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JP3962664B2 - Stern tube bearing and manufacturing method thereof - Google Patents
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JP3962664B2 - Stern tube bearing and manufacturing method thereof - Google Patents

Stern tube bearing and manufacturing method thereof Download PDF

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JP3962664B2
JP3962664B2 JP2002259196A JP2002259196A JP3962664B2 JP 3962664 B2 JP3962664 B2 JP 3962664B2 JP 2002259196 A JP2002259196 A JP 2002259196A JP 2002259196 A JP2002259196 A JP 2002259196A JP 3962664 B2 JP3962664 B2 JP 3962664B2
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Prior art keywords
bearing
stern
oil supply
stern tube
curvature
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JP2004098719A (en
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武朗 牧野
智裕 立石
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Mitsubishi Heavy Industries Ltd
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Mitsubishi Heavy Industries Ltd
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Description

【0001】
【発明の属する技術分野】
本発明は、船舶の、軸受内面に給油溝と給油孔とを備えたプロペラ軸受に用いられ、テーパーボーリング加工、又はスロープボーリング加工を施された船尾管軸受、或いは静圧ポケットを備えた船尾管軸受及びその製造方法に関する。
【0002】
【従来の技術】
船尾管軸受が使用される船舶の船尾構造を図5に示す。船体6の船尾に船尾管軸受1が設置され、プロペラ軸2が該船尾管軸受1と船体船尾部を貫通している。該船体船尾部は船尾管シール装置3によって封止され、船内への海水の流入と軸受で使用する潤滑油の海中への流出とを防止している。該プロペラ軸2の船尾側端部にプロペラ4が装着される。該プロペラ4より船尾側に舵5が、船体6に設置される。
以上のような船尾構造においては、プロペラ4の重量が大きい場合、プロペラ4の自重によってプロペラ軸2が撓み、該プロペラ軸2は船尾管軸受1の船尾側で片当たりし易かった。また、船舶の旋回時には、舵5と船体6の形状の相互作用によりプロペラ4に流入する海水の流れに偏流が生じてプロペラ4を水平方向へ移動させる大きな力が働き、プロペラ軸2が船尾管軸受1の船尾側で片当たりし易かった。そこで、従来は、これら重力方向、水平方向又はそれらの合成方向への片当たりを緩和するために、船尾管軸受の船尾側の内面形状を工夫していた。その例について次に述べる。
【0003】
図6は、テーパー軸受面9が船尾側に向かって広がるように、船首側の軸受面16の途中からテーパー状に軸受内面を加工した船尾管軸受である。(a)が軸心線に沿う断面図、(b)がCから見た側面図である。前記加工をテーパーボーリングという。該テーパーボーリングは前記船尾管軸受1の船尾側の軸方向L´の範囲に、且つ全周に施されている。Rは軸受面の曲率半径であり、Rはテーパー軸受面の曲率半径であり、それらの曲率中心はCで一致している。前記テーパーボーリング加工を施すことによって、船尾側に向かうにつれて撓んでいくプロペラ軸2の傾斜に対応してテーパー軸受面9の径が大きくなっていくので、プロペラ軸2の外周面とテーパー軸受面9の隙間を船尾側に向かって確保できる。その結果、船尾側での片当たりを緩和できる。
【0004】
図7は、軸受内面と同じ曲率半径Rで、船首側の軸受面16の途中からスロープ状に内面を加工した船尾管軸受である。(a)が軸心線に沿う断面図、(b)がDから見た側面図である。前記加工をスロープボーリングという。該スロープボーリングは前記船尾管軸受1の船尾側の軸方向L´の範囲に、且つ下半面に施されている。εは、該船尾管軸受1の船尾側端部における軸受面16の曲率中心Cとスロープ軸受面10の曲率中心Cとの距離である。
前記スロープボーリング加工を施すことによって、特に、重量の大きなプロペラ4を装着した場合に、船尾側に向かうにつれて撓んでいくプロペラ軸2の傾斜に対応して、軸受の軸中心線からスロープ軸受面10までの距離を船尾側に向かって大きく取れるので、プロペラ軸2の外周面とスロープ軸受面10の隙間を船尾側に向かって確保できる。その結果、船尾側での片当たりを緩和できる。
【0005】
図8は、油圧でプロペラ軸2を支持する静圧ポケット11を軸受内面に設けた船尾管軸受である。(a)が縦断面図、(b)がEから見た側面図である。
静圧ポケット11には、船尾管軸受1の外周面に連通する高圧給油管12が接続され、該外周面からは高圧配管13が接続され、コントロールバルブ14を介してポンプ15が接続されている。ポンプ15から静圧ポケット11に油圧を印加し、該静圧ポケット11内部の潤滑油を軸受面に供給することによってプロペラ軸荷重を支え、プロペラ軸2の片当たりを緩和する。
以上の図6ないし図8の何れかに示した船尾管軸受においては、軸受内側の両側面には軸方向に給油溝7が設けられ、各給油溝には複数の給油孔8が穿孔されている。船舶運航時には、該給油孔8から該給油溝7へ潤滑油が供給される。該潤滑油は、給油溝7に沿って軸方向に広がると共に、プロペラ軸と軸受内面の隙間に入り込みプロペラ軸の回転に伴って軸受内面全周に広がり、プロペラ軸と軸受内面との潤滑機能を果たす。その結果、プロペラ軸又は軸受内面の熱的損傷を防止している。
【0006】
油圧を利用する軸受装置は、特許文献1(特開平8−091292号公報)に開示されている。かかる公報においては、軸受の内面全周に渡って複数の給油孔を設け、プロペラ軸の低回転域において静圧を印加し、軸受負荷容量を確保している。
また、特許文献2(特開平6−321185号公報)には、二重反転プロペラ軸受構造において、プロペラ内軸を支持する軸受の内部に多数のオイル供給管路を設け、該管路の口が軸受内面全周に渡って開口している軸受装置が開示されている。該軸受自体もプロペラ内軸とは反対方向に回転している。このとき、回転している該軸受内部の該オイル供給管路が軸受装置の下面に来たときにオイルが供給されるように、オイル供給系を構成し、プロペラ軸荷重の大きい重力方向の軸受面の潤滑を確実にしている。
プロペラ軸の軸受については、非特許文献1(「1級舶用機関整備士指導書」(日本財団事業成果ライブラリー、日本舶用機関整備協会、平成8年度))に詳しく述べられている。
【0007】
【特許文献1】
特開平8−091292号公報
【特許文献2】
特開平6−321185号公報
【非特許文献1】
1級舶用機関整備士指導書(日本財団事業成果ライブラリー、日本舶用機関整備協会、平成8年度)
【0008】
【発明が解決しようとする課題】
以上に示した従来技術に係わる船尾管軸受においては、次のような問題点がある。通常、船尾管軸受の設計は、プロペラ軸とプロペラとを据え付ける時の静的な状態を想定して行われる。従って、プロペラ軸とプロペラとの重量に起因する船尾管軸受へのプロペラ軸の片当たりについては、軸受すきまの設定や該軸受の船体に対する設置角度などで対応することができる。しかし、船舶運航時の旋回に伴って流体力が発生する場合には、片当たりする方向が運転状態によって変化するので、設計時の軸受の設置角度の調整などでは対応困難である。特に、高速で回転するプロペラを備えた船舶の場合、プロペラが受ける荷重は、重力方向よりも流体力に起因する水平方向の方が大きくなる。従って、プロペラ軸の撓みは水平方向に大きくなるので、より船尾側でプロペラ軸荷重を支持する必要が生じる。
【0009】
以上の条件に対して、特許文献1及び特許文献2に示す軸受装置の場合、もしくは図6に示すテーパーボーリング加工を施す場合、船舶旋回時の流体力に対応してテーパー角度を最適化すると、該角度は船舶直進時のプロペラ軸とプロペラとの自重による片当たりに対応するよりも過剰となる。従って、軸受の船尾側端部よりも内部に油膜厚さが薄い部分ができ、軸受の潤滑が不十分となり、軸受又はプロペラ軸が熱的損傷を受ける場合がある。また、特許文献1及び特許文献2に示す軸受装置の場合、図7に示すスロープボーリング加工を施す場合、及び図8に示す静圧ポケットを設ける場合、プロペラ軸とプロペラとの重力方向荷重に対しては有効であるが、船舶旋回時の流体力に起因する水平方向荷重に対応できない。
【0010】
本発明は、かかる従来技術の欠点に鑑み、船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と給油孔とを設けた船尾管軸受において、プロペラ軸とプロペラとの重力方向荷重と船舶旋回時の流体力に起因する水平方向荷重との両荷重に同時に対応することによって、軸受又はプロペラ軸の熱的損傷の発生を防止でき、これによって船尾管軸受のメンテナンス作業頻度や作業コストの低減を図った船尾管軸受を、更にはコンパクトな船尾管軸受の提供を目的とする。
【0011】
【課題を解決するための手段】
本発明は係る課題を解決するため、請求項1記載の発明として、
船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受において、軸受の船尾側に、船首側の軸受面の途中から末広がりテーパー状に軸受内面を加工したテーパーボーリングによって形成された軸受面を有し、該テーパーボーリングの曲率中心位置C を前記船尾管軸受の軸中心位置C から上方へ外して設定したことを特徴とする船尾管軸受を提案する。
請求項1記載の発明によれば、船舶旋回時に水平方向荷重が負荷された場合、前記軸受の軸受面に対して、プロペラ軸荷重が軸方向に均等に負荷されるので、潤滑油膜圧力を軸受面に均等に分散させることができる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0012】
請求項2記載の発明は、請求項1記載の発明において、軸受内面の軸受すきま母線18とテーパーボーリングによって形成された軸受面の軸受すきま母線18とを一致させたことを特徴とする船尾管軸受を提案する。
請求項2記載の発明によれば、請求項1に加えて、船舶静止時若しくは直進時の重力方向の荷重に対しては、前記軸受を船体に傾斜させて据え付けることと軸受すきまの設定とで対応でき、船舶旋回時に水平方向荷重が負荷された場合には、前記軸受のテーパーボーリングされた軸受面に対して、プロペラ軸荷重が軸方向に均等に負荷されるので、潤滑油膜圧力を軸受面に均等に分散させることができる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0013】
請求項3記載の発明は、船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受において、該軸受の船尾側に、スロープボーリングによって形成された軸受面を設け、
更に前記スロープボーリングによって形成された軸受面の曲率半径を軸受内面の曲率半径と同一とするとともに、該スロープボーリングによって形成された軸受面の曲率中心を該軸受の軸中心から外して2箇所に設けたことを特徴とする船尾管軸受を提案する。
請求項3記載の発明によれば、請求項1に加えて、船舶静止時若しくは直進時の重力方向の荷重に対しては、前記軸受を船体に傾斜させて据え付けることと軸受すきまの設定とで対応でき、船舶旋回時に水平方向荷重が負荷された場合には、前記軸受のスロープボーリングされた軸受面に対して、プロペラ軸荷重が軸方向に均等に負荷されるので、潤滑油膜圧力を軸受面に均等に分散させることができる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0014】
請求項ないしの何れかに記載の発明は、請求項1ないし3の何れかに記載の船尾管軸受の製造方法に係るものである。
請求項に記載の発明は、船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受の製造方法において、ボーリング加工の曲率中心位置該軸受の曲率中心位置から外した位置に固定して、該加工の曲率半径を、前記軸受の船尾側端部では該軸受の曲率半径より大きく設定するとともに、船首側に向かうに従って前記軸受の曲率半径に一致するまで小さくなるように設定し、ボーリング加工工具を軸方向に送ることによってテーパーボーリング加工を施ことを特徴とする船尾管軸受の製造方法を提案する。
請求項に記載の発明は、船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受の製造方法において、ボーリング加工の曲率半径該軸受の曲率半径と同一として、該加工の曲率中心位置を、前記軸受の船尾側端部では軸中心から外して設定するとともに、船首側に向かうに従って前記軸受の軸中心位置に一致するまで径方向に移動させるように設定し、ボーリング加工工具を軸方向に送ることによってスロープボーリング加工を施ことを特徴とする船尾管軸受の製造方法を提案する。
【0015】
請求項ないしの何れかに記載の発明によれば、船舶静止時若しくは直進時の重力方向の荷重に、及び船舶旋回時の水平方向荷重に起因するプロペラ軸の片当たりが予想される方向の軸受内面をテーパーボーリング加工できるので、前記重力方向荷重及び前記水平方向荷重が前記プロペラ軸に負荷された場合でも、該プロペラ軸荷重が前記軸受の軸方向に均等に負荷されるので、潤滑油膜圧力を軸受面に均等に分散させることができる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0016】
請求項4記載の発明として、船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受において、該軸受の船尾側内面に複数の静圧ポケットを設け、更に前記静圧ポケットを側面及び下面に設けるとともに、側面に設ける静圧ポケットの位置を下面に設ける静圧ポケットの位置よりも船尾側に配置したことを特徴とする船尾管軸受を提案する。
請求項4記載の発明によれば、船舶静止時若しくは直進時の重力方向の荷重に対して、及び船舶旋回時の水平方向荷重に対して、前記軸受に設けた静圧ポケットに印加する油圧によってプロペラ軸を支持できるので、プロペラ軸の片当たりを防止できる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0017】
又本発明によれば、船舶静止時若しくは直進時の重力方向の荷重に対しては下面に設けた静圧ポケットに印加する油圧によって、また、船舶旋回時の水平方向荷重に対しては側面に設けた静圧ポケットに印加する油圧によってプロペラ軸を支持できるので、プロペラ軸の片当たりを防止できる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0018】
更に本発明によれば、前記効果に加えて、特に、船舶旋回時の水平方向荷重が船舶静止時若しくは直進時の重力方向の荷重よりも大きい場合に、船舶旋回時の水平方向荷重に対してはより船尾側に設けた静圧ポケットに印加する油圧によってプロペラ軸を支持できるので、プロペラ軸の片当たりを防止できる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0019】
請求項ないしに記載の発明は、請求項1ないし3の何れかの項に記載の発明において、船尾管軸受の船尾側内面に静圧ポケットを設けたことを特徴とする船尾管軸受を提案する。
請求項において、該軸受の下面から船尾側の側面に向けて静圧ポケットを設けたことを特徴とする。また、好ましくは請求項のように、側面の静圧ポケットの設置位置を下面の静圧ポケットの設置位置よりも船尾側に配置するのがよい。
請求項ないしに記載の発明によれば、請求項1ないし3の何れかの項に加えて、前記軸受に設けた静圧ポケットに油圧を印加することによってプロペラ軸を支持できるので、該軸受をコンパクトに設計できる。その結果、船尾管軸受の製造コストの低減、該軸受の設置スペースの節約、メンテナンス作業コストの低減を実現できる。
【0020】
【発明の実施形態】
以下、本発明を図に示した実施例を用いて詳細に説明する。但し、この実施例に記載されている構成部品の寸法、材質、形状、その相対位置などは、特定的な記載が特にない限り、この発明の範囲をそれのみに限定する趣旨ではなく、単なる説明例にすぎない。
【0021】
(実施形態1)
図1(a)は本願発明の実施形態1に係る船尾管軸受の構成を示す説明図であり、(a)は軸心線に沿う断面図、(b)はAから見た側面図である。
図1(a)において、円筒状の船尾管軸受1の船尾側端部にはフランジ17が加工されており、該船尾管軸受1を前記船尾管シール装置3又は船体6(図5参照)へ固定するために利用される。軸受面16内の対向する両側面に給油溝7が加工され、該給油溝7へは複数の給油孔8が、前記船尾管軸受1の外周面と連通するように穿孔されている。該給油孔8へは給油管(不図示)が接続され、プロペラ軸2と前記軸受面16との潤滑を図る潤滑油が供給される。
【0022】
図1の各記号はそれぞれ以下を示す。Lは船尾管軸受1の軸方向の全長を、Rは軸受面16の曲率半径を、Rは船尾側端部におけるテーパーボーリングの曲率半径を、L´はテーパーボーリングを施工する軸方向長さを示す。ここで、R>Rである。また、実線で示したプロペラ軸2は、船舶航行時に重力と船舶旋回時の水平方向荷重とによって、該プロペラ軸中心がCeから外れた様子を示している。一点鎖線で示すプロペラ軸2は、該プロペラ軸2を前期船尾管軸受1に取付ける時の初期位置を、つまり、該プロペラ軸中心位置と該船尾管軸受1の軸中心位置Ceとが一致している様子を示す。
【0023】
本実施形態では、テーパーボーリングの曲率中心位置Cを船尾管軸受1の軸中心位置Cから上方へ外して設定した。上方へ外す距離は、該船尾管軸受1の船尾側端部において、軸受面16の軸受すきま母線18とテーパー軸受面9の軸受すきま母線18とが一致する距離とした。このようなテーパーボーリング加工を施すことによって、該船尾管軸受1の船尾側下面の軸受面の曲率半径はRであり、下面から両側面へ向かうにつれて、その曲率半径がRまで徐々に大きくなるテーパー軸受面9を構成する。但し、テーパーボーリングを施工する箇所は、両側面の給油溝7までとし、上部半面には施工しないので、上部半面の軸受面の曲率半径はRである。
以上のように、船舶静止時若しくは直進時の、プロペラ軸2とプロペラ4との重力方向の荷重に対しては、船尾管軸受1を船体に傾斜させて据え付けることと軸受すきまの設定とで対応でき、船舶旋回時に水平方向荷重が負荷された場合には、前記軸受のテーパーボーリングされた軸受面に対して、プロペラ軸荷重が軸方向に均等に負荷されるので、潤滑油膜圧力を軸受面に均等に分散させることができる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0024】
以下に、テーパーボーリング加工法について示す。船尾管軸受1には、軸受面16、給油溝7及び給油孔8を予め加工しておく。次に、該軸受1を、大型回転テーブル上に、該軸受1の軸心線が該テーブル面と垂直方向になるように、かつ、該軸受1の軸中心Cと該テーブルの回転中心とが一致するように設置する。この時、該軸受の船首側端面が該テーブル面に接するように設置する。次に、該軸受1の船尾側端部に保持した加工工具を軸受内面に当て、大型回転テーブルを回転させることによって、軸受内面を切削し、テーパーボーリング加工を進める。
ここで、テーパーボーリング曲率中心位置Cは、前記テーブルの回転中心位置とずらして設定する。切削距離は、予め設計したテーパーボーリング曲率半径とテーパー角度に則り決める。テーパー角度は、軸受面16とテーパー軸受面9とがなす角度である。該角度とテーパーボーリング曲率半径とによって、テーパーボーリングを施工する軸方向長さL´が決まる。
ここで、船尾管軸受の半面にテーパーボーリングを施工する場合、例えば、図1(b)に示すように、該軸受の下半面に施工する場合は、切削の開始位置を一方の給油溝7とし、終了位置を反対側の給油溝7とする。切削の開始位置と終了位置を給油溝7とすることで、加工工具の当てと逃げとの空間を確保できる。
【0025】
(実施形態2)
図2は本願発明の実施形態2に係る船尾管軸受の構成を示す説明図であり、船尾管軸受を船尾側端部から見た図を示している。
円筒状の船尾管軸受1にフランジ17、給油溝7及び給油孔8が加工されているのは実施形態1と同様である。
図2の各記号はそれぞれ以下を示す。図1と同じ記号は同じものを示す。Rは軸受面16とスロープボーリングとの曲率半径を、Cはスロープボーリングの曲率中心位置を、εは該Cと船尾管軸受1の軸中心Cとの距離を示す。
【0026】
本実施形態では、前記船尾管軸受1に施工するスロープボーリングの曲率中心位置Cを、船尾管軸受1の軸中心Cから左右側面側下方に2箇所に外して設定した。このように加工することによって、該船尾管軸受1の船尾側端部の軸受面の曲率半径はRであるが、下面から両側面へ向かうにつれて、軸中心Cから軸受面までの距離は最大R+εに長くなり、スロープ軸受面10を構成する。但し、スロープボーリングを施工する箇所は、両側面の給油溝7までとし、上部半面には施工しないので、上部半面の軸受面の曲率半径はRである。
以上のように、船舶静止時若しくは直進時の、プロペラ軸2とプロペラ4との重力方向の荷重に対しては、船尾管軸受1を船体に傾斜させて据え付けることと軸受すきまの設定とで対応でき、船舶旋回時に水平方向荷重が負荷された場合には、該軸受のスロープボーリングされた軸受面に対して、プロペラ軸荷重が軸方向に均等に負荷されるので、潤滑油膜圧力を軸受面に均等に分散させることができる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0027】
以下に、スロープボーリング加工法について示す。船尾管軸受1には、軸受面16、給油溝7及び給油孔8を予め加工しておく。次に、該軸受1を、大型回転テーブル上に、該軸受1の軸心線が該テーブル面と垂直方向になるように、かつ、該軸受1の軸中心Cと該テーブルの回転中心とが一致するように設置する。この時、該軸受1の船首側端面が該テーブル面に接するように設置する。次に、前記大型回転テーブルを切削方向に対して傾斜させる。前記軸受1の船尾側端部に保持した加工工具を軸受内面に当て、前記大型回転テーブルを回転させることによって、軸受内面を切削し、スロープボーリング加工を進める。
ここで、スロープボーリング曲率半径Rは、前記軸受1の軸受面16の曲率半径Rと同じとする。前記大型回転テーブルを切削方向に対して傾斜させる角度は、図2に示すように、前記軸受1の船尾側端部において、スロープ軸受面10の曲率中心Cを軸中心Cからずらした距離εと、予め設計したスロープ軸受面10の軸方向距離とから決める。
【0028】
(実施形態3)
図3は本願発明の実施形態3に係る船尾管軸受の構成を示す説明図であり、船尾管軸受の軸心線に沿う断面図である。
円筒状の船尾管軸受1にフランジ17、給油溝7及び給油孔8が加工されているのは実施形態1と同様である。
本実施形態では、前記船尾管軸受1の船尾側の軸受面16に静圧ポケット11を設け、そこに該船尾管軸受1の外周面と連通する高圧給油管12を穿孔し、更に、高圧配管13とコントロールバルブ14とを介してポンプ15に配管接続した。ここで、静圧ポケット11は軸受面16において略長矩形の開口を有し、船尾管軸受1の下面から、より船尾側の両側面に向けて施工される。船舶運行時には、ポンプ15を用いて静圧ポケット11に潤滑油を加圧し、プロペラ軸2荷重を支える。加圧の程度は、該荷重の増減に対応してコントロールバルブ14の開度によって調整する。
【0029】
静圧ポケット11を軸受下面から、より船尾側の両側面に設けたので、船舶静止時若しくは直進時のプロペラ軸2とプロペラ4との重力方向の荷重に対して、及び船舶旋回の水平方向荷重に対して、静圧ポケットに印加する潤滑油の油圧を調整することによってプロペラ軸を支持できるので、プロペラ軸の片当たりを防止できる。特に、高速回転するプロペラ4を利用する場合には、水平方向荷重が負荷された時の片当たりの大きさが重力方向の荷重が負荷された時よりも大きくなり易い。つまり、プロペラ軸2は水平方向により大きく撓むので、油膜の最大圧力が船尾寄りの側面で必要になる。そこで、静圧ポケット11を側面に近づくほど船尾側に設けることにより、プロペラ軸2の撓みに対する復元力を大きくすることができる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0030】
(実施形態4)
図4は本願発明の実施形態4に係る船尾管軸受の構成を示す説明図であり、(a)は船尾管軸受の軸心線に沿う断面図、(b)はBから見た側面図である。
円筒状の船尾管軸受1にフランジ17、給油溝7及び給油孔8が加工されているのは実施形態1と同様である。
本実施形態では、前記船尾管軸受1の船尾側の下面に下面静圧ポケット11aを、より船尾側の両側面に側面静圧ポケット11bを設け、それぞれの静圧ポケットに該船尾管軸受1の外周面と連通する高圧給油管12を穿孔し、更に、高圧配管13とコントロールバルブ14とを介してポンプ15に配管接続した。ここで、静圧ポケット11aと11bとは、軸受面16において船尾管軸受1の周方向に長辺をもつ略矩形の開口を有する。
【0031】
このように構成することによって、ポンプ15によって潤滑油を静圧ポケット11aと11bとに加圧し、重力方向の荷重に対しては主に下面静圧ポケット11aに印加する油圧で、水平方向の荷重に対しては主に側面静圧ポケット11bに印加する油圧でプロペラ軸2を支える。加圧の程度は、各荷重の増減に対応して各々のコントロールバルブ14の開度によって調整する。
静圧ポケット11aと11bとを、軸受下面とより船尾側の両側面とに独立させて設けたので、船舶静止時若しくは直進時のプロペラ軸2とプロペラ4との重力方向の荷重に対しては軸受下面に設けた静圧ポケット11aに印加する潤滑油の油圧を、又、船舶旋回時の水平方向荷重に対しては両側面に設けた静圧ポケット11bに印加する潤滑油の油圧を調整することによってプロペラ軸を支持できるので、プロペラ軸の片当たりを防止できる。
【0032】
特に、高速回転するプロペラ4を利用する場合には、水平方向荷重が負荷された時の片当たりの大きさが重力方向の荷重が負荷された時よりも大きくなり易い。つまり、プロペラ軸2は重力方向よりも水平方向により大きく撓むので、油膜の最大圧力が船尾寄りの側面で必要になる。そこで、静圧ポケット11を側面に近づくほど船尾側に設けることにより、プロペラ軸2の撓みに対する復元力を大きくすることができる。
更に、船舶運行時に想定される軸荷重に適して、静圧ポケットの位置、個数、開口寸法、深さ等を設計すれば、コンパクトな船尾管軸受を製造できる。テーパーボーリング、スロープボーリング、及び周方向に角度を持った静圧ポケットのように、その作用を機能させるためにある程度の構造的な大きさを必要としないからである。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。更に、コンパクトな船尾管軸受を製造できるので、該軸受の製造コストの低減、該軸受の設置スペースの節約、メンテナンス作業コストの低減を実現できる。
【0033】
(実施形態5)
図示を省略した本発明の実施形態5は、実施形態1と実施形態3或いは実施形態4とを組み合わせた構造とする。または、実施形態2と実施形態3或いは実施形態4とを組み合わせた構造とする。
実施形態1に述べたテーパーボーリング、又は実施形態2に述べたスロープボーリングの施工に加えて、静圧ポケット11を設け、静圧ポケット11に印加する潤滑油の油圧を調整するので、船尾管軸受1が対応できる軸荷重の大きさの範囲が広がる。従って、同じ大きさの船尾管軸受1ならば対応できる軸荷重が大きくなる、同じ軸荷重ならば該軸受をコンパクトに構成できる。その結果、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。更に、コンパクトな船尾管軸受を製造できるので、該軸受の製造コストの低減、該軸受の設置スペースの節約、メンテナンス作業コストの低減を実現できる。
【0034】
【発明の効果】
以上記載の如く、請求項1ないし3及び請求項ないしの発明によれば、船尾管軸受の船尾側にテーパーボーリング及びスロープボーリングの何れか一方または双方を施し、それらの曲率中心を該軸受の軸中心から外して設定したので、船舶旋回時に水平方向荷重が負荷された場合、該軸受の軸受面に対して、プロペラ軸荷重が軸方向に均等に負荷され、潤滑油膜圧力を軸受面に均等に分散させることができる。これにより、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減に寄与する。
【0035】
また、請求項4の発明によれば、船尾管軸受の船尾側内面の下面から、より船尾側の両側面に向けて連通した静圧ポケットを設けたので、船舶静止時若しくは直進時の重力方向の荷重に対して、及び船舶旋回時の水平方向荷重に対して、該軸受に設けた静圧ポケットに印加する油圧によってプロペラ軸を支持でき、プロペラ軸の片当たりを防止できる。これにより、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減に寄与する。
【0036】
また、請求項の発明によれば、船尾管軸受の船尾側内面に複数の静圧ポケットを設けたので、船舶静止時若しくは直進時の重力方向の荷重に対しては下面に設けた静圧ポケットに印加する油圧によって、また、船舶旋回時の水平方向荷重に対しては側面に設けた静圧ポケットに印加する油圧によってプロペラ軸を支持できるので、プロペラ軸の片当たりを防止できる。これにより、軸受又はプロペラ軸の熱的損傷の発生を防止でき、船尾管軸受のメンテナンス作業頻度や作業コストの低減を実現できる。
【0037】
また、請求項ないしの発明によれば、請求項1ないし3の何れかの項に記載の発明において、船尾管軸受の船尾側内面に静圧ポケットを設け、好ましくは、該軸受の下面からより船尾側の側面に向けて静圧ポケットを設けたので、また、好ましくは、複数の静圧ポケットを設け、側面の静圧ポケットの設置位置を下面の静圧ポケットの設置位置よりも船尾側に配置したので、該静圧ポケットに油圧を印加する方法によってプロペラ軸を支持でき、該軸受をコンパクトに設計できる。これにより、船尾管軸受の製造コストの低減、該軸受の設置スペースの節約、メンテナンス作業コストの低減を実現できる。
【0038】
【図面の簡単な説明】
【図1】 本発明の実施形態1にかかる船尾管軸受の構成を示す説明図である。
【図2】 本発明の実施形態2にかかる船尾管軸受の構成を示す説明図である。
【図3】 本発明の実施形態3にかかる船尾管軸受の構成を示す説明図である。
【図4】 本発明の実施形態4にかかる船尾管軸受の構成を示す説明図である。
【図5】 船尾管軸受を設置する船体後部の構成を示す説明図である。
【図6】 船尾管軸受の従来技術を示す説明図である。
【図7】 船尾管軸受の従来技術を示す説明図である。
【図8】 船尾管軸受の従来技術を示す説明図である。
【符合の説明】
1 船尾管軸受
9 テーパー軸受面
10 スロープ軸受面
11 静圧ポケット
11a 下面静圧ポケット
11b 側面静圧ポケット
16 軸受面
18 軸受すきま母線
[0001]
BACKGROUND OF THE INVENTION
  The present invention is used for a propeller bearing having an oil supply groove and an oil supply hole on a bearing inner surface of a ship, and a stern tube bearing having a taper boring process or a slope boring process, or a stern pipe having a static pressure pocket. The present invention relates to a bearing and a manufacturing method thereof.
[0002]
[Prior art]
  FIG. 5 shows a stern structure of a ship in which stern tube bearings are used. A stern tube bearing 1 is installed at the stern of the hull 6, and the propeller shaft 2 passes through the stern tube bearing 1 and the hull stern. The hull stern portion is sealed by a stern tube sealing device 3 to prevent inflow of seawater into the ship and outflow of lubricating oil used in the bearing into the sea. A propeller 4 is mounted on the stern side end of the propeller shaft 2. A rudder 5 is installed on the hull 6 on the stern side of the propeller 4.
  In the stern structure as described above, when the weight of the propeller 4 is large, the propeller shaft 2 is bent by the own weight of the propeller 4, and the propeller shaft 2 is easily hit by one side on the stern side of the stern tube bearing 1. Further, when the ship turns, a large force is generated in the flow of seawater flowing into the propeller 4 due to the interaction between the shape of the rudder 5 and the hull 6 and the propeller shaft 2 moves to the stern tube. It was easy to hit on the stern side of the bearing 1. Therefore, conventionally, the inner surface shape of the stern side of the stern tube bearing has been devised in order to reduce the per unit contact in the gravity direction, the horizontal direction, or the combined direction thereof. An example is described below.
[0003]
  FIG. 6 shows a stern tube bearing in which the bearing inner surface is tapered from the middle of the bearing surface 16 on the bow side so that the tapered bearing surface 9 expands toward the stern side. (A) is sectional drawing which follows an axial center line, (b) is the side view seen from C. This process is called taper boring. The tapered boring is provided in the axial direction L ′ on the stern side of the stern tube bearing 1 and on the entire circumference. R2Is the radius of curvature of the bearing surface and R1Is the radius of curvature of the tapered bearing surface, and the center of curvature is CeMatch. By performing the taper boring process, the diameter of the taper bearing surface 9 increases corresponding to the inclination of the propeller shaft 2 which is bent toward the stern side, so that the outer peripheral surface of the propeller shaft 2 and the taper bearing surface 9 are increased. Can be secured toward the stern side. As a result, it is possible to alleviate the one-side hit on the stern side.
[0004]
  FIG. 7 shows the same radius of curvature R as the bearing inner surface.2Thus, it is a stern tube bearing whose inner surface is processed into a slope shape from the middle of the bearing surface 16 on the bow side. (A) is sectional drawing which follows an axial center line, (b) is the side view seen from D. This process is called slope boring. The slope boring is provided in the range of the stern side axial direction L ′ of the stern tube bearing 1 and on the lower half surface. ε is the center of curvature C of the bearing surface 16 at the stern end of the stern tube bearing 1.eAnd the center of curvature C of the slope bearing surface 102And the distance.
  By applying the slope boring process, in particular, when a heavy weight propeller 4 is mounted, the slope bearing surface 10 from the shaft center line of the bearing corresponds to the inclination of the propeller shaft 2 which is bent toward the stern side. Therefore, the clearance between the outer peripheral surface of the propeller shaft 2 and the slope bearing surface 10 can be secured toward the stern side. As a result, it is possible to alleviate the one-side hit on the stern side.
[0005]
  FIG. 8 shows a stern tube bearing in which a hydrostatic pocket 11 for supporting the propeller shaft 2 with hydraulic pressure is provided on the inner surface of the bearing. (A) is a longitudinal cross-sectional view, (b) is a side view seen from E.
  The static pressure pocket 11 is connected to a high-pressure oil supply pipe 12 that communicates with the outer peripheral surface of the stern tube bearing 1, a high-pressure pipe 13 is connected from the outer peripheral surface, and a pump 15 is connected via a control valve 14. . The hydraulic pressure is applied from the pump 15 to the static pressure pocket 11 and the lubricating oil in the static pressure pocket 11 is supplied to the bearing surface to support the load on the propeller shaft and to reduce the contact of the propeller shaft 2 with each other.
  In the stern tube bearing shown in any of FIGS. 6 to 8, the oil supply grooves 7 are provided in the axial direction on both side surfaces inside the bearing, and a plurality of oil supply holes 8 are formed in each oil supply groove. Yes. Lubricating oil is supplied from the oil supply hole 8 to the oil supply groove 7 during ship operation. The lubricating oil spreads in the axial direction along the oil supply groove 7 and enters the gap between the propeller shaft and the bearing inner surface, and spreads around the entire inner circumference of the bearing as the propeller shaft rotates, thereby providing a lubricating function between the propeller shaft and the bearing inner surface. Fulfill. As a result, thermal damage to the propeller shaft or the bearing inner surface is prevented.
[0006]
  A bearing device using hydraulic pressure is disclosed in Patent Document 1 (Japanese Patent Laid-Open No. 8-091292). In this publication, a plurality of oil supply holes are provided over the entire inner circumference of the bearing, and a static pressure is applied in a low rotation region of the propeller shaft to ensure a bearing load capacity.
  Further, in Patent Document 2 (Japanese Patent Laid-Open No. 6-321185), in a contra-rotating propeller bearing structure, a large number of oil supply pipes are provided inside a bearing that supports a propeller inner shaft, and the mouths of the pipes are provided. A bearing device that is open over the entire inner circumference of the bearing is disclosed. The bearing itself also rotates in the direction opposite to the propeller inner shaft. At this time, the oil supply system is configured so that oil is supplied when the oil supply pipeline inside the rotating bearing comes to the lower surface of the bearing device, and the bearing in the gravity direction with a large propeller shaft load is formed. Ensures surface lubrication.
  Propeller shaft bearings are described in detail in Non-Patent Document 1 (“Class 1 Marine Engine Mechanic Instruction Manual” (Japan Foundation Business Results Library, Japan Marine Engine Maintenance Association, 1996)).
[0007]
[Patent Document 1]
  JP-A-8-091292
[Patent Document 2]
  JP-A-6-321185
[Non-Patent Document 1]
  First-class marine engine mechanic instruction manual (Nippon Foundation Business Results Library, Japan Marine Engine Maintenance Association, 1996)
[0008]
[Problems to be solved by the invention]
  The stern tube bearings related to the prior art described above have the following problems. Usually, the design of the stern tube bearing is performed assuming a static state when the propeller shaft and the propeller are installed. Therefore, the contact of the propeller shaft with the stern tube bearing due to the weight of the propeller shaft and the propeller can be dealt with by setting the bearing clearance and the installation angle of the bearing with respect to the hull. However, when a fluid force is generated along with the turning at the time of marine vessel operation, the direction in which one hits is changed depending on the operating state, so that it is difficult to cope with adjustment of the installation angle of the bearing at the time of design. In particular, in the case of a ship equipped with a propeller that rotates at high speed, the load that the propeller receives is greater in the horizontal direction due to the fluid force than in the direction of gravity. Therefore, since the deflection of the propeller shaft increases in the horizontal direction, it is necessary to support the propeller shaft load on the stern side.
[0009]
  In the case of the bearing device shown in Patent Document 1 and Patent Document 2 or the taper boring process shown in FIG. 6 for the above conditions, when the taper angle is optimized in accordance with the fluid force at the time of ship turning, The angle is excessive as compared with the contact per piece due to the weight of the propeller shaft and the propeller when the ship goes straight. Therefore, a portion with a thin oil film thickness is formed inside the stern side end portion of the bearing, the lubrication of the bearing becomes insufficient, and the bearing or the propeller shaft may be thermally damaged. Further, in the case of the bearing devices shown in Patent Document 1 and Patent Document 2, when the slope boring process shown in FIG. 7 is performed and when the static pressure pocket shown in FIG. 8 is provided, the load in the gravity direction between the propeller shaft and the propeller is reduced. However, it cannot cope with the horizontal load caused by the hydrodynamic force when the ship turns.
[0010]
  In view of the shortcomings of the prior art, the present invention provides a stern tube bearing that supports a propeller shaft of a ship and is provided with an oil groove and an oil hole in the axial direction of the inner surface of the bearing, and in the gravitational load between the propeller shaft and the propeller. By coping with both the horizontal load and the horizontal load caused by the hydrodynamic force when turning the ship, thermal damage to the bearing or propeller shaft can be prevented, thereby reducing the maintenance work frequency and work cost of the stern tube bearing. The purpose is to provide a stern tube bearing with a reduced stern tube bearing and a compact stern tube bearing.
[0011]
[Means for Solving the Problems]
  In order to solve the problem, the present invention as claimed in claim 1,
  In a stern tube bearing that supports a propeller shaft of a ship and has an oil supply groove in the axial direction of the bearing inner surface and an oil supply hole that communicates with the oil supply groove.TheOn the stern side of the bearing,It has a bearing surface formed by a taper boring in which the bearing inner surface is machined into a taper shape spreading from the middle of the bearing surface on the bow side, and the center of curvature C of the taper boring 3 The axial center position C of the stern tube bearing e Set upward fromA stern tube bearing is proposed.
  According to the first aspect of the present invention, when a horizontal load is applied during turning of the ship, the propeller shaft load is evenly applied in the axial direction to the bearing surface of the bearing. It can be evenly distributed on the surface. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0012]
  The invention according to claim 2 is the stern tube bearing according to claim 1, wherein the bearing clearance bus 18 on the inner surface of the bearing and the bearing clearance bus 18 on the bearing surface formed by the taper boring are made to coincide. Propose.
  According to the invention described in claim 2, in addition to claim 1, for the load in the gravity direction when the ship is stationary or going straight, the bearing is inclined and installed in the hull and the bearing clearance is set. When a horizontal load is applied when turning a ship, the propeller shaft load is equally applied to the taper-bored bearing surface of the bearing in the axial direction. Can be evenly distributed. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0013]
  The invention described in claim 3A stern tube bearing that supports a propeller shaft of a ship and includes an oil supply groove in the axial direction of the bearing inner surface and an oil supply hole that communicates with the oil supply groove, and a bearing surface formed by slope boring on the stern side of the bearing Provided,
  Furthermore,The radius of curvature of the bearing surface formed by slope boring is made the same as the radius of curvature of the inner surface of the bearing, and the center of curvature of the bearing surface formed by the slope boring is removed from the shaft center of the bearing and provided at two locations. We propose a stern tube bearing characterized by
  According to the third aspect of the invention, in addition to the first aspect, with respect to the load in the gravity direction when the ship is stationary or straight, the bearing is inclined and installed in the hull and the bearing clearance is set. If a horizontal load is applied when turning the ship, the propeller shaft load is evenly applied in the axial direction to the slope-bored bearing surface of the bearing. Can be evenly distributed. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0014]
  Claim7Or8The invention according to any one of the claims relates to a method for manufacturing a stern tube bearing according to any one of claims 1 to 3.
  Claim7The invention described inIn a method for manufacturing a stern tube bearing that supports a propeller shaft of a ship and includes an oil supply groove in the axial direction of the bearing inner surface and an oil supply hole that communicates with the oil supply groove.BoringsurfaceCenter of curvatureTheThe radius of curvature of the machining is set larger than the radius of curvature of the bearing at the stern side end of the bearing, fixed at a position removed from the center of curvature of the bearing.As well asThe taper boring is performed by feeding the boring tool in the axial direction and setting it to become smaller until it matches the radius of curvature of the bearing toward the bow side.YouA method of manufacturing a stern tube bearing is proposed.
  Claim8The invention described inIn a method for manufacturing a stern tube bearing that supports a propeller shaft of a ship and includes an oil supply groove in the axial direction of the bearing inner surface and an oil supply hole that communicates with the oil supply groove.Curvature radius of boringTheSame as the radius of curvature of the bearing, the center of curvature of the machining is set off the shaft center at the stern end of the bearingAs well asSet to move in the radial direction until it coincides with the axial center position of the bearing as it goes to the bow side, and the slope boring is performed by sending the boring tool in the axial direction.YouA method of manufacturing a stern tube bearing is proposed.
[0015]
  Claim7Or8According to the invention described in any one of the above, the inner surface of the bearing is tapered in a direction in which the propeller shaft is expected to come into contact with one another due to the load in the gravity direction when the ship is stationary or straight ahead and the horizontal load when the ship is turning. Since boring can be performed, even when the gravity direction load and the horizontal direction load are applied to the propeller shaft, the propeller shaft load is equally applied in the axial direction of the bearing. Can be evenly distributed. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0016]
  According to a fourth aspect of the present invention, there is provided a stern tube bearing that supports a propeller shaft of a ship and includes an oil supply groove and an oil supply hole that communicates with the oil supply groove in an axial direction of the bearing inner surface.More than oneEstablish a static pressure pocketFurther, the static pressure pocket is provided on the side surface and the lower surface, and the position of the static pressure pocket provided on the side surface is arranged on the stern side of the position of the static pressure pocket provided on the lower surface.A stern tube bearing is proposed.
  According to the invention described in claim 4, the hydraulic pressure applied to the static pressure pocket provided in the bearing with respect to the load in the gravitational direction when the ship is stationary or going straight and against the horizontal load when the ship is turning. Since the propeller shaft can be supported, it is possible to prevent the propeller shaft from coming into contact with each other. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0017]
  This bookAccording to the invention, it is provided by the hydraulic pressure applied to the static pressure pocket provided on the lower surface for the load in the gravitational direction when the ship is stationary or going straight, and on the side surface for the horizontal load when the ship is turning. Since the propeller shaft can be supported by the hydraulic pressure applied to the static pressure pocket, it is possible to prevent the propeller shaft from coming into contact with each other. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0018]
  MoreAccording to the present invention,The effectIn addition, the static pressure provided on the stern side is more suitable for the horizontal load when turning the ship, especially when the horizontal load when turning the ship is greater than the load in the gravity direction when the ship is stationary or straight. Since the propeller shaft can be supported by the hydraulic pressure applied to the pocket, it is possible to prevent the propeller shaft from coming into contact with each other. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0019]
  Claim5Or6The invention according to claim 1 proposes a stern tube bearing characterized in that, in the invention according to any one of claims 1 to 3, a static pressure pocket is provided on the stern side inner surface of the stern tube bearing.
  Claim5In the above, a static pressure pocket is provided from the lower surface of the bearing toward the side surface on the stern side. Also preferably the claim6As described above, the installation position of the static pressure pocket on the side surface is preferably arranged closer to the stern side than the installation position of the static pressure pocket on the lower surface.
  Claim5Or6According to the invention described in claim 1, in addition to any one of claims 1 to 3, the hydraulic pressure is applied to the static pressure pocket provided in the bearing.thingCan support the propeller shaft, so that the bearing can be designed compactly. As a result, it is possible to reduce the manufacturing cost of the stern tube bearing, save the installation space of the bearing, and reduce the maintenance work cost.
[0020]
DETAILED DESCRIPTION OF THE INVENTION
  Hereinafter, the present invention will be described in detail with reference to the embodiments shown in the drawings. However, the dimensions, materials, shapes, relative positions, and the like of the components described in this embodiment are not intended to limit the scope of the present invention only to the description unless otherwise specified. It is just an example.
[0021]
(Embodiment 1)
  Fig.1 (a) is explanatory drawing which shows the structure of the stern tube bearing which concerns on Embodiment 1 of this invention, (a) is sectional drawing which follows an axial center line, (b) is the side view seen from A. .
  In FIG. 1 (a), a flange 17 is machined at the stern side end of a cylindrical stern tube bearing 1, and the stern tube bearing 1 is transferred to the stern tube sealing device 3 or the hull 6 (see FIG. 5). Used for fixing. Oil supply grooves 7 are machined on opposite side surfaces of the bearing surface 16, and a plurality of oil supply holes 8 are drilled into the oil supply grooves 7 so as to communicate with the outer peripheral surface of the stern tube bearing 1. An oil supply pipe (not shown) is connected to the oil supply hole 8, and lubricating oil for lubricating the propeller shaft 2 and the bearing surface 16 is supplied.
[0022]
  Each symbol in FIG. 1 indicates the following. L is the total axial length of the stern tube bearing 1, ReIs the radius of curvature of the bearing surface 16, R3Indicates the radius of curvature of the tapered boring at the stern end, and L ′ indicates the axial length of the taper boring. Where R3> ReIt is. Further, the propeller shaft 2 indicated by a solid line shows a state in which the propeller shaft center deviates from Ce due to gravity during ship navigation and horizontal load during ship turning. The propeller shaft 2 indicated by a one-dot chain line indicates an initial position when the propeller shaft 2 is attached to the stern tube bearing 1 in the previous period, that is, the propeller shaft center position and the shaft center position Ce of the stern tube bearing 1 coincide with each other. It shows how it is.
[0023]
  In this embodiment, the center of curvature C of the taper boring3The axial center position C of the stern tube bearing 1eIt was set off from above. The distance to be removed upward was the distance at which the bearing clearance bus 18 of the bearing surface 16 and the bearing clearance bus 18 of the tapered bearing surface 9 matched at the stern side end of the stern tube bearing 1. By performing such taper boring, the radius of curvature of the bearing surface of the stern side lower surface of the stern tube bearing 1 is R.eAnd the radius of curvature is R as it goes from the lower surface to both side surfaces.3A taper bearing surface 9 is formed which gradually increases until. However, the taper boring should be done up to the oil groove 7 on both sides and not on the upper half, so the radius of curvature of the bearing surface on the upper half is ReIt is.
  As described above, the load in the direction of gravity between the propeller shaft 2 and the propeller 4 when the ship is stationary or straight ahead can be handled by tilting the stern tube bearing 1 and setting the bearing clearance. When a horizontal load is applied when turning the ship, the propeller shaft load is evenly applied in the axial direction to the tapered bored bearing surface of the bearing, so the lubricating oil film pressure is applied to the bearing surface. Can be evenly distributed. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0024]
  The taper boring method will be described below. In the stern tube bearing 1, a bearing surface 16, an oil supply groove 7, and an oil supply hole 8 are processed in advance. Next, the bearing 1 is placed on a large rotary table so that the axis of the bearing 1 is perpendicular to the table surface, and the shaft center C of the bearing 1 is set.eAnd the table so that the center of rotation coincides. At this time, it installs so that the bow side end surface of this bearing may contact | connect this table surface. Next, the processing tool held at the stern side end of the bearing 1 is applied to the inner surface of the bearing, and the large rotary table is rotated to cut the inner surface of the bearing and advance the taper boring process.
  Here, taper boring curvature center position C3Is set to be shifted from the rotation center position of the table. The cutting distance is determined according to the taper boring curvature radius and taper angle designed in advance. The taper angle is an angle formed by the bearing surface 16 and the tapered bearing surface 9. The axial length L ′ for forming the taper boring is determined by the angle and the radius of curvature of the taper boring.
  Here, when taper boring is applied to the half surface of the stern tube bearing, for example, when it is applied to the lower half surface of the bearing, as shown in FIG. The end position is the opposite oil groove 7. By setting the start position and the end position of cutting to the oil supply groove 7, it is possible to secure a space between the contact and escape of the processing tool.
[0025]
(Embodiment 2)
  FIG. 2 is an explanatory view showing a configuration of a stern tube bearing according to Embodiment 2 of the present invention, and shows a view of the stern tube bearing as viewed from the stern side end.
  The flange 17, the oil supply groove 7, and the oil supply hole 8 are processed in the cylindrical stern tube bearing 1 as in the first embodiment.
  Each symbol in FIG. 2 indicates the following. The same symbols as those in FIG. R2Indicates the radius of curvature of the bearing surface 16 and the slope boring, C2Is the center of curvature of the slope boring, and ε is the C2And axis center C of stern tube bearing 1eAnd the distance.
[0026]
  In the present embodiment, the curvature center position C of the slope boring applied to the stern tube bearing 1.2Axis center C of stern tube bearing 1eFrom the left and right side sides, the two were removed and set. By processing in this way, the radius of curvature of the bearing surface at the stern side end of the stern tube bearing 1 is R.2However, as it goes from the lower surface to both side surfaces, the axial center CeDistance from bearing surface to maximum R2It becomes longer to + ε and constitutes the slope bearing surface 10. However, the slope boring is made up to the oil groove 7 on both sides and not on the upper half, so the radius of curvature of the bearing surface on the upper half is R2It is.
  As described above, the load in the direction of gravity between the propeller shaft 2 and the propeller 4 when the ship is stationary or going straight can be handled by tilting the stern tube bearing 1 and setting the bearing clearance. If a horizontal load is applied when the ship is turning, the propeller shaft load is evenly applied in the axial direction to the bearing surface on which the slope boring of the bearing is performed. Can be evenly distributed. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0027]
  The slope boring method will be described below. In the stern tube bearing 1, a bearing surface 16, an oil supply groove 7, and an oil supply hole 8 are processed in advance. Next, the bearing 1 is placed on a large rotary table so that the axis of the bearing 1 is perpendicular to the table surface, and the shaft center C of the bearing 1 is set.eAnd the table so that the center of rotation coincides. At this time, it installs so that the bow side end surface of this bearing 1 may contact | connect this table surface. Next, the large rotary table is inclined with respect to the cutting direction. A processing tool held at the stern side end of the bearing 1 is applied to the inner surface of the bearing, and the large rotary table is rotated to cut the inner surface of the bearing and advance the slope boring process.
  Where slope boring radius of curvature R2Is the radius of curvature R of the bearing surface 16 of the bearing 1.2Same as As shown in FIG. 2, the angle at which the large rotary table is inclined with respect to the cutting direction is the center of curvature C of the slope bearing surface 10 at the stern side end of the bearing 1.2Axis center CeIs determined from the distance ε shifted from the axial distance of the slope bearing surface 10 designed in advance.
[0028]
(Embodiment 3)
  FIG. 3 is an explanatory view showing a configuration of a stern tube bearing according to Embodiment 3 of the present invention, and is a cross-sectional view taken along the axial center line of the stern tube bearing.
  The flange 17, the oil supply groove 7, and the oil supply hole 8 are processed in the cylindrical stern tube bearing 1 as in the first embodiment.
  In this embodiment, a static pressure pocket 11 is provided on the stern side bearing surface 16 of the stern tube bearing 1, a high pressure oil supply pipe 12 communicating with the outer peripheral surface of the stern tube bearing 1 is drilled there, and further, high pressure piping is provided. 13 and a control valve 14 were connected to the pump 15 by piping. Here, the static pressure pocket 11 has a substantially rectangular opening in the bearing surface 16, and is constructed from the lower surface of the stern tube bearing 1 toward both side surfaces on the stern side. During the operation of the ship, the lubricating oil is pressurized to the static pressure pocket 11 using the pump 15 to support the load on the propeller shaft 2. The degree of pressurization is adjusted by the opening degree of the control valve 14 corresponding to the increase or decrease of the load.
[0029]
  Since the static pressure pockets 11 are provided on both side surfaces on the stern side from the bearing lower surface, the load in the gravity direction between the propeller shaft 2 and the propeller 4 when the vessel is stationary or going straight, and the horizontal load of the vessel turning On the other hand, since the propeller shaft can be supported by adjusting the hydraulic pressure of the lubricating oil applied to the static pressure pocket, it is possible to prevent the propeller shaft from coming into contact with one another. In particular, when the propeller 4 that rotates at a high speed is used, the size per piece when a horizontal load is applied is likely to be larger than when a load in the gravity direction is applied. That is, since the propeller shaft 2 is greatly bent in the horizontal direction, the maximum pressure of the oil film is necessary on the side surface close to the stern. Therefore, by providing the static pressure pocket 11 closer to the side surface, the restoring force against the deflection of the propeller shaft 2 can be increased. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0030]
(Embodiment 4)
  4A and 4B are explanatory views showing the configuration of a stern tube bearing according to Embodiment 4 of the present invention. FIG. 4A is a cross-sectional view taken along the axial center line of the stern tube bearing, and FIG. is there.
  The flange 17, the oil supply groove 7, and the oil supply hole 8 are processed in the cylindrical stern tube bearing 1 as in the first embodiment.
  In this embodiment, a lower surface static pressure pocket 11a is provided on the lower surface on the stern side of the stern tube bearing 1, and a side surface static pressure pocket 11b is provided on both side surfaces on the stern side, and the stern tube bearing 1 is provided in each static pressure pocket. A high-pressure oil supply pipe 12 communicating with the outer peripheral surface was drilled, and further connected to a pump 15 via a high-pressure pipe 13 and a control valve 14. Here, the static pressure pockets 11 a and 11 b have a substantially rectangular opening having a long side in the circumferential direction of the stern tube bearing 1 on the bearing surface 16.
[0031]
  With this configuration, the lubricant is pressurized by the pump 15 to the static pressure pockets 11a and 11b, and the load in the horizontal direction is mainly applied to the lower surface static pressure pocket 11a with respect to the load in the gravity direction. In contrast, the propeller shaft 2 is supported mainly by the hydraulic pressure applied to the side surface static pressure pocket 11b. The degree of pressurization is adjusted by the opening degree of each control valve 14 corresponding to the increase or decrease of each load.
  Since the static pressure pockets 11a and 11b are provided independently on the bearing lower surface and both side surfaces on the stern side, with respect to the load in the direction of gravity between the propeller shaft 2 and the propeller 4 when the vessel is stationary or straight ahead The hydraulic pressure of the lubricating oil applied to the static pressure pocket 11a provided on the lower surface of the bearing is adjusted, and the hydraulic pressure of the lubricating oil applied to the static pressure pocket 11b provided on both sides is adjusted with respect to the horizontal load when the ship turns. Thus, the propeller shaft can be supported, so that the propeller shaft can be prevented from coming into contact with each other.
[0032]
  In particular, when the propeller 4 that rotates at a high speed is used, the size per piece when a horizontal load is applied is likely to be larger than when a load in the gravity direction is applied. That is, since the propeller shaft 2 bends more largely in the horizontal direction than in the direction of gravity, the maximum pressure of the oil film is required on the side surface near the stern. Therefore, by providing the static pressure pocket 11 closer to the side surface on the stern side, it is possible to increase the restoring force against the deflection of the propeller shaft 2.
  Furthermore, a compact stern tube bearing can be manufactured if the position, number, opening size, depth, etc. of the static pressure pocket are designed in accordance with the axial load assumed during ship operation. This is because, like a taper boring, a slope boring, and a static pressure pocket having an angle in the circumferential direction, a certain amount of structural size is not required for the function to function. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced. Furthermore, since a compact stern tube bearing can be manufactured, it is possible to reduce the manufacturing cost of the bearing, save the installation space of the bearing, and reduce the maintenance work cost.
[0033]
(Embodiment 5)
  The fifth embodiment of the present invention (not shown) has a structure in which the first embodiment is combined with the third or fourth embodiment. Or it is set as the structure which combined Embodiment 2 and Embodiment 3 or Embodiment 4. FIG.
  In addition to the taper boring described in the first embodiment or the slope boring described in the second embodiment, the static pressure pocket 11 is provided, and the hydraulic pressure of the lubricating oil applied to the static pressure pocket 11 is adjusted. The range of the magnitude of the axial load that 1 can deal with widens. Therefore, if the stern tube bearing 1 has the same size, the shaft load that can be handled becomes large. If the shaft load is the same, the bearing can be made compact. As a result, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced. Furthermore, since a compact stern tube bearing can be manufactured, it is possible to reduce the manufacturing cost of the bearing, save the installation space of the bearing, and reduce the maintenance work cost.
[0034]
【The invention's effect】
  As described above, claims 1 to 3 and claims7Or8According to the invention, since one or both of the taper boring and the slope boring is provided on the stern side of the stern tube bearing and the center of curvature thereof is set off from the shaft center of the bearing, the horizontal load is applied when the ship turns. Is applied, the propeller shaft load is evenly applied in the axial direction to the bearing surface of the bearing, and the lubricant film pressure can be evenly distributed over the bearing surface. Thereby, generation | occurrence | production of the thermal damage of a bearing or a propeller shaft can be prevented, and it contributes to the reduction of the maintenance work frequency and work cost of a stern tube bearing.
[0035]
  Further, according to the invention of claim 4, since the static pressure pockets are provided which are communicated from the lower surface of the stern side inner surface of the stern tube bearing toward the both side surfaces of the stern side, the gravity direction when the ship is stationary or when traveling straight The propeller shaft can be supported by the hydraulic pressure applied to the static pressure pockets provided in the bearings against the load and the horizontal load at the time of turning of the ship, and the propeller shaft can be prevented from hitting one side. Thereby, generation | occurrence | production of the thermal damage of a bearing or a propeller shaft can be prevented, and it contributes to the reduction of the maintenance work frequency and work cost of a stern tube bearing.
[0036]
  Claims4According to the invention, since the plurality of static pressure pockets are provided on the stern side inner surface of the stern tube bearing, the hydraulic pressure applied to the static pressure pocket provided on the lower surface with respect to the load in the gravity direction when the ship is stationary or straight ahead In addition, since the propeller shaft can be supported by the hydraulic pressure applied to the static pressure pocket provided on the side surface with respect to the horizontal load at the time of turning the ship, it is possible to prevent the propeller shaft from hitting one side. Thereby, the occurrence of thermal damage to the bearing or the propeller shaft can be prevented, and the maintenance work frequency and work cost of the stern tube bearing can be reduced.
[0037]
  Claims5Or6According to the invention, in the invention according to any one of claims 1 to 3, the hydrostatic pocket is provided on the stern side inner surface of the stern tube bearing, and preferably on the side surface on the stern side from the lower surface of the bearing. Since the static pressure pockets are provided, and preferably, a plurality of static pressure pockets are provided, and the installation position of the static pressure pockets on the side surface is disposed closer to the stern side than the installation position of the static pressure pockets on the lower surface. The propeller shaft can be supported by a method of applying hydraulic pressure to the static pressure pocket, and the bearing can be designed compactly. Thereby, the manufacturing cost of the stern tube bearing can be reduced, the installation space of the bearing can be saved, and the maintenance work cost can be reduced.
[0038]
[Brief description of the drawings]
FIG. 1 is an explanatory diagram showing a configuration of a stern tube bearing according to a first embodiment of the present invention.
FIG. 2 is an explanatory diagram showing a configuration of a stern tube bearing according to a second embodiment of the present invention.
FIG. 3 is an explanatory diagram showing a configuration of a stern tube bearing according to a third embodiment of the present invention.
FIG. 4 is an explanatory diagram showing a configuration of a stern tube bearing according to a fourth embodiment of the present invention.
FIG. 5 is an explanatory view showing a configuration of a rear part of a hull in which a stern tube bearing is installed.
FIG. 6 is an explanatory view showing a prior art of a stern tube bearing.
FIG. 7 is an explanatory view showing a prior art of a stern tube bearing.
FIG. 8 is an explanatory view showing a prior art of a stern tube bearing.
[Explanation of sign]
  1 Stern tube bearing
  9 Tapered bearing surface
10 Slope bearing surface
11 Static pressure pocket
11a Underside static pressure pocket
11b Side static pressure pocket
16 Bearing surface
18 Bearing clearance busbar

Claims (8)

船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受において、該軸受の船尾側に、船首側の軸受面の途中から末広がりテーパー状に軸受内面を加工したテーパーボーリングによって形成された軸受面を有し、該テーパーボーリングの曲率中心位置C を前記船尾管軸受の軸中心位置C から上方へ外して設定したことを特徴とする船尾管軸受。In a stern tube bearing that supports a propeller shaft of a ship and has an oil supply groove in the axial direction of the bearing inner surface and an oil supply hole that communicates with the oil supply groove, on the stern side of the bearing, from the middle of the bearing surface on the bow side it has a bearing surface formed by the processed taper boring the bearing inner surface diverging tapered that it has set off upward curvature center position C 3 of the tapered borehole from the axial center position C e of the stern tube bearing Stern tube bearing featured. 前記軸受内面の軸受すきま母線と前記テーパーボーリングによって形成された軸受面の軸受すきま母線とを一致させたことを特徴とする請求項1記載の船尾管軸受。  The stern tube bearing according to claim 1, wherein a bearing clearance bus bar on the inner surface of the bearing and a bearing clearance bus bar on a bearing surface formed by the tapered boring are matched. 船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受において、該軸受の船尾側に、スロープボーリングによって形成された軸受面を設け、
更に前記スロープボーリングによって形成された軸受面の曲率半径を軸受内面の曲率半径と同一とするとともに、該スロープボーリングによって形成された軸受面の曲率中心を該軸受の軸中心から外して2箇所に設けたことを特徴とする船尾管軸受。
A stern tube bearing that supports a propeller shaft of a ship and includes an oil supply groove in the axial direction of the bearing inner surface and an oil supply hole that communicates with the oil supply groove, and a bearing surface formed by slope boring on the stern side of the bearing Provided,
Further, the radius of curvature of the bearing surface formed by the slope boring is made the same as the radius of curvature of the bearing inner surface, and the center of curvature of the bearing surface formed by the slope boring is removed from the shaft center of the bearing and provided at two locations. ship tail tube bearing you, characterized in that the.
船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受において、該軸受の船尾側内面に複数の静圧ポケットを設け、更に前記静圧ポケットを側面及び下面に設けるとともに、側面に設ける静圧ポケットの位置を下面に設ける静圧ポケットの位置よりも船尾側に配置したことを特徴とする船尾管軸受。In a stern tube bearing that supports a propeller shaft of a ship and has an oil supply groove in the axial direction of the bearing inner surface and an oil supply hole that communicates with the oil supply groove , a plurality of static pressure pockets are provided on the inner surface of the stern side of the bearing , Further , the stern tube bearing is characterized in that the static pressure pocket is provided on the side surface and the lower surface, and the position of the static pressure pocket provided on the side surface is arranged on the stern side of the position of the static pressure pocket provided on the lower surface . 前記軸受の船尾側内面に、該軸受の下面から船尾側の側面に向けて静圧ポケットを設けたことを特徴とする請求項1ないしの何れかの項に記載の船尾管軸受。The stern tube bearing according to any one of claims 1 to 2 , wherein a static pressure pocket is provided on a stern side inner surface of the bearing from a lower surface of the bearing toward a stern side surface. 前記軸受の船尾側内面に、側面の静圧ポケットの設置位置を下面の静圧ポケットの設置位置よりも船尾側に配置したことを特徴とする請求項記載の船尾管軸受。The stern tube bearing according to claim 4, wherein the installation position of the static pressure pocket on the side surface is arranged closer to the stern side than the installation position of the static pressure pocket on the lower surface on the inner surface of the stern side of the bearing. 船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受の製造方法において、ボーリング加工面の曲率中心位置を該軸受の曲率中心位置から外した位置に固定して、該加工の曲率半径を、前記軸受の船尾側端部では該軸受の曲率半径より大きく設定するとともに、船首側に向かうに従って前記軸受の曲率半径に一致するまで小さくなるように設定し、ボーリング加工工具を軸方向に送ることによってテーパーボーリング加工を施すことを特徴とする船尾管軸受の製造方法。  In a method for manufacturing a stern tube bearing that supports a propeller shaft of a ship and has an oil supply groove in the axial direction of the bearing inner surface and an oil supply hole that communicates with the oil supply groove, the center of curvature of the boring surface is the curvature of the bearing. The radius of curvature of the machining is set larger than the radius of curvature of the bearing at the stern end of the bearing and coincides with the radius of curvature of the bearing toward the bow side. A method for manufacturing a stern tube bearing, wherein taper boring is performed by feeding a boring tool in an axial direction. 船舶のプロペラ軸を支持し、軸受内面の軸方向に給油溝と該給油溝に連通される給油孔とを設けた船尾管軸受の製造方法において、ボーリング加工の曲率半径を該軸受の曲率半径と同一として、該加工の曲率中心位置を、前記軸受の船尾側端部では軸中心から外して設定するとともに、船首側に向かうに従って前記軸受の軸中心位置に一致するまで径方向に移動させるように設定し、ボーリング加工工具を軸方向に送ることによってスロープボーリング加工を施すことを特徴とする船尾管軸受の製造方法。  In a manufacturing method of a stern tube bearing that supports a propeller shaft of a ship and has an oil supply groove and an oil supply hole that communicates with the oil supply groove in the axial direction of the inner surface of the bearing, the curvature radius of boring is defined as the curvature radius of the bearing. As the same, the center of curvature of the machining is set off the shaft center at the stern end of the bearing, and is moved in the radial direction until it coincides with the shaft center position of the bearing toward the bow side. A method for manufacturing a stern tube bearing, characterized in that slope boring is performed by setting and sending a boring tool in an axial direction.
JP2002259196A 2002-09-04 2002-09-04 Stern tube bearing and manufacturing method thereof Expired - Fee Related JP3962664B2 (en)

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CN114413845B (en) * 2021-12-16 2024-04-02 上海江南长兴造船有限责任公司 Method for measuring ship stern tube bearing slope in internal field
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