US20150132495A1 - Machine component with a cavitation resistant coating - Google Patents
Machine component with a cavitation resistant coating Download PDFInfo
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- US20150132495A1 US20150132495A1 US14/598,922 US201514598922A US2015132495A1 US 20150132495 A1 US20150132495 A1 US 20150132495A1 US 201514598922 A US201514598922 A US 201514598922A US 2015132495 A1 US2015132495 A1 US 2015132495A1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/011—Layered products comprising a layer of metal all layers being exclusively metallic all layers being formed of iron alloys or steels
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- 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
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/20—Ferrous alloys, e.g. steel alloys containing chromium with copper
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/34—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/36—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.7% by weight of carbon
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- 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
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- 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
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
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- 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
- C23C24/00—Coating starting from inorganic powder
- C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
- C23C24/10—Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
- C23C24/103—Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
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- 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
- C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
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- 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
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
- C23C30/005—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process on hard metal substrates
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- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/004—Cylinder liners
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- 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.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
- Y10T428/12958—Next to Fe-base component
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- 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.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
- Y10T428/12958—Next to Fe-base component
- Y10T428/12965—Both containing 0.01-1.7% carbon [i.e., steel]
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- 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.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
- Y10T428/12972—Containing 0.01-1.7% carbon [i.e., steel]
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- 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.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
- Y10T428/12972—Containing 0.01-1.7% carbon [i.e., steel]
- Y10T428/12979—Containing more than 10% nonferrous elements [e.g., high alloy, stainless]
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- 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
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
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- 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
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- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
Definitions
- the present disclosure relates generally to a cavitation resistant coating, and more particularly, to a machine component with a cavitation resistant coating.
- Coatings are sometimes used to impart desirable properties to machine components.
- a coating may be used to increase the cavitation resistance of a component.
- Cavitation is material damage caused by the formation and collapse of bubbles, in a liquid. The cavities typically arise from rapid changes in pressure due to vibrations or turbulent flow. During cavitation, the implosion of the bubbles formed in the liquid on the component surface erodes the surface. Cavitation is a source of concern in machine parts that are subject to vibratory forces while in contact with a liquid. Different materials offer different levels of resistance to cavitation.
- Cast iron is a material known to have relatively low resistance to cavitation. Examples of cast iron machine components that are susceptible to cavitation include, among others, housings of pumps and liners of engine cylinders.
- a cylinder liner (referred to herein as a “liner”) is a removable cylindrical part fitted into an engine block of an internal combustion engine to form a cylinder.
- liners are made of steel or cast iron.
- An inside surface of the liner bounds the combustion chamber of the cylinder.
- the liners get heated due to the combustion of fuel in the combustion chamber.
- a liquid coolant such as, water
- the outer surface of the liner is in direct contact with the coolant circulating through the cooling jacket. It is known that the region of the liner in contact with the coolant experiences erosion from cavitation.
- the outer surface of the liner may be treated to increase its resistance to cavitation.
- U.S. Pat. No. 7,617,805 discloses a method of heat treating the outer surface of the liner to provide a hardened layer of purely martensitic microstructure to inhibit cavitation induced erosion. While the hardened outer layer of the '805 patent may provide some protection from cavitation induced erosion, it may not provide sufficient cavitation protection and/or be suitable for all applications.
- the present disclosure is directed to overcoming these or other limitations in existing technology.
- a machine component may include a body made of an iron alloy.
- the body may include a surface and a coating fused to the surface.
- the coating may be an alloy including phosphorous, carbon, and iron.
- the coating may have a solidus temperature of less than or equal to about 1000° C., and a hardness greater than or equal to about 50 HRC.
- a method of forming a cavitation-resistant coating on a surface of a machine component may include preparing the surface of the component for coating, and applying a coating to the surface.
- the coating may include phosphorous, carbon, and iron.
- the method may also include heating the surface to at least partially melt the applied coating at a temperature less than or equal to about 1000° C.
- the method may further include cooling the at least partially melted coating to fuse the coating to the surface.
- the fused coating may have a hardness greater than or equal to about 50 HRC.
- a machine component may include a body having a surface, and a coating fused to the surface.
- the coating may be an alloy including between about 4-12% by weight of phosphorous, about 0.5-3.5% by weight of carbon, and iron.
- the coating may have a solidus temperature less than or equal to about 1000° C.
- FIG. 1 is a cross-sectional view of part of an engine with a cylinder liner
- FIG. 2 is a flow chart illustrating an exemplary method of making a cavitation resistant coating of the cylinder liner of FIG. 1 .
- FIG. 1 is a cross-sectional view of part of an engine 10 with a cylinder liner 12 (“liner 12 ”).
- Engine 10 includes an engine block 14 comprising a piston bore 16 .
- Liner 12 may be removably mounted in the piston bore 16 .
- Liner 12 has a hollow generally cylindrical body extending along a longitudinal axis 20 with an inner surface 22 and an outer surface 24 .
- the liner 12 may be securely retained in piston bore 16 in any manner.
- a cylinder head 34 secured to the engine block 14 , forms a combustion chamber of the engine 10 within the bore 16 .
- the combustion chamber is bounded on the sides by the inner surface 22 of the liner 12 .
- combustion that occurs in the combustion chamber heats the liner 12 .
- Engine block 14 may include a cooling jacket 18 , which circulates a coolant (for example, water) along the outer surface 24 , to cool the liner 12 .
- a coolant for example, water
- FIG. 1 illustrates a single annular cooling jacket 18 around the liner 12 , as is known in the art, other configurations are possible.
- multiple discrete or connected cooling jackets 18 may extend along portions of the liner 12 .
- the surface of the liner 12 in contact with the coolant in cooling jacket 18 is susceptible to cavitation.
- Liner 12 may be made of various iron alloys, including cast iron and steel. During operation of engine 10 , vibrations induced in the liner 12 (as a result of normal engine operation) result in the formation of vapor bubbles in the coolant in cooling jacket 18 . These bubbles may implode against an outer surface 24 of the liner 12 and cause cavitation damage (or pitting) on the outer surface 24 . To protect the outer surface 24 from cavitation damage (or to restore the cavitation damaged outer surface 24 ), a cavitation resistant coating 42 may be applied to the outer surface 24 . Coating 42 may be an iron-based alloy fused to the outer surface 24 of the liner 12 . It is known that materials having high hardness generally exhibit better cavitation resistance.
- coating 42 is selected to have a hardness greater than or equal to about 50 HRC.
- the coating 42 may extend substantially along an entire length of the liner 12 , or may only extend along selected portions of the length of the liner 12 .
- the coating 42 may cover the outer surface 24 of the liner 12 that is exposed to the coolant in coolant jacket 18 .
- coating 42 may extend circumferentially around liner 12 over substantially all portions of the liner 12 that forms a boundary wall of the coolant jacket 18 .
- Coating 42 may include an iron-based alloy that may be deposited or otherwise applied to the outer surface 24 of liner 12 and fused (at least partially melted and bonded) to the outer surface 24 .
- the materials that form coating 42 may be applied as a paste, thermal sprayed, or deposited in some other manner (as would be known to a person of ordinary skill in the art) to outer surface 24 .
- the coated outer surface 24 may be heated to above the solidus temperature of the coating 42 , to at least partially melt and fuse the coating 42 to the outer surface 24 .
- the solidus temperature of the coating 42 is the temperature at which melting of the coating 42 begins.
- the coating 42 may not be melted completely (i.e., the solidus is not necessarily a melting point), and the coating 42 will exist as a mixture of solid and liquid phases. In embodiments where the coating 42 is heated to the liquidus temperature or above, the coating 42 will be completely melted. While the coating 42 is above the solidus temperature, the coating 42 (which will be at least partially melted) will enter and fill (partially or fully) crevices and/or surface irregularities (such as, cavitation holes) on outer surface 24 and form a surface layer securely attached to the outer surface 24 .
- the fusing of the coating 42 to the underlying outer surface 24 increases the bond strength of the coating 42 to be more than after typical deposition techniques.
- the thickness of coating may be between 0.5-4 mm. In some embodiments, the coating thickness may be between about 1-2 mm.
- a liner 12 (or another component that the coating 42 is applied on) is exposed to during fusing of the coating 42 .
- cast iron has a melting temperature of about 1300° C. Therefore, during application of a coating 42 on a cast iron liner 12 , it is desirable to maintain the processing temperature of the cast iron liner 12 to well below 1300° C.
- the solidus temperature of coating 42 is selected to be less than or equal to about 1100° C. Solidus temperatures above about 1100° C. may induce heat related damage (softening, warping, etc.) to the liner 12 .
- the solidus temperature of the coating 42 may be selected to be less than or equal to about 1000° C.
- the coated outer surface 24 may be heated to above the solidus temperature of the coating 42 by any suitable heating process (for example, using a torch, induction heating, laser heating, placing in a furnace) at any ramp rate.
- the outer surface 24 (or the entire liner 12 ) may be soaked at the maximum temperature for a sufficient time to ensure that all regions of the coating 42 are heated.
- a brazing-like heating cycle may be used to fuse the coating 42 on the outer surface 24 .
- the outer surface 24 may be cooled to room or ambient temperature.
- the coating 42 may be cooled to ambient temperature by any means.
- the coating 42 may be cooled to ambient temperature at a fast cooling rate (for example, ⁇ 100° C./sec) using liquid quenching or cooling under a high pressure gas stream (gas quenching).
- a fast cooling rate for example, ⁇ 100° C./sec
- gas quenching liquid quenching
- liquid and gas quenching may be avoided, and the coated component may be cooled to ambient temperature at a cooling rate of less than or equal to about 10° C./sec in still or forced gas such as, for example, air (air cooling).
- the coating 42 will transform to martensite (that is, harden). Avoiding a quenching step during cooling may simplify the coating process. Avoiding a quenching step may also improve the durability of the coated liner 12 by eliminating thermal shock associated with quenching.
- the chemistry of the coating 42 may be selected so that the coating 42 does not need to be quenched in order for the coating 42 to achieve the desired hardness of greater than about 50 HRC (Rockwell C).
- Coating 42 may include phosphorous (P) and carbon (C) in a matrix of iron (Fe). Phosphorous and carbon will decrease the solidus temperature of the coating 42 .
- the iron-carbon-phosphorous ternary phase diagram may be used to determine the percentage ranges of phosphorous and carbon (the balance being iron) in coating 42 that may produce an Fe—P—C alloy having a solidus temperature less than or equal to the desired value (for example, 1000° C.).
- an Fe—P—C alloy of about 7% by weight of phosphorous and about 2% by weight of carbon and about 91% by weight of iron referred to as Fe-7P-2C alloy
- Fe-7P-2C alloy has a solidus temperature of about 950° C.
- the coating 42 may include about 7% by weight of phosphorous, about 2% by weight of carbon, and about 91% by weight of iron. Other concentrations of phosphorous and carbon also result in an alloy having a solidus temperature less than or equal to about 1000° C.
- the Fe—P—C ternary phase diagram (or software applications such as, for example, Thermo-Calc) may be used to find Fe—P—C alloys that have a solidus temperature below about 1000° C. (or below some other desired temperature).
- coating 42 may have between about 4-12% by weight of phosphorous, and about 0.5-3.5% by weight of carbon, and balance iron. In some embodiments, coating 42 may have about 7-9% by weight of phosphorous, and about 1.5-2.5% by weight of carbon, and balance iron.
- Addition of copper (Cu) may further reduce the solidus temperature.
- addition of about 5% of copper to the Fe-7P-2C alloy may decrease the solidus temperature of the alloy to about 930° C. Therefore, in some embodiments, coating 42 may also include copper.
- copper may have a concentration between about 0.1-15% by weight. That is, a coating 42 having about 4-12% by weight of phosphorous and about 0.5-3.5% by weight of carbon may include any amount of copper between about 0.1-15% by weight. In some embodiments of coating 42 , the concentration of copper (if present) may be between about 5-10% by weight. Addition of other elements may also decrease the solidus temperature of the coating 42 .
- the addition of about 0.5% of boron (B) to an iron-based coating 42 having about 4-12% by weight of phosphorous and about 0.5-3.5% by weight of carbon (with or without about 0.1-15% by weight of copper) further decreases the solidus temperature by about 10° C. Therefore, in some embodiments, the coating 42 may also include boron.
- Coating 42 may also include other elements for other desirable properties.
- coating 42 may include one or more of chromium (Cr), manganese (Mn), silicon (Si), nickel (Ni), molybdenum (Mo), vanadium (V), tungsten (W), and cobalt (Co) to improve the air-hardenability of the coating 42 . That is, one or more of these elements may be added to coating 42 so that the coating 42 has a martensitic microstructure with a hardness greater than or equal to about 50 HRC upon air cooling (that is, when the fused coating is cooled to ambient temperature without a quenching step). The amount of these hardenability improving elements may depend upon the application.
- the amount of these elements in coating 42 may be sufficient to provide the desired level of hardness upon air cooling without substantially increasing the cost of the coated component.
- Table 1 below shows the chemistry of different exemplary embodiments (marked a, b, c, etc.) of coating 42 . It should be noted that the concentration of elements in coating 42 are indicated as being approximate (in Table I and in the text) because of expected experimental variations. These experimental variations are expected to less than about 10% of a measured value (that is, an alloy having about (or approximately) 0.1% Cu may have copper from 0.09%-0.11%). It should be noted that, although not individually listed herein, an embodiment of coating 42 in Table I may have any composition within a listed range.
- a coating of embodiment “a” may include coatings 42 having compositions Fe-7P-2C-5Cu, Fe-6P-3C-4Cu-0.5B, Fe-8P-2.5C-2Ni-1Cr, Fe-5P-3C-1B-4Ni, etc.
- a Fe-7P-2C-5Cu coating includes about 7% of phosphorous, about 2% of carbon, about 5% of copper, with the remaining (that is, about 86%) being iron.
- coating 42 may have any concentration of constituents within a listed range that yields an alloy have a solidus temperature less than or equal to about 1000° C. and a hardness greater than or equal to about 50 HRC.
- the concentration of a constituent above the maximum value listed in Table I may increase the cost and/or impart undesirable properties to the coated component.
- amounts of Mn and Ni above that listed in Table I may increase the cost of the coated component and decrease the hardness of the resulting coating 42 .
- coating 42 is describes as being used to increase the cavitation resistance of a component, this is not a limitation. In some embodiments, coating 42 may be applied to impart other desirable properties to a component. For instance, it is contemplated that in some embodiments, a coating 42 may be applied to increase the wear resistance of a crank shaft.
- the disclosed machine component may be applied in any application where it is desired to increase the resistance of the component to cavitation-induced damage.
- a cavitation resistant coating may be fused to a surface of the machine component that operates in communication with a liquid, and may therefore be subjected to cavitation-induced erosion.
- the fused cavitation resistant coating has a solidus temperature less than or equal to about 1100° C. (or about 1000° C.) and a hardness greater than or equal to about 50 HRC.
- the coating may include phosphorous and carbon in a matrix of iron with limited amounts of other elements.
- FIG. 2 discloses an exemplary method of applying the coating 42 on the liner 12 .
- the outer surface 24 of the liner 12 may be prepared for applying the coating 42 (step 100 ).
- Liner 12 may be a newly fabricated liner 12 or a previously used liner 12 that is being refurbished.
- the outer surface 24 may first be cleaned. The cleaning process may involve degreasing and removal of remnants, if any, of a previous coating from the outer surface 24 .
- Powders of elements in a desired concentration may be mixed with a commercial binder (glue, etc.) to form a paste or a slurry (step 110 ).
- the slurry may be applied to the outer surface 24 (step 120 ) of the liner 12 . Any process (such as, for example, painting) may be used to apply the slurry to the outer surface 24 .
- the applied slurry may then be dried in air or in a low temperature furnace.
- the outer surface 24 may then be heated to above the solidus temperature (for example, of less than or equal to about 1000° C.) to at least partially melt the slurry (step 130 ). Any heating process may be used to heat the outer surface 24 .
- the liner 12 with the applied slurry may be placed in a furnace maintained at a temperature slightly above the solidus temperature for about 10 minutes to evenly heat the slurry.
- the soak time (the time for which the component is maintained at the temperature above the solidus temperature of the slurry) may depend on the application (size of the component, number of components in the furnace, etc.).
- the liner 12 may then be cooled to ambient temperature in air (step 140 ).
- Cooling the liner 12 may include cooling the coating 42 under a cooling rate of less than or equal to about 10° C./sec in still gas or a forced gas stream.
- air cooling may include shutting the furnace off and allowing the coated liner 12 to cool slowly in the furnace. Air cooling may also include removing the coated liner 12 from the furnace and allowing the liner 12 to cool to ambient temperature outside the furnace.
- cooling the liner 12 may include any method of cooling, the liner 12 to ambient temperature without quenching the liner 12 .
- the at least partially melted slurry may fuse with the outer surface 24 to form a coating 42 having a hardness greater than or equal to about 50 HRC.
- a coating 42 of the current disclosure may be applied to any iron alloy component. It will be apparent to those skilled in the art that various modifications and variations can be made to the disclosed machine component. Other embodiments will be apparent to those skilled in the art from consideration of the specification and practice of the disclosed machine component. It is intended that the specification and examples be considered as exemplary only, with a true scope being indicated by the following claims and their equivalents.
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Abstract
A machine component may include a body made of an iron alloy. The body may include a surface, and a coating fused to the surface. The coating may be an alloy including phosphorous, carbon, and iron. The coating may have solidus temperature of less than or equal to about 1000° C., and a hardness greater than or equal to about 50 HRC.
Description
- The present disclosure relates generally to a cavitation resistant coating, and more particularly, to a machine component with a cavitation resistant coating.
- Coatings are sometimes used to impart desirable properties to machine components. For instance, a coating may be used to increase the cavitation resistance of a component. Cavitation is material damage caused by the formation and collapse of bubbles, in a liquid. The cavities typically arise from rapid changes in pressure due to vibrations or turbulent flow. During cavitation, the implosion of the bubbles formed in the liquid on the component surface erodes the surface. Cavitation is a source of concern in machine parts that are subject to vibratory forces while in contact with a liquid. Different materials offer different levels of resistance to cavitation. Cast iron is a material known to have relatively low resistance to cavitation. Examples of cast iron machine components that are susceptible to cavitation include, among others, housings of pumps and liners of engine cylinders.
- A cylinder liner (referred to herein as a “liner”) is a removable cylindrical part fitted into an engine block of an internal combustion engine to form a cylinder. Typically, liners are made of steel or cast iron. An inside surface of the liner bounds the combustion chamber of the cylinder. During operation of the engine, the liners get heated due to the combustion of fuel in the combustion chamber. To cool the liner, a liquid coolant (such as, water) is circulated through a cooling jacket extending about a portion of the outer surface of the liner. Typically, the outer surface of the liner is in direct contact with the coolant circulating through the cooling jacket. It is known that the region of the liner in contact with the coolant experiences erosion from cavitation. Typically, the outer surface of the liner may be treated to increase its resistance to cavitation.
- U.S. Pat. No. 7,617,805 (the '805 patent) discloses a method of heat treating the outer surface of the liner to provide a hardened layer of purely martensitic microstructure to inhibit cavitation induced erosion. While the hardened outer layer of the '805 patent may provide some protection from cavitation induced erosion, it may not provide sufficient cavitation protection and/or be suitable for all applications.
- The present disclosure is directed to overcoming these or other limitations in existing technology.
- In one aspect, a machine component is disclosed. The component may include a body made of an iron alloy. The body may include a surface and a coating fused to the surface. The coating may be an alloy including phosphorous, carbon, and iron. The coating may have a solidus temperature of less than or equal to about 1000° C., and a hardness greater than or equal to about 50 HRC.
- In another aspect, a method of forming a cavitation-resistant coating on a surface of a machine component is disclosed. The method may include preparing the surface of the component for coating, and applying a coating to the surface. The coating may include phosphorous, carbon, and iron. The method may also include heating the surface to at least partially melt the applied coating at a temperature less than or equal to about 1000° C. The method may further include cooling the at least partially melted coating to fuse the coating to the surface. The fused coating may have a hardness greater than or equal to about 50 HRC.
- In yet another aspect, a machine component is disclosed. The component may include a body having a surface, and a coating fused to the surface. The coating may be an alloy including between about 4-12% by weight of phosphorous, about 0.5-3.5% by weight of carbon, and iron. The coating may have a solidus temperature less than or equal to about 1000° C.
-
FIG. 1 is a cross-sectional view of part of an engine with a cylinder liner; and -
FIG. 2 is a flow chart illustrating an exemplary method of making a cavitation resistant coating of the cylinder liner ofFIG. 1 . -
FIG. 1 is a cross-sectional view of part of anengine 10 with a cylinder liner 12 (“liner 12”).Engine 10 includes anengine block 14 comprising apiston bore 16.Liner 12 may be removably mounted in thepiston bore 16.Liner 12 has a hollow generally cylindrical body extending along alongitudinal axis 20 with aninner surface 22 and anouter surface 24. Theliner 12 may be securely retained inpiston bore 16 in any manner. Acylinder head 34, secured to theengine block 14, forms a combustion chamber of theengine 10 within thebore 16. The combustion chamber is bounded on the sides by theinner surface 22 of theliner 12. During operation of theengine 10, combustion that occurs in the combustion chamber heats theliner 12.Engine block 14 may include acooling jacket 18, which circulates a coolant (for example, water) along theouter surface 24, to cool theliner 12. AlthoughFIG. 1 illustrates a singleannular cooling jacket 18 around theliner 12, as is known in the art, other configurations are possible. For example, in some embodiments, multiple discrete or connectedcooling jackets 18 may extend along portions of theliner 12. The surface of theliner 12 in contact with the coolant incooling jacket 18 is susceptible to cavitation. -
Liner 12 may be made of various iron alloys, including cast iron and steel. During operation ofengine 10, vibrations induced in the liner 12 (as a result of normal engine operation) result in the formation of vapor bubbles in the coolant incooling jacket 18. These bubbles may implode against anouter surface 24 of theliner 12 and cause cavitation damage (or pitting) on theouter surface 24. To protect theouter surface 24 from cavitation damage (or to restore the cavitation damaged outer surface 24), a cavitationresistant coating 42 may be applied to theouter surface 24.Coating 42 may be an iron-based alloy fused to theouter surface 24 of theliner 12. It is known that materials having high hardness generally exhibit better cavitation resistance. It was determined that a hardness of about 50 HRC (Rockwell C) provides sufficient cavitation resistance for typical machine components. Therefore,coating 42 is selected to have a hardness greater than or equal to about 50 HRC. Thecoating 42 may extend substantially along an entire length of theliner 12, or may only extend along selected portions of the length of theliner 12. In some embodiments, thecoating 42 may cover theouter surface 24 of theliner 12 that is exposed to the coolant incoolant jacket 18. In some embodiments, coating 42 may extend circumferentially aroundliner 12 over substantially all portions of theliner 12 that forms a boundary wall of thecoolant jacket 18. -
Coating 42 may include an iron-based alloy that may be deposited or otherwise applied to theouter surface 24 ofliner 12 and fused (at least partially melted and bonded) to theouter surface 24. The materials that formcoating 42 may be applied as a paste, thermal sprayed, or deposited in some other manner (as would be known to a person of ordinary skill in the art) toouter surface 24. After application, the coatedouter surface 24 may be heated to above the solidus temperature of thecoating 42, to at least partially melt and fuse thecoating 42 to theouter surface 24. As would be known to a person or ordinary skill in the art, the solidus temperature of thecoating 42 is the temperature at which melting of thecoating 42 begins. At the solidus temperature, thecoating 42 may not be melted completely (i.e., the solidus is not necessarily a melting point), and thecoating 42 will exist as a mixture of solid and liquid phases. In embodiments where thecoating 42 is heated to the liquidus temperature or above, thecoating 42 will be completely melted. While thecoating 42 is above the solidus temperature, the coating 42 (which will be at least partially melted) will enter and fill (partially or fully) crevices and/or surface irregularities (such as, cavitation holes) onouter surface 24 and form a surface layer securely attached to theouter surface 24. The fusing of thecoating 42 to the underlyingouter surface 24 increases the bond strength of thecoating 42 to be more than after typical deposition techniques. In some embodiments, after fusing, the thickness of coating may be between 0.5-4 mm. In some embodiments, the coating thickness may be between about 1-2 mm. - In some embodiments, it is desirable to minimize the maximum temperature that a liner 12 (or another component that the
coating 42 is applied on) is exposed to during fusing of thecoating 42. For instance, cast iron has a melting temperature of about 1300° C. Therefore, during application of acoating 42 on acast iron liner 12, it is desirable to maintain the processing temperature of thecast iron liner 12 to well below 1300° C. To ensure thatcoating 42 is suitable for application on common iron alloys used for machine components, the solidus temperature ofcoating 42 is selected to be less than or equal to about 1100° C. Solidus temperatures above about 1100° C. may induce heat related damage (softening, warping, etc.) to theliner 12. For increased margin and reliablity, in some embodiments, the solidus temperature of thecoating 42 may be selected to be less than or equal to about 1000° C. The coatedouter surface 24 may be heated to above the solidus temperature of thecoating 42 by any suitable heating process (for example, using a torch, induction heating, laser heating, placing in a furnace) at any ramp rate. In some embodiments, the outer surface 24 (or the entire liner 12) may be soaked at the maximum temperature for a sufficient time to ensure that all regions of thecoating 42 are heated. In some embodiments, a brazing-like heating cycle may be used to fuse thecoating 42 on theouter surface 24. - After heating the
coating 42 to above the solidus temperature to at least partially melt thecoating 42, the outer surface 24 (or the liner 12) may be cooled to room or ambient temperature. Thecoating 42 may be cooled to ambient temperature by any means. In some embodiments, thecoating 42 may be cooled to ambient temperature at a fast cooling rate (for example, ≧100° C./sec) using liquid quenching or cooling under a high pressure gas stream (gas quenching). In some embodiments, liquid and gas quenching may be avoided, and the coated component may be cooled to ambient temperature at a cooling rate of less than or equal to about 10° C./sec in still or forced gas such as, for example, air (air cooling). As thecoating 42 cools, thecoating 42 will transform to martensite (that is, harden). Avoiding a quenching step during cooling may simplify the coating process. Avoiding a quenching step may also improve the durability of thecoated liner 12 by eliminating thermal shock associated with quenching. In such embodiments, the chemistry of thecoating 42 may be selected so that thecoating 42 does not need to be quenched in order for thecoating 42 to achieve the desired hardness of greater than about 50 HRC (Rockwell C). -
Coating 42 may include phosphorous (P) and carbon (C) in a matrix of iron (Fe). Phosphorous and carbon will decrease the solidus temperature of thecoating 42. In general, the iron-carbon-phosphorous ternary phase diagram may be used to determine the percentage ranges of phosphorous and carbon (the balance being iron) incoating 42 that may produce an Fe—P—C alloy having a solidus temperature less than or equal to the desired value (for example, 1000° C.). For instance, an Fe—P—C alloy of about 7% by weight of phosphorous and about 2% by weight of carbon and about 91% by weight of iron (referred to as Fe-7P-2C alloy) has a solidus temperature of about 950° C. Therefore, in some embodiments, thecoating 42 may include about 7% by weight of phosphorous, about 2% by weight of carbon, and about 91% by weight of iron. Other concentrations of phosphorous and carbon also result in an alloy having a solidus temperature less than or equal to about 1000° C. As is known in the art, the Fe—P—C ternary phase diagram (or software applications such as, for example, Thermo-Calc) may be used to find Fe—P—C alloys that have a solidus temperature below about 1000° C. (or below some other desired temperature). In general, coating 42 may have between about 4-12% by weight of phosphorous, and about 0.5-3.5% by weight of carbon, and balance iron. In some embodiments, coating 42 may have about 7-9% by weight of phosphorous, and about 1.5-2.5% by weight of carbon, and balance iron. - Addition of copper (Cu) may further reduce the solidus temperature. For example, addition of about 5% of copper to the Fe-7P-2C alloy may decrease the solidus temperature of the alloy to about 930° C. Therefore, in some embodiments, coating 42 may also include copper. If present in
coating 42, copper may have a concentration between about 0.1-15% by weight. That is, acoating 42 having about 4-12% by weight of phosphorous and about 0.5-3.5% by weight of carbon may include any amount of copper between about 0.1-15% by weight. In some embodiments ofcoating 42, the concentration of copper (if present) may be between about 5-10% by weight. Addition of other elements may also decrease the solidus temperature of thecoating 42. For example, the addition of about 0.5% of boron (B) to an iron-basedcoating 42 having about 4-12% by weight of phosphorous and about 0.5-3.5% by weight of carbon (with or without about 0.1-15% by weight of copper) further decreases the solidus temperature by about 10° C. Therefore, in some embodiments, thecoating 42 may also include boron. -
Coating 42 may also include other elements for other desirable properties. For example, in some embodiments, coating 42 may include one or more of chromium (Cr), manganese (Mn), silicon (Si), nickel (Ni), molybdenum (Mo), vanadium (V), tungsten (W), and cobalt (Co) to improve the air-hardenability of thecoating 42. That is, one or more of these elements may be added to coating 42 so that thecoating 42 has a martensitic microstructure with a hardness greater than or equal to about 50 HRC upon air cooling (that is, when the fused coating is cooled to ambient temperature without a quenching step). The amount of these hardenability improving elements may depend upon the application. In general, the amount of these elements incoating 42 may be sufficient to provide the desired level of hardness upon air cooling without substantially increasing the cost of the coated component. Table 1 below shows the chemistry of different exemplary embodiments (marked a, b, c, etc.) ofcoating 42. It should be noted that the concentration of elements incoating 42 are indicated as being approximate (in Table I and in the text) because of expected experimental variations. These experimental variations are expected to less than about 10% of a measured value (that is, an alloy having about (or approximately) 0.1% Cu may have copper from 0.09%-0.11%). It should be noted that, although not individually listed herein, an embodiment ofcoating 42 in Table I may have any composition within a listed range. For example, a coating of embodiment “a” may includecoatings 42 having compositions Fe-7P-2C-5Cu, Fe-6P-3C-4Cu-0.5B, Fe-8P-2.5C-2Ni-1Cr, Fe-5P-3C-1B-4Ni, etc. Further, as discussed previously, a Fe-7P-2C-5Cu coating includes about 7% of phosphorous, about 2% of carbon, about 5% of copper, with the remaining (that is, about 86%) being iron. In general, coating 42 may have any concentration of constituents within a listed range that yields an alloy have a solidus temperature less than or equal to about 1000° C. and a hardness greater than or equal to about 50 HRC. -
Approximate percentage concentration (%) by weight Elements (a) (b) (c) (f) (g) (h) (i) P 4-12 4-12 5-10 6-8 6-8 6-8 7-9 C 0.5-3.5 0.5-3.5 1.5-3 1.0-2.5 1.0-2.5 1.0-2.5 1.5-2.5 Cu 0.1-15 0.5-15 2-10 — 3-7 — 5-10 B 0-1 0.2-1 0.25-1 — — 0.25-1 — Si 0-3 0.2-3 0.5-3 — — — — Mn 0-1.5 0.2-1.5 0.5-1.5 — — — 1-2.5 Ni 0-5 0-5 0-2 — — — — Cr 0-15 0.1-15 5-10 5-13 5-13 5-13 5-13 Mo 0-11 0.2-11 0.5-3 — — — — V 0-6 0.2-6 0.1-2 — — — — Fe Balance Balance Balance Balance Balance Balance Balance - In some applications of
coating 42, the concentration of a constituent above the maximum value listed in Table I may increase the cost and/or impart undesirable properties to the coated component. For example, in some applications, amounts of Mn and Ni above that listed in Table I may increase the cost of the coated component and decrease the hardness of the resultingcoating 42. - It should be noted that, although the
coating 42 is describes as being used to increase the cavitation resistance of a component, this is not a limitation. In some embodiments, coating 42 may be applied to impart other desirable properties to a component. For instance, it is contemplated that in some embodiments, acoating 42 may be applied to increase the wear resistance of a crank shaft. - The disclosed machine component may be applied in any application where it is desired to increase the resistance of the component to cavitation-induced damage. A cavitation resistant coating may be fused to a surface of the machine component that operates in communication with a liquid, and may therefore be subjected to cavitation-induced erosion. The fused cavitation resistant coating has a solidus temperature less than or equal to about 1100° C. (or about 1000° C.) and a hardness greater than or equal to about 50 HRC. In general, the coating may include phosphorous and carbon in a matrix of iron with limited amounts of other elements. An exemplary method of forming a cavitation
resistant coating 42 on theouter surface 24 of acylinder liner 12 is described below. -
FIG. 2 discloses an exemplary method of applying thecoating 42 on theliner 12. Theouter surface 24 of theliner 12 may be prepared for applying the coating 42 (step 100).Liner 12 may be a newly fabricatedliner 12 or a previously usedliner 12 that is being refurbished. To prepare theliner 12 for application of the coating, theouter surface 24 may first be cleaned. The cleaning process may involve degreasing and removal of remnants, if any, of a previous coating from theouter surface 24. Powders of elements in a desired concentration (for example, about 6-8% by weight of phosphorous, about 1-3% by weight of carbon, about 3-7% by weight of copper, with balance being iron) may be mixed with a commercial binder (glue, etc.) to form a paste or a slurry (step 110). The slurry may be applied to the outer surface 24 (step 120) of theliner 12. Any process (such as, for example, painting) may be used to apply the slurry to theouter surface 24. The applied slurry may then be dried in air or in a low temperature furnace. Theouter surface 24, with the applied slurry, may then be heated to above the solidus temperature (for example, of less than or equal to about 1000° C.) to at least partially melt the slurry (step 130). Any heating process may be used to heat theouter surface 24. In some embodiments, theliner 12 with the applied slurry may be placed in a furnace maintained at a temperature slightly above the solidus temperature for about 10 minutes to evenly heat the slurry. In general, the soak time (the time for which the component is maintained at the temperature above the solidus temperature of the slurry) may depend on the application (size of the component, number of components in the furnace, etc.). Theliner 12 may then be cooled to ambient temperature in air (step 140). Cooling theliner 12 may include cooling thecoating 42 under a cooling rate of less than or equal to about 10° C./sec in still gas or a forced gas stream. In embodiments where theliner 12 is heated in a furnace, air cooling may include shutting the furnace off and allowing thecoated liner 12 to cool slowly in the furnace. Air cooling may also include removing thecoated liner 12 from the furnace and allowing theliner 12 to cool to ambient temperature outside the furnace. In general, cooling theliner 12 may include any method of cooling, theliner 12 to ambient temperature without quenching theliner 12. During cooling, the at least partially melted slurry may fuse with theouter surface 24 to form acoating 42 having a hardness greater than or equal to about 50 HRC. - Although aspects of the current disclosure are described using a cylinder liner, in general, a
coating 42 of the current disclosure may be applied to any iron alloy component. It will be apparent to those skilled in the art that various modifications and variations can be made to the disclosed machine component. Other embodiments will be apparent to those skilled in the art from consideration of the specification and practice of the disclosed machine component. It is intended that the specification and examples be considered as exemplary only, with a true scope being indicated by the following claims and their equivalents.
Claims (8)
1-10. (canceled)
11. A method of forming a cavitation-resistant coating on a surface of a machine component, comprising:
preparing the surface of the component for coating;
applying a coating including phosphorous, carbon, and iron to the surface;
heating the surface to at least partially melt the applied coating at a temperature less than or equal to about 1000° C.; and
cooling the at least partially melted coating to fuse the coating to the surface, the fused coating having a hardness greater than or equal to about 50 HRC.
12. The method of claim 11 , wherein cooling the at least partially melted coating includes cooling the coating to ambient temperature at cooling rate of less than or equal to about 10° C./sec.
13. The method of claim 11 , wherein applying the coating includes applying a coating including about 4-12% by weight of phosphorous, and about 0.5-3.5% by weight of carbon to the surface.
14. The method of claim 13 , wherein the coating further includes copper between about 0.1-15% by weight.
15. The method of claim 13 , wherein the coating further includes at least one of boron less than or equal to 1% by weight, silicon less than or equal to about 3% by weight, manganese between about 0.1-5% by weight, nickel less than or equal to about 5% by weight, chromium between about 0.1-15% by weight, molybdenum less than or equal to about 11% by weight, and vanadium less than or equal to 6% by weight.
16. The method of claim 11 , wherein applying the coating includes applying a coating including about 7-9% by weight of phosphorous, and about 1.5-2.5% by weight of carbon.
17-20. (canceled)
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US9528171B2 (en) | 2014-09-16 | 2016-12-27 | Caterpillar Inc. | Alloy for seal ring, seal ring, and method of making seal ring for seal assembly of machine |
BR112019026489B1 (en) * | 2017-06-21 | 2023-02-07 | Höganäs Ab | ALLOY TO IRON BASE SUITABLE FOR PROVIDING ON A SUBSTRATE A HARD AND WEAR-RESISTANT COATING, ARTICLE HAVING A HARD AND WEAR-RESISTANT COATING, AND METHOD FOR FORMING THEREOF |
US10400707B2 (en) * | 2017-07-26 | 2019-09-03 | GM Global Technology Operations LLC | Method and system for processing an automotive engine block |
US11028799B2 (en) | 2019-08-30 | 2021-06-08 | Deere & Company | Selective engine block channeling for enhanced cavitation protection |
CN114807820B (en) * | 2022-05-17 | 2023-05-23 | 中国科学院兰州化学物理研究所 | Early warning protective coating with cavitation erosion luminescence function and preparation method thereof |
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US6197437B1 (en) * | 1999-02-22 | 2001-03-06 | Wall Colmonoy Corporation | Casting alloys and method of making composite barrels used in extrusion and injection molding |
US6767419B1 (en) * | 2000-11-09 | 2004-07-27 | Bechtel Bwxt Idaho, Llc | Methods of forming hardened surfaces |
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US20130157081A1 (en) | 2013-06-20 |
WO2013095778A1 (en) | 2013-06-27 |
US9017823B2 (en) | 2015-04-28 |
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