US2588422A - Application of spray metal linings for aluminum engine cylinders of or for reciprocating engines - Google Patents
Application of spray metal linings for aluminum engine cylinders of or for reciprocating engines Download PDFInfo
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- US2588422A US2588422A US792836A US79283647A US2588422A US 2588422 A US2588422 A US 2588422A US 792836 A US792836 A US 792836A US 79283647 A US79283647 A US 79283647A US 2588422 A US2588422 A US 2588422A
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- metal
- molybdenum
- aluminum
- spray
- sprayed
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- 229910052751 metal Inorganic materials 0.000 title claims description 96
- 239000002184 metal Substances 0.000 title claims description 96
- 239000007921 spray Substances 0.000 title claims description 53
- 229910052782 aluminium Inorganic materials 0.000 title claims description 49
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 49
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 48
- 239000011733 molybdenum Substances 0.000 claims description 42
- 229910052750 molybdenum Inorganic materials 0.000 claims description 42
- 238000000576 coating method Methods 0.000 claims description 26
- 239000011248 coating agent Substances 0.000 claims description 24
- 238000000034 method Methods 0.000 description 22
- 238000005507 spraying Methods 0.000 description 19
- 230000003750 conditioning effect Effects 0.000 description 8
- 229910001182 Mo alloy Inorganic materials 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 7
- 239000000203 mixture Substances 0.000 description 7
- 238000007788 roughening Methods 0.000 description 7
- 229910000831 Steel Inorganic materials 0.000 description 5
- 239000007789 gas Substances 0.000 description 5
- 150000002739 metals Chemical class 0.000 description 5
- 239000002245 particle Substances 0.000 description 5
- 239000010959 steel Substances 0.000 description 5
- 229910000975 Carbon steel Inorganic materials 0.000 description 4
- 238000005422 blasting Methods 0.000 description 4
- 239000010962 carbon steel Substances 0.000 description 4
- 230000001788 irregular Effects 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000000227 grinding Methods 0.000 description 3
- 239000004576 sand Substances 0.000 description 3
- 229910000906 Bronze Inorganic materials 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910001018 Cast iron Inorganic materials 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 239000010974 bronze Substances 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- MGRWKWACZDFZJT-UHFFFAOYSA-N molybdenum tungsten Chemical compound [Mo].[W] MGRWKWACZDFZJT-UHFFFAOYSA-N 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 238000013517 stratification Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910001339 C alloy Inorganic materials 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910000760 Hardened steel Inorganic materials 0.000 description 1
- 229910000677 High-carbon steel Inorganic materials 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 239000012809 cooling fluid Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010291 electrical method Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Classifications
-
- 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
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- 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
- C23C4/08—Metallic material containing only metal elements
Definitions
- This invention relatesto new and useful improvements in spray. metal linings for aluminum engine cylinders ofor for reciprocating engines.
- Sprayed metal offers advantageous bearing characteristics due to its porosity and inherent oil retention properties. Furthermore hard sprayed metals can be applied, such as hardened steels, at temperatures which do not. affect the physical properties of the aluminum.
- metal spraying In metal spraying the metalto be applied is projected against the surface to be covered in the form of a spray, the particles of which are in a molten or heat plastic condition.
- metal spraying is carried outwith "the use "of metal spray guns, i. e.,devices in which the metal is fed to a heating zone from which zonemetal particles, at least someof'whichare molten or in a heat plastic condition, are propelled against the surface to be sprayed. 'The propulsionmay be --effected either by centrifugal means'or by means of-a'blast of air or other gas.
- Suchrod or wire may be a relatively solid rod or Wire of such metal, or alternatively it maybe composed of particles of. such metal bonded together by. a suitable binder such as a plastic material. In the latter case the binder is usually of the kind-which willvolatilize asthe result of ;the applied heat of .the spray gun.
- the applied spray metaladheres to the surface of the cylinderwall with a high degree of bond for otherwise the applied spray metal may come off.
- the. surface to which the spray metal is to beapplied must be,-.as a, rule, suitably pre-conditioned.
- pre-conditioning treatment has been generally of two kinds, roughening and heating. vRoughening has been carried out by mechanical roughening and also rougheningby the deposition of metalby an electricalfusing.ora welding procedure.
- Mechanical rougheningof the aluminumcylinder surface to adapt the same to receive and retain applied spray metalmust be of a type involving the formation of multiple number of closely spaced cavities with peened and splayed edges and interspaces forming a ,multitudeyof keyways.
- the.most common method of procuring has been by sand or grit blasting.
- Sand or grit blasting alone, however, does not, produce a sufficiently strong bond to aluminum to. retain the applied, spraymetal under the conditions of serviceto which analuminum: engine cylinder is subjected.
- the cost of the finished product includes the extra cost of grooving the entire "inside: surface of the cylinder, such as by threading, by the amount of additional sprayed metal which must be sprayed to fill the grooves and particularly by the cost of machining or grinding the sprayed cylinder to remove the eXcess metal which must be sprayed on the ridges between the grooves.
- Another limitation of this procedure is due to the weakening effect and consequent reduction in fatigue strength of the aluminum cylinder.
- the heating method of surface conditioning a metallic base to bond thereto applied spray metal involves the heating of the surface to a relatively high temperature and thereafter spraying the hot surface with metal.
- This method is not widely used and requires, as a general rule, considerable skill and elaborate equipment and is relatively expensive.
- the temperature to which the surface or base must be heated usually is so high that it tends to seriously weaken the aluminum.
- a further limitation in the method of heating to produce bonding resides in the fact that aluminum oxidizes to an objectionable degree when heated in air.
- One object of the invention comprises, inter alia, a method for applying spray metal to the bore of aluminum engine cylinders which is substantially free from the aforementioned limitations inherent in hitherto known practices.
- Another object of the invention is to provide a method for applying spray metal to the bore of aluminum engine cylinders with a high degree of bond and without materially affecting more than a thin skin of the surface of said cylinder bore.
- a further object of the invention is an aluminum engine cylinder lined with a spray metal substantially adhering thereto with a high degree ofbond and preferably one substantially harder than the'aluminum of the cylinder.
- the method in accordance with the invention essentially embraces an improvement in the application of spray metal to the bore surface of an aluminum engine cylinderwith a high degree of bond, which comprises conditioning such surface for spray metal bonding by spraying at least a flash coating of molybdenum thereon and thereafter spraying a metal, and preferably a metal substantially harder than the aluminum of said bore, onto the thusly coated surface.
- 1y comprises an engine cylinder having an aluminum bore surface, a layer of spray metal, preferably substantially harder than the aluminum of said bore surface, and intermediate said layer of spray metal and said bore surface, in surface-to-surface bond therewith, sprayed molybdenum of at least flash coating thickness.
- aluminum engine cylinder or similar term is used herein, it is intended to denote thereby the cylinder of any engine having an aluminum or aluminum alloy bore surface and in which a reciprocating piston operates, whether or not the engine is used for the production of power or simply the application of power, such as engine cylinders of, for instance, internal combustion engines, steam engines, gas compressors, pumps, refrigeration compressors, positive displacement hydraulic pumps, etc.
- the metal spraying is preferably carried out by use of a metal spray gun, using wire or rod as a source of metal.
- the molybdenum that I may use in accordance with my invention may be pure molybdenum or a molybdenum alloy or composition. In the latter case I prefer a relatively high molybdenum content, such as an alloy or composition having or more molybdenum. I may, however, use any alloy of molybdenum having 60% or greater molybdenum content and alloyed with any other metals which are known to alloy with molybde-.
- molybdenum is used herein, it is intended to designate thereby substantially pure molybdenum as well as alloys or compositions containing at least 60% molybdenum.
- a molybdenum composition I mean thereby a composition containing finely divided metallic molybdenum in combination with other elements or metal and not necessarily alloyed therewith.
- the surface of the aluminum cylinder bore tobe metal sprayed may be perfectly smooth and no roughening or other conditioning treatment other than cleaning (if necessary) is required.
- the surface to be sprayed upon with molybdenum should, however, be a clean surface.
- any metal which is capable of being sprayed may then be sprayed directly on to the molybdenum sprayed surface.
- the final metal to be sprayed should be selected according to its characteristics to meet the requirement of the particular engine cylinder being done.
- a. common metal to use for an ordinary internal combustion engine would be a high carbon steel, in cases where the final finishing can be done by grinding. -Where the finishing must be done by boring with a tool, a low carbon steel could be used.
- stainless steel or bronze or other metals are recommended to provide the particular wear-resistant and corrosion-resistant requirements of the particular engine being manufactured.
- the preheating may be unnecessary and is carried out at relatively low temperatures (as compared with the temperatures required by heat bonding methods).
- the primary purpose of such a preheat step is to cause expansion of the cylinder before the application of. the final sprayed coating to reduce the stress onthe bond at the interface between sprayed coating and aluminum cylinder bore.
- the temperatures commonlyused for this purpose are of the order of magnitude of about 300 F.
- Such grooves or other irregular contours have several advantageous functions although they are not a necessary requirement of the procedure set forth in this invention.
- One of the advantageous functions of grooves or other irregular contours of the base is the increase in surface area which such contours provide, which results in an increase in bond to the sprayed metal due to such increased area of bonding.
- Another advantageous function of such contours is the beneficial effect on the structure of the sprayed metal layer. Such beneficial effect is due to the folding of the stratification layers of such sprayed metal structure. Sprayed metal structures resulting from spraying onto a surface with an irregular contour are generally stronger due to the folding of stratifications or laminations than the structures resulting from the spraying of the same metal onto a substantially even surface.
- a metallizing gunof the-wires type is used for the carrying out of my ;inven'tion,.I prefer to use arod or wire of essentially. pure molybdenum produced by sintering wpowdered molybdenum.
- a sintered rodor Wire may be sprayed directly in such.
- Example An automotive internal combustionengine aluminum cylinder block is first bored for the'cylinder holes using a conventional machine tool and method.
- the last boring operation iswdone dry, without oil or cooling fluids, so .as to produce a clean metal surface.
- Reasonably fast machine feeds may be used since it is notnecessaryto produce-a particularly smooth finish.
- 'A reasonable tolerance for the size of this bore. is allowed. such as a tolerance of .005 inch.
- the size of the bore is made sufficiently over size to provide sufiicient space for the sprayed metal coatingsof the desired thickness.
- a practical thickness to use in this case is a total thickness of sprayed metal layers of .032 inch measured on a side so that the boreof the cylinder is approximately .064; inch larger than the desired finished size.
- the cylinder block is then preheated in an oven to a temperatureof 300 F.
- a. flash coating in,this case about .002 inch thick, of molybdenum is .applied to the surface of each cylinder bore by metal spraying.
- This coating isapplied by a conventional metallizing gunof the wire feed type, utilizing .091 inch diameter sintered and drawn molybdenum wire.
- An angular gun nozzle-extension is used and held with its nozzle end .at a' distance of about 2 inches from. the. bore; surface.
- the total length of the extension is about 1.- foot, and it is so constructed-thatthe heatinguand atomizing portion is at theend of the extension.
- Such an extension is fittedwith an angular nozzle Which sprays at an angle of approximately 40.
- the extension is advanced co-axially into the cylinder, with the nozzle approximately 21/; inches from the wall of the cylinder.
- the spray stream is approximately i inches in length and strikes the surface at an angle of about 40.
- the cylinder is rotated about its center duringthe application of the molybdenum coating and the extension moved co-axially so that the impinging spray traverses the length of the bore surface of the cylinder.
- the desired thickness may be applied in one or more passes.
- a spray metal coating of a hard metal, in this case .80 per centum carbon steel is applied to the molybdenum sprayed cylinder bores.
- This coating is applied using the same metallizing gun, 8.
- a diameter wire of the steel being utilized in the gun and employing a standard spraying procedure by moving the spraying gun nozzle back and forth over the bore surface sufficiently rapidly to produce layers of approximately 003-1306 inch thick with each pass of the gun.
- the gun is held with its extended nozzle approximately 2' inches distant from the surface of the cylinder.
- This steel coating is applied to a thickness of approximately .037 inch to .040 inch on a side. This provides a finish allowance of approximately from .005 inch to .08 inch.
- the cylinder bores are then ground to the desired size. They are either ground to the final finish size if a ground finish is considered to be satisfactory or they are ground to a slightly smaller size and honed as a final operation if a hone finish is required, Instead of grinding, a tool boring operation may be substituted if the final sprayed metal coating is that of a steel with a lower carbon content, for instance, .10 per centum carbon.
- the metal spray gun of the wire feed type used in the above described example is one having a normal capacity for spraying about pounds of a inch .10% carbon steel wire per hour. Guns of different capacity or other metal spraying devices of different type may be used, in which case the particular operating conditions are to be adapted to those regulating the normal spraying procedure of the particular equipment used, and if necessary with the additional provision of appropriate safeguards or adjustment to avoid excessive oxidizing conditions.
- the molybdenum wire specified in the example is a commercial sintered and drawn molybdenum wire conventionally designated as black oxide finish-no ,anneal. It is a substantially pure molybdenum wire.
- Other wires or rods of molybdenum or molybdenum alloys or compositions may be substituted for the specific molybdenum used in the aforedescribed example with good results.
- Such are, for instance, molybdenum wire or rods commercially designated as hydrogen cleaned and annealed and chemical plus hydrogen cleaned and annealed and also such molybdenum alloys or compositions as 60-40 molybdenum-tungsten, 90-10 molybdenum-tungsten, 70-molybdenum 30-iron, and the like.
- a spray metal lined aluminum engine cylinder which comprises an engine cylinder having an aluminum bore surface, a layer of spray metal, and intermediate said layer of spray metal and said bore surface, in surface-to-surface bond therewith, sprayed molybdenum of at least flash coatin thickness.
- a spray metal lined aluminum engine cylinder in accordance with claim 2 in which said molybdenum is substantially pure molybdenum and in which said spray metal layer is composed of a metal substantially harder than the aluminum of said bore surface.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Coating By Spraying Or Casting (AREA)
Description
Patented Mar. 11, 1952 APPLICATION OF SPRAY METAL LININGS FOR ALUMINUM ENGINE CYLINDERS OF "OR FOR RECIPROCATING ENGINES .Arthur P. Shepard, Flushing,iN.l.Y., assignor to MetallizingiEngineering Co. 1110.; Long Island City, N. Y., a'corporation of NewJersey NoDrawing. .Application December 19,1947, .Serial No. 792,836
7 Claims. ,1
This invention relatesto new and useful improvements in spray. metal linings for aluminum engine cylinders ofor for reciprocating engines.
In the past, there has been no satisfactory means for lining aluminum engine cylinders with sprayed metal. In the construction ofthe aluminum cylinders it has been the practice, in the past, to either construct the cylinders without liners or to construct them with solid sleeveliners, such as cast iron sleeves. These latter are commonly cast in place in the aluminum cylinder by placing them in the mold prior to, thecasting of the aluminum.
Although cast iron liners have, proved relatively satisfactory, the use of them has the disadvantage of high cost of construction, excessive weight, and the limitations of metals which can be used for the liners. Hardened steel liners can notbe used as sleeves for inserts because the heat of casting would soften previously hardened liners and any attempt to harden the liners after casting would be detrimental to the aluminum. Where aluminum is used for engine cylinders without lining, they have been found relatively unsatisfactory becausealuminum is not sufiiciently Wear-resistant to withstand the wearing action of the piston orthepiston rings.
Sprayed metal offers advantageous bearing characteristics due to its porosity and inherent oil retention properties. Furthermore hard sprayed metals can be applied, such as hardened steels, at temperatures which do not. affect the physical properties of the aluminum.
'It has therefore been proposed in the past to line aluminum engine cylinders with sprayed metal so as to overcome the above mentioned disadvantages. These, however, have not proved practical. The primary reason for this resides in the inherent limitations of known means for bonding such sprayed metal coatings to thewalls of the aluminum cylinders.
In metal spraying the metalto be applied is projected against the surface to be covered in the form of a spray, the particles of which are in a molten or heat plastic condition. Asa rule, metal spraying is carried outwith "the use "of metal spray guns, i. e.,devices in which the metal is fed to a heating zone from which zonemetal particles, at least someof'whichare molten or in a heat plastic condition, are propelled against the surface to be sprayed. 'The propulsionmay be --effected either by centrifugal means'or by means of-a'blast of air or other gas. One of the most widely used forms of spraying device is a metal spray gunutilizing the metal to'be'spraye'd 1n= theform of a rod or wire which is fed byua '2 suitable feed mechanism into a heating ,1 zone which is produced by the .combustion of a .combustible and. a combustion-supporting gas. Suchrod or wire may be a relatively solid rod or Wire of such metal, or alternatively it maybe composed of particles of. such metal bonded together by. a suitable binder such as a plastic material. In the latter case the binder is usually of the kind-which willvolatilize asthe result of ;the applied heat of .the spray gun.
, In its application to aluminum engine cylinders it is essential that the applied spray metaladheres to the surface of the cylinderwall with a high degree of bond, for otherwise the applied spray metal may come off. For the purpose of securing therequisite degree of bonding, the. surface to which the spray metal is to beapplied must be,-.as a, rule, suitably pre-conditioned. In the past, such pre-conditioning treatment. has been generally of two kinds, roughening and heating. vRoughening has been carried out by mechanical roughening and also rougheningby the deposition of metalby an electricalfusing.ora welding procedure.
Mechanical rougheningof the aluminumcylinder surface to adapt the same to receive and retain applied spray metalmust be of a type involving the formation of multiple number of closely spaced cavities with peened and splayed edges and interspaces forming a ,multitudeyof keyways. In the.past,,the.most common method of procuring. such type surfaces has been by sand or grit blasting. Sand or grit blasting alone, however, does not, produce a sufficiently strong bond to aluminum to. retain the applied, spraymetal under the conditions of serviceto which analuminum: engine cylinder is subjected.
An alternative .form of mechanical surface roughening for spray metal bonding purposes is that of machine roughening a surface uto be sprayed in a particular mannerdesigned to procure the above mentioned surface characteristics essentialfor spray. metal bonding. ,Such surface roughening methods, however, have the same 'inherent limitation as the ones involving sander grit blasting.
It has been found possible tosecureea moderately strong bond between sprayed metal and aluminum by cutting relatively deep grooves. into the aluminumsurface and thereafter roughening the grooved surface, such as :by sand orgrit blasting. This method has the basic limitation, however, of-being too expensive for, use on mostaluminum' engine cylinders. When this procedure.
is used, the cost of the finished product includes the extra cost of grooving the entire "inside: surface of the cylinder, such as by threading, by the amount of additional sprayed metal which must be sprayed to fill the grooves and particularly by the cost of machining or grinding the sprayed cylinder to remove the eXcess metal which must be sprayed on the ridges between the grooves. Another limitation of this procedure is due to the weakening effect and consequent reduction in fatigue strength of the aluminum cylinder.
Electrical methods of fusing or welding elec trode metal to a base metal to produce a roughened surface consisting of the applied electrode metal have been used as a means for pre-conditioning metal surfaces for receiving and bond ing applied spray metal. This method, however, has the disadvantage of producing only a very weak bond between aluminum and applied spray metal and this bond has proved inadequate for meeting the service conditions required of aluminum engine cylinders.
The heating method of surface conditioning a metallic base to bond thereto applied spray metal involves the heating of the surface to a relatively high temperature and thereafter spraying the hot surface with metal. This method is not widely used and requires, as a general rule, considerable skill and elaborate equipment and is relatively expensive. Furthermore, in the case of aluminum engine cylinders, the temperature to which the surface or base must be heated usually is so high that it tends to seriously weaken the aluminum. A further limitation in the method of heating to produce bonding resides in the fact that aluminum oxidizes to an objectionable degree when heated in air.
There is one basic limitation inherent in practically all of the hitherto used conditioning methods for rendering metal surfaces capable of satisfactory bonding applied spray metal. This limitation resides in the fact that all hitherto used conditioning methods materially adversely effect the surface condition of the base to which they are applied and all such methods require a distinct and costly step of pre-conditioning the base surface before the metal spraying operation can be performed.
One object of the invention comprises, inter alia, a method for applying spray metal to the bore of aluminum engine cylinders which is substantially free from the aforementioned limitations inherent in hitherto known practices.
Another object of the invention is to provide a method for applying spray metal to the bore of aluminum engine cylinders with a high degree of bond and without materially affecting more than a thin skin of the surface of said cylinder bore.
A further object of the invention is an aluminum engine cylinder lined with a spray metal substantially adhering thereto with a high degree ofbond and preferably one substantially harder than the'aluminum of the cylinder.
The foregoing and still further objects of the invention may be seen from the following description:
The method in accordance with the invention essentially embraces an improvement in the application of spray metal to the bore surface of an aluminum engine cylinderwith a high degree of bond, which comprises conditioning such surface for spray metal bonding by spraying at least a flash coating of molybdenum thereon and thereafter spraying a metal, and preferably a metal substantially harder than the aluminum of said bore, onto the thusly coated surface.
1y comprises an engine cylinder having an aluminum bore surface, a layer of spray metal, preferably substantially harder than the aluminum of said bore surface, and intermediate said layer of spray metal and said bore surface, in surface-to-surface bond therewith, sprayed molybdenum of at least flash coating thickness.
Wherever the expression aluminum engine cylinder or similar term is used herein, it is intended to denote thereby the cylinder of any engine having an aluminum or aluminum alloy bore surface and in which a reciprocating piston operates, whether or not the engine is used for the production of power or simply the application of power, such as engine cylinders of, for instance, internal combustion engines, steam engines, gas compressors, pumps, refrigeration compressors, positive displacement hydraulic pumps, etc.
The spray metal lined aluminum engine cylin- Within the broad concept of the invention the molybdenum sprayed onto the aluminum bore surface, to be thereafter coated with spray metal,
rapid onceor twice-over application of the molybdenum spraying gun and not necessarily presenting a continuous coating. The more continuous the coating is, however, the better will be the bonding strength with which the sub sequently applied spray metal will adhere to the base surface. For best results I find it of advantage to apply a substantially continuous flash coating of molybdenum onto the bore surface. Within the preferred embodiment of the invention at least .005 inch and preferably .002 inch of substantially continuous molybdenum coating is recommended. The upper limit of the molybdenum coating is only dictated by practical and economical considerations. Once a coating thickness of the desired bonding characteristics is applied, any additional thickness will not further substantially improve the bonding characteristics of the molybdenum layer.
The metal spraying is preferably carried out by use of a metal spray gun, using wire or rod as a source of metal.
The molybdenum that I may use in accordance with my invention may be pure molybdenum or a molybdenum alloy or composition. In the latter case I prefer a relatively high molybdenum content, such as an alloy or composition having or more molybdenum. I may, however, use any alloy of molybdenum having 60% or greater molybdenum content and alloyed with any other metals which are known to alloy with molybde-.
num.
Wherever the term molybdenum is used herein, it is intended to designate thereby substantially pure molybdenum as well as alloys or compositions containing at least 60% molybdenum. When referring to a molybdenum composition I mean thereby a composition containing finely divided metallic molybdenum in combination with other elements or metal and not necessarily alloyed therewith.
The surface of the aluminum cylinder bore tobe metal sprayed may be perfectly smooth and no roughening or other conditioning treatment other than cleaning (if necessary) is required. The surface to be sprayed upon with molybdenum should, however, be a clean surface.
7 Cleaning may be accomplished satisfactorily in numerous ways, such as by abrasion, light sand blast ing,
acid-etching, andythelike procedures. These are particularly to be used when there is any danger of oxides being present on the surface. If the surface -is relatively clean of oxides and is merely to. be freed from dirt particles or greasy matter, it may suffice if the same is cleaned with a suitable solvent or the like. Ordinarily, if the cylinder has been recently bored Without the use of a lubricantor coolant, a surface emerges sufliciently clean to be immediately sprayed upon with molybdenum.
Any metal which is capable of being sprayed may then be sprayed directly on to the molybdenum sprayed surface. The final metal to be sprayed should be selected according to its characteristics to meet the requirement of the particular engine cylinder being done. For example, a. common metal to use for an ordinary internal combustion engine would be a high carbon steel, in cases where the final finishing can be done by grinding. -Where the finishing must be done by boring with a tool, a low carbon steel could be used. In some cases stainless steel or bronze or other metals are recommended to provide the particular wear-resistant and corrosion-resistant requirements of the particular engine being manufactured.
Sometimes it is advantageous to preheat the aluminum cylinder before the application of the metal sprayed molybdenum and sometimes it is desirable to preheat the cylinder just prior to the application of the final coating of sprayed metal. In either case, the preheating may be unnecessary and is carried out at relatively low temperatures (as compared with the temperatures required by heat bonding methods). The primary purpose of such a preheat step is to cause expansion of the cylinder before the application of. the final sprayed coating to reduce the stress onthe bond at the interface between sprayed coating and aluminum cylinder bore. The temperatures commonlyused for this purpose are of the order of magnitude of about 300 F.
Sometimes it is of .advantage to provide grooves and ridges or other forms of an irregular contour on the surface of the baseto be metal sprayed. Such grooves or other irregular contours have several advantageous functions although they are not a necessary requirement of the procedure set forth in this invention. One of the advantageous functions of grooves or other irregular contours of the base, is the increase in surface area which such contours provide, which results in an increase in bond to the sprayed metal due to such increased area of bonding. Another advantageous function of such contours is the beneficial effect on the structure of the sprayed metal layer. Such beneficial effect is due to the folding of the stratification layers of such sprayed metal structure. Sprayed metal structures resulting from spraying onto a surface with an irregular contour are generally stronger due to the folding of stratifications or laminations than the structures resulting from the spraying of the same metal onto a substantially even surface.
In accordance with the invention, it is entirely practical not only to select a molybdenum or molybdenum alloy for the first coating applied to the surface of the aluminum engine cylinder, but also to use the same or another molybdenum or molybdenum alloy for the subseqently applied spray metal coating. In this case, the entire coating would be of molybdenum. The use of molybdenum for the subsequently applied spray metal layer is particularly advantageous foruthin coatings which must stand considerable :wear.
When within the preferred application of the molybdenum .a metallizing gunof the-wires type is used for the carrying out of my ;inven'tion,.I prefer to use arod or wire of essentially. pure molybdenum produced by sintering wpowdered molybdenum. Such a sintered rodor Wire may be sprayed directly in such. a metallizing gunbut I prefer to mechanically work the sintered material by swaging and/or;.drawing: to; produce.the final rod or wire.
Although the application 1 of one subsequent metal to the first coatingof' molybdenum alloy on the bore surfaceto be metal sprayed hasbeen previously discussed, it is obvious that:.anynumber of different metals maybesubsequently-applied to form as many layers of different kinds. of metal as desired.
The following example is furnished bywayrof illustration but not of limitation:
Example An automotive internal combustionengine aluminum cylinder block is first bored for the'cylinder holes using a conventional machine tool and method. The last boring operation iswdone dry, without oil or cooling fluids, so .as to produce a clean metal surface. Reasonably fast machine feeds may be used since it is notnecessaryto produce-a particularly smooth finish. 'A. reasonable tolerance for the size of this bore. is allowed. such as a tolerance of .005 inch. The size of the bore is made sufficiently over size to provide sufiicient space for the sprayed metal coatingsof the desired thickness. A practical thickness to use in this case is a total thickness of sprayed metal layers of .032 inch measured on a side so that the boreof the cylinder is approximately .064; inch larger than the desired finished size.
The cylinder block is then preheated in an oven to a temperatureof 300 F.
Immediately after heating and while the cylinder block is still hot, a. flash coating, in,this case about .002 inch thick, of molybdenum is .applied to the surface of each cylinder bore by metal spraying. This coating isapplied by a conventional metallizing gunof the wire feed type, utilizing .091 inch diameter sintered and drawn molybdenum wire. An angular gun nozzle-extension is used and held with its nozzle end .at a' distance of about 2 inches from. the. bore; surface. The total length of the extension is about 1.- foot, and it is so constructed-thatthe heatinguand atomizing portion is at theend of the extension. Such an extension is fittedwith an angular nozzle Which sprays at an angle of approximately 40. The extension is advanced co-axially into the cylinder, with the nozzle approximately 21/; inches from the wall of the cylinder. Thus the spray stream is approximately i inches in length and strikes the surface at an angle of about 40. The cylinder is rotated about its center duringthe application of the molybdenum coating and the extension moved co-axially so that the impinging spray traverses the length of the bore surface of the cylinder. The desired thickness may be applied in one or more passes.
After the application of the molybdenum coating and while the cylinder block is still hot, a spray metal coating of a hard metal, in this case .80 per centum carbon steel is applied to the molybdenum sprayed cylinder bores. This coating is applied using the same metallizing gun, 8. A diameter wire of the steel being utilized in the gun and employing a standard spraying procedure by moving the spraying gun nozzle back and forth over the bore surface sufficiently rapidly to produce layers of approximately 003-1306 inch thick with each pass of the gun. The gun is held with its extended nozzle approximately 2' inches distant from the surface of the cylinder. This steel coating is applied to a thickness of approximately .037 inch to .040 inch on a side. This provides a finish allowance of approximately from .005 inch to .08 inch.
The cylinder bores are then ground to the desired size. They are either ground to the final finish size if a ground finish is considered to be satisfactory or they are ground to a slightly smaller size and honed as a final operation if a hone finish is required, Instead of grinding, a tool boring operation may be substituted if the final sprayed metal coating is that of a steel with a lower carbon content, for instance, .10 per centum carbon.
The metal spray gun of the wire feed type used in the above described example is one having a normal capacity for spraying about pounds of a inch .10% carbon steel wire per hour. Guns of different capacity or other metal spraying devices of different type may be used, in which case the particular operating conditions are to be adapted to those regulating the normal spraying procedure of the particular equipment used, and if necessary with the additional provision of appropriate safeguards or adjustment to avoid excessive oxidizing conditions.
The molybdenum wire specified in the example is a commercial sintered and drawn molybdenum wire conventionally designated as black oxide finish-no ,anneal. It is a substantially pure molybdenum wire. Other wires or rods of molybdenum or molybdenum alloys or compositions may be substituted for the specific molybdenum used in the aforedescribed example with good results. Such are, for instance, molybdenum wire or rods commercially designated as hydrogen cleaned and annealed and chemical plus hydrogen cleaned and annealed and also such molybdenum alloys or compositions as 60-40 molybdenum-tungsten, 90-10 molybdenum-tungsten, 70-molybdenum 30-iron, and the like.
During spraying operations it is necessary, as
'for instance set forth in the example, to avoid 9 conditions of oxidation during spraying. The reason is that excessive oxidation of the subdivided molybdenum particles will impair the adhesion characteristics of the ultimately applied spray metal coating to the base. Excessive gas or by utilizing a substantially inert gas as the blast conveying gas for the propulsion of the spray metal or by both the expedients.
Wherever reference herein is made to carbon steel or the like expression, the same is used in its broad connotation, being intended to designate all alloys of carbon and steel including those which also include other alloying elements such as for instance nickel, chromium, vanadium, molybdenum, etc.
The foregoing specific description is for the purposes of illustration and not of limitation and it is therefore my intention that the invention be limited only by the appended claims or their equivalent wherein I have endeavored to claim broadly all inherent novelty.
I claim:
1. A spray metal lined aluminum engine cylinder which comprises an engine cylinder having an aluminum bore surface, a layer of spray metal, and intermediate said layer of spray metal and said bore surface, in surface-to-surface bond therewith, sprayed molybdenum of at least flash coatin thickness.
2. A spray metal lined aluminum engine cylinder in accordance with claim 1 in which said sprayed molybdenum forms a layer of at least about .0005 inch thick.
3. A spray metal lined aluminum engine cylinder in accordance with claim 1 in which said sprayed molybdenum forms a layer of at least about .002 inch thick.
4. A spray metal lined aluminum engine cylinder in accordance with claim 2 in which said molybdenum is substantially pure molybdenum and in which said spray metal layer is composed of a metal substantially harder than the aluminum of said bore surface.
5. A spray metal lined aluminum engine cylinder in accordance with claim 4 in which said spray metal layer is composed of carbon steel.
6. A spray metal lined aluminum engine cylinder in accordance with claim 4 in which said spray metal layer is composed of bronze.
7. A spray metal lined aluminum engine cylinder in accordance with claim 4 in which said spray metal layer is composed of stainless steel.
ARTHUR P. SHEPARD.
REFERENQES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,923,790 Moore Aug. 22, 1933 2,166,634 Lesage July 18, 1939 FOREIGN PATENTS Number Country Date 376,117 Great Britain July 7, 1932 392,145 Great Britain 1933 510,404 Great Britain Aug. 1, 1939
Claims (1)
1. A SPRAY METAL LINED ALUMINUM ENGINE CYLINDER WHICH COMPRISES AN ENGINE CYLINDER HAVING AN ALUMINUM BORE SURFACE, A LAYER OF SPRAY METAL, AND INTERMEDIATE SAID LAYER OF SPRAY METAL AND SAID BORE SURFACE, IN SURFACE-TO-FURFACE BOND THEREWITH, SPRAYED MOLYBDENUM OF AT LEAST FLASH COATING THICKNESS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US792836A US2588422A (en) | 1947-12-19 | 1947-12-19 | Application of spray metal linings for aluminum engine cylinders of or for reciprocating engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US792836A US2588422A (en) | 1947-12-19 | 1947-12-19 | Application of spray metal linings for aluminum engine cylinders of or for reciprocating engines |
Publications (1)
Publication Number | Publication Date |
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US2588422A true US2588422A (en) | 1952-03-11 |
Family
ID=25158221
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US792836A Expired - Lifetime US2588422A (en) | 1947-12-19 | 1947-12-19 | Application of spray metal linings for aluminum engine cylinders of or for reciprocating engines |
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Cited By (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2820375A (en) * | 1954-12-22 | 1958-01-21 | Owens Illinois Glass Co | Forming glass molding tools |
US2833264A (en) * | 1954-12-22 | 1958-05-06 | John Altorfer | Internal combustion engine |
US2864696A (en) * | 1956-01-31 | 1958-12-16 | Duriron Co | Nickel base alloys |
US2908068A (en) * | 1955-01-29 | 1959-10-13 | Hans Sickinger | Inking roller with porous corrosion resistant coating |
US3038563A (en) * | 1956-10-30 | 1962-06-12 | Gen Motors Corp | Brakes |
DE1222761B (en) * | 1954-09-29 | 1966-08-11 | Darcey Engineering Corp | Method for firmly adhering a metallic layer to aluminum or an aluminum alloy, in particular by spraying |
US3285680A (en) * | 1963-06-26 | 1966-11-15 | Helen G Dailey | Bearing |
DE1273955B (en) * | 1958-05-21 | 1968-07-25 | Jean Claude Rey | Process for lining cylinder liners of internal combustion engines by metal spraying |
US3658576A (en) * | 1968-05-01 | 1972-04-25 | Berliet Automobiles | Friction elements of machines subjected to heavy loads |
US3711310A (en) * | 1971-07-26 | 1973-01-16 | United Aircraft Corp | Repair process for aluminum and magnesium articles |
FR2402008A1 (en) * | 1977-09-01 | 1979-03-30 | Audi Ag | METHOD FOR APPLYING COATS OF METAL BY SPRAYING ON THE INTERNAL SURFACE OF A HOLLOW BODY |
US4338360A (en) * | 1980-05-01 | 1982-07-06 | General Motors Corporation | Method for coating porous metal structure |
US5130163A (en) * | 1991-04-26 | 1992-07-14 | General Motors Corporation | Porous laminate surface coating method |
US5334235A (en) * | 1993-01-22 | 1994-08-02 | The Perkin-Elmer Corporation | Thermal spray method for coating cylinder bores for internal combustion engines |
DE19549403A1 (en) * | 1995-10-31 | 1997-05-07 | Volkswagen Ag | Sliding surface production by machining sprayed layer |
US5691004A (en) * | 1996-07-11 | 1997-11-25 | Ford Global Technologies, Inc. | Method of treating light metal cylinder bore walls to receive thermal sprayed metal coatings |
DE19628786A1 (en) * | 1996-07-17 | 1998-04-30 | Volkswagen Ag | Sliding surface production |
US5820938A (en) * | 1997-03-31 | 1998-10-13 | Ford Global Technologies, Inc. | Coating parent bore metal of engine blocks |
US5958521A (en) * | 1996-06-21 | 1999-09-28 | Ford Global Technologies, Inc. | Method of depositing a thermally sprayed coating that is graded between being machinable and being wear resistant |
US5958520A (en) * | 1998-07-13 | 1999-09-28 | Ford Global Technologies, Inc. | Method of staggering reversal of thermal spray inside a cylinder bore |
WO2000037789A1 (en) | 1998-12-18 | 2000-06-29 | Volkswagen Aktiengesellschaft | Cylinder housing and method for producing a cylinder housing |
US6095126A (en) * | 1995-10-31 | 2000-08-01 | Volkswagen Ag | Method of producing a slide surface on a light metal alloy |
US6159554A (en) * | 1995-10-31 | 2000-12-12 | Volkswagen Ag | Method of producing a molybdenum-steel slide surface on a light metal alloy |
EP1340834A3 (en) * | 2002-02-27 | 2004-03-31 | Sulzer Metco AG | Coated running surfaces of combustion-engine cylinders and process of its manufacture |
US6756083B2 (en) | 2001-05-18 | 2004-06-29 | Höganäs Ab | Method of coating substrate with thermal sprayed metal powder |
US20060048605A1 (en) * | 2004-06-17 | 2006-03-09 | Caterpillar Inc. | Composite powder and gall-resistant coating |
US20120067203A1 (en) * | 2009-05-27 | 2012-03-22 | Marcus Kennedy | Sliding element with exposed functional surface |
WO2017012769A1 (en) * | 2015-07-23 | 2017-01-26 | Volkswagen Aktiengesellschaft | Method for coating a cylinder barrel of a cylinder crankcase, cylinder crankcase with a coated cylinder barrel and engine |
WO2018011362A1 (en) | 2016-07-13 | 2018-01-18 | Oerlikon Metco Ag, Wohlen | Coating cylinder bores without prior activation of the surface |
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GB376117A (en) * | 1930-12-31 | 1932-07-07 | Metallisator Berlin Ag | Improvements in or relating to the cylinders and/or pistons of internal combustion engines |
GB392145A (en) * | 1930-08-29 | 1933-05-11 | Gen Electric | Improvements in and relating to means for preventing the erosion of metals |
US1923790A (en) * | 1928-11-24 | 1933-08-22 | Aluminum Co Of America | Chromium plated article and method of making the same |
US2166634A (en) * | 1937-02-15 | 1939-07-18 | Lesage Alfred | Process for making engine cylinders with an inner lining |
GB510404A (en) * | 1938-05-03 | 1939-08-01 | Bernhard Berghaus | Improvements in and relating to light metal pistons and coatings therefor |
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US1923790A (en) * | 1928-11-24 | 1933-08-22 | Aluminum Co Of America | Chromium plated article and method of making the same |
GB392145A (en) * | 1930-08-29 | 1933-05-11 | Gen Electric | Improvements in and relating to means for preventing the erosion of metals |
GB376117A (en) * | 1930-12-31 | 1932-07-07 | Metallisator Berlin Ag | Improvements in or relating to the cylinders and/or pistons of internal combustion engines |
US2166634A (en) * | 1937-02-15 | 1939-07-18 | Lesage Alfred | Process for making engine cylinders with an inner lining |
GB510404A (en) * | 1938-05-03 | 1939-08-01 | Bernhard Berghaus | Improvements in and relating to light metal pistons and coatings therefor |
Cited By (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1222761B (en) * | 1954-09-29 | 1966-08-11 | Darcey Engineering Corp | Method for firmly adhering a metallic layer to aluminum or an aluminum alloy, in particular by spraying |
US2820375A (en) * | 1954-12-22 | 1958-01-21 | Owens Illinois Glass Co | Forming glass molding tools |
US2833264A (en) * | 1954-12-22 | 1958-05-06 | John Altorfer | Internal combustion engine |
US2908068A (en) * | 1955-01-29 | 1959-10-13 | Hans Sickinger | Inking roller with porous corrosion resistant coating |
US2864696A (en) * | 1956-01-31 | 1958-12-16 | Duriron Co | Nickel base alloys |
US3038563A (en) * | 1956-10-30 | 1962-06-12 | Gen Motors Corp | Brakes |
DE1273955B (en) * | 1958-05-21 | 1968-07-25 | Jean Claude Rey | Process for lining cylinder liners of internal combustion engines by metal spraying |
US3285680A (en) * | 1963-06-26 | 1966-11-15 | Helen G Dailey | Bearing |
US3658576A (en) * | 1968-05-01 | 1972-04-25 | Berliet Automobiles | Friction elements of machines subjected to heavy loads |
US3711310A (en) * | 1971-07-26 | 1973-01-16 | United Aircraft Corp | Repair process for aluminum and magnesium articles |
FR2402008A1 (en) * | 1977-09-01 | 1979-03-30 | Audi Ag | METHOD FOR APPLYING COATS OF METAL BY SPRAYING ON THE INTERNAL SURFACE OF A HOLLOW BODY |
US4302482A (en) * | 1977-09-01 | 1981-11-24 | Audi Nsu Auto Union Aktiengesellschaft | Process for applying metallic sprayed coats to the inner surface of a hollow body |
US4338360A (en) * | 1980-05-01 | 1982-07-06 | General Motors Corporation | Method for coating porous metal structure |
US5130163A (en) * | 1991-04-26 | 1992-07-14 | General Motors Corporation | Porous laminate surface coating method |
US5334235A (en) * | 1993-01-22 | 1994-08-02 | The Perkin-Elmer Corporation | Thermal spray method for coating cylinder bores for internal combustion engines |
DE19549403A1 (en) * | 1995-10-31 | 1997-05-07 | Volkswagen Ag | Sliding surface production by machining sprayed layer |
US6095126A (en) * | 1995-10-31 | 2000-08-01 | Volkswagen Ag | Method of producing a slide surface on a light metal alloy |
US6280796B1 (en) | 1995-10-31 | 2001-08-28 | Volkswagen Ag | Method of producing a slide surface on a light metal alloy |
DE19549403C2 (en) * | 1995-10-31 | 1999-12-09 | Volkswagen Ag | Method of making a sliding surface on an aluminum alloy |
US6159554A (en) * | 1995-10-31 | 2000-12-12 | Volkswagen Ag | Method of producing a molybdenum-steel slide surface on a light metal alloy |
US5958521A (en) * | 1996-06-21 | 1999-09-28 | Ford Global Technologies, Inc. | Method of depositing a thermally sprayed coating that is graded between being machinable and being wear resistant |
US5691004A (en) * | 1996-07-11 | 1997-11-25 | Ford Global Technologies, Inc. | Method of treating light metal cylinder bore walls to receive thermal sprayed metal coatings |
DE19628786A1 (en) * | 1996-07-17 | 1998-04-30 | Volkswagen Ag | Sliding surface production |
US5820938A (en) * | 1997-03-31 | 1998-10-13 | Ford Global Technologies, Inc. | Coating parent bore metal of engine blocks |
US5958520A (en) * | 1998-07-13 | 1999-09-28 | Ford Global Technologies, Inc. | Method of staggering reversal of thermal spray inside a cylinder bore |
WO2000037789A1 (en) | 1998-12-18 | 2000-06-29 | Volkswagen Aktiengesellschaft | Cylinder housing and method for producing a cylinder housing |
US6756083B2 (en) | 2001-05-18 | 2004-06-29 | Höganäs Ab | Method of coating substrate with thermal sprayed metal powder |
US20040206204A1 (en) * | 2001-05-18 | 2004-10-21 | Hoganas Ab | Metal powder including diffusion alloyed molybdenum |
EP1340834A3 (en) * | 2002-02-27 | 2004-03-31 | Sulzer Metco AG | Coated running surfaces of combustion-engine cylinders and process of its manufacture |
US20060048605A1 (en) * | 2004-06-17 | 2006-03-09 | Caterpillar Inc. | Composite powder and gall-resistant coating |
US7404841B2 (en) * | 2004-06-17 | 2008-07-29 | Caterpillar Inc. | Composite powder and gall-resistant coating |
US20120067203A1 (en) * | 2009-05-27 | 2012-03-22 | Marcus Kennedy | Sliding element with exposed functional surface |
US8985009B2 (en) * | 2009-05-27 | 2015-03-24 | Federal-Mogul Burscheid Gmbh | Sliding element with exposed functional surface |
WO2017012769A1 (en) * | 2015-07-23 | 2017-01-26 | Volkswagen Aktiengesellschaft | Method for coating a cylinder barrel of a cylinder crankcase, cylinder crankcase with a coated cylinder barrel and engine |
WO2018011362A1 (en) | 2016-07-13 | 2018-01-18 | Oerlikon Metco Ag, Wohlen | Coating cylinder bores without prior activation of the surface |
US10920308B2 (en) | 2016-07-13 | 2021-02-16 | Oerlikon Metco Ag, Wohlen | Coating cylinder bores without prior activation of the surface |
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