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JP7086802B2 - Maintenance method, design method, and pumping equipment of pumping equipment - Google Patents
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JP7086802B2 - Maintenance method, design method, and pumping equipment of pumping equipment - Google Patents

Maintenance method, design method, and pumping equipment of pumping equipment Download PDF

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JP7086802B2
JP7086802B2 JP2018180828A JP2018180828A JP7086802B2 JP 7086802 B2 JP7086802 B2 JP 7086802B2 JP 2018180828 A JP2018180828 A JP 2018180828A JP 2018180828 A JP2018180828 A JP 2018180828A JP 7086802 B2 JP7086802 B2 JP 7086802B2
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trailing edge
blade
pressure surface
impeller
blades
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実 作田
裕之 井上
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Kubota Corp
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Description

本発明は、複数の羽根を有する羽根車が備えられたポンプ装置の維持管理方法、設計方法、及びポンプ装置に関する。 The present invention relates to a maintenance method, a design method, and a pump device of a pump device provided with an impeller having a plurality of blades.

産業用、農業用、雨水排水用など様々な用途において、最高効率点以外でも広い範囲で運転可能な斜流羽根車や、軸流羽根車が備えられたポンプ装置が用いられる。 In various applications such as industrial use, agricultural use, and rainwater drainage, a mixed flow impeller that can be operated in a wide range other than the highest efficiency point and a pump device equipped with an axial flow impeller are used.

特許文献1には、複数の羽根を有する斜流羽根車と、この斜流羽根車に接続された立軸の回転軸とが備えられたポンプ装置が開示されている。 Patent Document 1 discloses a pump device including a mixed flow impeller having a plurality of blades and a rotating shaft of a vertical shaft connected to the mixed flow impeller.

このようなポンプ装置において、吸込水位の低下等による吸込圧力が低下した運転環境下では、羽根まわりにキャビテーションが発生することが知られている。なお、キャビテーションとは、液体の流れの中で圧力が液体の飽和蒸気圧よりも低くなった箇所に気泡が発生する現象を言う。 In such a pump device, it is known that cavitation occurs around the blades in an operating environment in which the suction pressure is lowered due to a drop in the suction water level or the like. Cavitation is a phenomenon in which bubbles are generated in a liquid flow where the pressure becomes lower than the saturated vapor pressure of the liquid.

キャビテーションにより発生した気泡は、液体の圧力上昇に応じて次第に小さくなり消滅する場合に気泡部分に生じる非常に高い圧力が羽根の表面に衝撃的に作用する結果、その衝撃によって羽根の表面に凹みや傷が発生する。これをキャビテーションエロージョン(以下、壊食と記す。)と言う。 Bubbles generated by cavitation gradually become smaller and disappear as the pressure of the liquid rises, and when the bubbles disappear, the very high pressure generated on the bubble part impacts the surface of the blade, and as a result, the impact causes dents on the surface of the blade. Scratches occur. This is called cavitation erosion (hereinafter referred to as erosion).

したがって、壊食は、キャビテーションの発生する位置に発生するのではなく、気泡が崩壊する近辺の金属面(すなわち羽根の表面)に発生する。壊食が、特に、羽根の表面に発生すると、ポンプ装置の性能が大きく低下するという問題があった。 Therefore, erosion does not occur at the position where cavitation occurs, but on the metal surface (that is, the surface of the blade) in the vicinity where the bubbles collapse. When erosion occurs, especially on the surface of the blade, there is a problem that the performance of the pump device is greatly deteriorated.

特開2010-121467号公報Japanese Unexamined Patent Publication No. 2010-12146

本発明は、上述した問題点に鑑みてなされたもので、壊食が発生した羽根車の性能低下を防止することができるポンプ装置の維持管理方法を提供することを目的とする。 The present invention has been made in view of the above-mentioned problems, and an object of the present invention is to provide a maintenance method for a pump device capable of preventing performance deterioration of an impeller where erosion has occurred.

上述の目的を達成するための、本発明に係るポンプ装置の維持管理方法の特徴構成は、複数の羽根を有する羽根車が備えられたポンプ装置の維持管理方法であって、前記各羽根のうち少なくともいずれかの羽根の後縁に壊食又は壊食の兆候が発生しているか否かを確認する確認工程と、前記確認工程において、壊食又は壊食の兆候が発生していることが確認された場合に、前記各羽根の各後縁の負圧面側を前記各羽根の前縁へ向けて削る、又は前記各後縁を丸めるように削る加工工程とを有する点にある。 The characteristic configuration of the maintenance method of the pump device according to the present invention for achieving the above-mentioned object is the maintenance method of the pump device provided with the impeller having a plurality of blades, and among the above-mentioned blades. In the confirmation step of confirming whether or not there is a sign of erosion or erosion on the trailing edge of at least one of the blades, and in the confirmation step, it is confirmed that a sign of erosion or erosion has occurred. When this is done, the point is that the negative pressure surface side of each trailing edge of each of the blades is scraped toward the leading edge of each of the blades, or the trailing edge of each of the blades is scraped so as to be rounded.

ポンプ装置において、ポンプ効率と、吸込性能の改善を両立させ、全体的にコンパクト化を図ると、羽根車の羽根の翼面の単位面積当たりの負荷を小さくする設計になる。このとき羽根は三次元的に大きく捩じれ、かつ、後縁は羽根の断面視において尖鋭化した形状となる。 In the pump device, if both pump efficiency and improvement of suction performance are achieved and the overall compactness is achieved, the load per unit area of the blade surface of the impeller will be reduced. At this time, the blade is greatly twisted three-dimensionally, and the trailing edge has a sharpened shape in the cross-sectional view of the blade.

羽根車の回転によって、羽根の正圧面側は基本的に高圧となるが、尖鋭化した後縁の少し上流側において低圧領域が発生する。この低圧領域においてキャビテーションが発生し、又は上流側で発生したキャビテーションが増大し、その気泡は後縁の近傍の高圧領域において崩壊するため、後縁が壊食され、羽根車の性能低下が発生する。 Due to the rotation of the impeller, the positive pressure surface side of the blade is basically high pressure, but a low pressure region is generated slightly upstream of the sharpened trailing edge. Cavitation occurs in this low pressure region, or cavitation generated on the upstream side increases, and the bubbles collapse in the high pressure region near the trailing edge, so that the trailing edge is eroded and the performance of the impeller deteriorates. ..

そこで、ポンプ装置の定期的な点検時に確認工程を実行し、羽根の後縁に壊食が発生しているか否かを確認し、壊食が発生していることが確認されたら、加工工程を実行するのである。 Therefore, the confirmation process is executed during the periodic inspection of the pump device, it is confirmed whether or not the trailing edge of the blade is eroded, and if it is confirmed that the erosion has occurred, the processing process is performed. Do it.

発明者らの鋭意研究の結果、加工工程によって、羽根の後縁の負圧面の形状を変更することによって、羽根の後縁の正圧面側の低圧領域の圧力を、削り加工前に比べて上昇させることができることが判明した。これにより、羽根の後縁の正圧面側の低圧領域の圧力と羽根の後縁の近傍の高圧領域の圧力との圧力差は小さくなる。したがって、キャビテーション自体が発生しづらく、仮にキャビテーションによって気泡が発生したとしてもその崩壊が発生しづらい状態となる。これによって新たな壊食が抑制され、羽根車の性能低下が改善する。 As a result of diligent research by the inventors, the pressure in the low pressure region on the positive pressure surface side of the trailing edge of the blade is increased by changing the shape of the negative pressure surface of the trailing edge of the blade by the machining process. It turned out that it could be done. As a result, the pressure difference between the pressure in the low pressure region on the positive pressure surface side of the trailing edge of the blade and the pressure in the high pressure region near the trailing edge of the blade becomes small. Therefore, cavitation itself is unlikely to occur, and even if bubbles are generated by cavitation, their collapse is unlikely to occur. As a result, new erosion is suppressed and the performance deterioration of the impeller is improved.

なお、加工工程は、確認工程において羽根の後縁で実際に壊食が発生していることが確認された場合に限らず、後縁に壊食の発生が確認されない場合であってもその兆候が確認された場合に実行される。 The processing step is not limited to the case where it is confirmed that the trailing edge of the blade is actually eroded in the confirmation step, and even if the trailing edge is not confirmed to be eroded, it is a sign. Is executed when is confirmed.

また、羽根車に複数の羽根が備えられている場合において、吸込の偏流や、羽根車の製作時の各羽根の取付角の微差等に起因して、壊食は全ての羽根に均等に発生するとは限らない。したがって、複数の羽根のうち少なくともいずれかの羽根の後縁に壊食が発生しているか、壊食の兆候が発生していることが確認された場合に、後縁において壊食又はその兆候の発生が確認できていない羽根であっても経時的に壊食が発生する虞があるため、該羽根を含む全ての羽根に対して加工工程が実行される。このとき羽根車のバランス調整が同時に行われることが好ましい。 In addition, when the impeller is equipped with a plurality of blades, erosion is evenly distributed to all the blades due to the drift of suction and the slight difference in the mounting angle of each blade when the impeller is manufactured. It does not always occur. Therefore, if it is confirmed that at least one of the multiple blades has erosion on the trailing edge or signs of erosion, the trailing edge of the erosion or its signs. Even if the blades have not been confirmed to be generated, corrosion may occur over time. Therefore, the processing step is executed for all the blades including the blades. At this time, it is preferable that the balance of the impeller is adjusted at the same time.

なお、該維持管理方法は、羽根の後縁の近傍に局地的に、前記各後縁から、前記各後縁の下流側に設けられている整流羽根に至るまでの空間における圧力(以下、周囲圧力という。)の平均よりも20%以上(多くの場合は50%以下)程度圧力が高い高圧領域を有するポンプ装置において有効である。その際、ポンプ装置が、羽根の後縁の正圧面側に、負圧となるような、周囲圧力よりも極端に低い低圧領域を有する場合により有効である。
このような条件を有するポンプ装置であれば、羽根車は斜流羽根車や軸流羽根車であってもよいし、遠心羽根車であってもよい。
In the maintenance method, the pressure in the space from each trailing edge to the rectifying vane provided on the downstream side of each trailing edge locally in the vicinity of the trailing edge of the blade (hereinafter referred to as “)”. It is effective in a pump device having a high pressure region where the pressure is about 20% or more (in many cases 50% or less) higher than the average of ambient pressure). At that time, it is more effective when the pump device has a low pressure region extremely lower than the ambient pressure, such as a negative pressure, on the positive pressure surface side of the trailing edge of the blade.
As long as the pump device has such a condition, the impeller may be a mixed flow impeller, an axial flow impeller, or a centrifugal impeller.

さらに、該維持管理方法は、羽根車が、羽根の翼角が変更可能に構成された羽根車であるポンプ装置において有効である。羽根の翼角の変更が設計どおりに行われない不具合が生じた場合に、壊食が発生しやすいからである。なお、壊食が発生しないように設計されている固定翼の羽根車であっても、吸込水位の変動によって、吐出圧力が変化するため、壊食が発生し得る。したがって、該維持管理方法は固定翼の羽根車においても有効である。 Further, the maintenance method is effective in a pump device in which the impeller is an impeller configured so that the blade angle of the blade can be changed. This is because erosion is likely to occur when there is a problem that the blade angle is not changed as designed. Even with a fixed-wing impeller designed to prevent erosion, erosion can occur because the discharge pressure changes due to fluctuations in the suction water level. Therefore, the maintenance method is also effective for a fixed-wing impeller.

さらに、該維持管理方法は、羽根車の羽根が、前縁から後縁にかけて翼長の中腹に最大肉厚となる羽根の断面形状をもつ(すなわち厚みが一定ではない)羽根であるポンプ装置において有効である。 Further, the maintenance method is performed in a pump device in which the blade of the impeller is a blade having a cross-sectional shape (that is, the thickness is not constant) of the blade having the maximum wall thickness in the middle of the blade length from the leading edge to the trailing edge. It is valid.

またさらに、該維持管理方法は、比速度nが概ね500以上、すなわち斜流羽根車や、軸流羽根車を有するポンプ装置において特に有効である。 Furthermore, the maintenance method is particularly effective in a pump device having a specific speed ns of about 500 or more, that is, a mixed flow impeller or an axial flow impeller.

本発明においては、前記確認工程は、前記各羽根のうちいずれの羽根の後縁にも壊食の発生が確認されない場合であっても、前記いずれかの羽根の正圧面に、該ポンプ装置の運転中にキャビテーションが発生している又は発生していたことが確認された場合は、前記羽根車に流体解析を実施する流体解析工程を有し、前記流体解析工程の結果、前記各羽根のうち少なくともいずれかの羽根の後縁の正圧面側に低圧領域が発生し、かつ前記後縁の近傍に局所的な高圧領域が発生することが確認され、前記低圧領域の圧力と前記高圧領域の圧力との圧力差が所定の閾値を越えている場合に、前記後縁に壊食の兆候が発生していると判断すると好適である。 In the present invention, in the confirmation step, even if cavitation is not confirmed on the trailing edge of any of the blades, the pump device is placed on the positive pressure surface of any of the blades. When it is confirmed that cavitation has occurred or has occurred during operation, the impeller has a fluid analysis step of performing fluid analysis, and as a result of the fluid analysis step, among the blades, It was confirmed that a low pressure region was generated on the positive pressure surface side of the trailing edge of at least one of the blades, and a local high pressure region was generated in the vicinity of the trailing edge. When the pressure difference between the two and the above exceeds a predetermined threshold value, it is preferable to determine that a sign of cavitation has occurred at the trailing edge.

羽根の後縁に壊食が発生していなくても、いずれかの羽根の正圧面に、例えば、該ポンプ装置の運転中にキャビテーションの発生が直接確認された場合や、塗装の傷や剥がれ等の、該ポンプ装置の運転中にキャビテーションが発生していた痕跡が確認された場合は流体解析工程を実行する。流体解析工程によって、後縁の正圧面側に低圧領域が発生し、後縁の近傍に局所的な高圧領域が発生することが確認され、低圧領域の圧力と高圧領域の圧力との圧力差が所定の閾値を越えている場合は、後縁において壊食又はその兆候の発生が確認できていない羽根であっても経時的に壊食が発生する虞があるため、該羽根を含む全ての羽根に対して予め加工工程を実行するのである。これによって、羽根の後縁における壊食を抑制することができる。なお、所定の閾値は、ポンプ装置の設計に応じて個別に定まる値である。 Even if the trailing edge of the blade is not eroded, cavitation is directly confirmed on the positive pressure surface of any of the blades, for example, during the operation of the pump device, or the paint is scratched or peeled off. If traces of cavitation occurring during the operation of the pump device are confirmed, the fluid analysis step is executed. By the fluid analysis process, it was confirmed that a low pressure region was generated on the positive pressure surface side of the trailing edge and a local high pressure region was generated near the trailing edge, and the pressure difference between the pressure in the low pressure region and the pressure in the high pressure region was large. If the predetermined threshold is exceeded, erosion may occur over time even if the blades have not been confirmed to have erosion or signs of erosion at the trailing edge. Therefore, all the blades including the blades. The processing process is executed in advance. This makes it possible to suppress erosion at the trailing edge of the blade. The predetermined threshold value is a value individually determined according to the design of the pump device.

本発明においては、前記加工工程において前記後縁の負圧面側を前記各羽根の前縁へ向けて削る場合は、前記羽根車の回転軸に対して内側より外側ほど、前記前縁に向けて加工範囲が広まるように加工すると好適である。 In the present invention, when the negative pressure surface side of the trailing edge is shaved toward the leading edge of each blade in the processing step, the direction from the inside to the outside of the rotation axis of the impeller is toward the leading edge. It is preferable to process so that the processing range is widened.

発明者らの鋭意研究の結果、羽根車の回転軸に対して内側より外側ほど壊食が発生しやすいことが判明した。上述の構成によると、壊食が発生しやすい箇所に対して、より効果的に壊食を抑制することができる。 As a result of diligent research by the inventors, it was found that erosion is more likely to occur from the inside to the outside with respect to the axis of rotation of the impeller. According to the above configuration, it is possible to more effectively suppress erosion in a portion where erosion is likely to occur.

本発明においては、前記加工工程において前記後縁を丸めるように削る場合は、前記羽根車の回転軸に対して内側より外側ほど、前記後縁が前記前縁に近づくように加工すると好適である。 In the present invention, when the trailing edge is rounded in the machining step, it is preferable to process the trailing edge so that the trailing edge is closer to the leading edge than the inside to the rotation axis of the impeller. ..

発明者らの鋭意研究の結果、羽根車の回転軸に対して内側より外側ほど壊食が発生しやすいことが判明した。上述の構成によると、壊食が発生しやすい箇所に対して、より効果的に壊食を抑制することができる。 As a result of diligent research by the inventors, it was found that erosion is more likely to occur from the inside to the outside with respect to the axis of rotation of the impeller. According to the above configuration, it is possible to more effectively suppress erosion in a portion where erosion is likely to occur.

上述の目的を達成するための、本発明に係るポンプ装置の設計方法の特徴構成は、複数の羽根を有する羽根車が備えられたポンプ装置の設計方法であって、所定の形状に形成された前記羽根車に対して、流体解析を実施する流体解析工程と、前記流体解析工程において、前記各羽根のうち少なくともいずれかの羽根の後縁の正圧面側に低圧領域が発生し、かつ前記後縁の近傍に局所的な高圧領域が発生することが確認され、前記低圧領域の圧力と前記高圧領域の圧力との圧力差が所定の閾値を越えている場合に、前記各羽根の各後縁が前記各羽根の前縁及び正圧面へ向けて近づき、これにより前記各羽根の負圧面に凸形状が形成されるように、前記各羽根の負圧面の形状を変更する、又は前記各後縁が丸まるように形状を変更する調整工程とを有する点にある。 The characteristic configuration of the design method of the pump device according to the present invention for achieving the above-mentioned object is the design method of the pump device provided with the impeller having a plurality of blades, and is formed in a predetermined shape. In the fluid analysis step of performing the fluid analysis on the impeller and the fluid analysis step, a low pressure region is generated on the positive pressure surface side of the trailing edge of at least one of the blades, and the rear It is confirmed that a local high pressure region is generated in the vicinity of the edge, and when the pressure difference between the pressure in the low pressure region and the pressure in the high pressure region exceeds a predetermined threshold value, each trailing edge of each blade. Approaches the leading edge and the positive pressure surface of each of the blades, thereby changing the shape of the negative pressure surface of each of the blades so that a convex shape is formed on the negative pressure surface of each of the blades, or each of the above. The point is that it has an adjustment step of changing the shape so that the trailing edge is rounded.

ポンプ装置において、ポンプ効率と、吸込性能の改善を両立させ、全体的にコンパクト化を図ると、羽根車の羽根の翼面の単位面積当たりの負荷を小さくする設計になる。このとき羽根は三次元的に大きく捩じれ、かつ、後縁は羽根の断面視において尖鋭化した形状となる。このときの形状を所定の形状という。 In the pump device, if both pump efficiency and improvement of suction performance are achieved and the overall compactness is achieved, the load per unit area of the blade surface of the impeller will be reduced. At this time, the blade is greatly twisted three-dimensionally, and the trailing edge has a sharpened shape in the cross-sectional view of the blade. The shape at this time is called a predetermined shape.

このような所定の形状に形成された羽根車は、後縁の正圧面側に低圧領域が発生しやすく、キャビテーションによって発生した気泡が、尖鋭化した後縁の近傍の高圧領域において崩壊すると後縁が壊食されやすい。そこで、ポンプ装置の製造時に流体解析工程を実行し、羽根の後縁の正圧面側に低圧領域が発生し、かつ前記後縁の近傍に局所的な高圧領域が発生することが確認されたら、調整工程を実行するのである。 An impeller formed in such a predetermined shape tends to generate a low pressure region on the positive pressure surface side of the trailing edge, and when the bubbles generated by cavitation collapse in the high pressure region near the sharpened trailing edge, the trailing edge Is easily eroded. Therefore, if a fluid analysis step is executed during the manufacturing of the pump device and it is confirmed that a low pressure region is generated on the positive pressure surface side of the trailing edge of the blade and a local high pressure region is generated in the vicinity of the trailing edge. The adjustment process is carried out.

発明者らの鋭意研究の結果、調整工程によって、羽根の後縁の負圧面の形状を変更することによって、羽根の後縁の正圧面側の低圧領域の圧力を、削り加工前に比べて上昇させることができることが判明した。これにより、羽根の後縁の正圧面側の低圧領域の圧力と羽根の後縁の近傍の高圧領域の圧力との圧力差は小さくなる。したがって、キャビテーション自体が発生しづらく、仮にキャビテーションによって気泡が発生したとしてもその崩壊が発生しづらい状態となる。これによって壊食が抑制され、羽根車の性能低下が改善する。 As a result of diligent research by the inventors, the pressure in the low pressure region on the positive pressure surface side of the trailing edge of the blade is increased by changing the shape of the negative pressure surface of the trailing edge of the blade by the adjustment process. It turned out that it could be done. As a result, the pressure difference between the pressure in the low pressure region on the positive pressure surface side of the trailing edge of the blade and the pressure in the high pressure region near the trailing edge of the blade becomes small. Therefore, cavitation itself is unlikely to occur, and even if bubbles are generated by cavitation, their collapse is unlikely to occur. As a result, erosion is suppressed and the performance deterioration of the impeller is improved.

本発明においては、前記調整工程において前記後縁が前記各羽根の前縁及び正圧面へ向けて近づき、これにより前記各羽根の負圧面に凸形状が形成されるように、前記各羽根の負圧面の形状を変更する場合は、前記後縁と負圧面の前記凸形状とにより画定された範囲が、前記羽根車の回転軸に対して内側より外側ほど広がるように変更する点にある。 In the present invention, the blades are arranged so that the trailing edge approaches the leading edge and the positive pressure surface of the blades in the adjustment step, whereby a convex shape is formed on the negative pressure surface of the blades . When changing the shape of the negative pressure surface, the range defined by the trailing edge and the convex shape of the negative pressure surface is changed so as to extend from the inside to the outside with respect to the rotation axis of the impeller. At the point.

発明者らの鋭意研究の結果、羽根車の回転軸に対して内側より外側ほど壊食が発生しやすいことが判明した。上述の構成によると、壊食が発生しやすい箇所に対して、より効果的に壊食を抑制することができる。 As a result of diligent research by the inventors, it was found that erosion is more likely to occur from the inside to the outside with respect to the axis of rotation of the impeller. According to the above configuration, it is possible to more effectively suppress erosion in a portion where erosion is likely to occur.

本発明においては、前記調整工程において前記後縁が丸まるように形状を変更する場合は、前記羽根車の回転軸に対して内側より外側ほど、前記後縁が前記前縁に近づくように変更すると好適である。 In the present invention, when the shape is changed so that the trailing edge is rounded in the adjusting step, the trailing edge is changed so as to be closer to the leading edge than the inside with respect to the rotation axis of the impeller. Suitable.

発明者らの鋭意研究の結果、羽根車の回転軸に対して内側より外側ほど壊食が発生しやすいことが判明した。上述の構成によると、壊食が発生しやすい箇所に対して、より効果的に壊食を抑制することができる。 As a result of diligent research by the inventors, it was found that erosion is more likely to occur from the inside to the outside with respect to the axis of rotation of the impeller. According to the above configuration, it is possible to more effectively suppress erosion in a portion where erosion is likely to occur.

上述の目的を達成するための、本発明に係るポンプ装置の特徴構成は、複数の羽根を有する斜流羽根車と、前記斜流羽根車に接続された立軸の回転軸とが備えられたポンプ装置であって、前記羽根は、該羽根の流体搬送方向に直交する断面が、正圧面において凸形状であり、負圧面において凹形状であるとともに、該羽根の後縁近傍の負圧面において凸形状を有し、負圧面の前記凸形状は、前記斜流羽根車を回転させた際の前記羽根の回転範囲の外周面と重なり、正圧面と連続する面である回転外周面を負圧面に投影したときに生じる投影面を超えて該羽根の前縁側に位置する点にある。 A characteristic configuration of the pump device according to the present invention for achieving the above object is a pump provided with a mixed flow impeller having a plurality of blades and a rotating shaft of a vertical shaft connected to the mixed flow impeller. The blade is a device, and the cross section orthogonal to the fluid transport direction of the blade has a convex shape on a positive pressure surface, a concave shape on a negative pressure surface, and a convex shape on a negative pressure surface near the trailing edge of the blade. The convex shape of the negative pressure surface overlaps with the outer peripheral surface of the rotation range of the blade when the oblique flow impeller is rotated, and the rotation outer peripheral surface which is a surface continuous with the positive pressure surface is projected onto the negative pressure surface. It is located at a point located on the front edge side of the blade beyond the projection plane generated at the time of rotation .

通常、ポンプ装置において、ポンプ効率と、吸込性能の改善を両立させ、全体的にコンパクト化を図ると、羽根車の羽根の翼面の単位面積当たりの負荷を小さくする設計になる。このとき羽根は三次元的に大きく捩じれ、かつ、後縁は羽根の断面視において尖鋭化した形状となる。 Normally, in a pump device, if both pump efficiency and improvement of suction performance are achieved and the overall size is reduced, the design is such that the load per unit area of the blade surface of the impeller is reduced. At this time, the blade is greatly twisted three-dimensionally, and the trailing edge has a sharpened shape in the cross-sectional view of the blade.

このような形状の羽根車は、後縁の正圧面側に低圧領域が発生しやすく、キャビテーションによって発生した気泡が、尖鋭化した後縁の近傍の高圧領域において崩壊すると後縁が壊食されやすい。 An impeller having such a shape tends to generate a low pressure region on the positive pressure surface side of the trailing edge, and when bubbles generated by cavitation collapse in the high pressure region near the sharpened trailing edge, the trailing edge is likely to be eroded. ..

発明者らの鋭意研究の結果、羽根を、該羽根の流体搬送方向に直交する断面が、正圧面において凸形状であり、負圧面において凹形状であるとともに、該羽根の後縁近傍の負圧面において凸形状を有し、負圧面の前記凸形状が、前記斜流羽根車を回転させた際の前記羽根の回転範囲の外周面と重なり、正圧面と連続する面である回転外周面を負圧面に投影したときに生じる投影面を超えて該羽根の前縁側に位置するように構成すると、羽根の後縁の正圧面側の低圧領域の圧力が、後縁の負圧面において凸形状を有していない羽根に比べて高くなることが判明した。 As a result of diligent research by the inventors, the cross section of the blade orthogonal to the fluid transport direction of the blade is convex on the positive pressure surface and concave on the negative pressure surface, and the negative pressure surface near the trailing edge of the blade. The convex shape of the negative pressure surface overlaps with the outer peripheral surface of the rotation range of the blade when the oblique flow impeller is rotated, and the rotation outer peripheral surface which is a surface continuous with the positive pressure surface is negative. When configured to be located on the front edge side of the blade beyond the projection surface generated when projected onto the pressure surface, the pressure in the low pressure region on the positive pressure surface side of the trailing edge of the blade has a convex shape on the negative pressure surface of the trailing edge. It turned out to be higher than the blades that did not.

このような羽根は、羽根の後縁の正圧面側の低圧領域の圧力と羽根の後縁の近傍の高圧領域の圧力との圧力差は小さくなる。したがって、キャビテーション自体が発生しづらく、仮にキャビテーションによって気泡が発生したとしてもその崩壊が発生しづらい状態となる。これによって壊食が抑制され、羽根車の性能低下が改善する。 In such a blade, the pressure difference between the pressure in the low pressure region on the positive pressure surface side of the trailing edge of the blade and the pressure in the high pressure region near the trailing edge of the blade becomes small. Therefore, cavitation itself is unlikely to occur, and even if bubbles are generated by cavitation, their collapse is unlikely to occur. As a result, erosion is suppressed and the performance deterioration of the impeller is improved.

本発明においては、前記後縁と負圧面の前記凸形状とにより画定された範囲が、前記斜流羽根車の回転軸に対して内側より外側ほど広がるような形状を有する点にある。 In the present invention, the range defined by the convex shape of the trailing edge and the negative pressure surface has a shape that extends from the inside to the outside with respect to the rotation axis of the mixed flow impeller. ..

発明者らの鋭意研究の結果、羽根車の回転軸に対して内側より外側ほど壊食が発生しやすいことが判明した。上述の構成によると、壊食が発生しやすい箇所に対して、より効果的に壊食を抑制することができる。 As a result of diligent research by the inventors, it was found that erosion is more likely to occur from the inside to the outside with respect to the axis of rotation of the impeller. According to the above configuration, it is possible to more effectively suppress erosion in a portion where erosion is likely to occur.

本発明においては、前記後縁は、前記斜流羽根車の回転軸に対して内側より外側ほど、前記後縁が該羽根の前縁に近づくように丸められた形状を有すると好適である。 In the present invention, it is preferable that the trailing edge has a shape rounded so that the trailing edge approaches the leading edge of the blade toward the outside from the inside with respect to the rotation axis of the oblique impeller.

発明者らの鋭意研究の結果、羽根車の回転軸に対して内側より外側ほど壊食が発生しやすいことが判明した。上述の構成によると、壊食が発生しやすい箇所に対して、より効果的に壊食を抑制することができる。 As a result of diligent research by the inventors, it was found that erosion is more likely to occur from the inside to the outside with respect to the axis of rotation of the impeller. According to the above configuration, it is possible to more effectively suppress erosion in a portion where erosion is likely to occur.

ポンプ装置の概略図Schematic diagram of the pump device 羽根車の正面図Front view of impeller 羽根の断面図Cross section of the blade 羽根の断面図Cross section of the blade 解析に基づいた羽根まわりにおける圧力領域の説明図Explanatory drawing of the pressure region around the blade based on the analysis 解析に基づいた羽根まわりにおける圧力領域の説明図Explanatory drawing of the pressure region around the blade based on the analysis

以下、本発明の実施形態に係るポンプ装置の維持管理方法、設計方法及びポンプ装置を図面を参照しながら説明する。 Hereinafter, the maintenance method, the design method, and the pump device according to the embodiment of the present invention will be described with reference to the drawings.

図1には、ポンプ装置10が示されている。ポンプ装置10は、ケーシング11内において回転自在に配設された立軸の回転軸12と、回転軸12の下端部に設けられ回転軸12と一体回転する斜流羽根車13と、ケーシング11の上側に連設された揚水管14と、揚水管14の上側に連結された吐出曲管15と、ケーシング11の下側に連設された吸込ケーシング16と、を備えている。なお、吐出曲管15の下流側に吐出管17が連設される。 FIG. 1 shows the pump device 10. The pump device 10 includes a rotary shaft 12 of a vertical shaft rotatably arranged in the casing 11, a mixed flow impeller 13 provided at the lower end of the rotary shaft 12 and rotating integrally with the rotary shaft 12, and an upper side of the casing 11. A pumping pipe 14 connected to the above, a discharge curved pipe 15 connected to the upper side of the pumping pipe 14, and a suction casing 16 connected to the lower side of the casing 11 are provided. The discharge pipe 17 is continuously provided on the downstream side of the discharge curved pipe 15.

ケーシング11には、斜流羽根車13の下流側に整流羽根18が備えられている。整流羽根18は、斜流羽根車13から吐出した流体を軸方向に整流してスムーズに揚水管14に導くために設けられている。 The casing 11 is provided with a rectifying blade 18 on the downstream side of the mixed flow impeller 13. The rectifying blade 18 is provided to rectify the fluid discharged from the mixed flow impeller 13 in the axial direction and smoothly guide the fluid to the pumping pipe 14.

吐出曲管15の上部にはモータ30が設けられ、回転軸12とモータ30の出力軸31とがカップリング29を介して連結されている。 A motor 30 is provided on the upper portion of the discharge curved pipe 15, and the rotary shaft 12 and the output shaft 31 of the motor 30 are connected via a coupling 29.

図2に示すように、斜流羽根車13は、回転軸12に固定的に支持されるボス部32と、ボス部32の周囲に固定的に配置された4枚の羽根33を備えている。なお、羽根33の枚数は例示である。ボス部32や羽根33は、ステンレス鋼やねずみ鋳鉄等の、流体に対して強度と耐食性のある材質から形成されている。 As shown in FIG. 2, the mixed flow impeller 13 includes a boss portion 32 fixedly supported by the rotating shaft 12 and four blades 33 fixedly arranged around the boss portion 32. .. The number of blades 33 is an example. The boss portion 32 and the blade 33 are made of a material having strength and corrosion resistance against a fluid, such as stainless steel and gray cast iron.

羽根33は、羽根33の流体搬送方向に直交する断面が、正圧面33cにおいて凸形状であり、負圧面33dにおいて凹形状であり、前縁33aから後縁33bにかけて翼長の中腹に最大肉厚となる羽根の断面形状をもった(すなわち厚みが一定ではない)形状を有する。 The blade 33 has a cross section orthogonal to the fluid transport direction of the blade 33 having a convex shape on the positive pressure surface 33c and a concave shape on the negative pressure surface 33d, and has a maximum wall thickness in the middle of the blade length from the leading edge 33a to the trailing edge 33b. It has a shape having a cross-sectional shape of a blade (that is, the thickness is not constant).

ポンプ装置10は、羽根33の後縁33bの近傍に局地的に、各後縁33bから、各後縁33bの下流側に設けられている整流羽根18に至るまでの空間における圧力(以下、周囲圧力という。)の平均よりも20%以上(多くの場合は50%以下)程度圧力が高い高圧領域HPを有し、羽根33の後縁33bの正圧面33c側に、負圧となるような、周囲圧力よりも極端に低い低圧領域LPを有する状態となる場合がある(図5参照)。 The pump device 10 is a pressure in the space from each trailing edge 33b to the straightening vane 18 provided on the downstream side of each trailing edge 33b locally in the vicinity of the trailing edge 33b of the blade 33 (hereinafter referred to as “)”. It has a high pressure region HP whose pressure is about 20% or more (in many cases 50% or less) higher than the average of ambient pressure), and negative pressure is applied to the positive pressure surface 33c side of the trailing edge 33b of the blade 33. In addition, it may be in a state of having a low pressure region LP extremely lower than the ambient pressure (see FIG. 5).

その場合、ポンプ装置10は、羽根33に壊食が発生しにくいように設計されているものの、例えば吸込水位の変動によって、吸込圧力が変化するため、羽根33のまわりの圧力状態が許容以上に低下し、これによってキャビテーションが発生し易くなり、羽根33の特に後縁33bにキャビテーションによる壊食が発生する虞がある。 In that case, although the pump device 10 is designed so that cavitation does not easily occur in the blade 33, for example, the suction pressure changes due to the fluctuation of the suction water level, so that the pressure state around the blade 33 becomes more than acceptable. It is lowered, which makes it easy for cavitation to occur, and there is a possibility that cavitation-induced erosion may occur especially on the trailing edge 33b of the blade 33.

羽根33の後縁33bに壊食が発生するとポンプ装置10の性能が大きく低下するため、一定期間ごとの例えば1年ごとの保守点検時に、本発明に係る維持管理方法が実行される。 If the trailing edge 33b of the blade 33 is eroded, the performance of the pump device 10 is significantly deteriorated. Therefore, the maintenance method according to the present invention is executed at regular intervals, for example, annual maintenance and inspection.

維持管理方法は、4枚の羽根33のうち少なくともいずれかの羽根33の後縁33bに壊食又は壊食の兆候が発生しているか否かを確認する確認工程と、確認工程において、羽根33の後縁33bにおいて実際に壊食が発生している場合、又は、後縁33bに壊食の発生が確認されない場合であってもその兆候が発生していることが確認された場合に、4枚の羽根の各後縁33bを削る加工工程とを有する。 The maintenance method includes a confirmation step of confirming whether or not a sign of erosion or erosion has occurred on the trailing edge 33b of at least one of the four blades 33, and the blade 33 in the confirmation step. 4 When it is confirmed that erosion is actually occurring at the trailing edge 33b, or even if the occurrence of erosion is not confirmed at the trailing edge 33b, it is confirmed that the sign is occurring. It has a processing step of scraping each trailing edge 33b of a single blade.

さらに、維持管理方法は、4枚の羽根33のうちいずれの羽根33の後縁33bにも壊食の発生が確認されない場合であっても、いずれかの羽根33の正圧面33cに、該ポンプ装置10の運転中にキャビテーションが発生していることが目視等によって直接確認された場合や、塗装の傷や剥がれ等の、該ポンプ装置10の運転中にキャビテーションが発生していた痕跡が確認された場合は、斜流羽根車13に流体解析を実施する流体解析工程を有する。 Further, in the maintenance method, even if cavitation is not confirmed on the trailing edge 33b of any of the four blades 33, the pump is applied to the positive pressure surface 33c of any of the blades 33. When it was directly confirmed visually or the like that cavitation had occurred during the operation of the device 10, or there were traces of cavitation occurring during the operation of the pump device 10, such as scratches or peeling of the paint, were confirmed. If so, the mixed flow impeller 13 has a fluid analysis step of performing the fluid analysis.

流体解析工程の結果、4枚の羽根33のうち少なくともいずれかの羽根33の後縁33bの正圧面33c側に低圧領域が発生し、かつ後縁33bの近傍に局所的な高圧領域が発生することが確認され、低圧領域LP(図5参照)の圧力と高圧領域HP(図5参照)の圧力との圧力差が所定の閾値を越えている場合に、後縁33bに壊食の兆候が発生していると判断する。なお、所定の閾値は、ポンプ装置10の設計に応じて個別に定まる値である。 As a result of the fluid analysis step, a low pressure region is generated on the positive pressure surface 33c side of the trailing edge 33b of at least one of the four blades 33, and a local high pressure region is generated in the vicinity of the trailing edge 33b. It was confirmed that when the pressure difference between the pressure in the low pressure region LP (see FIG. 5) and the pressure in the high pressure region HP (see FIG. 5) exceeds a predetermined threshold, there is a sign of erosion on the trailing edge 33b. Judge that it has occurred. The predetermined threshold value is a value individually determined according to the design of the pump device 10.

図3に示すように、4枚の羽根33のうち少なくともいずれかの羽根33の後縁33bに壊食が発生しているか、壊食の兆候が発生していることが確認された場合に、後縁33bにおいて壊食又はその兆候の発生が確認できていない羽根33であっても経時的に壊食が発生する虞があるため、該羽根33を含む全ての羽根33に対して加工工程が実行される。図3において、加工前の羽根33の輪郭が二点鎖線で表され、加工後の羽根33の輪郭が実線で表される。これによって、全ての羽根33の後縁33bにおける壊食を抑制することができる。なお、加工工程において、斜流羽根車13のバランス調整が同時に行われる。 As shown in FIG. 3, when it is confirmed that erosion has occurred or a sign of erosion has occurred on the trailing edge 33b of at least one of the four blades 33. Even if the blade 33 for which the occurrence of erosion or its sign has not been confirmed at the trailing edge 33b, erosion may occur over time. Therefore, the processing step is performed on all the blades 33 including the blade 33. Will be executed. In FIG. 3, the contour of the blade 33 before processing is represented by a two-dot chain line, and the contour of the blade 33 after processing is represented by a solid line. This makes it possible to suppress erosion at the trailing edges 33b of all the blades 33. In the processing process, the balance of the mixed flow impeller 13 is adjusted at the same time.

加工工程においては、性能変化(HQ、効率、キャビテーション)に悪影響の出ない範囲、すなわち正圧面33cを削らない回転外周面33eの範囲において、4枚の羽根の各後縁33bの負圧面33d側を各羽根33の前縁33aへ向けて削る。なお、回転外周面33eは、羽根車13を回転させた際の羽根33の回転範囲の外周面と重なり、正圧面33cと羽根33の前縁33a側で連続する面であり、羽根車13の設計時には考慮しない領域である。 In the processing process, in the range where the performance change (HQ, efficiency, cavitation) is not adversely affected, that is, in the range of the rotating outer peripheral surface 33e where the positive pressure surface 33c is not cut, the negative pressure surface 33d side of each trailing edge 33b of the four blades. Is scraped toward the leading edge 33a of each blade 33. The rotation outer peripheral surface 33e overlaps with the outer peripheral surface of the rotation range of the blade 33 when the impeller 13 is rotated, and is a continuous surface between the positive pressure surface 33c and the leading edge 33a side of the blade 33. This is an area that is not considered when designing.

具体的には、後縁33bの近傍の羽根33の厚みに対して、数倍、例えば3倍くらいの奥行きの範囲内において削る。その際、斜流羽根車13の回転軸に対して内側より外側ほど、前縁33a側へと加工範囲が広まるように加工する(図2において、加工前の羽根33の輪郭が実線で表され、加工後の羽根33の輪郭が一点鎖線で表される。)。これにより、4枚の羽根33の各後縁33bの負圧面33dにおいて、各羽根33の前縁33aへ向けて削られたような凸形状となる。 Specifically, it is cut within a depth range of several times, for example, about 3 times the thickness of the blade 33 in the vicinity of the trailing edge 33b. At that time, processing is performed so that the processing range is widened toward the leading edge 33a side from the inside to the outside with respect to the rotation axis of the mixed flow impeller 13 (in FIG. 2, the contour of the blade 33 before processing is represented by a solid line. , The contour of the blade 33 after processing is represented by a alternate long and short dash line.) As a result, the negative pressure surface 33d of each trailing edge 33b of the four blades 33 has a convex shape as if it were shaved toward the leading edge 33a of each blade 33.

加工工程によって、羽根33の後縁33bの負圧面33dの形状を変更することによって、羽根33の後縁33bの正圧面33c側の低圧領域LP(図6参照)の圧力を、削り加工前に比べて上昇させることができる。 By changing the shape of the negative pressure surface 33d of the trailing edge 33b of the blade 33 by the machining process, the pressure in the low pressure region LP (see FIG. 6) on the positive pressure surface 33c side of the trailing edge 33b of the blade 33 is reduced before the machining. Can be raised in comparison.

これにより、羽根33の後縁33bの正圧面33c側の低圧領域LP(図6参照)の圧力と羽根33の後縁33bの近傍の高圧領域HP(図6参照)の圧力との圧力差は小さくなる。したがって、キャビテーション自体が発生しづらく、仮にキャビテーションによって気泡が発生したとしてもその崩壊が発生しづらい状態となる。これによって新たな壊食が抑制され、斜流羽根車13の性能低下が改善する。 As a result, the pressure difference between the pressure in the low pressure region LP (see FIG. 6) on the positive pressure surface 33c side of the trailing edge 33b of the blade 33 and the pressure in the high pressure region HP (see FIG. 6) near the trailing edge 33b of the blade 33 is reduced. It gets smaller. Therefore, cavitation itself is unlikely to occur, and even if bubbles are generated by cavitation, their collapse is unlikely to occur. As a result, new erosion is suppressed, and the performance deterioration of the mixed flow impeller 13 is improved.

なお、図5には、後縁33bの負圧面33d側が加工される前の羽根33が示されている。解析によると、後縁33bの正圧面33cの低圧領域LPと、羽根33の後縁33bの近傍の局地的な高圧領域HPとの圧力差がポンプ全揚程の約1.7倍である。このように、圧力差が高い場合は、キャビテーションによる壊食が発生する虞が高い。 Note that FIG. 5 shows the blade 33 before the negative pressure surface 33d side of the trailing edge 33b is machined. According to the analysis, the pressure difference between the low pressure region LP of the positive pressure surface 33c of the trailing edge 33b and the local high pressure region HP in the vicinity of the trailing edge 33b of the blade 33 is about 1.7 times the total head of the pump. As described above, when the pressure difference is high, there is a high possibility that cavitation-induced erosion will occur.

図6に、羽根33に対して、維持管理方法が実行されたあとの、すなわち後縁33bの負圧面33d側が加工されたあとの羽根33が示されている。解析によると、維持管理方法を実行したあとの、斜流羽根車13は、前記圧力差がポンプ全揚程の約0.5倍まで低下した。そして、このような加工後の羽根33において、後縁33bの壊食が発生しないことが確認された。 FIG. 6 shows the blade 33 after the maintenance method has been executed for the blade 33, that is, after the negative pressure surface 33d side of the trailing edge 33b has been machined. According to the analysis, after executing the maintenance method, the pressure difference of the mixed flow impeller 13 decreased to about 0.5 times the total head of the pump. Then, it was confirmed that the trailing edge 33b did not corrode in the blade 33 after such processing.

なお、上述の説明においては、維持管理方法の加工工程において、羽根33の各後縁33bの負圧面33d側を各羽根33の前縁33aへ向けて削る場合について説明したが、これに限らない。加工工程においては、性能変化(HQ、効率、キャビテーション)に悪影響の出ない範囲において、すなわち正圧面33cを削らない回転外周面33eの範囲において、各後縁33bを丸めるように削ってもよい。 In the above description, in the processing step of the maintenance method, the case where the negative pressure surface 33d side of each trailing edge 33b of the blade 33 is shaved toward the leading edge 33a of each blade 33 has been described, but the present invention is not limited to this. .. In the processing step, each trailing edge 33b may be rounded in a range where the performance change (HQ, efficiency, cavitation) is not adversely affected, that is, in the range of the rotary outer peripheral surface 33e where the positive pressure surface 33c is not cut.

具体的には、図4に示すように、後縁33bを、後縁33bの近傍の羽根33の厚みを直径とする半円状に削る。図4において、加工前の羽根33の輪郭が二点鎖線で表され、加工後の羽根33の輪郭が実線で表される。その際、斜流羽根車13の回転軸に対して内側より外側ほど、前縁33a側へと近づくように加工する(図2において、加工前の羽根33の輪郭が実線で表され、加工後の羽根33の輪郭が一点鎖線で表される。)。これにより、4枚の羽根33の各後縁33bは丸められ、負圧面33d側において凸形状となる。 Specifically, as shown in FIG. 4, the trailing edge 33b is cut into a semicircle having the thickness of the blade 33 in the vicinity of the trailing edge 33b as the diameter. In FIG. 4, the contour of the blade 33 before processing is represented by a two-dot chain line, and the contour of the blade 33 after processing is represented by a solid line. At that time, the blade 33 is processed so as to be closer to the leading edge 33a side than the inner side with respect to the rotation axis of the mixed flow impeller 13 (in FIG. 2, the contour of the blade 33 before processing is represented by a solid line, and after processing. The contour of the blade 33 is represented by a alternate long and short dash line.) As a result, each trailing edge 33b of the four blades 33 is rounded to form a convex shape on the negative pressure surface 33d side.

本発明に係る維持管理方法は、既存の、斜流羽根車13が備えられたポンプ装置10に対して実行されるものであるが、新規に製造される斜流羽根車、すなわち複数の羽根33を有する斜流羽根車13が備えられたポンプ装置10の設計方法にも応用することができる。 The maintenance method according to the present invention is executed for the existing pump device 10 provided with the mixed flow impeller 13, but a newly manufactured mixed flow impeller, that is, a plurality of blades 33. It can also be applied to the design method of the pump device 10 provided with the mixed flow impeller 13 having the above.

すなわち、該設計方法は、所定の形状に形成された斜流羽根車13に対して、流体解析を実施する流体解析工程と、流体解析工程において、複数の羽根33のうち少なくともいずれかの羽根33の後縁33bの正圧面33c側に低圧領域LPが発生し、かつ後縁33bの近傍に局所的な高圧領域HPが発生することが確認された場合に、複数の羽根33の各後縁33bの負圧面33d側が各羽根33の前縁33aへ向けて近づくように形状を変更する、又は各後縁33bが丸まるように形状を変更する調整工程とを有する。 That is, the design method includes a fluid analysis step of performing a fluid analysis on a mixed flow impeller 13 formed in a predetermined shape, and a blade 33 of at least one of a plurality of blades 33 in the fluid analysis step. When it is confirmed that a low-pressure region LP is generated on the positive pressure surface 33c side of the trailing edge 33b and a local high-pressure region HP is generated in the vicinity of the trailing edge 33b, each trailing edge 33b of the plurality of blades 33 It has an adjustment step of changing the shape so that the negative pressure surface 33d side of the blade 33 approaches the leading edge 33a of each blade 33, or changing the shape so that each trailing edge 33b is rounded.

その際、調整工程において後縁33bの負圧面33d側が各羽根33の前縁33aへ向けて近づくように形状を変更する場合は、羽根車13の回転軸12に対して内側より外側ほど、前縁33aに向けて近づく範囲が広がるように変更するのが好ましく、調整工程において後縁33bが丸まるように形状を変更する場合は、羽根車13の回転軸12に対して内側より外側ほど、後縁33bが前縁33aに近づくように変更するのが好ましい。 At that time, when changing the shape so that the negative pressure surface 33d side of the trailing edge 33b approaches the leading edge 33a of each blade 33 in the adjustment step, the front side of the rotation shaft 12 of the impeller 13 is closer to the outside than the inside. It is preferable to change the shape so that the range closer to the edge 33a is widened, and when the shape is changed so that the trailing edge 33b is rounded in the adjustment step, the trailing edge 33b is rearward from the inside to the outside of the rotating shaft 12 of the impeller 13. It is preferable to change the edge 33b so as to approach the leading edge 33a.

なお、このような設計方法によって製造された斜流羽根車13が備えられたポンプ装置10に対しても、本発明に係る維持管理方法を実行することができる。 The maintenance method according to the present invention can also be executed for the pump device 10 provided with the mixed flow impeller 13 manufactured by such a design method.

また、上述のような設計方法によって製造された斜流羽根車13が備えられたポンプ装置10自体も本発明の範囲にある。すなわち、該ポンプ装置10は、複数の羽根33を有する斜流羽根車13と、斜流羽根車13に接続された立軸の回転軸12とが備えられたポンプ装置10であって、羽根33は、該羽根33の流体搬送方向に直交する断面が、正圧面33cにおいて凸形状であり、負圧面33dにおいて凹形状であるとともに、該羽根33の後縁33bの負圧面33dにおいて凸形状を有する。その際、後縁33bの負圧面33d側が、斜流羽根車13の回転軸12に対して内側より外側ほど、該羽根33の前縁33aに向けて近づく範囲が広まるような形状を有する、又は後縁33bが該羽根33の前縁33aに近づくように丸められた形状を有する。 Further, the pump device 10 itself provided with the mixed flow impeller 13 manufactured by the design method as described above is also within the scope of the present invention. That is, the pump device 10 is a pump device 10 provided with a mixed flow impeller 13 having a plurality of blades 33 and a rotary shaft 12 of a vertical shaft connected to the mixed flow impeller 13, and the blades 33 are. The cross section of the blade 33 orthogonal to the fluid transport direction has a convex shape on the positive pressure surface 33c, a concave shape on the negative pressure surface 33d, and a convex shape on the negative pressure surface 33d of the trailing edge 33b of the blade 33. At that time, the negative pressure surface 33d side of the trailing edge 33b has a shape so that the range closer to the leading edge 33a of the blade 33 becomes wider than the inside to the rotation shaft 12 of the mixed flow impeller 13. The trailing edge 33b has a shape rounded so as to approach the leading edge 33a of the blade 33.

なお、斜流羽根車13に対する流体解析工程に替えて、例えば実験設備に備えられた実験用のポンプ装置10に組み込んで運転してみて、実際のキャビテーションの発生の様子を目視確認するようにしてもよい。ただし、キャビテーションが発生した場合に、必ずしも壊食が発生するとは限らない。 Instead of the fluid analysis process for the mixed flow impeller 13, for example, by incorporating it into the experimental pump device 10 provided in the experimental equipment and operating it, the actual state of cavitation is visually confirmed. May be good. However, when cavitation occurs, erosion does not always occur.

上述した実施形態において、斜流羽根車13の羽根33は、ボス部32に対して固定的に備えられている場合について説明したがこれに限らない。斜流羽根車13は、羽根33の翼角が変更可能に構成されていてもよい。羽根33の翼角の変更が設計どおりに行われない不具合が生じた場合に、壊食が発生しやすいため、本発明に係るポンプ装置の維持管理方法、設計方法及びポンプ装置によれば、そのような壊食を効果的に抑制することができるからである。 In the above-described embodiment, the case where the blade 33 of the mixed flow impeller 13 is fixedly provided with respect to the boss portion 32 has been described, but the present invention is not limited to this. The oblique impeller 13 may be configured such that the blade angle of the blade 33 can be changed. If a defect occurs in which the blade angle of the blade 33 is not changed as designed, erosion is likely to occur. Therefore, according to the maintenance method, design method, and pump device of the pump device according to the present invention. This is because such erosion can be effectively suppressed.

上述した実施形態において、ポンプ装置10に斜流羽根車13が備えられている場合について説明したがこれに限らない。ポンプ装置10は、斜流羽根車13に替えて、軸流羽根車又は遠心羽根車が備えられていてもよい。 In the above-described embodiment, the case where the pump device 10 is provided with the mixed flow impeller 13 has been described, but the present invention is not limited to this. The pump device 10 may be provided with an axial flow impeller or a centrifugal impeller instead of the mixed flow impeller 13.

上述した実施形態は、いずれも本発明の一例であり、該記載により本発明が限定されるものではなく、各部の具体的構成は本発明の作用効果が奏される範囲で適宜変更設計可能である。 The above-described embodiments are all examples of the present invention, and the description thereof does not limit the present invention, and the specific configuration of each part can be appropriately modified and designed within the range in which the effects of the present invention are exhibited. be.

10 :ポンプ装置
12 :回転軸
13 :斜流羽根車(羽根車)
18 :整流羽根
33 :羽根
33a :前縁
33b :後縁
33c :正圧面
33d :負圧面
HP :高圧領域
LP :低圧領域
10: Pump device 12: Rotating shaft 13: Diagonal flow impeller (impeller)
18: Rectifying blade 33: Blade 33a: Leading edge 33b: Trailing edge 33c: Positive pressure surface 33d: Negative pressure surface HP: High pressure region LP: Low pressure region

Claims (9)

複数の羽根を有する羽根車が備えられたポンプ装置の維持管理方法であって、
前記各羽根のうち少なくともいずれかの羽根の後縁に壊食又は壊食の兆候が発生しているか否かを確認する確認工程と、
前記確認工程において、壊食又は壊食の兆候が発生していることが確認された場合に、前記各羽根の各後縁の負圧面側を前記各羽根の前縁へ向けて削る、又は前記各後縁を丸めるように削る加工工程とを有することを特徴とするポンプ装置の維持管理方法。
It is a maintenance method of a pump device equipped with an impeller having multiple blades.
A confirmation step for confirming whether or not erosion or signs of erosion have occurred on the trailing edge of at least one of the blades.
When it is confirmed that erosion or a sign of erosion has occurred in the confirmation step, the negative pressure surface side of each trailing edge of each blade is scraped toward the leading edge of each blade, or the above. A maintenance method for a pump device, which comprises a processing step of shaving each trailing edge so as to be rounded.
前記確認工程は、前記各羽根のうちいずれの羽根の後縁にも壊食の発生が確認されない場合であっても、前記いずれかの羽根の正圧面に、該ポンプ装置の運転中にキャビテーションが発生している又は発生していたことが確認された場合は、前記羽根車に流体解析を実施する流体解析工程を有し、
前記流体解析工程の結果、前記各羽根のうち少なくともいずれかの羽根の後縁の正圧面側に低圧領域が発生し、かつ前記後縁の近傍に局所的な高圧領域が発生することが確認され、前記低圧領域の圧力と前記高圧領域の圧力との圧力差が所定の閾値を越えている場合に、前記後縁に壊食の兆候が発生していると判断する請求項1に記載のポンプ装置の維持管理方法。
In the confirmation step, even if no erosion is confirmed on the trailing edge of any of the blades, cavitation is generated on the positive pressure surface of any of the blades during the operation of the pump device. If it has occurred or has been confirmed to have occurred, the impeller has a fluid analysis step to perform fluid analysis.
As a result of the fluid analysis step, it was confirmed that a low pressure region was generated on the positive pressure surface side of the trailing edge of at least one of the blades, and a local high pressure region was generated in the vicinity of the trailing edge. The pump according to claim 1, wherein when the pressure difference between the pressure in the low pressure region and the pressure in the high pressure region exceeds a predetermined threshold value, it is determined that a sign of erosion has occurred at the trailing edge. Equipment maintenance method.
前記加工工程において前記後縁の負圧面側を前記各羽根の前縁へ向けて削る場合は、前記羽根車の回転軸に対して内側より外側ほど、前記前縁に向けて加工範囲が広まるように加工する請求項1又は2に記載のポンプ装置の維持管理方法。 When the negative pressure surface side of the trailing edge is shaved toward the leading edge of each blade in the machining step, the machining range is widened toward the leading edge from the inside to the outside with respect to the rotation axis of the impeller. The maintenance method of the pump device according to claim 1 or 2. 前記加工工程において前記後縁を丸めるように削る場合は、前記羽根車の回転軸に対して内側より外側ほど、前記後縁が前記前縁に近づくように加工する請求項1又は2に記載のポンプ装置の維持管理方法。 The invention according to claim 1 or 2, wherein when the trailing edge is rounded in the machining step, the trailing edge is machined so as to be closer to the leading edge from the inside to the outside with respect to the rotation axis of the impeller. Maintenance method of pump equipment. 複数の羽根を有する羽根車が備えられたポンプ装置の設計方法であって、
所定の形状に形成された前記羽根車に対して、流体解析を実施する流体解析工程と、
前記流体解析工程において、前記各羽根のうち少なくともいずれかの羽根の後縁の正圧面側に低圧領域が発生し、かつ前記後縁の近傍に局所的な高圧領域が発生することが確認され、前記低圧領域の圧力と前記高圧領域の圧力との圧力差が所定の閾値を越えている場合に、前記各羽根の各後縁が前記各羽根の前縁及び正圧面へ向けて近づき、これにより前記各羽根の負圧面に凸形状が形成されるように、前記各羽根の負圧面の形状を変更する、又は前記各後縁が丸まるように形状を変更する調整工程とを有することを特徴とするポンプ装置の設計方法。
A method of designing a pump device equipped with an impeller with multiple blades.
A fluid analysis step of performing fluid analysis on the impeller formed in a predetermined shape, and
In the fluid analysis step, it was confirmed that a low pressure region was generated on the positive pressure surface side of the trailing edge of at least one of the blades, and a local high pressure region was generated in the vicinity of the trailing edge. When the pressure difference between the pressure in the low pressure region and the pressure in the high pressure region exceeds a predetermined threshold value, each trailing edge of each blade approaches the leading edge and positive pressure surface of each blade. The present invention includes an adjustment step of changing the shape of the negative pressure surface of each blade so that a convex shape is formed on the negative pressure surface of each blade, or changing the shape so that the trailing edge of each blade is rounded. How to design a featured pumping device.
前記調整工程において前記後縁が前記各羽根の前縁及び正圧面へ向けて近づき、これにより前記各羽根の負圧面に凸形状が形成されるように、前記各羽根の負圧面の形状を変更する場合は、前記後縁と負圧面の前記凸形状とにより画定された範囲が、前記羽根車の回転軸に対して内側より外側ほど広がるように変更する請求項5に記載のポンプ装置の設計方法。 The shape of the negative pressure surface of each blade so that the trailing edge approaches the leading edge and the positive pressure surface of each blade in the adjustment step, whereby a convex shape is formed on the negative pressure surface of each blade. 5. The fifth aspect of the present invention is to change the range defined by the trailing edge and the convex shape of the negative pressure surface so as to extend from the inside to the outside with respect to the rotation axis of the impeller. How to design a pumping device. 前記調整工程において前記後縁が丸まるように形状を変更する場合は、前記羽根車の回転軸に対して内側より外側ほど、前記後縁が前記前縁に近づくように変更する請求項5に記載のポンプ装置の設計方法。 The fifth aspect of claim 5 is that when the shape is changed so that the trailing edge is rounded in the adjusting step, the trailing edge is changed so as to be closer to the leading edge than the inside to the rotation axis of the impeller. How to design a pumping device. 複数の羽根を有する斜流羽根車と、前記斜流羽根車に接続された立軸の回転軸とが備えられたポンプ装置であって、
前記羽根は、該羽根の流体搬送方向に直交する断面が、正圧面において凸形状であり、負圧面において凹形状であるとともに、該羽根の後縁近傍の負圧面において凸形状を有し、
負圧面の前記凸形状は、前記斜流羽根車を回転させた際の前記羽根の回転範囲の外周面と重なり、正圧面と連続する面である回転外周面を負圧面に投影したときに生じる投影面を超えて該羽根の前縁側に位置することを特徴とするポンプ装置。
A pump device provided with a mixed flow impeller having a plurality of blades and a rotating shaft of a vertical shaft connected to the mixed flow impeller.
The blade has a cross section orthogonal to the fluid transport direction of the blade having a convex shape on the positive pressure surface, a concave shape on the negative pressure surface, and a convex shape on the negative pressure surface near the trailing edge of the blade .
The convex shape of the negative pressure surface overlaps with the outer peripheral surface of the rotation range of the blade when the oblique flow impeller is rotated, and occurs when the rotation outer peripheral surface which is a surface continuous with the positive pressure surface is projected onto the negative pressure surface. A pump device characterized by being located on the front edge side of the blade beyond the projection plane .
前記後縁と負圧面の前記凸形状とにより画定された範囲が、前記斜流羽根車の回転軸に対して内側より外側ほど広がるような形状を有する請求項8に記載のポンプ装置。 The pump device according to claim 8, wherein the range defined by the convex shape of the trailing edge and the negative pressure surface has a shape that extends from the inside to the outside with respect to the rotation axis of the mixed flow impeller. ..
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Citations (2)

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Publication number Priority date Publication date Assignee Title
JP2003083284A (en) 2001-09-12 2003-03-19 Mitsubishi Heavy Ind Ltd Pump
JP2013249804A (en) 2012-06-01 2013-12-12 Ebara Corp Erosion prediction method, erosion prediction system, erosion characteristics database used in this prediction, and method for constructing the same

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JP3353668B2 (en) * 1997-10-15 2002-12-03 株式会社日立製作所 Erosion prediction method for hydraulic machinery

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003083284A (en) 2001-09-12 2003-03-19 Mitsubishi Heavy Ind Ltd Pump
JP2013249804A (en) 2012-06-01 2013-12-12 Ebara Corp Erosion prediction method, erosion prediction system, erosion characteristics database used in this prediction, and method for constructing the same

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