206981 U JP3206981 U JP 3206981U JP 3206981 U JP3206981 U JP 3206981U JP S623357 Y2 JPS623357 Y2 JP S623357Y2
Authority
JP
Japan
Prior art keywords
blade root
boss
propulsion
blade
wall
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
JP3206981U
Other languages
Japanese (ja)
Other versions
JPS57144795U (en
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 filed Critical
Priority to JP3206981U priority Critical patent/JPS623357Y2/ja
Publication of JPS57144795U publication Critical patent/JPS57144795U/ja
Application granted granted Critical
Publication of JPS623357Y2 publication Critical patent/JPS623357Y2/ja
Expired legal-status Critical Current

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Description

【考案の詳細な説明】 〔産業上の利用分野〕 船舶用可変ピツチプロペラは、推進軸の回転方
向、回転数を変えることなく推進翼のピツチを変
節することによつて、前進又は後進方向に推力を
うることができるのみならず、推進翼のピツチの
角度を調節することによつて、推力を0〜100%
無段でうることができる推進器である。この考案
はこの種可変ピツチプロペラのボス機構に関する
ものである。
[Detailed description of the invention] [Field of industrial application] Variable pitch propellers for ships can move forward or backward by changing the pitch of the propelling blades without changing the rotational direction or rotation speed of the propulsion shaft. Not only can you obtain thrust, but you can also adjust the thrust from 0 to 100% by adjusting the pitch angle of the propulsion blades.
It is a propulsion device that can be propelled steplessly. This invention relates to a boss mechanism for this type of variable pitch propeller.

〔従来の技術〕[Conventional technology]

従前の可変ピツチプロペラは、推進器ボスに変
節機構を内蔵するため、ボスは空洞化し、ボス壁
が薄くなり、強度が低下するという欠点があつ
た。更に推進翼を翼結合材で空洞化したボス壁に
植立するため、推進翼の重心は軸心よりも高く、
推進翼の推力に比例して発生するてこ作用又は推
力0%時若しくは荒天時の空転によつて発生する
遠心力等の荷重に対して全く弱い構造で、上記荷
重のすべてに耐えるために、ボス壁の内厚を厚く
する必要性から、ボスの直径は固定ピツチプロペ
ラに比して大きくならざるを得ず、プロペラ効率
が悪いという宿命的な欠陥を有していた。
Conventional variable pitch propellers have a variable pitch mechanism built into the thruster boss, which has the disadvantage of making the boss hollow, making the boss wall thinner, and reducing its strength. Furthermore, since the propulsion blades are installed in the boss wall hollowed out using the blade bonding material, the center of gravity of the propulsion blades is higher than the axis.
The structure is completely weak against loads such as the lever action that occurs in proportion to the thrust of the propulsion blades, or the centrifugal force that occurs when the thrust is 0% or when spinning in rough weather.In order to withstand all of the above loads, the boss Due to the necessity of increasing the inner thickness of the wall, the diameter of the boss had to be larger than that of a fixed pitch propeller, which had the fateful drawback of poor propeller efficiency.

これに対して第5図及び第6図に示すように、
翼根結合棚15をボス尾部13″内壁に、推進軸
12側に向けて植立新設し、翼根14を翼根結合
部17において、推進翼11同士結合し、回転に
よつて発生する遠心力を互いに釣り合わせ、ボス
壁13′への作用を少なくしてボス壁13′の肉厚
を削減し、ボス13の直径を細くし、ボス比を小
さくすることによつて、プロペラ効率を改善する
試みがなされた。
On the other hand, as shown in Figures 5 and 6,
A new blade root connecting shelf 15 is installed on the inner wall of the boss tail portion 13'' toward the propulsion shaft 12 side, and the blade roots 14 are connected to each other in the blade root connecting portion 17 to connect the propulsion blades 11 to each other, thereby reducing the centrifugal force generated by rotation. Propeller efficiency is improved by balancing the forces against each other, reducing the action on the boss wall 13', reducing the wall thickness of the boss wall 13', reducing the diameter of the boss 13, and reducing the boss ratio. An attempt was made to do so.

〔考案が解決しようとする問題点〕[Problem that the invention attempts to solve]

推力使用時に推進翼11を力点とし、ボス13
の図のP点又はP′点を支点とし、翼根結合部17
を作用点として、推力によつて発生するてこ作用
の荷重が翼根結合棚15を介してボス尾部1
3″、ボス壁13に作用するため、ボス尾部1
3″、ボス壁13の肉厚をあまり削減することが
できず、期待されるほどプロペラ効率は改善され
なかつた。更に翼根結合棚15がボス尾部13″
内壁に植立新設されたことにより、推進器の重心
位置がボス尾部13″側の寄つたため、推進器の
首振り運動の質量が大きくなり、推進器や船体の
振動が発生しやすくなつた。
When using thrust, the propulsion blade 11 is the point of effort, and the boss 13
Using point P or P' in the figure as a fulcrum, connect the blade root joint 17.
The lever action load generated by the thrust is applied to the boss tail part 1 via the blade root connecting shelf 15 with
3″, to act on the boss wall 13, the boss tail 1
3'', the wall thickness of the boss wall 13 could not be reduced much, and the propeller efficiency was not improved as much as expected.Furthermore, the blade root coupling shelf 15 was removed from the boss tail 13''.
Due to the new planting on the inner wall, the center of gravity of the propeller moved closer to the 13'' side of the boss tail, which increased the mass of the propeller's oscillating motion, making it easier for the propeller and the hull to vibrate. .

〔問題点を解決するための手段〕[Means for solving problems]

ここにおいてこの考案は可変ピツチプロペラボ
ス内の推進軸末端にボス尾部側に向けて翼根受結
合棚を突出植立し、この翼根結合棚に翼根を挿入
する翼根嵌合孔を設け、この翼根嵌合孔の内周と
翼根の外周とに結合部をそれぞれ設け、結合材で
推進翼が翼根の円周方向には回転しうるが半径方
向には関係変位不能に結合してなる可変ピツチプ
ロペラボス機構を提案するものであつて、このよ
うな構成とすることによつて推進翼に回転によつ
て発生する遠心力及び推力によつて発生するてこ
作用の荷重をボス壁になるべく作用しない推進器
の構造とし、ボス壁3′の肉厚を薄くし、ボス3
の直径をできるだけ小さくして、プロペラ効率を
よくするとともに、更に推進器の重心をできるだ
け推進軸2側に寄せて、推進器の首振運動の質量
を小さくし、推進軸系や船体の振動及び船尾管軸
受の磨損を少なくしようとするものである。
The idea here is to erect a blade root receiving coupling shelf protruding from the end of the propulsion shaft in the variable pitch propeller boss toward the tail of the boss, and to provide a blade root fitting hole into which the blade root is inserted into the blade root coupling shelf. A connecting part is provided on the inner periphery of this blade root fitting hole and the outer periphery of the blade root, and the propelling blade is connected with a connecting material so that it can rotate in the circumferential direction of the blade root but cannot be displaced in the radial direction. The present invention proposes a variable pitch propeller boss mechanism, which has a variable pitch propeller boss mechanism.With this configuration, the lever action load generated by the centrifugal force and thrust generated by the rotation of the propeller blades is absorbed by the boss. The structure of the thruster is such that it does not act on the wall as much as possible, and the wall thickness of the boss wall 3' is made thinner.
The diameter of the propeller is made as small as possible to improve propeller efficiency, and the center of gravity of the propulsion device is moved as close to the propulsion shaft 2 as possible to reduce the mass of the propulsion device's oscillating motion, reducing vibrations and vibrations of the propulsion shaft system and the ship's hull. This is intended to reduce wear and tear on the stern tube bearing.

〔作用〕[Effect]

次にこの考案を詳細に説明する。 Next, this idea will be explained in detail.

第1図及び第2図に示すように、翼根受結合棚
5を推進軸末端2′にボス尾部3″に向けて植立新
設し、翼根受結合棚5に翼根4を挿入する翼根嵌
合孔6を設け、この翼根嵌合孔6の内周と翼根4
の外周にそれぞれ結合部7を設け、結合材8で推
進翼1が翼根4の円周方向には回転しうるか半径
方向には関係変位不能に翼根4と翼根受結合棚5
を結合するもである。
As shown in FIGS. 1 and 2, a new blade root receiving coupling shelf 5 is installed at the end of the propulsion shaft 2' toward the boss tail 3'', and the blade root 4 is inserted into the blade root receiving coupling shelf 5. A blade root fitting hole 6 is provided, and the inner periphery of the blade root fitting hole 6 and the blade root 4
Connecting parts 7 are provided on the outer periphery of the blade roots 4 and the blade root receiving coupling shelf 5, and a connecting member 8 connects the blade roots 4 and the blade root receiving joint shelf 5 so that the propulsion blades 1 can rotate in the circumferential direction of the blade root 4 but cannot be displaced in the radial direction.
It is also a combination.

なお結合方法として図示のような結合材に限定
するものではなく、第1図及び第2図では結合材
8に充填球を、第3図は結合材8′にねじ環、第
4図は結合材8″に嵌入リングをそれぞれ用いた
実施例を示す。
Note that the bonding method is not limited to the bonding materials shown in the figures; in FIGS. 1 and 2, a filled ball is used as the bonding material 8, in FIG. 3, a screw ring is used as the bonding material 8', and in FIG. An example is shown in which a fitting ring is used for each member 8''.

この考案は上述のように翼根受結合棚5の翼根
嵌合孔6内周と、翼根4の外周にそれぞれ設けた
結合部7に結合材8を充填し、推進翼1同士を翼
根受結合棚5を介して結合し、推進器の回転によ
つて推進翼1に発生する遠心力を翼根受結合棚5
を介して釣り合わせ、ボス壁3′、ボス尾部3″に
作用しないようにし、また推力によつて推進翼1
を力点とし、ボス3のP点又はP′点近傍を支点と
し、翼根受結合部7、翼根嵌合孔6を作用点とし
て発生するてこ作用の荷重は、翼根受結合棚5を
ボス尾部3′方向又は推進軸2方向に押すが、そ
の荷重を翼根受結合棚5を植立する推進軸2に逃
がし、ボス壁3′、ボス尾部3″に作用しなくした
ものであり、更に翼根受結合棚5を推進軸末端
2′に植立して、推進器の重心位置を推進軸2側
に移動し、推進器の首振運動の質量を小さくし、
推進軸系や船体への振動を少くしたものである。
As described above, in this invention, the inner periphery of the blade root fitting hole 6 of the blade root receiving coupling shelf 5 and the joint part 7 provided on the outer periphery of the blade root 4 are filled with a bonding material 8, and the propulsion blades 1 are connected to each other. The centrifugal force generated in the propulsion blade 1 due to the rotation of the propeller is transferred to the blade root support connection shelf 5.
to prevent the boss wall 3' and the boss tail 3'' from acting on the propeller blade 1.
is the point of force, the vicinity of point P or P' of the boss 3 is the fulcrum, and the lever action load generated with the blade root receiving joint 7 and the blade root fitting hole 6 as the application points is applied to the blade root receiving joint shelf 5. Although the load is pushed in the direction of the boss tail 3' or the propulsion shaft 2, the load is released to the propulsion shaft 2 on which the blade root receiver coupling shelf 5 is erected, so that it does not act on the boss wall 3' and the boss tail 3''. Furthermore, a blade root receiving coupling shelf 5 is installed at the end 2' of the propulsion shaft to move the center of gravity of the propulsion device toward the propulsion shaft 2 side, thereby reducing the mass of the swinging motion of the propulsion device.
This reduces vibrations to the propulsion shaft system and hull.

〔考案の効果〕[Effect of idea]

1 推進器ボス壁3′に作用する遠心力を、推進
翼1同士翼根受結合棚5を介して釣り合わせ、
ボス壁3′に作用させない構造としたことによ
つてボス壁3′の肉厚を削減することができ、
プロペラ効率が良くなつた。
1 Balance the centrifugal force acting on the propulsion boss wall 3' between the propulsion blades 1 via the blade root receiving shelf 5,
By adopting a structure that does not act on the boss wall 3', the thickness of the boss wall 3' can be reduced.
Improved propeller efficiency.

2 推力によつて推進翼1に発生し翼根受結合棚
5に作用するてこ作用の荷重を、推進軸2に逃
がしたことにより、ボス壁3′、ボス尾部3″の
肉厚を大量に削減することができ、ボス比が小
さくなり、プロペラ効率を飛躍的に向上させ
た。
2 By releasing the leverage load generated on the propulsion blade 1 due to thrust and acting on the blade root receiver coupling shelf 5 to the propulsion shaft 2, the wall thickness of the boss wall 3' and the boss tail 3'' can be increased by a large amount. This reduced the boss ratio and dramatically improved propeller efficiency.

3 翼根受結合棚5を推進軸末端2′に植立した
ことと、ボス尾部3″の肉厚を大量に削減した
ことによつて、推進器の重心が推進軸2側に移
動し、推進器の首振運動の質量が小さくなり、
軸系及び船体の振動が減少して、船尾管軸受の
磨損を少なくした。
3. The center of gravity of the propulsion device is moved to the propulsion shaft 2 side by installing the blade root receiver coupling shelf 5 at the end of the propulsion shaft 2' and by reducing the wall thickness of the boss tail 3'' by a large amount. The mass of the thruster's oscillating motion becomes smaller,
Vibration of the shaft system and hull is reduced, reducing wear and tear on the stern tube bearing.

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

図中第1図及び第2図はこの考案のボス機構の
側断面図及び正面竪断面図、第3図及び第4図は
一部分の変更例を示す正面竪断面図で、第5図及
び第6図は従来例の側断面図及び正面竪断面図で
ある。 なお図において、1……推進翼、2……推進
軸、2′……推進軸末端、3……可変ピツチプロ
ペラボス、3″……ボス尾部、4……翼根、5…
…翼根結合棚、6……翼根嵌合孔、7……結合
部、8,8′,8″……結合材である。
In the drawings, FIGS. 1 and 2 are side sectional views and front vertical sectional views of the boss mechanism of this invention, FIGS. 3 and 4 are front vertical sectional views showing examples of partial changes, and FIGS. FIG. 6 is a side sectional view and a front vertical sectional view of the conventional example. In the figure, 1...propulsion blade, 2...propulsion shaft, 2'...propulsion shaft end, 3...variable pitch propeller boss, 3''...boss tail, 4...blade root, 5...
...Blade root connecting shelf, 6...Blade root fitting hole, 7...Connecting portion, 8, 8', 8''...Binding material.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 可変ピツチプロペラボス3内の推進軸末端2′
にボス尾部3″側に向けて翼根受結合棚5を突出
植立し、この翼根結合棚5に翼根4を挿入する翼
根嵌合孔6を設け、この翼根嵌合孔6の内周と翼
根4の外周とに結合部7をそれぞれ設け、結合材
8で推進翼1が翼根4の円周方向には回転しうる
が半径方向には関係変位不能に結合してなる可変
ピツチプロペラボス機構。
Propulsion shaft end 2' in variable pitch propeller boss 3
A blade root receiving coupling shelf 5 is planted protrudingly toward the boss tail portion 3'' side, and a blade root fitting hole 6 into which the blade root 4 is inserted is provided in the blade root coupling shelf 5. A connecting portion 7 is provided on the inner periphery of the blade root 4 and the outer periphery of the blade root 4, respectively, and a connecting member 8 connects the propulsion blade 1 so that it can rotate in the circumferential direction of the blade root 4 but cannot be displaced in the radial direction. Variable pitch propeller boss mechanism.
JP3206981U 1981-03-07 1981-03-07 Expired JPS623357Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3206981U JPS623357Y2 (en) 1981-03-07 1981-03-07

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3206981U JPS623357Y2 (en) 1981-03-07 1981-03-07

Publications (2)

Publication Number Publication Date
JPS57144795U JPS57144795U (en) 1982-09-11
JPS623357Y2 true JPS623357Y2 (en) 1987-01-26

Family

ID=29829469

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3206981U Expired JPS623357Y2 (en) 1981-03-07 1981-03-07

Country Status (1)

Country Link
JP (1) JPS623357Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102554556B (en) * 2010-12-14 2013-12-04 上海船厂船舶有限公司 Machining method for eliminating wear of propeller hub and blades of adjustable propeller device

Also Published As

Publication number Publication date
JPS57144795U (en) 1982-09-11

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