EP4396456B1 - Bucket of a pelton turbine and method for production - Google Patents

Bucket of a pelton turbine and method for production Download PDF

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Publication number
EP4396456B1
EP4396456B1 EP22730477.1A EP22730477A EP4396456B1 EP 4396456 B1 EP4396456 B1 EP 4396456B1 EP 22730477 A EP22730477 A EP 22730477A EP 4396456 B1 EP4396456 B1 EP 4396456B1
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Prior art keywords
substrate
coating
tip
depression
cutting edge
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German (de)
French (fr)
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EP4396456A1 (en
Inventor
Reiner Mack
Axel Kratzsch
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Voith Patent GmbH
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Voith Patent GmbH
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B1/00Engines of impulse type, i.e. turbines with jets of high-velocity liquid impinging on blades or like rotors, e.g. Pelton wheels; Parts or details peculiar thereto
    • F03B1/02Buckets; Bucket-carrying rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/12Blades; Blade-carrying rotors
    • F03B3/121Blades, their form or construction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00Manufacture
    • F05B2230/90Coating; Surface treatment
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2280/00Materials; Properties thereof
    • F05B2280/60Properties or characteristics given to material by treatment or manufacturing
    • F05B2280/6011Coating

Definitions

  • the present invention relates to a Pelton turbine with increased durability and a method for manufacturing the turbine.
  • the present invention relates to the buckets of the turbine with a coated substrate and a method for providing and coating the substrate.
  • Erosion-resistant coatings are often used on hydropower turbine components, especially on Pelton turbine impellers, which are susceptible to erosion by sediments contained in the turbine water.
  • the EP 3 647 585 B1 a component of a hydroelectric turbine comprising a wedge-shaped substrate having a tip portion and at least two side portions, wherein an erosion-resistant coating is applied to the wedge-shaped substrate, and wherein the erosion-resistant coating applied to the tip portion is at least 2 times stronger than the erosion-resistant coating applied to the side portions, and wherein the erosion-resistant coating comprises at least 99.5% density.
  • the application of the erosion-resistant coating is carried out by the high-velocity air-fuel process (HVAF).
  • HVAF high-velocity air-fuel process
  • the EP 3 647 585 B1 Buckets of a Pelton turbine runner which are constructed in this way.
  • the object of the invention is to provide an impeller of a Pelton type turbine which has an alternative structure and is manufactured by an alternative method, wherein the resistance of the impeller to erosion is comparably high as the resistance of the impellers known from the prior art.
  • FIG 1 shows a section through a bucket of a Pelton type turbine in a schematic representation according to the state of the art.
  • the bucket comprises a substrate which is designated with 1.
  • the substrate is made of steel.
  • the main cutting edge which is designated with 2, is arranged centrally in the bucket.
  • the main cutting edge splits the water jet directed onto the turbine into two partial jets, which are deflected by the two halves of the bucket.
  • the main cutting edge is therefore also often referred to as a "splitter”.
  • the Figure 1 The cut shown runs perpendicular to the direction of the main cutting edge.
  • the inside of the cup is coated with an erosion-resistant coating, which is marked with 3.
  • the substrate already has essentially the same contour as the coated cup.
  • Figure 2 shows the main cutting edge 2 degraded by erosion from Figure 1 . Since the abrasion is strongest at the tip of the cutting edge, which is hit by the undivided water jet, the coating is removed there first and then the substrate underneath. The coating remaining on the flanks is removed less quickly than the substrate, so that a characteristic groove is formed. It is clear that such a profile of the main cutting edge leads to considerable losses in efficiency, so that an impeller that is degraded in this way must be replaced.
  • the described degradation process can be slowed down by providing as much resistant material as possible at the point of the strongest abrasion.
  • This is achieved by ensuring that the erosion resistant coating applied to the tip section is at least 2 times thicker than the erosion resistant coating applied to the side sections.
  • An undesirable side effect of this is that the tip radius on the main cutting edge is increased, which leads to a reduced initial efficiency of the turbine.
  • the inventors therefore looked for a way to arrange as much resistant material as possible at the point of greatest stress without the tip radius increasing accordingly. They realized that this can be achieved by giving the substrate a contour before coating that resembles the contour of a degraded cup (see Figure 2 ) corresponds.
  • Figure 3 shows the main cutting edge of a cup according to the invention.
  • the substrate has a wedge-shaped form in the area of the main cutting edge, whereby the end of the wedge does not end in a single tip, but rather there is a depression or groove arranged between two tips at this point.
  • the wedge-shaped substrate comprises a first and a second tip section and a total of four side sections in the area of the main cutting edge, whereby a depression extends between the tip sections, whereby two side sections are assigned to each tip section, and whereby two of the side sections are arranged on the outside of the wedge-shaped substrate, and the two remaining side sections are oriented towards the depression on the inside.
  • the lines formed by the end points of the two tip sections run parallel to the cutting line of the main cutting edge.
  • the depression forms a "valley" between the tip sections, so to speak.
  • the depression is first filled with erosion-resistant material.
  • the coating process is then carried out in This process is continued in this area until the coating material has formed a raised area there in order to form the tip of the main cutting edge.
  • the surface of the coating in the area of the deepest point of the depression must protrude at least slightly above the surface of the coating on the two tip sections.
  • the outer side sections and the rest of the Pelton cup are then coated. The outer side sections and the rest of the Pelton cup could just as well be coated first, ie before coating the depression as described above.
  • Figure 4 shows the main cutting edge according to the invention, with certain characteristic dimensions being marked. These dimensions relate to the layer thickness of the coating at certain points on the substrate, with the thickness of the coating being measured in a direction perpendicular to the substrate surface at the relevant point.
  • D A indicates the thickness of the coating in the area of an outer side section.
  • D I indicates the thickness of the coating in the area of an inner side section.
  • Ds indicates the thickness of the coating at a tip section.
  • a main cutting edge according to the invention is characterized in that the following relation is fulfilled for the thicknesses of the coating mentioned: D A ⁇ D S ⁇ D I
  • Typical layer thicknesses in the area of the outer side sections are in the range of 0.3 mm ⁇ D A ⁇ 0.7 mm.
  • Figure 5 shows the main cutting edge according to the invention, with certain further characteristic dimensions being marked.
  • W is the distance between the two tip sections of the substrate, this distance being perpendicular to the axis of symmetry of the cutting edge and perpendicular to the cutting line.
  • H is the height of the tip sections in relation to the deepest point of the recess. H is removed parallel to the axis of symmetry of the cutting edge.
  • D is the thickness of the coating at the point where the axis of symmetry of the main cutting edge intersects the substrate, ie in the middle of the recess, which usually has its deepest point there.
  • the exact shape of the recess is not crucial. The easiest way to do this is to mill such a recess into the substrate, e.g. with a cove milling cutter.
  • the erosion-resistant coating is applied.
  • suitable materials and compositions of the erosion-resistant coating see sections [0027] and [0028] of the EP 3 647 585 B1
  • the combination of tungsten carbide particles with a matrix of CoCr is considered to be particularly suitable.
  • the coating can be carried out using HVOF or HVAF. HVOF is considered to be particularly suitable. Details of these processes can be found in the EP 3 647 585 B1 be taken.
  • step S1 must be carried out before steps S2 and S3.
  • the order of steps S2 and S3 can then be arbitrary.
  • the coating process described can be carried out on separate buckets when the buckets are attached as a whole to a hub during the manufacture of a Pelton impeller.
  • the coating process described is carried out when the entire bucket is on the hub.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

Die vorliegende Erfindung betrifft eine Pelton-Turbine mit erhöhter Lebensdauer und ein Verfahren zur Herstellung der Turbine. Insbesondere betrifft die vorliegende Erfindung die Becher der Turbine mit einem beschichteten Substrat und ein Verfahren zur Bereitstellung und Beschichtung des Substrats.The present invention relates to a Pelton turbine with increased durability and a method for manufacturing the turbine. In particular, the present invention relates to the buckets of the turbine with a coated substrate and a method for providing and coating the substrate.

Erosionsbeständige Beschichtungen werden häufig auf Komponenten von Wasserkraftturbinen verwendet, insbesondere auch bei Laufrädern von Pelton-Turbinen, die anfällig für Erosion durch im Triebwasser enthaltene Sedimente sind.Erosion-resistant coatings are often used on hydropower turbine components, especially on Pelton turbine impellers, which are susceptible to erosion by sediments contained in the turbine water.

So offenbart z.B. die EP 3 647 585 B1 ein Bauteil einer hydroelektrischen Turbine, das ein keilförmiges Substrat mit einem Spitzenabschnitt und mindestens zwei Seitenabschnitten umfasst, wobei eine erosionsbeständige Beschichtung auf dem keilförmigen Substrat aufgebracht ist, und wobei die erosionsbeständige Beschichtung, die auf dem Spitzenabschnitt aufgebracht ist, mindestens 2 Mal stärker ist als die erosionsbeständige Beschichtung, die auf den Seitenabschnitten aufgebracht ist, und wobei die erosionsbeständige Beschichtung mindestens 99,5% Dichte umfasst. Dabei erfolgt die Applikation der erosionsbeständigen Beschichtung durch den Hochgeschwindigkeits-Air-Fuel-Prozess (HVAF). Insbesondere offenbart die EP 3 647 585 B1 Becher eines Pelton-Turbinenlaufrades, welche so aufgebaut sind.For example, the EP 3 647 585 B1 a component of a hydroelectric turbine comprising a wedge-shaped substrate having a tip portion and at least two side portions, wherein an erosion-resistant coating is applied to the wedge-shaped substrate, and wherein the erosion-resistant coating applied to the tip portion is at least 2 times stronger than the erosion-resistant coating applied to the side portions, and wherein the erosion-resistant coating comprises at least 99.5% density. The application of the erosion-resistant coating is carried out by the high-velocity air-fuel process (HVAF). In particular, the EP 3 647 585 B1 Buckets of a Pelton turbine runner, which are constructed in this way.

Die Aufgabe der Erfindung ist es, ein Laufrad einer Turbine vom Typ Pelton anzugeben, das einen alternativen Aufbau aufweist, und durch ein alternatives Verfahren hergestellt wird, wobei die Beständigkeit des Laufrades gegen Erosion vergleichbar hoch ist, wie die Beständigkeit der aus dem Stand der Technik bekannten Laufräder.The object of the invention is to provide an impeller of a Pelton type turbine which has an alternative structure and is manufactured by an alternative method, wherein the resistance of the impeller to erosion is comparably high as the resistance of the impellers known from the prior art.

Die Aufgabe wird erfindungsgemäß durch eine Ausführung entsprechend dem unabhängigen Anspruch gelöst. Weitere vorteilhafte Ausführungsformen der vorliegenden Erfindung finden sich in den Unteransprüchen.The object is achieved according to the invention by an embodiment according to the independent claim. Further advantageous embodiments of the present invention can be found in the subclaims.

Im Folgenden wird die Erfindung anhand von Figuren erläutert. Die Figuren zeigen im Einzelnen:

Fig.1
Becher einer Pelton-Turbine gemäß dem Stand der Technik
Fig.2
Degradierte Hauptschneide
Fig.3
Hauptschneide eines erfindungsgemäßen Bechers
Fig.4
Hauptschneide eines erfindungsgemäßen Bechers
Fig.5
Hauptschneide eines erfindungsgemäßen Bechers
The invention is explained below using figures. The figures show in detail:
Fig.1
Bucket of a Pelton turbine according to the state of the art
Fig.2
Degraded main cutting edge
Fig.3
main cutting edge of a cup according to the invention
Fig.4
main cutting edge of a cup according to the invention
Fig.5
main cutting edge of a cup according to the invention

Figur 1 zeigt einen Schnitt durch einen Becher einer Turbine vom Typ Pelton in schematischer Darstellung gemäß dem Stand der Technik. Der Becher umfasst ein Substrat, welches mit 1 bezeichnet ist. Das Substrat besteht aus Stahl. Zentral im Becher ist die Hauptschneide angeordnet, welche mit 2 bezeichnet ist. Durch die Hauptschneide wird der auf die Turbine gelenkte Wasserstrahl in zwei Teilstrahlen aufgeteilt, welche durch die zwei Becherhälften umgelenkt werden. Die Hauptschneide wird daher auch gern als "Splitter" bezeichnet. Der in Figur 1 gezeigte Schnitt verläuft senkrecht zur Richtung der Hauptschneide. Zum Schutz des Bechers gegen Erosion ist der Becher auf der Innenseite mit einer erosionsbeständigen Beschichtung überzogen, welche mit 3 bezeichnet ist. Wie aus Figur 1 ersichtlich ist, weist dabei das Substrat bereits im Wesentlichen dieselbe Kontur auf, welche der beschichtete Becher aufweist. Figure 1 shows a section through a bucket of a Pelton type turbine in a schematic representation according to the state of the art. The bucket comprises a substrate which is designated with 1. The substrate is made of steel. The main cutting edge, which is designated with 2, is arranged centrally in the bucket. The main cutting edge splits the water jet directed onto the turbine into two partial jets, which are deflected by the two halves of the bucket. The main cutting edge is therefore also often referred to as a "splitter". The Figure 1 The cut shown runs perpendicular to the direction of the main cutting edge. To protect the cup against erosion, the inside of the cup is coated with an erosion-resistant coating, which is marked with 3. As can be seen from Figure 1 As can be seen, the substrate already has essentially the same contour as the coated cup.

Figur 2 zeigt die durch Erosion degradierte Hauptschneide 2 aus Figur 1. Da die Abrasion an der Spitze der Schneide, auf die der ungeteilte Wasserstrahl auftrifft, am stärksten ist, wird dort zuerst die Beschichtung und nach Abtragung derselben das darunter liegende Substrat abgetragen. Die noch an den Flanken verbleibende Beschichtung wird dabei weniger schnell abgetragen als das Substrat, so dass sich eine charakteristische Rinne ausbildet. Es ist klar, dass ein solches Profil der Hauptschneide zu erheblichen Wirkungsgradverlusten führt, so dass ein so degradiertes Laufrad ausgetauscht werden muss. Figure 2 shows the main cutting edge 2 degraded by erosion from Figure 1 . Since the abrasion is strongest at the tip of the cutting edge, which is hit by the undivided water jet, the coating is removed there first and then the substrate underneath. The coating remaining on the flanks is removed less quickly than the substrate, so that a characteristic groove is formed. It is clear that such a profile of the main cutting edge leads to considerable losses in efficiency, so that an impeller that is degraded in this way must be replaced.

Der beschriebene Degradationsprozess kann dadurch verlangsamt werden, dass an der Stelle der stärksten Abrasion möglichst viel widerstandsfähiges Material vorgesehen wird. In der Lösung gemäß der EP 3 647 585 B1 wird das dadurch erreicht, dass die erosionsbeständige Beschichtung, die auf dem Spitzenabschnitt aufgebracht ist, mindestens 2 Mal stärker ist als die erosionsbeständige Beschichtung, die auf den Seitenabschnitten aufgebracht ist. Ein unerwünschter Nebeneffekt ist dabei, dass so der Spitzenradius an der Hauptschneide vergrößert wird, was zu einem reduzierten Anfangswirkungsgrad der Turbine führt.The described degradation process can be slowed down by providing as much resistant material as possible at the point of the strongest abrasion. In the solution according to the EP 3 647 585 B1 This is achieved by ensuring that the erosion resistant coating applied to the tip section is at least 2 times thicker than the erosion resistant coating applied to the side sections. An undesirable side effect of this is that the tip radius on the main cutting edge is increased, which leads to a reduced initial efficiency of the turbine.

Die Erfinder haben daher nach einer Möglichkeit gesucht, um möglichst viel widerstandsfähiges Material an der am stärksten beanspruchten Stelle anordnen zu können, ohne dass der Spitzenradius entsprechend stark anwächst. Sie haben erkannt, dass sich das dadurch erreichen lässt, dass das Substrat vor der Beschichtung eine Kontur aufweist, welche der Kontur eines degradierten Bechers (siehe Figur 2) entspricht.The inventors therefore looked for a way to arrange as much resistant material as possible at the point of greatest stress without the tip radius increasing accordingly. They realized that this can be achieved by giving the substrate a contour before coating that resembles the contour of a degraded cup (see Figure 2 ) corresponds.

Figur 3 zeigt die Hauptschneide eines erfindungsgemäßen Bechers. Das Substrat hat im Bereich der Hauptschneide eine keilförmige Gestalt, wobei das Ende des Keils nicht in einer einzelnen Spitze ausläuft, sondern sich an dieser Stelle eine zwischen zwei Spitzen angeordnete Vertiefung bzw. Rinne befindet. Mit anderen Worten: Das keilförmige Substrat umfasst im Bereich der Hauptschneide einen ersten und einen zweiten Spitzenabschnitt und insgesamt vier Seitenabschnitte, wobei sich zwischen den Spitzenabschnitten eine Vertiefung erstreckt, und wobei je einem Spitzenabschnitt zwei Seitenabschnitte zugeordnet sind, und wobei zwei der Seitenabschnitte außen am keilförmigen Substrat angeordnet sind, und die beiden übrigen Seitenabschnitte innen zur Vertiefung hin orientiert sind. Es ist dabei klar, dass die Linien, welche durch die Endpunkte der beiden Spitzenabschnitte gebildet werden, parallel zur Schneidenlinie der Hauptschneide verlaufen. Die Vertiefung bildet sozusagen ein "Tal" zwischen den Spitzenabschnitten. Figure 3 shows the main cutting edge of a cup according to the invention. The substrate has a wedge-shaped form in the area of the main cutting edge, whereby the end of the wedge does not end in a single tip, but rather there is a depression or groove arranged between two tips at this point. In other words: the wedge-shaped substrate comprises a first and a second tip section and a total of four side sections in the area of the main cutting edge, whereby a depression extends between the tip sections, whereby two side sections are assigned to each tip section, and whereby two of the side sections are arranged on the outside of the wedge-shaped substrate, and the two remaining side sections are oriented towards the depression on the inside. It is clear that the lines formed by the end points of the two tip sections run parallel to the cutting line of the main cutting edge. The depression forms a "valley" between the tip sections, so to speak.

Bei der Beschichtung eines solchen Substrats wird zunächst die Vertiefung mit erosionsbeständigen Material aufgefüllt. Danach wird der Beschichtungsvorgang in diesem Bereich so lange fortgesetzt bis das Beschichtungsmaterial dort eine Überhöhung gebildet hat, um die Spitze der Hauptschneide zu formen. Dazu muss die Oberfläche der Beschichtung im Bereich des tiefsten Punktes der Vertiefung wenigstens etwas über die Oberfläche der Beschichtung an den beiden Spitzenabschnitten hinausragen. Es ist jedoch von Vorteil, wenn die Überhöhung möglichst stark ausgebildet wird. Anschließend werden die äußeren Seitenabschnitte und der Rest des Pelton-Bechers beschichtet. Genauso gut könnten die äußeren Seitenabschnitte und der Rest des Pelton-Bechers zuerst beschichtet werden, d.h. vor der Beschichtung der Vertiefung wie zuvor beschrieben. Aus Figur 3 ist ersichtlich, dass der Spitzenradius einer so erzeugten Hauptschneide in Relation zur Menge an erosionsbeständigem Material an dieser Stelle vergleichsweise klein ist. Außerdem ist die Verbindung zwischen Beschichtung und Substrat in diesem hochbelasteten Bereich sehr fest, da die Vertiefung einen Formschluss ermöglicht.When coating such a substrate, the depression is first filled with erosion-resistant material. The coating process is then carried out in This process is continued in this area until the coating material has formed a raised area there in order to form the tip of the main cutting edge. To do this, the surface of the coating in the area of the deepest point of the depression must protrude at least slightly above the surface of the coating on the two tip sections. However, it is advantageous if the raised area is as high as possible. The outer side sections and the rest of the Pelton cup are then coated. The outer side sections and the rest of the Pelton cup could just as well be coated first, ie before coating the depression as described above. Figure 3 It is clear that the tip radius of a main cutting edge produced in this way is comparatively small in relation to the amount of erosion-resistant material at this point. In addition, the connection between the coating and the substrate in this highly stressed area is very strong, as the recess enables a positive fit.

Figur 4 zeigt die erfindungsgemäße Hauptschneide, wobei bestimmte charakteristische Maße eingezeichnet sind. Diese Maße betreffen die Schichtdicke der Beschichtung an bestimmten Stellen des Substrates, wobei die Dicke der Beschichtung jeweils in senkrechter Richtung zur Substratoberfläche an der betreffenden Stelle gemessen wird. DA gibt die Dicke der Beschichtung im Bereich eines außen gelegenen Seitenabschnittes an. DI gibt die Dicke der Beschichtung im Bereich eines innen gelegenen Seitenabschnittes an. Ds gibt die Dicke der Beschichtung an einem Spitzenabschnitt an. Eine erfindungsgemäße Hauptschneide zeichnet sich dadurch aus, dass für die genannten Dicken der Beschichtung folgende Relation erfüllt ist: D A < D S D I

Figure imgb0001
Figure 4 shows the main cutting edge according to the invention, with certain characteristic dimensions being marked. These dimensions relate to the layer thickness of the coating at certain points on the substrate, with the thickness of the coating being measured in a direction perpendicular to the substrate surface at the relevant point. D A indicates the thickness of the coating in the area of an outer side section. D I indicates the thickness of the coating in the area of an inner side section. Ds indicates the thickness of the coating at a tip section. A main cutting edge according to the invention is characterized in that the following relation is fulfilled for the thicknesses of the coating mentioned: D A < D S D I
Figure imgb0001

Typische Schichtdicken im Bereich der äußeren Seitenabschnitte liegen in einem Bereich von 0,3 mm ≤ DA ≤ 0,7 mm.Typical layer thicknesses in the area of the outer side sections are in the range of 0.3 mm ≤ D A ≤ 0.7 mm.

Figur 5 zeigt die erfindungsgemäße Hauptschneide, wobei bestimmte weitere charakteristische Maße eingezeichnet sind. W ist der Abstand zwischen den beiden Spitzenabschnitten des Substrats, wobei dieser Abstand senkrecht zur Symmetrieachse der Schneide und senkrecht zur Schneidenlinie gemessen wird. H ist die Höhe der Spitzenabschnitte in Bezug auf den tiefsten Punkt der Vertiefung. H wird parallel zu Symmetrieachse der Schneide abgetragen. D ist die Dicke der Beschichtung an der Stelle, an der die Symmetrieachse der Hauptschneide das Substrat schneidet, d.h. in der Mitte der Vertiefung, welche dort in der Regel ihren tiefsten Punkt aufweist. Figure 5 shows the main cutting edge according to the invention, with certain further characteristic dimensions being marked. W is the distance between the two tip sections of the substrate, this distance being perpendicular to the axis of symmetry of the cutting edge and perpendicular to the cutting line. H is the height of the tip sections in relation to the deepest point of the recess. H is removed parallel to the axis of symmetry of the cutting edge. D is the thickness of the coating at the point where the axis of symmetry of the main cutting edge intersects the substrate, ie in the middle of the recess, which usually has its deepest point there.

Für viele gängige Geometrien von Pelton-Bechern liegen die genannten Maße erfindungsgemäß in den folgenden vorteilhaften Wertebereichen: W = 3 7 mm

Figure imgb0002
H = 0,1 0,7 mm
Figure imgb0003
D 1 mm
Figure imgb0004
For many common geometries of Pelton buckets, the dimensions mentioned lie in the following advantageous value ranges according to the invention: W = 3 7 mm
Figure imgb0002
H = 0.1 0.7 mm
Figure imgb0003
D 1 mm
Figure imgb0004

Die genaue Form der Vertiefung ist nicht ausschlaggebend. Am einfachsten kann eine solche Vertiefung in das Substrat eingefräst werden, z.B. mit einem Hohlkehlfräser. Nachdem das Substrat mit der Vertiefung bereitgestellt worden ist, wird die erosionsbeständige Beschichtung aufgebracht. Zu den geeigneten Materialien und Zusammensetzungen der erosionsbeständigen Beschichtung wird auf die Abschnitte [0027] und [0028] der EP 3 647 585 B1 verwiesen. Als besonders geeignet wird die Kombination von Wolframkarbid-Partikeln mit einer Matrix aus CoCr angesehen. Erfindungsgemäß kann die Beschichtung mittels HVOF oder HVAF erfolgen. Als bevorzugt geeignet wird HVOF betrachtet. Details zu diesen Verfahren können der EP 3 647 585 B1 entnommen werden.The exact shape of the recess is not crucial. The easiest way to do this is to mill such a recess into the substrate, e.g. with a cove milling cutter. After the substrate with the recess has been prepared, the erosion-resistant coating is applied. For suitable materials and compositions of the erosion-resistant coating, see sections [0027] and [0028] of the EP 3 647 585 B1 The combination of tungsten carbide particles with a matrix of CoCr is considered to be particularly suitable. According to the invention, the coating can be carried out using HVOF or HVAF. HVOF is considered to be particularly suitable. Details of these processes can be found in the EP 3 647 585 B1 be taken.

Das erfindungsgemäße Herstellungsverfahren umfasst folgende Schritte:

  • S1: Bereitstellung eines Substrates 1 mit einer Vertiefung, welche zwischen zwei Spitzenabschnitten angeordnet ist, und wobei zwei Seitenabschnitte außen an den Spitzenabschnitten angeordnet sind;
  • S2: Aufbringung einer erosionsbeständigen Beschichtung 3 auf das Substrat 1 im Bereich der Vertiefung, wobei dieselbe mit erosionsbeständigen Material aufgefüllt und danach der Beschichtungsvorgang in diesem Bereich so lange fortgesetzt wird bis das Beschichtungsmaterial dort eine Überhöhung gebildet hat;
  • S3: Aufbringung einer erosionsbeständigen Beschichtung 3 auf das Substrat im Bereich der äußeren Seitenabschnitte.
The manufacturing process according to the invention comprises the following steps:
  • S1: Providing a substrate 1 having a recess arranged between two tip portions and wherein two side portions are arranged externally on the tip portions;
  • S2: Application of an erosion-resistant coating 3 to the substrate 1 in the region of the depression, wherein the latter is filled with erosion-resistant material and the coating process is then continued in this region until the coating material has formed an elevation there;
  • S3: Application of an erosion-resistant coating 3 to the substrate in the area of the outer side sections.

Es ist klar, dass Schritt S1 vor den Schritten S2 und S3 ausgeführt werden muss. Die Reihenfolge der Schritte S2 und S3 kann dann beliebig sein.It is clear that step S1 must be carried out before steps S2 and S3. The order of steps S2 and S3 can then be arbitrary.

Abschließend ist anzumerken, dass der beschriebene Beschichtungsvorgang an separaten Bechern ausgeführt werden kann, wenn die Becher bei der Herstellung eines Pelton-Laufrades im Ganzen an eine Nabe angebracht werden. Wenn jedoch die Becher integral mit der Nabe gefertigt werden, oder nur Teile der Becher an die Nabe angebracht werden, wobei der übrige Teil der Becher integral mit der Nabe gefertigt wird, dann wird der beschriebene Beschichtungsvorgang dann ausgeführt, wenn sich der gesamte Becher an der Nabe befindet.Finally, it should be noted that the coating process described can be carried out on separate buckets when the buckets are attached as a whole to a hub during the manufacture of a Pelton impeller. However, when the buckets are manufactured integrally with the hub, or only parts of the buckets are attached to the hub, with the remainder of the buckets being manufactured integrally with the hub, then the coating process described is carried out when the entire bucket is on the hub.

Bezugszeichenlistelist of reference symbols

11
Substratsubstrate
22
Hauptschneide bzw. Splittermain cutting edge or splinter
33
Beschichtungcoating

Claims (6)

  1. Bucket of a turbine of the Pelton type comprising a substrate (1), a main cutting edge (2) and an erosion-resistant coating (3) covering the substrate (1), wherein the substrate (1) has a wedge-shaped configuration in the region of the main cutting edge (2), characterised in that the substrate (1) comprises a first and a second tip section and a total of four side sections in the region of the main cutting edge (2), wherein a depression extends between the tip portions, and wherein two side sections are associated with each tip section, and wherein two of the side sections are arranged on the outside of the wedge-shaped substrate and the two remaining side sections are orientated inwards towards the depression, and wherein the coating (3) forms an elevation in the region of the depression in order to form the tip of the main cutting edge (2).
  2. The bucket according to claim 1, wherein the two tip sections are arranged such that they have a distance W of 3 to 7 mm.
  3. The bucket according to claim 1 or 2, wherein the two tip sections and the depression are formed such that the tip sections have a height H with respect to a deepest point of the depression which is between 0.1 mm and 0.7 mm.
  4. The bucket according to any one of the preceding claims, wherein the coating (3) has a thickness D of at least 1 mm in the centre of the depression.
  5. Bucket according to one of the preceding claims, wherein the coating (3) consists of a matrix of CoCr with embedded tungsten carbide particles.
  6. A method of manufacturing a bucket of a Pelton type turbine according to any one of the preceding claims, the method comprising the following steps:
    S1: providing a substrate (1) having a depression arranged between two tip sections, and wherein two side portions are arranged on the outside of the tip sections;
    S2: Application of an erosion-resistant coating (3) to the substrate (1) in the region of the recess, the latter being filled with erosion-resistant material and the coating process then being continued in this region until the coating material has formed an elevation there;
    S3: Application of an erosion-resistant coating (3) to the substrate (1) in the region of the outer side sections.
EP22730477.1A 2021-09-02 2022-05-25 Bucket of a pelton turbine and method for production Active EP4396456B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102021122700 2021-09-02
PCT/EP2022/064163 WO2023030704A1 (en) 2021-09-02 2022-05-25 Bucket of a pelton turbine and method for production

Publications (2)

Publication Number Publication Date
EP4396456A1 EP4396456A1 (en) 2024-07-10
EP4396456B1 true EP4396456B1 (en) 2024-12-04

Family

ID=82058267

Family Applications (1)

Application Number Title Priority Date Filing Date
EP22730477.1A Active EP4396456B1 (en) 2021-09-02 2022-05-25 Bucket of a pelton turbine and method for production

Country Status (6)

Country Link
EP (1) EP4396456B1 (en)
CN (1) CN117916460A (en)
CL (1) CL2024000606A1 (en)
CO (1) CO2024001990A2 (en)
PE (1) PE20240870A1 (en)
WO (1) WO2023030704A1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001153019A (en) * 1999-11-30 2001-06-05 Toshiba Corp Pelton turbine bucket, needle valve and Pelton turbine
EP2072176A1 (en) * 2007-12-21 2009-06-24 Sulzer Markets and Technology AG Method of manufacturing an erosion protection steel layer using laser buildup; Component with such an erosion protection steel layer
FR2941639B1 (en) * 2009-01-30 2012-04-20 Alstom Hydro France NOVEL HYDRAULIC MACHINE COMPONENT, METHOD FOR MANUFACTURING OR MAINTENANCE OF SUCH COMPONENT
EP3647585B1 (en) 2018-11-02 2021-04-28 GE Renewable Technologies Hydro-electric turbine component having enhanced life span and method for forming the same

Also Published As

Publication number Publication date
WO2023030704A1 (en) 2023-03-09
PE20240870A1 (en) 2024-04-24
CN117916460A (en) 2024-04-19
CO2024001990A2 (en) 2024-03-07
EP4396456A1 (en) 2024-07-10
CL2024000606A1 (en) 2024-08-09

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