EP0379699A1 - Method for enhancing the corrosion and erosion resistance of the blade of a rotary thermal apparatus and blade produced ba said method - Google Patents
Method for enhancing the corrosion and erosion resistance of the blade of a rotary thermal apparatus and blade produced ba said method Download PDFInfo
- Publication number
- EP0379699A1 EP0379699A1 EP89123291A EP89123291A EP0379699A1 EP 0379699 A1 EP0379699 A1 EP 0379699A1 EP 89123291 A EP89123291 A EP 89123291A EP 89123291 A EP89123291 A EP 89123291A EP 0379699 A1 EP0379699 A1 EP 0379699A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- blade
- corrosion
- protective layer
- base material
- weight
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
- C23C4/067—Metallic material containing free particles of non-metal elements, e.g. carbon, silicon, boron, phosphorus or arsenic
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/937—Sprayed metal
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/1275—Next to Group VIII or IB metal-base component
- Y10T428/12757—Fe
Definitions
- Buckets for rotating thermal machines such as steam turbines, gas turbines, turbo compressors etc. and their effective protection against operational attacks such as oxidation, corrosion, wear and damage.
- the invention relates to improving the resistance to corrosion and erosion of blades of rotating thermal machines by further developing the methods for applying suitable protective layers.
- the invention relates to a method for increasing the corrosion and erosion resistance of a blade of a rotating thermal machine, which in consists essentially of a ferritic and / or ferritic-martensitic base material, by applying a firmly adhering surface protective layer.
- the blades of rotating thermal machines are often provided with protective layers. This is used for both steam and gas turbine blades as well as for compressor blades. The main thing is to increase resistance to corrosion and oxidizing attack as well as erosion and wear (wear and tear).
- the element Cr, Al, Si forming the oxide cover layers occupy a special position.
- Layers which have a high Al content have been used, inter alia, as filler material for carbide-containing coatings (Cr2C3; WC) in engine construction.
- the invention has for its object a method for increasing the corrosion (Cl and SO4 ions) and erosion resistance (particle and drop impact erosion) of a blade of a rotating thermal machine in the presence of H2O steam and comparatively moderate temperatures (450 ° C ) which is particularly suitable for ferritic and / or ferritic-martensitic base material of the blade, a suitable surface layer being to be achieved inexpensively and without great effort.
- the occurrence of pitting corrosion should be avoided or min be delayed to ensure a longer lifespan for the bucket.
- a protective layer consisting of 6 to 15% by weight of Si, remainder Al is sprayed onto the surface of the base material by the high-speed process at a particle speed of at least 300 m / s.
- a compressor blade for an axial compressor was provided with a protective layer.
- the scoop was first degreased and cleaned in trichloroethane, whereupon the blade and the pale / foot transition were sandblasted.
- the coating of the blade was carried out using a high-speed flame spraying process with a particle speed of 400 m / s and a gas speed of 1000 m / s with nitrogen as the conveying gas.
- the aluminum alloy powder was conveyed by means of nitrogen into a combustion chamber operated with propane and oxygen.
- the liquefied particles were thrown onto the workpiece as fine drops under high excess pressure.
- the blade stood in a device that covered the blade root.
- the protective layer was applied with the hand-held spray gun.
- the applied protective layer was measured using a metallographic cut and was in Average 8 to 15 ⁇ m.
- a plastic in the present case polytetrafluoroethylene was applied to this metal protective layer using a conventional paint spraying process.
- This smooth surface layer had an average thickness of 6 to 10 ⁇ m and a roughness of approximately 2 ⁇ m.
- the coated compressor blade was subjected to a corrosion resistance test. For this purpose, it was immersed in a test solution and then stored in a climatic cabinet for 4 hours. This cycle was repeated a total of 60 times.
- a compressor blade of the same dimensions and composition was coated according to Example 1 with an aluminum alloy and a plastic. Now a scratch of 10 mm length and a total of 25 ⁇ m depth parallel to the longitudinal axis was made on the coated blade, the profile of which just barely grasped the base material with its tip. The blade was then subjected to the same corrosion tests as in Example 1. Thanks to the local element formation (aluminum layer functions as a "sacrificial anode”), the base material was largely protected, while the aluminum layer on the flanks of the scratch was only slightly degraded.
- the protective layer according to the invention can be expected to have a long service life under practical conditions of use.
- a compressor blade was provided with a protective layer.
- the material of the blade consisted of a martensitic-austenitic two-phase steel with a low austenite content and was available in a tempered condition.
- the aluminum alloy was sprayed on using an industrial robot. 3 spray coats were carried out. The thickness of the applied layer averaged 90 to 100 ⁇ m. A plastic layer of approx. 10 to 15 ⁇ m thickness was additionally applied to this metal protective layer using a conventional paint spraying process. The coated blade was subjected to the same corrosion test as in Example 1. No attack was then found.
- a used compressor blade with wing profile was provided with a protective layer.
- the blade was coated using customary methods and showed considerable operational damage in the form of pitting corrosion, which in some cases also extended to the base material.
- This used shovel was first degreased, ground and sandblasted to remove the damage. Then the surface zone of the base material was compacted by shot peening.
- the metal layer was sprayed on by hand using the high-speed flame spraying process.
- the thickness of the protective layer fluctuated between 25 and 45 ⁇ m.
- the metallographic tests after the corrosion test indicated above showed an unchanged, unaffected surface zone.
- the invention is not restricted to the exemplary embodiments.
- the method for increasing the corrosion and erosion resistance of a blade of a rotating thermal machine which essentially consists of a ferritic and / or ferritic-martensitic base material, is carried out by applying a firmly adhering surface protective layer by a Protective layer consisting of 6 to 15 wt .-% Si, remainder Al is sprayed onto the surface of the base material by the high-speed method with a particle speed of at least 300 m / s.
- the base material preferably consists of a chromium-containing steel with 12 to 13% by weight of Cr and further additives.
- the protective layer advantageously contains 10 to 12% by weight of Si, the rest of Al.
- a cover layer made of a heat-resistant plastic is preferably additionally applied to said protective layer.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Plasma & Fusion (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Coating By Spraying Or Casting (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
Verfahren zur Erhöhung des Korrosions- und Erosionswiderstandes einer Schaufel einer rotierenden thermischen Maschine, welche vorwiegend aus einem ferritischen und/oder ferritisch-martensitischen Grundmaterial besteht, indem eine feste haftende Oberflächenschutzschicht bestehend aus 6 bis 15 Gew.-% Si, Rest Al nach dem Hochgeschwindigkeitsverfahren mit einer Partikelgeschwindigkeit von mindestens 300 m/s auf die Oberfläche des Grundmaterials aufgespritzt wird.Process for increasing the corrosion and erosion resistance of a blade of a rotating thermal machine, which mainly consists of a ferritic and / or ferritic-martensitic base material, by a firmly adhering surface protection layer consisting of 6 to 15% by weight Si, the rest Al according to the high-speed process is sprayed onto the surface of the base material at a particle speed of at least 300 m / s.
Description
Schaufeln für rotierende thermische Maschinen wie Dampfturbinen, Gasturbinen, Turbokompressoren etc. und deren wirksamer Schutz gegen betriebliche Angriffe wie Oxydation, Korrosion, Verschleiss und Beschädigung.Buckets for rotating thermal machines such as steam turbines, gas turbines, turbo compressors etc. and their effective protection against operational attacks such as oxidation, corrosion, wear and damage.
Die Erfindung bezieht sich auf die Verbesserung des Widerstandes gegen Korrosion und Erosion von Schaufeln rotierender thermischer Maschinen durch Weiterentwicklung der Verfahren zum Aufbringen von geeigneten Schutzschichten.The invention relates to improving the resistance to corrosion and erosion of blades of rotating thermal machines by further developing the methods for applying suitable protective layers.
Insbesondere betrifft die Erfindung ein Verfahren zur Erhöhung des Korrosions- und Erosionswiderstandes einer Schaufel einer rotierenden thermischen Maschine, die im wesentlichen aus einem ferritischen und/oder ferritischmartensitischen Grundmaterial besteht, durch Aufbringen einer fest haftenden Oberflächenschutzschicht.In particular, the invention relates to a method for increasing the corrosion and erosion resistance of a blade of a rotating thermal machine, which in consists essentially of a ferritic and / or ferritic-martensitic base material, by applying a firmly adhering surface protective layer.
Um den zahlreichen Beanspruchungen Genüge leisten zu können, werden die Schaufeln rotierender thermischer Maschinen vielfach mit Schutzschichten versehen. Davon wird sowohl bei Dampf- und Gasturbinenschaufeln wie bei Kompressorschaufeln Gebrauch gemacht. Es gilt vor allem, den Widerstand gegen Korrosion und oxydierenden Angriff sowie gegen Erosion und Abnutzung (Verschleiss) zu erhöhen. Unter den verwendeten Stoffen für Schutzschichten nehmen die oxydische Deckschichten bildenden Element Cr, Al, Si eine Sonderstellung ein. Schichten, die einen hohen Al-Gehalt aufweisen, sind unter anderem als Füllmaterial für karbidhaltige Ueberzüge (Cr₂C₃; WC) im Triebswerkbau verwendet worden.In order to be able to meet the numerous demands, the blades of rotating thermal machines are often provided with protective layers. This is used for both steam and gas turbine blades as well as for compressor blades. The main thing is to increase resistance to corrosion and oxidizing attack as well as erosion and wear (wear and tear). Among the substances used for protective layers, the element Cr, Al, Si forming the oxide cover layers occupy a special position. Layers which have a high Al content have been used, inter alia, as filler material for carbide-containing coatings (Cr₂C₃; WC) in engine construction.
Zum Stand der Technik werden folgende Druckschriften angegeben:
- F.N. Davis, C.E. Grinnell, "Engine Experience of Turbine Rotor Blade Materials and Coatings", The American Society of Mechanical Engineers, 345 E. 47 ST. New York, N.Y. 10017, 82-GT-244
- SermeTel Technische Information: "SermaLoy J-Prozess STS", SermeTel GmbH, Weilenburgstrasse 49, D-5628 Heiligenhaus, BRD
- Mark F. Mosser and Bruce G. McMordie, "Evaluation of Aluminium/Ceramic Coating on Fasteners to Eliminate Galvanic Corrosion", Reprinted from SP-649-Corrosion: Coatings and Steels, International Congress and Exposition, Detroit, Michigan, February 24-28, 1986, ISSN 0148-7191, Copyright 1986 Society of Automotive Engineers, Inc.
- Thomas F. Lewis III, "Gator-Gard, The Process, Coatings, and Turbomachinery Applications", Presented at the International Gas Turbine Conference and Exhibit, Düsseldorf, West Germany - June 8-12, 1986, The American Society of Mechanical Engineers, 345 E. 47 St., New York, N.Y. 10017, 86-GT-306
- H.J. Kolkman, "New Erosion Resistant Compressor Coatings", Presented at the Gas Turbine and Aeroengine Congress, Amsterdam, The Netherlands - June 6-9, 1988, The American Society of Mechanical Engineers, 345 E. 47. St., New York, N.Y. 10017, 88-GT-186.The following publications are given regarding the state of the art:
- FN Davis, CE Grinnell, "Engine Experience of Turbine Rotor Blade Materials and Coatings", The American Society of Mechanical Engineers, 345 E. 47 ST. New York, NY 10017, 82-GT-244
- SermeTel Technical Information: "SermaLoy J-Process STS", SermeTel GmbH, Weilenburgstrasse 49, D-5628 Heiligenhaus, FRG
- Mark F. Mosser and Bruce G. McMordie, "Evaluation of Aluminum / Ceramic Coating on Fasteners to Eliminate Galvanic Corrosion ", Reprinted from SP-649-Corrosion: Coatings and Steels, International Congress and Exposition, Detroit, Michigan, February 24-28, 1986, ISSN 0148-7191, Copyright 1986 Society of Automotive Engineers, Inc.
- Thomas F. Lewis III, "Gator-Gard, The Process, Coatings, and Turbomachinery Applications", Presented at the International Gas Turbine Conference and Exhibit, Duesseldorf, West Germany - June 8-12, 1986, The American Society of Mechanical Engineers , 345 E. 47 St., New York, NY 10017, 86-GT-306
- HJ Kolkman, "New Erosion Resistant Compressor Coatings", Presented at the Gas Turbine and Aeroengine Congress, Amsterdam, The Netherlands - June 6-9, 1988, The American Society of Mechanical Engineers, 345 E. 47th St., New York , NY 10017, 88-GT-186.
Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren zur Erhöhung des Korrosions- (Cl- und SO₄-Ionen) und Erosionswiderstandes (Partikel- und Tropfenschlagerosion) einer Schaufel einer rotierenden thermischen Maschine bei Anwesenheit von H₂O-Dampf und vergleichsweise mässigen Temperaturen (450 °C) auzugeben, welches sich besonders für ferritisches und/oder ferritisch-martensitisches Grundmaterial der Schaufel eignet, wobei kostengünstig und ohne grossen Aufwand eine geeignete Oberflächenschicht erzielt werden soll. Es soll insbesondere das Auftreten von Lochfrass-Korrosion vermieden oder min destens hinausgezögert werden, um der Schaufel eine längere Lebensdauer zu gewährleisten.The invention has for its object a method for increasing the corrosion (Cl and SO₄ ions) and erosion resistance (particle and drop impact erosion) of a blade of a rotating thermal machine in the presence of H₂O steam and comparatively moderate temperatures (450 ° C ) which is particularly suitable for ferritic and / or ferritic-martensitic base material of the blade, a suitable surface layer being to be achieved inexpensively and without great effort. In particular, the occurrence of pitting corrosion should be avoided or min be delayed to ensure a longer lifespan for the bucket.
Diese Aufgabe wird dadurch gelöst, dass im eingangs erwähnten Verfahren eine Schutzschicht bestehend aus 6 bis 15 Gew.-% Si, Rest Al nach dem Hochgeschwindigkeitsverfahren mit einer Partikelgeschwindigkeit von mindestens 300 m/s auf die Oberfläche des Grundmaterials aufgespritzt wird.This object is achieved in that, in the process mentioned at the outset, a protective layer consisting of 6 to 15% by weight of Si, remainder Al is sprayed onto the surface of the base material by the high-speed process at a particle speed of at least 300 m / s.
Die Erfindung wird anhand der nachfolgenden Ausführungsbeispiele beschrieben:The invention is described using the following exemplary embodiments:
Eine Verdichterschaufel für einen Axialkompressor wurde mit einer Schutzschicht versehen. Die Schicht hatte Traflügelprofil, wobei das Schaufelblatt folgende Abmessungen aufwies:
Breite = 80 mm
Grösste Dicke = 9 mm
Profilhöhe = 14 mm
Radiale Länge = 210 mmA compressor blade for an axial compressor was provided with a protective layer. The layer had a wing profile, and the airfoil had the following dimensions:
Width = 80 mm
Biggest thickness = 9 mm
Profile height = 14 mm
Radial length = 210 mm
Der Werkstoff der Schaufel war ein martensitischer Stahl, der im voll vergüteten Gefügezustand vorlag und folgende Zusammensetzung aufwies:
Cr = 12 Gew.-%
Mo = 1 Gew.-%
Ni = 0,5 Gew.-%
C = 0,25 Gew.-%
Fe = RestThe material of the blade was a martensitic steel, which was in the fully tempered structural state and had the following composition:
Cr = 12% by weight
Mo = 1% by weight
Ni = 0.5% by weight
C = 0.25% by weight
Fe = rest
Die Schaufel wurde zunächst in Trichloräthan entfettet und gereinigt, worauf das Blatt und der Uebergang Blass/Fuss sandgestrahlt wurde. Die Beschichtung der Schaufel wurde nach einem Hochgeschwindigkeits-Flammspritzverfahren mit einer Partikelgeschwindigkeit von 400 m/s und einer Gasgeschwindigkeit von 1000 m/s mit Stickstoff als Fördergas durchgeführt. Als Beschichtungsmaterial wurde eine Aluminiumlegierung der nachfolgenden Zusammen-setzung verwendet, die in Pulverform vorlag:
Si = 12,8 Gew.-%
Mn = 0,22 Gew.-%
Mg = 0,34 Gew.-%
Ti = 0,1 Gew.-%
Al = RestThe scoop was first degreased and cleaned in trichloroethane, whereupon the blade and the pale / foot transition were sandblasted. The coating of the blade was carried out using a high-speed flame spraying process with a particle speed of 400 m / s and a gas speed of 1000 m / s with nitrogen as the conveying gas. An aluminum alloy of the following composition, which was in powder form, was used as the coating material:
Si = 12.8% by weight
Mn = 0.22% by weight
Mg = 0.34% by weight
Ti = 0.1% by weight
Al = rest
Gemäss dem hier angewendeten Beschichtungsverfahren mit der Markenbezeichnung "Jet-Kote" wurde das Aluminiumlegie rungspulver mittels Stickstoff in eine mit Propan und Sauerstoff betriebene Brennkammer gefördert. Die verflüssigten Partikel wurden als feine Tropfen unter hohem Ueberdruck auf das Werkstück geschleudert. Dabei stand die Schaufel in einer Vorrichtung, die den Schaufelfuss abdeckte. Die Aufbringung der Schutzschicht erfolgte mit der von Hand geführten Spritzpistole. Die aufgetragene Schutzschicht wurde anhand eines metallographischen Schliffes gemessen und betrug im Mittel 8 bis 15 µm. Auf diese Metall-Schutzschicht wurde nach einem herkömmlichen Lackspritzverfahren ein Kunststoff (im vorliegenden Fall Polytetrafluoräthylen) aufgetragen. Diese glatte Oberflächenschicht hatte eine durchschnittliche Dicke von 6 bis 10 µm und eine Rauheit von ca. 2 µm.According to the coating process used here with the brand name "Jet-Kote", the aluminum alloy powder was conveyed by means of nitrogen into a combustion chamber operated with propane and oxygen. The liquefied particles were thrown onto the workpiece as fine drops under high excess pressure. The blade stood in a device that covered the blade root. The protective layer was applied with the hand-held spray gun. The applied protective layer was measured using a metallographic cut and was in Average 8 to 15 µm. A plastic (in the present case polytetrafluoroethylene) was applied to this metal protective layer using a conventional paint spraying process. This smooth surface layer had an average thickness of 6 to 10 µm and a roughness of approximately 2 µm.
Die beschichtete Verdichterschaufel wurde einer Prüfung auf Korrosionsbeständigkeit unterworfen. Zu diesem Zweck wurde sie in eine Prüflösung getaucht und danach in einem Klimaschrank während 4 h ausgelagert. Dieser Zyklus wurde insgesamt 60 x wiederholt. Die Prüflösung bestand aus einer wässrigen Lösung der folgenden Salze:
220 g/l (NH₄)₂FeSO₄ . 6H₂O
50 g/l NaCl
pH = 3 - 3,5
Temperatur Klimaschrank = 45 °C
Luftfeuchtigkeit = 100 %
Prüfdauer/Zyklus = 4 h
Zahl der Zyklen = 60The coated compressor blade was subjected to a corrosion resistance test. For this purpose, it was immersed in a test solution and then stored in a climatic cabinet for 4 hours. This cycle was repeated a total of 60 times. The test solution consisted of an aqueous solution of the following salts:
220 g / l (NH₄) ₂FeSO₄. 6H₂O
50 g / l NaCl
pH = 3 - 3.5
Temperature cabinet = 45 ° C
Humidity = 100%
Test duration / cycle = 4 h
Number of cycles = 60
Die metallographischen Untersuchungen zeigten, dass nach diesen Korrosionsversuchen weder an den aufgebrachten Schichten noch am Grundmaterial irgendwelche Veränderungen festgestellt werden konnten.
Zum Vergleich wurde eine nach einem herkömmlichen Spritzverfahren mit je einer Aluminiumschicht und einer Kunststoffschicht versehene Verdichterschaufel geprüft. Nach 60 Prüfzylen waren die Schutzschichten weitgehend zerstört und lamellenförmige Schuppen herausgebrochen.The metallographic examinations showed that after these corrosion tests, no changes could be found either on the applied layers or on the base material.
For comparison, a compressor blade was tested using a conventional spraying method, each with an aluminum layer and a plastic layer. After 60 test cycles, the protective layers were largely destroyed and lamellar scales broke out.
Eine Verdichterschaufel gleicher Abmessungen und Zusammensetzung wurde gemäss Beispiel 1 mit einer Aluminiumlegierung und einem Kunststoff beschichtet. Nun wurde auf der beschichteten Schaufel ein der Längsachse paralleler Kratzer von 10 mm Länge und total durchschnittlich 25 µm Tiefe angebracht, dessen Profil also mit seiner Spitze gerade noch das Grundmaterial knapp erfasste. Dann wurde die Schaufel den gleichen Korrosionsprüfungen wie in Beispiel 1 unterworfen. Dank der Lokalelementbildung (Aluminiumschicht funktioniert als "Opferanode") wurde das Grundmaterial weitgehend geschützt, während die Aluminiumschicht an den Flanken des Kratzers nur geringfügig abgebaut wurde. Durch die Wanderung der Al-Ionen im korrosiven Medium als "Elektrolyt" und deren Entladung an der elektropositiven Elektrode (Fe) des Grundmaterials kommt der korrosive Angriff in vielen Fällen zum Stillstand. Durch diese Simulierung der Oberflächenbeschädigung durch auftreffende Partikel im Betrieb und deren Verhalten unter korrosiver Atmosphäre wurde bewiesen, dass die erfindungsgemässe Schutzschicht unter praktischen Einsatzbedingungen eine lange Lebensdauer zu erwarten lässt.A compressor blade of the same dimensions and composition was coated according to Example 1 with an aluminum alloy and a plastic. Now a scratch of 10 mm length and a total of 25 µm depth parallel to the longitudinal axis was made on the coated blade, the profile of which just barely grasped the base material with its tip. The blade was then subjected to the same corrosion tests as in Example 1. Thanks to the local element formation (aluminum layer functions as a "sacrificial anode"), the base material was largely protected, while the aluminum layer on the flanks of the scratch was only slightly degraded. Due to the migration of the Al ions in the corrosive medium as an "electrolyte" and their discharge at the electropositive electrode (Fe) of the base material, the corrosive attack comes to a standstill in many cases. By simulating the surface damage caused by impinging particles during operation and their behavior under a corrosive atmosphere, it was proven that the protective layer according to the invention can be expected to have a long service life under practical conditions of use.
Eine Verdichterschaufel wurde mit einer Schutzschicht versehen. Der Tragflügel des Schaufelblattes hatte die nachfolgenden Abmessungen:
Breite = 100 mm
Grösste Dicke = 10,5 mm
Profilhöhe = 18 mm
Radiale Länge = 265 mmA compressor blade was provided with a protective layer. The airfoil wing had the following dimensions:
Width = 100 mm
Greatest thickness = 10.5 mm
Profile height = 18 mm
Radial length = 265 mm
Der Werkstoff der Schaufel bestand aus einem martensitisch-austenitischen Zweiphasenstahl mit geringem Austenitanteil und lag im vergüteten Zustand vor. Die Zusammensetzung war die folgende:
CR = 15,5 Gew.-%
Mo = 1,28 Gew.-%
Ni = 5,4 Gew.-%
C = 0,2 Gew.-%
Fe = RestThe material of the blade consisted of a martensitic-austenitic two-phase steel with a low austenite content and was available in a tempered condition. The composition was as follows:
CR = 15.5% by weight
Mo = 1.28% by weight
Ni = 5.4% by weight
C = 0.2% by weight
Fe = rest
Nach dem üblichen Entfetten, Reinigen und Sandstrahlen wurde das Schaufelblatt zusätzlich gezielt kugelgestrahlt. Durch diese Oberflächenbehandlung wurde die Randzone des Grundmaterials kaltverformt und verdichtet, so dass sie Druckeigenspannungen aufwies. Damit wurde erreicht, dass die Wechselfestigkeit (Ermüdungsfestigkeit) durch Abbau der Spannungen auf der Zugseite im Betrieb erhöht wurde. Für die Beschichtung der Schaufel nach dem Hochgeschwindigkeits-Flammspritzverfahren mit einer Partikelgeschwindigkeit von 450 m/s und einer Gasgeschwindigkeit von 1200 m/s mit Stickstoff als Fördermittel wurde eine Aluminiumlegierung der nachfolgenden Zusammensetzung verwendet:
Si = 10,65 Gew.-%
Mn = 0,37 Gew.-%
Mg = 0,1 Gew.-%
Al = RestAfter the usual degreasing, cleaning and sandblasting, the airfoil was also shot peened. As a result of this surface treatment, the edge zone of the base material was cold worked and compressed so that it had residual compressive stresses. It was thus achieved that the fatigue strength was increased by reducing the tension on the train side during operation. An aluminum alloy of the following composition was used to coat the blade using the high-speed flame spraying process with a particle speed of 450 m / s and a gas speed of 1200 m / s with nitrogen as the conveying medium:
Si = 10.65% by weight
Mn = 0.37% by weight
Mg = 0.1% by weight
Al = rest
Das Aufspritzen der Aluminiumlegierung erfolgte mit einem Industrieroboter. Es wurden 3 Spritzgänge durchgeführt. Die Dicke der aufgetragenen Schicht betrug im Durchschnitt 90 bis 100 µm. Auf diese Metall-Schutzschicht wurde zusätzlich eine Kunststoffschicht von ca. 10 bis 15 µm Dicke nach einem üblichen Lackspritzverfahren aufgetragen.
Die beschichtete Schaufel wurde der gleichen Prüfung auf Korrosion unterzogen wie in Beispiel 1. Es konnte danach keinerlei Angriff festgestellt werden.The aluminum alloy was sprayed on using an industrial robot. 3 spray coats were carried out. The thickness of the applied layer averaged 90 to 100 μm. A plastic layer of approx. 10 to 15 µm thickness was additionally applied to this metal protective layer using a conventional paint spraying process.
The coated blade was subjected to the same corrosion test as in Example 1. No attack was then found.
Eine gebrauchte Verdichterschaufel mit Tragflügelprofil wurde mit einer Schutzschicht versehen. Das Schaufelblatt hatte die nachfolgenden Abmessungen:
Breite = 63 mm
Grösste Dicke = 8 mm
Profilhöhe = 12 mm
Radiale Länge = 140 mmA used compressor blade with wing profile was provided with a protective layer. The airfoil had the following dimensions:
Width = 63 mm
Biggest thickness = 8 mm
Profile height = 12 mm
Radial length = 140 mm
Das Grundmaterial der Schaufel war ein martensitischer Stahl im hochfest vergüteten Gefügezustand, dessen Zusammensetzung nachstehend wiedergegeben ist:
Cr = 11,73 Gew.-%
Mo = 0,8 Gew.-%
V = 0,1 Gew.-%
C = 0,22 Gew.-%
Fe = RestThe base material of the shovel was a martensitic steel in a highly strengthened structural state, the composition of which is shown below:
Cr = 11.73% by weight
Mo = 0.8% by weight
V = 0.1% by weight
C = 0.22% by weight
Fe = rest
Im vorliegenden Fall handelte es sich um eine nach üblichen Verfahren beschichtete Schaufel, welche beträchtliche Betriebsschäden in Form von Lochfrass-Korrosion, die sich teilweise auch auf das Grundmaterial erstreckte, aufwies. Diese gebrauchte Schaufel wurde zunächst entfettet, überschliffen und sandgestrahlt, um die Schäden zu beseitigen. Dann wurde die Oberflächenzone des Grundmaterials durch Kugelstrahlen verdichtet. Die Beschichtung erfolgte mit einer Aluminiumlegierung folgender Zusammensetzung:
Si = 6,84 Gew.-%
Mn = 0,3 Gew.-%
Mg = 0,36 Gew.-%
Ti = 0,1 Gew.-%
Al = RestIn the present case, the blade was coated using customary methods and showed considerable operational damage in the form of pitting corrosion, which in some cases also extended to the base material. This used shovel was first degreased, ground and sandblasted to remove the damage. Then the surface zone of the base material was compacted by shot peening. The coating was made with an aluminum alloy of the following composition:
Si = 6.84% by weight
Mn = 0.3% by weight
Mg = 0.36% by weight
Ti = 0.1% by weight
Al = rest
Das Aufspritzen der Metallschicht erfolgte von Hand nach dem Hochgeschwindigkeits-Flammspritzverfahren. Die Dicke der Schutzschicht schwankte zwischen 25 und 45 µm. Die metallographischen Prüfungen nach dem oben angegebenen Korrosionsversuch ergaben eine unveränderte, nicht angegriffene Oberflächenzone.The metal layer was sprayed on by hand using the high-speed flame spraying process. The thickness of the protective layer fluctuated between 25 and 45 µm. The metallographic tests after the corrosion test indicated above showed an unchanged, unaffected surface zone.
Die Erfindung ist nicht auf die Ausführungsbeispiele beschränkt.The invention is not restricted to the exemplary embodiments.
Das Verfahren zur Erhöhung des Korrosions- und Erosionswiderstandes einer Schaufel einer rotierenden thermischen Maschine, die im wesentlichen aus einem ferritischen und/oder ferritisch-martensitischen Grundmaterial besteht, wird durch Aufbringen einer fest haftenden Oberflächenschutzschicht durchgeführt, indem eine Schutzschicht bestehend aus 6 bis 15 Gew.-% Si, Rest Al nach dem Hochgeschwindigkeitsverfahren mit einer Partikelgeschwindigkeit von mindestens 300 m/s auf die Oberfläche des Grundmaterials aufgespritzt wird. Vorzugsweise besteht das Grundmaterial aus einem chromhaltigen Stahl mit 12 bis 13 Gew.-% Cr und weiteren Zusätzen. Die Schutzschicht enthält in vorteilhafter Weise 10 bis 12 Gew.-% Si, Rest Al. Auf die besagte Schutzschicht wird zur Verfeinerung der Oberfläche vorzugsweise zusätzlich eine Deckschicht aus einem wärmebständigen Kunststoff aufgetragen.The method for increasing the corrosion and erosion resistance of a blade of a rotating thermal machine, which essentially consists of a ferritic and / or ferritic-martensitic base material, is carried out by applying a firmly adhering surface protective layer by a Protective layer consisting of 6 to 15 wt .-% Si, remainder Al is sprayed onto the surface of the base material by the high-speed method with a particle speed of at least 300 m / s. The base material preferably consists of a chromium-containing steel with 12 to 13% by weight of Cr and further additives. The protective layer advantageously contains 10 to 12% by weight of Si, the rest of Al. To refine the surface, a cover layer made of a heat-resistant plastic is preferably additionally applied to said protective layer.
Claims (5)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH252/89 | 1989-01-26 | ||
CH252/89A CH678067A5 (en) | 1989-01-26 | 1989-01-26 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0379699A1 true EP0379699A1 (en) | 1990-08-01 |
EP0379699B1 EP0379699B1 (en) | 1993-10-06 |
Family
ID=4182772
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP89123291A Expired - Lifetime EP0379699B1 (en) | 1989-01-26 | 1989-12-15 | Method for enhancing the corrosion and erosion resistance of the blade of a rotary thermal apparatus and blade produced ba said method |
Country Status (5)
Country | Link |
---|---|
US (1) | US5120613A (en) |
EP (1) | EP0379699B1 (en) |
JP (1) | JP2895135B2 (en) |
CH (1) | CH678067A5 (en) |
DE (1) | DE58905843D1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5547769A (en) * | 1992-10-05 | 1996-08-20 | Siemens Aktiengesellschaft | Method and coating for protecting against corrosive and erosive attacks |
WO2000070190A1 (en) * | 1999-05-14 | 2000-11-23 | Siemens Aktiengesellschaft | Component and method for producing a protective coating on a component |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9218859D0 (en) * | 1992-09-05 | 1992-10-21 | Rolls Royce Plc | Aluminide-silicide coatings |
SE508860C2 (en) * | 1997-03-18 | 1998-11-09 | Abb Stal Ab | Device on a guide rail arranged in a rotor machine and a rotatable turbine rail |
US7546683B2 (en) * | 2003-12-29 | 2009-06-16 | General Electric Company | Touch-up of layer paint oxides for gas turbine disks and seals |
DE102007028321A1 (en) * | 2007-06-15 | 2008-12-18 | Alstom Technology Ltd. | Process for surface treatment of Cr steels |
FR2978931B1 (en) | 2011-08-10 | 2014-05-09 | Snecma | METHOD FOR PRODUCING A PROTECTIVE REINFORCEMENT ON THE EDGE OF A BLADE |
US9309895B2 (en) | 2012-06-18 | 2016-04-12 | Kennametal Inc. | Closed impeller with a coated vane |
US9737933B2 (en) | 2012-09-28 | 2017-08-22 | General Electric Company | Process of fabricating a shield and process of preparing a component |
KR20160053121A (en) * | 2014-10-31 | 2016-05-13 | 현대자동차주식회사 | Coating method for shift fork and shift fork with amorphous coating layer by using the same |
JP6375238B2 (en) * | 2015-02-05 | 2018-08-15 | 三菱日立パワーシステムズ株式会社 | Steam turbine and surface treatment method thereof |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1148292A (en) * | 1955-05-02 | 1957-12-05 | Union Carbide & Carbon Corp | Method of applying high melting point materials in the pulverized state |
GB973012A (en) * | 1962-03-27 | 1964-10-21 | Grundy Teddington Ltd | Method of marking metal articles such as casks and like containers |
EP0114232A1 (en) * | 1982-12-20 | 1984-08-01 | Goetze Ag | Flame spray powder for producing wear-resistant coatings |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS56102546A (en) * | 1980-01-22 | 1981-08-17 | Toyota Motor Corp | Sliding member |
GB2116215B (en) * | 1982-03-06 | 1985-09-25 | Rolls Royce | Improvements in or relating to flame sprayed coatings |
US4500364A (en) * | 1982-04-23 | 1985-02-19 | Exxon Research & Engineering Co. | Method of forming a protective aluminum-silicon coating composition for metal substrates |
JPS60149761A (en) * | 1984-01-13 | 1985-08-07 | Showa Denko Kk | Coating method for providing corrosion resistance |
US4707379A (en) * | 1985-12-24 | 1987-11-17 | Ceskoslovenska Akademie Ved | Protective layer for carbonaceous materials and method of applying the same |
JPS63303048A (en) * | 1987-06-03 | 1988-12-09 | Toyota Motor Corp | Shift fork |
-
1989
- 1989-01-26 CH CH252/89A patent/CH678067A5/de not_active IP Right Cessation
- 1989-12-15 EP EP89123291A patent/EP0379699B1/en not_active Expired - Lifetime
- 1989-12-15 DE DE89123291T patent/DE58905843D1/en not_active Expired - Fee Related
-
1990
- 1990-01-26 JP JP2015157A patent/JP2895135B2/en not_active Expired - Lifetime
-
1991
- 1991-04-09 US US07/683,472 patent/US5120613A/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1148292A (en) * | 1955-05-02 | 1957-12-05 | Union Carbide & Carbon Corp | Method of applying high melting point materials in the pulverized state |
GB973012A (en) * | 1962-03-27 | 1964-10-21 | Grundy Teddington Ltd | Method of marking metal articles such as casks and like containers |
EP0114232A1 (en) * | 1982-12-20 | 1984-08-01 | Goetze Ag | Flame spray powder for producing wear-resistant coatings |
Non-Patent Citations (3)
Title |
---|
PATENT ABSTRACTS OF JAPAN, Band 13, Nr. 137 (C-582)[3485], 5. April 1989; & JP-A-63 303 048 (TOYOTA MOTOR CORP.) 09-12-1988 * |
PATENT ABSTRACTS OF JAPAN, Band 5, Nr. 178 (C-78)[850], 14. November 1981; & JP-A-56 102 546 (TOYOTA JIDOSHA KOGYO K.K.) 17-08-1981 * |
PATENT ABSTRACTS OF JAPAN, Band 9, Nr. 309 (C-318)[2032], 5. Dezember 1985; & JP-A-60 149 761 (SHOWA DENKO K.K.) 07-08-1985 * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5547769A (en) * | 1992-10-05 | 1996-08-20 | Siemens Aktiengesellschaft | Method and coating for protecting against corrosive and erosive attacks |
WO2000070190A1 (en) * | 1999-05-14 | 2000-11-23 | Siemens Aktiengesellschaft | Component and method for producing a protective coating on a component |
US6755613B1 (en) | 1999-05-14 | 2004-06-29 | Siemens Aktiengesellschaft | Component and method for producing a protective coating on a component |
Also Published As
Publication number | Publication date |
---|---|
DE58905843D1 (en) | 1993-11-11 |
JPH02230902A (en) | 1990-09-13 |
CH678067A5 (en) | 1991-07-31 |
US5120613A (en) | 1992-06-09 |
JP2895135B2 (en) | 1999-05-24 |
EP0379699B1 (en) | 1993-10-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69924591T2 (en) | Repair of high-pressure scraper rings of turbines | |
EP2088225B1 (en) | Erosion and corrosion-resistant coating system and process therefor | |
KR100836972B1 (en) | Cobalt-based alloy for the coating of organs subject to erosion by liquid | |
DE102009010110B4 (en) | Erosion protection coating system for gas turbine components | |
KR20080063449A (en) | Method for treating organs subject to erosion by liquids and anti-erosion coating alloy | |
US20100247321A1 (en) | Anti-fouling coatings and articles coated therewith | |
EP0379699B1 (en) | Method for enhancing the corrosion and erosion resistance of the blade of a rotary thermal apparatus and blade produced ba said method | |
DE69123631T2 (en) | Coating of steel bodies | |
US5547769A (en) | Method and coating for protecting against corrosive and erosive attacks | |
Swadźba et al. | Influence of coatings obtained by PVD on the properties of aircraft compressor blades | |
US20090004364A1 (en) | Method For Protecting New/Used Engine Parts | |
DE2842848C2 (en) | Material for covering objects | |
US20050158460A1 (en) | Method for protecting new/used engine parts | |
Sartwell et al. | HVOF thermal spray coatings replace hard chrome | |
WO2009049597A2 (en) | Wear protection coating | |
DE69109077T2 (en) | Aluminumization of objects, protected by a thermally blocked coating system. | |
US6383658B1 (en) | Thermally sprayed coatings having an interface with controlled cleanliness | |
EP1291449B1 (en) | Coating process and coated substrate subject to friction | |
EP0451512B1 (en) | Process for coating impeller blades | |
JP2012527537A (en) | Method for improving the corrosion and oxidation resistance of the lower platform region of a gas turbine blade | |
JP2012527536A (en) | Corrosion-resistant article | |
DE102020000848B4 (en) | Process for coating blades of compressors, turbines and propellers | |
WO1982001898A1 (en) | Method for coating a metal with a protection layer resistant to hot gas corrosion | |
WO2005005690A1 (en) | Method for producing a protective layer, protective layer, use thereof, and part provided with a protective layer | |
WO1997028289A1 (en) | Iron-based spray material for producing a corrosion-resistant coating, process for producing the coating and use of the coat |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): CH DE GB LI |
|
17P | Request for examination filed |
Effective date: 19901229 |
|
17Q | First examination report despatched |
Effective date: 19920629 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): CH DE GB LI |
|
REF | Corresponds to: |
Ref document number: 58905843 Country of ref document: DE Date of ref document: 19931111 |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 19931215 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20011116 Year of fee payment: 13 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 20011120 Year of fee payment: 13 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20011208 Year of fee payment: 13 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20021215 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20021231 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20021231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20030701 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20021215 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |