JP3132950B2 - Stern bearing for contra-rotating propeller - Google Patents

Stern bearing for contra-rotating propeller

Info

Publication number
JP3132950B2
JP3132950B2 JP05185634A JP18563493A JP3132950B2 JP 3132950 B2 JP3132950 B2 JP 3132950B2 JP 05185634 A JP05185634 A JP 05185634A JP 18563493 A JP18563493 A JP 18563493A JP 3132950 B2 JP3132950 B2 JP 3132950B2
Authority
JP
Japan
Prior art keywords
bearing
inner shaft
shaft
propeller
diameter cylindrical
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 - Fee Related
Application number
JP05185634A
Other languages
Japanese (ja)
Other versions
JPH0710086A (en
Inventor
邦夫 佐木
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP05185634A priority Critical patent/JP3132950B2/en
Publication of JPH0710086A publication Critical patent/JPH0710086A/en
Application granted granted Critical
Publication of JP3132950B2 publication Critical patent/JP3132950B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/32Other parts
    • B63H23/321Bearings or seals specially adapted for propeller shafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/32Other parts
    • B63H23/321Bearings or seals specially adapted for propeller shafts
    • B63H2023/323Bearings for coaxial propeller shafts, e.g. for driving propellers of the counter-rotative type

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明は、二重反転プロペラー装
置に適用される船尾軸受に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a stern bearing applied to a contra-rotating propeller device.

【0002】[0002]

【従来の技術】船舶の二重反転プロペラー推進装置にお
いては、従来、図4に示すように、図示しないディーゼ
ル機関などの原動機にて反転装置を介して、先端に後部
プロペラー01を有する内軸02と、先端に前部プロペ
ラー03を有する中空外軸04とを同軸的に互いに逆回
転させて推進力を得るようにしている。これらの2つの
プロペラー軸を支持するために、外軸04と船体05
間に外軸支持軸受06,07が必要であるとともに、
内軸02と外軸04との間に内軸支持軸受08,09が
必要である。また、潤滑油の漏洩防止のために船尾シー
ル010,011を設ける。外軸支持軸受06,07
通常の船尾管軸受と作用が同一であり、特に、技術的困
難性はないが、内軸支持軸受08,09は、軸受と軸
が互いに反対方向に回転するので、通常船尾管軸受とは
作動が異なる。この場合、真円形状のすべり軸受では、
流体潤滑負荷能力が小さくなる。この点を解決する手段
として、特願昭60−250471号に示す構造が提案
されている。本発明はこの発明の改良に関するものであ
る。すなわち、図5において、内軸軸受09は前部プロ
ペラーボス03に一体的に嵌合されている。内軸02に
はその中心線上に給油孔012が設けられており、内軸
軸受09に向かい合う位置で複数本の放射状給油孔01
3と連通させ、各給油孔013はそれぞれオリフィス0
14を介して、高圧油を内軸軸受09の軸受面へ噴出さ
せ、静圧軸受作用を生じさせる構造となっている。内軸
軸受材09−1は、油潤滑軸受では、ホワイトメタルを
用いた金属軸受である。
2. Description of the Related Art Conventionally, in a contra-rotating propeller propulsion device for a ship, as shown in FIG. 4, an inner shaft 02 having a rear propeller 01 at a tip end via a reversing device by a motor such as a diesel engine (not shown). And a hollow outer shaft 04 having a front propeller 03 at the tip are coaxially rotated in opposite directions to obtain a propulsion force. To support these two propeller shafts, the outer shaft 04 and the hull 05
The outer shaft support bearings 06 and 07 are required between
It is required inner shaft support bearing 08, 09 between the inner shaft 02 and outer shaft 04. Also, stern seals 010 and 011 are provided to prevent leakage of lubricating oil. Outer shaft support bearing 06, 07 is the same action as the conventional stern tube bearing, particularly, though not technical difficulties, the inner shaft support bearing 08, 09, opposite <br/> the bearing and the shaft to each other Because it rotates in the direction, the operation is different from that of the normal stern tube bearing. In this case, with a perfect circular plain bearing,
Fluid lubrication load capacity decreases. As a means for solving this problem, a structure disclosed in Japanese Patent Application No. 60-250471 has been proposed. The present invention relates to an improvement of the present invention. That is, in FIG. 5, the inner shaft bearing 09 is integrally fitted to the front propeller boss 03. The inner shaft 02 is provided with a lubrication hole 012 on the center line thereof, and a plurality of radial lubrication holes 01 is provided at a position facing the inner shaft bearing 09.
3 and each oil supply hole 013 has an orifice 0
High pressure oil is ejected to the bearing surface of the inner shaft bearing 09 via the bearing 14 to generate a hydrostatic bearing effect. The inner shaft bearing material 99-1 is a metal bearing using white metal in an oil lubricated bearing.

【0003】[0003]

【発明が解決しようとする課題】しかしながら、この種
の軸受には下記のような問題がある。すなわち、内軸0
2は後部プロペラーの自重やプロペラーに作用する流体
力によって曲げ変形を生ずる。また、内軸軸受09を内
する前部プロペラーボス03も自重やプロペラーに作
用する流体力によって、曲げ変形を生ずる。この結果、
内軸軸受09において、内軸02は傾き、軸受負荷能力
は傾きのない場合に比べて、大幅に減少する。特に、二
重反転プロペラーにおいては、プロペラーに作用する流
体力が回転方向が異なるために、後部プロペラーと前部
プロペラーとでは逆方向になり、内軸軸受09に相対的
な内軸02の傾きは、一層拡大され、軸受と軸とが接触
し、焼付損傷を生じやすい。この損傷防止のために、内
軸02,外軸04の直径を大きくして曲がりを小さくす
ることや、給油孔12に供給する潤滑油の圧力を高く
しなければならない。これらに伴う欠点をまとめると次
のようになる。 (1)内,外軸径を大きくすることにより、シール径も
大きくなり、シールの信頼性が低下し、しかも高コスト
となる。 (2)高圧油を供給することにより、給油ポンプの消費
動力が大きくなる。給油箱に大きな耐圧性が要求され、
高コストとなる。 (3)高圧油の軸受面への噴出流速がくなり、ホワイ
トメタルのエロージョン摩耗が生じやすくなる。
However, this type of bearing has the following problems. That is, the inner axis 0
2 is bent by the weight of the rear propeller and the fluid force acting on the propeller. Also, the inner shaft bearing 09 is
The stored front propeller boss 03 also undergoes bending deformation due to its own weight and fluid force acting on the propeller. As a result,
In the inner shaft bearing 09, the inner shaft 02 is tilted, and the bearing load capacity is greatly reduced as compared with the case where there is no tilt. In particular, in the contra-rotating propeller, since the fluid force acting on the propeller has a different rotation direction, the rear propeller and the front propeller have opposite directions, and the inclination of the inner shaft 02 relative to the inner shaft bearing 09 is The bearing is further enlarged, and the bearing and the shaft come into contact with each other, which easily causes seizure damage. In order to prevent this damage, it is necessary to increase the diameter of the inner shaft 02 and the outer shaft 04 to reduce the bending, and to increase the pressure of the lubricating oil supplied to the oil supply hole 012 . The drawbacks associated with these are summarized as follows. (1) Increasing the diameter of the inner and outer shafts increases the diameter of the seal, lowers the reliability of the seal, and increases the cost. (2) Supplying high-pressure oil increases power consumption of the oil supply pump. Oil tanks are required to have great pressure resistance,
High cost. (3) release speed of the bearing surface of the high-pressure oil is quickly no longer, erosion wear of the white metal is likely to occur.

【0004】本発明はこのような事情に鑑みて提案され
たもので、内軸と外軸との相対的傾き、あるいは内軸と
前部プロペラーボスとの相対的傾きが大きくても内外軸
径を大きくすることなく、また潤滑油圧を高めることな
く、軸受負荷能力の低下を防止する経済的な二重反転プ
ロペラー用船尾軸受を提供することを課題とする。
[0004] The present invention has been proposed in view of such circumstances, and even if the relative inclination between the inner shaft and the outer shaft or the relative inclination between the inner shaft and the front propeller boss is large, the diameter of the inner and outer shafts is reduced. It is an object of the present invention to provide an economical contra-rotating propeller stern bearing that prevents a decrease in bearing load capacity without increasing the size and lubricating oil pressure.

【0005】[0005]

【課題を解決するための手段】上述の課題を解決するた
め、本発明の二重反転プロペラー用船尾軸受は、先端に
前部プロペラーを有する中空外軸の中心孔に先端に後部
プロペラーを有する内軸を内挿し、両軸を互いに反対方
向に同軸的に回動する二重反転プロペラーのための
であって、上記内軸をすべり軸受を介して上記外軸に軸
支し、上記内軸の中心孔を経て供給される高圧油を同内
の半径方向に放射状に穿設された複数の油孔を経て
すべり軸受に供給するようにしたものにおいて、外周
面が前部プロペラーボスの中心穴内面又は外軸後部付近
内面に嵌着された大径円筒状バックメタルと内周面に
内軸が内挿され外周面が上記バックメタルの内面に一
体的に嵌着されたゴム等高分子材料からなる小径円筒部
とで構成された2層構造の円筒体と、上記小径円筒部の
内部及び又は上記バックメタルとの界面上に円周方向
等間隔で形成された複数の互いに平行する軸方向貫通油
孔とを具えたことを特徴とする。
Means for Solving the Problems To solve the above problems,
Therefore, the stern bearing for the contra-rotating propeller of the present invention, the inner shaft having the rear propeller at the tip is inserted into the center hole of the hollow outer shaft having the front propeller at the tip, and both shafts are coaxially opposed to each other. a bearings <br/> for counter-rotating propeller to rotate, high pressure oil via a sliding bearing to the inner shaft rotatably supported in the outer shaft, it is fed through the center hole of the inner shaft Within
Up through multiple oil holes radially drilled in the radial direction of the shaft
In those is supplied to the serial sliding bearing, the outer peripheral surface on the center hole inner surface or is fitted to the outer shaft rear near the inner surface large diameter cylindrical back metal and the inner circumferential surface of the front propeller boss
A small-diameter cylindrical portion made of a polymer material such as rubber and having an inner shaft inserted therein and an outer peripheral surface integrally fitted to the inner surface of the back metal.
Internal and or axially parallel to one another formed by <br/> equal intervals in the circumferential direction on the interface between the back metal of the cylindrical body and said small-diameter cylindrical portion of the two-layer structure constituted by the And a through oil hole.

【0006】[0006]

【作用】このような構成によれば、前部プロペラーボ
相対的に内軸が傾いた場合、本発明軸受は、軸受面が
内軸に沿って変形し、軸受と内軸の相対的傾きが小さ
くなる作用が生ずる。軸受に相対的に内軸が傾いた場
合、軸方向の油膜厚さは一様でなく、一方の軸受端の油
膜厚さが薄くなる。油膜厚さが薄いところでは、軸受面
には大きな油圧が発生する。この発生油圧でゴムや高分
子の軸受面は低弾性率のために、圧縮変形を受け、軸と
軸受面の相対傾斜角は小さくなる。このため、軸方向に
広い範囲にわたって、大きな静圧分布が確保され、軸受
負荷能力の低下が、剛な金属軸受に比べて、小さくな
る。このようにして、片当たりによる焼付損傷が生じに
くくなる。
[Action] According to such a configuration, the front Puroperabo scan
When the inner shaft is relatively inclined, the bearing of the present invention has an effect that the bearing surface is deformed along the inner shaft, and the relative inclination between the bearing and the inner shaft is reduced. When the inner shaft is inclined relatively to the bearing, the oil film thickness in the axial direction is not uniform, and the oil film thickness at one bearing end is thin. Where the oil film thickness is small, a large oil pressure is generated on the bearing surface. Due to the generated hydraulic pressure, the rubber or polymer bearing surface is subjected to compressive deformation due to a low elastic modulus, and the relative inclination angle between the shaft and the bearing surface is reduced. For this reason, a large static pressure distribution is secured over a wide range in the axial direction, and a decrease in bearing load capacity is smaller than that of a rigid metal bearing. In this manner, seizure damage due to one-side contact is less likely to occur.

【0007】[0007]

【実施例】本発明の一実施例を図面について説明する
と、図1はその内軸軸受部を示す縦断面図、図2は図1
のII−II矢視横断面図、図3は図1において内軸が傾い
た場合の内軸軸受部の作用効果を示す説明図である。
DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described with reference to the drawings. FIG. 1 is a longitudinal sectional view showing an inner shaft bearing portion, and FIG.
3 is an explanatory view showing the operation and effect of the inner shaft bearing when the inner shaft is inclined in FIG.

【0008】図1〜3において、図4および図5の符号
から0を省略した符号は同図と同一の部材を示す。な
お、本発明が図4および図5の構造と大きく相違すると
ころは、内軸に接する部分の軸受部材の材質をホワイト
メタルの代わりにゴムで代表される高分子材料とすると
ともに、同高分子材料を容易に変形可能とし、かつヒス
テリシス変形に伴う同高分子材料内部の発熱を除去する
ために軸方向の貫通油孔を多数設けた点にある。
In FIGS. 1 to 3 , the reference numerals in FIG. 4 and FIG. 5 in which 0 is omitted indicate the same members as those in FIG. 4 and 5 is that the material of the bearing member in contact with the inner shaft is made of a polymer material represented by rubber instead of white metal. The point is that a large number of axial through-holes are provided in order to make the material easily deformable and to remove heat generated inside the polymer material due to hysteresis deformation.

【0009】すなわち、図1および図2に示すように、
内軸軸受9は二重構造となっており、バックメタル9−
3の内面に、ゴムあるいは高分子材からなる小径円筒部
9−2がモールド処理などで、固着されている。バック
メタル9−3と小径円筒部9−2は一体となり、プロ
ペラーボス3内に圧入等で固定されている。ゴム層ある
いは高分子層からなる小径円筒部9−2には、軸方向に
貫通する排油孔としての軸方向貫通油孔15が周方向に
等間隔で複数並設されている。同図では軸方向貫通油孔
15は、バックメタル9−3との界面に設けているが、
ゴム層あるいは高分子層としての小径円筒部9−2の
内部に設けられてもよい。排油をより円滑にするため
に、バックメタル9−3の外周面にも軸方向に貫通する
排油溝16が設けられている。なお、小径円筒部9−2
の表面(軸受面)には、水潤滑船尾管ゴム軸受で公知の
軸方向溝は設けず、同表面は円形の断面形状となってい
る。
That is, as shown in FIGS. 1 and 2,
The inner shaft bearing 9 has a double structure, and the back metal 9-
A small-diameter cylindrical portion 9-2 made of rubber or a polymer material is fixed to the inner surface of the third member 3 by molding or the like. Come together the back metal 9-3 and the small-diameter cylindrical portion 9-2, and is fixed by press-fitting or the like to the propeller boss 3. The small-diameter cylindrical portion 9-2 made of a rubber layer or a polymer layer is more juxtaposed axial through oil holes 15 at equal intervals in the circumferential direction of the oil discharge holes extending in the axial direction. Although the axial through- hole 15 is provided at the interface with the back metal 9-3 in FIG.
It may be provided in a layer <br/> inside the small-diameter cylindrical portion 9-2 of the rubber layer or a polymer layer. In order to make oil drainage smoother, an oil drainage groove 16 penetrating in the axial direction is also provided on the outer peripheral surface of the back metal 9-3. The small-diameter cylindrical portion 9-2
On the surface (bearing surface) of (1), a well-known axial groove of a water-lubricated stern tube rubber bearing is not provided, and the surface has a circular cross-sectional shape.

【0010】このような内軸軸受構造において、図3に
示すように、内軸2がプロペラーボス3に対して相対的
に傾いた場合、内軸2と内軸軸受9の小径円筒部9−2
は、片当たりを生じようとする。この片当たりを生じ
ようとする部分ではオリフィス14を出た潤滑油の圧力
が高くなる。この高圧油は、低弾性体であるゴム層ある
は高分子層としての小径円筒部9−2を圧縮変形させ、
図示B部のように変形し、片当たり接触を防止する。
その結果、内軸2とB部はほぼ平行となるので、この
部分では軸方向にほぼ一様な静圧が保持され、軸受の静
圧潤滑負荷能力は軸受の変形がほとんどない場合(図中
破線)に比べて、大幅に向上する。このため、片当たり
による焼付損傷の防止が可能になる。また軸方向貫通油
孔15を設けたことにより、以下の効果を奏する。
軸受から排出された潤滑油が軸方向貫通油孔15を通っ
て排油されるので、ゴム層などから成る小径円筒部9−
2の繰り返し変形に伴う発熱を除去し、同小径円筒部
−2の温度上昇を抑制するから、その劣化防止され
る。 軸方向貫通孔15があるために、ゴム層など
からなる小径円筒部9−2の圧縮変形が容易になり、片
当たり防止に有効である。 軸方向貫通孔15は、
円周方向等間隔で複数本設けられているので、変形後
の軸受面は、真円形状から偏差する。反転すべり軸受で
は、通常すべり軸受とは異なり、動圧流体潤滑負荷能力
が小さくなるが、これは、軸受面の形状が真円形状の場
合であり、真円形状から偏差すると、動圧流体潤滑負荷
能力が改善される方向となる。したがって、軸方向貫通
孔15によ、静圧流体潤滑作用に加えて、動圧流体
潤滑作用も発揮させることができる。
In such an inner shaft bearing structure, FIG.
As shown, the inner shaft 2 is relative to the propeller boss 3
When tilted to the inner shaft 2Small diameter cylindrical part of inner shaft bearing 99-2
WhenCaused a rammingTryingYou. This pieceProduce
Try toWhere the pressure of the lubricating oil exiting the orifice 14
Will be higher. This high-pressure oil has a rubber layer that is a low elastic body
Is the polymer layerSmall diameter cylindrical part as9-2 is compressed and deformed,
IllustratedofIt deforms like part B, preventing one-sided contact.
As a result, inner shaft 2 and part BWhenAre almost parallel, so this
In this part, almost uniform static pressure is maintained in the axial direction, and the static
The pressure lubrication load capacity is obtained when there is almost no deformation of the bearing (in the figure,
This is greatly improved as compared with (dashed line). Because of this,
Can prevent seizure damageNanaYou. Also axial penetrationOil passing
Hole 15By providingThe following effects are obtained.
Lubricating oil discharged from the bearingAxial penetrationThrough oil hole 15
So that the rubber layerSmall-diameter cylindrical part consisting of9-
Remove the heat generated by the repeated deformation of 2,Small diameter cylindrical part9
-2 to suppress the temperature rise, ThatDeteriorationButPreventionIs
You. Axial penetrationoilRubber layer due to holes 15Such
Small diameter cylindrical part9-2 can be easily compressed and deformed.
It is effective for hit prevention.Axial directionPenetratingoilHole 15 is
Circumferential directionToSince a plurality are provided at equal intervals, after deformation
Deviates from a perfect circular shape. With reversing plain bearings
Is different from a plain bearing in that it has a dynamic fluid lubrication load capacity
Is smaller when the shape of the bearing surface is a perfect circle.
If it deviates from a perfect circle, the dynamic fluid lubrication load
Ability to improve. Therefore,Axial directionPenetrating
oilBy hole 15R, In addition to hydrostatic lubrication, dynamic pressure fluid
A lubricating action can also be exerted.

【0011】[0011]

【発明の効果】このような構造の内軸軸受によれば、従
来の金属製軸受に比べ下記の効果が奏せられる。 (1) 片当たりに対する耐焼付性が大きくなる。 (2) 給油圧力を従来の軸受より下げることが可能で
ある。 (3) プロペラーフォースによる片当たりが顕著にな
る大出力の二重反転プロペラー用内軸軸受に特に好適で
ある。 (4) 本発明軸受は外軸後部付近内面に設けることも
できる。要するに本発明によれば、先端に前部プロペラ
ーを有する中空外軸の中心孔に先端に後部プロペラーを
有する内軸を内挿し、両軸を互いに反対方向に同軸的に
回動する二重反転プロペラーのためのであって、
内軸をすべり軸受を介して上記外軸に軸支し、上記
軸の中心孔を経て供給される高圧油を同内軸の半径方向
に放射状に穿設された複数の油孔を経て上記すべり軸受
に供給するようにしたものにおいて、外周面が前部プロ
ペラーボスの中心穴内面又は外軸後部付近内面に嵌着さ
れた大径円筒状バックメタルと内周面に上記内軸が内挿
され外周面が上記バックメタルの内面に一体的に嵌着さ
れたゴム等高分子材料からなる小径円筒部とで構成され
2層構造の円筒体と、上記小径円筒部の内部及び又は
上記バックメタルとの界面上に円周方向等間隔で形成
された複数の互いに平行する軸方向貫通油孔とを具えた
ことにより、内軸と外軸との相対的傾き、あるいは内軸
と前部プロペラーボスとの相対的傾きが大きくても内外
軸径を大きくすることなく、また潤滑油圧を高めること
なく、軸受負荷能力の低下を防止する経済的な二重反転
プロペラー用船尾軸受を得るから、本発明は産業上極め
て有益なものである。
According to the inner shaft bearing having such a structure, the following effects can be obtained as compared with the conventional metal bearing. (1) the magnitude seizure resistance against uneven contact Kunar. (2) It is possible to reduce the lubrication pressure compared to conventional bearings. (3) It is particularly suitable for a large output contra-rotating propeller inner shaft bearing in which one-sided contact due to the propeller force becomes remarkable. (4) The bearing of the present invention can be provided on the inner surface near the rear portion of the outer shaft. In short, according to the present invention, a contra-rotating propeller in which an inner shaft having a rear propeller at a tip is inserted into a center hole of a hollow outer shaft having a front propeller at a tip, and both shafts are coaxially rotated in opposite directions to each other. a bearings for the upper
Via the sliding bearing the serial inner shaft rotatably supported in the outer shaft, through a plurality of oil holes a high-pressure oil supplied through a central hole drilled radially in the radial direction of the inner shaft of the inner shaft in that then supplied to the sliding bearing, the outer peripheral surface of the inner shaft interpolation the center hole inner surface or is fitted to the outer shaft rear near the inner surface large diameter cylindrical back metal and the inner circumferential surface of the front propeller boss is the outer circumferential surface is composed of a small-diameter cylindrical portion made of rubber or the like polymeric material is integrally fitted to the inner surface of the back metal
And a cylindrical body having a two-layer structure, and the inside of the small-diameter cylindrical portion and / or
By equipped with the axial through oil holes parallel plurality of mutually formed at equal intervals in the circumferential direction on the interface between the back metal, the relative inclination between the inner shaft and the outer shaft or the inner shaft, and Even if the relative inclination with respect to the front propeller boss is large, an economical contra-rotating propeller stern bearing that prevents a decrease in bearing load capacity without increasing the inner and outer shaft diameters and without increasing the lubricating oil pressure is obtained. The present invention is extremely useful in industry.

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

【図1】本発明の一実施例を示す内軸軸受部の縦断面図
である。
FIG. 1 is a longitudinal sectional view of an inner shaft bearing portion showing one embodiment of the present invention.

【図2】図1のII−II矢視横断面図である。FIG. 2 is a cross-sectional view taken along the line II-II of FIG.

【図3】図1において内軸が傾いた場合の内軸軸受部の
作用,効果を示す説明図である。
FIG. 3 is an explanatory view showing the operation and effect of the inner shaft bearing when the inner shaft is inclined in FIG.

【図4】従来の二重反転プロペラー軸の軸受部を示す側
面図である。
FIG. 4 is a side view showing a bearing portion of a conventional contra-rotating propeller shaft.

【図5】図4の内軸軸受部を示す拡大図である。FIG. 5 is an enlarged view showing the inner shaft bearing of FIG.

【符号の説明】[Explanation of symbols]

1 後部プロペラー 2 内軸 3 前部プロペラー(前部プロペラーボス) 4 外軸 5 船体 6,7 外軸支持軸受 8 内軸前部軸受 9 内軸後部軸受 9−1 ホワイトメタル 9−2 ゴムあるいは高分子層からなる小径円筒部 9−3 バックメタル 10,11 船尾シール 12 内軸給油孔 13 放射状給油孔 14 オリフィス 15 軸方向貫通油孔 16 排油溝Reference Signs List 1 rear propeller 2 inner shaft 3 front propeller (front propeller boss) 4 outer shaft 5 hull 6,7 outer shaft support bearing 8 inner shaft front bearing 9 inner shaft rear bearing 9-1 white metal 9-2 rubber or polymer Small-diameter cylindrical portion 9-3 composed of layers Back metal 10, 11 Stern seal 12 Inner shaft oil supply hole 13 Radial oil supply hole 14 Orifice 15 Axial through oil hole 16 Oil drain groove

フロントページの続き (56)参考文献 特開 昭62−110595(JP,A) 特開 平5−126138(JP,A) 実開 平3−85722(JP,U) 実開 昭62−36900(JP,U) 実開 昭57−12824(JP,U) 特公 昭48−18965(JP,B1) 特公 昭48−18403(JP,B1) (58)調査した分野(Int.Cl.7,DB名) B63H 23/36 B63H 5/10 F16C 17/00 Continuation of front page (56) References JP-A-62-110595 (JP, A) JP-A-5-126138 (JP, A) JP-A-3-85722 (JP, U) JP-A-62-36900 (JP, A) , U) Shokai Sho 57-12824 (JP, U) JP-B 48-18965 (JP, B1) JP-B 48-18403 (JP, B1) (58) Fields surveyed (Int. Cl. 7 , DB Name) B63H 23/36 B63H 5/10 F16C 17/00

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 先端に前部プロペラーを有する中空外軸
の中心孔に先端に後部プロペラーを有する内軸を内挿
し、両軸を互いに反対方向に同軸的に回動する二重反転
プロペラーのためのであって、上記内軸をすべり軸
受を介して上記外軸に軸支し、上記内軸の中心孔を経て
供給される高圧油を同内軸の半径方向に放射状に穿設さ
れた複数の油孔を経て上記すべり軸受に供給するように
したものにおいて、外周面が前部プロペラーボスの中心
穴内面又は外軸後部付近内面に嵌着された大径円筒状バ
ックメタルと内周面に上記内軸が内挿され外周面が上記
バックメタルの内面に一体的に嵌着されたゴム等高分子
材料からなる小径円筒部とで構成された2層構造の円筒
体と、上記小径円筒部の内部及び又は上記バックメタル
との界面上に円周方向等間隔で形成された複数の互い
に平行する軸方向貫通油孔とを具えたことを特徴とする
二重反転プロペラー用船尾軸受。
1. A interpolates inner shaft having a rear propeller at the tip in the central hole of the hollow outer shaft having a front propeller on the tip, for counter-rotating propeller which coaxially rotate both axes in opposite directions a of bearings, via a sliding bearing to the inner shaft rotatably supported in the outer shaft, is drilled radially in the radial direction of the inner shaft high-pressure oil supplied through the center hole of the inner shaft The bearing is supplied to the above-mentioned plain bearing through a plurality of oil holes.
Rubber height outer circumferential surface the inner shaft is inserted into the large-diameter cylindrical back metal and the inner circumferential surface is integrally fitted to the inner surface of the back metal which is fitted into the hole inner surface or the outer shaft rear near the inner surface and the cylindrical body of the two-layer structure constituted by a small-diameter cylindrical portion formed of a molecular material, a plurality of parallel formed at equal intervals in the circumferential direction on the interface between the inner and or the back metal of the small-diameter cylindrical portion A stern bearing for a contra-rotating propeller, comprising:
JP05185634A 1993-06-29 1993-06-29 Stern bearing for contra-rotating propeller Expired - Fee Related JP3132950B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP05185634A JP3132950B2 (en) 1993-06-29 1993-06-29 Stern bearing for contra-rotating propeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP05185634A JP3132950B2 (en) 1993-06-29 1993-06-29 Stern bearing for contra-rotating propeller

Publications (2)

Publication Number Publication Date
JPH0710086A JPH0710086A (en) 1995-01-13
JP3132950B2 true JP3132950B2 (en) 2001-02-05

Family

ID=16174209

Family Applications (1)

Application Number Title Priority Date Filing Date
JP05185634A Expired - Fee Related JP3132950B2 (en) 1993-06-29 1993-06-29 Stern bearing for contra-rotating propeller

Country Status (1)

Country Link
JP (1) JP3132950B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110566579B (en) * 2019-08-20 2020-07-14 中国石油大学(华东) Ship stern bearing suitable for all-condition propulsion system and propulsion system thereof

Also Published As

Publication number Publication date
JPH0710086A (en) 1995-01-13

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