US20020106978A1 - Chemical mechanical machining and surface finishing - Google Patents

Chemical mechanical machining and surface finishing Download PDF

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Publication number
US20020106978A1
US20020106978A1 US10/071,533 US7153302A US2002106978A1 US 20020106978 A1 US20020106978 A1 US 20020106978A1 US 7153302 A US7153302 A US 7153302A US 2002106978 A1 US2002106978 A1 US 2002106978A1
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United States
Prior art keywords
workpiece
tool
mating
conversion coating
active chemistry
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Abandoned
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US10/071,533
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English (en)
Inventor
Mark Michaud
Gary Sroka
Lane Winkelmann
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Rem Technologies Inc
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Rem Chemicals Inc
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Publication date
Application filed by Rem Chemicals Inc filed Critical Rem Chemicals Inc
Priority to US10/071,533 priority Critical patent/US20020106978A1/en
Assigned to REM CHEMICALS, INC. reassignment REM CHEMICALS, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MICHAUD, MARK D., SROKA, GARY, WINKELMANN, LANE
Publication of US20020106978A1 publication Critical patent/US20020106978A1/en
Assigned to REM TECHNOLOGIES, INC. reassignment REM TECHNOLOGIES, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: REM CHEMICALS, INC.
Priority to US11/012,518 priority patent/US20050164610A1/en
Abandoned legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B37/00—Lapping machines or devices; Accessories
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B37/00—Lapping machines or devices; Accessories
    • B24B37/04—Lapping machines or devices; Accessories designed for working plane surfaces
    • B24B37/042—Lapping machines or devices; Accessories designed for working plane surfaces operating processes therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B33/00—Honing machines or devices; Accessories therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B37/00—Lapping machines or devices; Accessories
    • B24B37/11—Lapping tools
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B5/00—Machines or devices designed for grinding surfaces of revolution on work, including those which also grind adjacent plane surfaces; Accessories therefor
    • B24B5/36—Single-purpose machines or devices
    • B24B5/42—Single-purpose machines or devices for grinding crankshafts or crankpins
    • 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
    • C23C22/00—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C22/73—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals characterised by the process
    • 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
    • C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
    • C23F3/00—Brightening metals by chemical means

Definitions

  • the machine that guides the cutting tool has its own inherent set of limitations that inhibit high precision and accuracy.
  • Some limitations of the mechanical devices moving the tool include geometric errors, feed rate errors, drive wear, vibration, and hysteresis, to name a few.
  • the machines are usually massive in size so as to maintain the required rigidity to accurately apply the high forces that are necessary to remove metal especially from hard workpieces.
  • Significant thermal distortions and structural deflections caused by the cutting load can also be problematic, especially for delicate workpieces.
  • chatter and machine lines are typically reduced by a multiple step process.
  • the gear In the case of a high quality gear, the gear must be ground, and then honed to reduce the chatter and machine lines generated by machining.
  • the grinding and honing processes can cause severe metallurgical damage to the critical contact surface of workpieces. Workpiece quality can only be ensured by costly 100% inspection.
  • One method of surface finishing such workpieces is to machine the surfaces by conventional multi-step, successively finer grinding, honing and lapping. Attaining a ground surface with a ⁇ 2 microinch R a requires time, multiple steps and state of the art technology. A complex surface geometry calls for expensive and highly sophisticated machinery, expensive tooling and time consuming maintenance. In addition to the cost, this process produces directional lines and the potential for tempering and microcracks that damage the integrity of the heat treated surface. As previously discussed, a quality workpiece requires costly 100% inspection of the ground and hardened surface with a technique such as nital etching. Another shortcoming of this approach is the possibility of abrasive particles being impregnated into the surface resulting in stress raisers, lubricant debris and/or wear.
  • the invention described herein discloses a chemical mechanical machining and surface finishing process.
  • An active chemistry is reacted with the surface of a workpiece so that a soft conversion coating is formed on the surface of a workpiece.
  • the conversion coating is insoluble in the active chemistry in that it protects the basis metal of the workpiece from further chemical reaction with the active chemistry.
  • the conversion coating is removed from the workpiece via relative motion with a contact tool, thereby exposing fresh metal for further reaction with the active chemistry, which allows the conversion coating to reform on the workpiece.
  • machining equipment can be completely eliminated, wherein mating workpieces in relative motion and load act as the tools for the removal of the conversion coatings from their opposing contact surfaces.
  • the present invention lends itself to a very controlled rate of metal removal, and can just surface finish the workpiece, or if desired, surface finish the workpiece simultaneously with the shaping and/or sizing of the workpiece.
  • surface finishing means to remove metal from the surface of a workpiece to reduce roughness, waviness, lays and flaws.
  • Size means to uniformly remove metal from the surface of a workpiece to bring it to its proper dimension.
  • shapeing means to differentially remove metal from a workpiece to bring it to its proper geometry. “Shaping” includes drilling, sawing, boring, cutting, milling, turning, grinding, planing, and the like.
  • FIG. 1 shows an example of a Falex Corporation FLC Lubricity Tester as used in examples 2 and 3.
  • FIG. 2 shows another example of a Falex Corporation FLC Lubricity Tester as used in examples 4 and 5.
  • the chemical mechanical machining and surface finishing process disclosed herein uses water-based or organic-based active chemistry capable of reacting with the surface of a metal workpiece, common metals being iron, titanium, nickel, chromium, cobalt, tungsten, uranium, and alloys thereof.
  • the active chemistry is first introduced into the shaping, sizing and/or surface finishing machine so as to react with the basis metal of the workpiece to form a soft conversion coating.
  • the conversion coating is insoluble in the active chemistry in that it protects the basis metal of the workpiece from further chemical reaction with the active chemistry.
  • the conversion coating can comprise, for example, metal oxides, metal phosphates, metal oxalates, metal sulfates, metal sulfamates, or metal chromates.
  • the formation of the conversion coating is followed by appropriate tooling contact having a relative motion between the tool and the workpiece.
  • the relative motion can be produced by movement of the tool across a stationary work piece, by movement of the workpiece across a stationary tool, or by movement of both the tool and the workpiece.
  • the conversion coating is rubbed off by the tool, thereby exposing fresh metal on the workpiece, allowing for the re-formation of the conversion coating on the exposed metal.
  • the metal removal rate is proportional to the rate of reaction of the active chemistry with the metal to form the conversion coating. This reaction rate can be increased by raising the temperature and by using chemical accelerants. As the reaction rate increases, the metal removal rate will be controlled by the rate of conversion coating removal.
  • This process of rubbing and re-formation is repeated until such time as the desired surface finishing and/or shaping and/or sizing is achieved. No metallurgical damage occurs.
  • the machining tool requires very little force to remove the conversion coating, and thus the machine's mass, complexity and cost can be significantly reduced as compared to conventional machining while machining precision and accuracy can be increased.
  • the relative motion and contact force of the tool and workpiece is less than the plastic deformation, shear strength and/or tensile strength of the workpiece such that thermal degradation temperatures are not produced on the workpiece.
  • the contact between the tool and the workpiece causes metal to be removed from the workpiece at a theoretical resolution of 1.0 microinch. Because of the small force applied to the workpiece from the tool, tool wear is minimized and/or eliminated. This chemical mechanical process lends itself to a very controlled rate of metal removal, and can surface finish the workpiece simultaneously with the shaping and/or sizing process.
  • a conversion coating is formed on the surface of the workpiece that is softer than the basis metal of the workpiece.
  • Any active chemistry that can form such a chemical conversion coating on the surface of the workpiece is within the contemplation of the invention. Although the properties exhibited by the conversion coating produced on the basis metal are important to the successful practice of the present process, the formulation of the active chemistry is not.
  • One such conversion coating is described in U.S. Pat. No. 4,818,333, assigned to REM Chemicals, Inc., the contents of which are herein incorporated by reference.
  • the active chemistry preferably is capable of quickly and effectively producing, under the conditions of operation, a soft conversion coating of the basis metal.
  • the conversion coating must further be substantially insoluble in the active chemistry and protect the basis metal from further reaction so as to ensure that metal removal occurs primarily by rubbing and reformation rather than by dissolution.
  • the active chemistry can also include activators, accelerators, oxidizing agents and, in some instances, inhibitors and/or a wetting agents. It should be noted that the amount of the added ingredients may exceed solubility limits without adverse effect. The presence of an insoluble fraction may be beneficial from the standpoint of maintaining a supply of active ingredients for replenishment of the active chemistry during the course of operations.
  • the active chemistry will typically comprise phosphate salts or phosphoric acid, oxalate salts or oxalic acid, sulfamate salts or sulfamic acid, sulfate salts or sulfuric acid, chromates or chromic acid, or mixtures thereof.
  • activators or accelerators may be added to the active chemistry such as, but not limited to, selenium, zinc, copper, manganese, magnesium and iron phosphates, as well as inorganic and organic oxidizers, such as but not limited to persulfates, peroxides, meta-nitrobenzenes, chlorates, chlorites, nitrates and nitrites.
  • the active chemistry used in this invention can be diluted or dispersed.
  • the diluent or dispersant will most commonly be water, but can also be a material other than water such as, but not limited to, paraffinic oil, organic liquid, silicone oil, synthetic oil, other oils, greases, or lubricants. It is also anticipated that under certain conditions it might be preferable to create the conversion coating with highly concentrated acids such as sulfuric acid, methane sulfonic acid or phosphoric acid where water is a very minor component.
  • an oil or lubricant can be used as the diluent or dispersant if desirable. This is desired when, for example, sulfuric acid is used with a mineral oil. Sulfuric acid is not appreciably soluble in mineral oils, but the mineral oil will act as a dispersant, as the sulfuric acid will be dispersed, instead of dissolved, throughout the mineral oil.
  • any tool that can remove the soft conversion coating, previously described, to expose fresh metal without exceeding the plastic deformation, shear strength and/or tensile strength of the workpiece such that thermal degradation temperatures are not produced on the workpiece is within the contemplation of the invention.
  • the properties of the tool are important to the successful practice of removing the conversion coating, the tool design is not.
  • the tool can be the mating surface of the workpiece or a facsimile thereof.
  • the workpiece can comprise a gear, and the tool can comprise a mating gear or facsimile thereof.
  • the workpiece can comprise a bearing race, and the tool can comprise a plurality of mating bearing balls or rollers or facsimile thereof.
  • the tool can be either rigid or flexible.
  • the tool can be a rigid, slightly abrasive cylinder sized such that it will contact all desired recessed areas to remove machine and/or grind lines and/or shot peening pattern.
  • a flexible and/or expandable tool that conforms to the workpiece can be used to improve the surface finish by removing forming lines or welding seams.
  • the tool is not reactive with the active chemistry, in that the chemically induced conversion coating is not formed on the tool.
  • Contemplated non-reactive materials that the tool can be made from are wood, paper, cloth, ceramic, plastic, polymer, elastomer, and metal, but any material that is not reactive with the active chemistry can be used.
  • the workpiece is a gear
  • the tool may be a non-reactive mating gear designed to impart the required shaping and/or surface finishing properties while running in mesh with the reactive workpiece.
  • This process achieves a well-controlled metal removal rate capable of producing workpieces with high dimensional precision and accuracy. Metal can be removed with a resolution of approximately 1.0 microinch. This process also has the ability to simultaneously shape and/or size and/or surface finish, thereby reducing the gross number of processing steps. Since less force needs to be imparted to effect metal removal, a smaller, less complex and less expensive machine can be used to guide the tool. Tool speed is also much lower than that required in conventional machining, and tool costs and wear are significantly reduced.
  • machining surface areas can be shaped and/or sized and/or surface finished at one time. This process also virtually eliminates burrs, machine lines, chatter, plastic deformation, and other surface deformities on the workpiece.
  • a further advantage of the present process is a cool and burn-free machining process that causes little or no stress or metallurgical damage such as oxidation, phase change, stress raisers, and hardness changes. This process is usually carried out at or below the thermal degradation temperature of the metal. The low temperature also can help to eliminate the thermal deformation of delicate workpieces. In addition, structural deflections are minimized under the reduced tool pressure, which is especially important on delicate workpieces, minimizing and/or eliminating structural distortion and like deformities. Finally, the precision and accuracy of the machining process is tremendously improved.
  • in-situ shaping and/or sizing and/or surface finishing of metal-to-metal contact surfaces can be accomplished. This is done by adding active chemistry, with or without a fine abrasive, to the assembled apparatus so that a conversion coating is formed on the individual reactive metal surfaces of both the workpiece and the tool. Initially the apparatus can be operated under low load, which can be gradually increased to full load conditions. The conversion coating will be removed only at the critical contact surface where the rubbing, rolling, sliding, and the like occur to expose fresh metal for further reaction. Chemical mechanical machining and surface finishing will occur only at the critical contact surfaces to remove asperities that ultimately results in a line-free or nearly line-free surface.
  • the process can be continued, if desired, to attain a superfinished surface and/or final shaping and/or sizing of mating workpieces to their ideal geometry.
  • each mating surface will have an ideal matching contact surface area.
  • the in-situ process can correct minor dimensional or geometrical errors in the mating components with highly controlled precision by adjusting the active chemistry characteristics, processing time and temperature, contact loading and contact speed.
  • In-situ surface finishing or superfinishing also has other advantages, such as making it possible to finish all of the critical contact surfaces of an entire assembly, such as a transmission, that significantly reduces the cost of finishing each individual workpiece.
  • the surface finishing is extremely reproducible, and can be accomplished easily in a factory environment, thus eliminating the need for 100% final inspection.
  • the process can be carried out in or outside of the housing, and can concurrently final shape and/or size assembled mechanisms by removing minor dimensional/geometrical errors in the mating components. In gear and bearing applications, for example, this process reduces break-in periods, wear, scuffing, operating temperatures, friction, vibration and noise.
  • One embodiment of this in-situ process is two mating gears.
  • the active chemistry can be introduced onto a first mating gear, forming a conversion coating on the first mating gear, while simultaneously forming a conversion coating on the second mating gear.
  • the two mating gears are contacted with a relative motion therebetween that simultaneously removes the conversion coatings from the two gears.
  • both gears are exposed to further reaction with the active chemistry such that the conversion coating is allowed to be re-formed and removed on the gears, until a desired surface property, such as surface finishing, shaping, sizing or combination thereof, of both gears is reached.
  • the gears are located within a transmission or gearbox, wherein the contact between the gears occurs during operation of the transmission or gearbox.
  • a bearing race and a plurality of mating rolling elements are provided.
  • the active chemistry is introduced onto the bearing race, simultaneously forming a conversion coating on the bearing race and the rolling elements.
  • the bearing race and mating rolling elements are contacted with a relative motion therebetween that simultaneously removes the conversion coatings from the bearing race and the mating rolling elements.
  • both the bearing race and the mating rolling elements are exposed to further reaction with the active chemistry such that the conversion coating is allowed to be re-formed and removed, until a desired surface property, such as surface finishing, shaping, sizing or combination thereof, of the bearing race and mating rolling elements is reached.
  • Coupon 2 was placed in a solution of 60 g/L oxalic acid and 20 g/L sodium metanitrobenzene sulfonate with its traditionally mechanically polished surface facing up. The traditionally mechanically polished surface of Coupon 1 was then placed in contact perpendicular to the traditionally mechanically polished surface of Coupon 2 . Coupon 2 was held in a fixed position, and Coupon 1 was moved by hand in a back-and-forth and circular motion to simulate sliding motion of critical contact surfaces. Only very light pressure was applied. This was continued for approximately 10 minutes. The final R a and R max of Coupon 1 at the metal-to-metal contact surface were 1.71 ⁇ in. and 27.6 ⁇ in., respectively. The final R a and R max of Coupon 2 at the metal-to-metal contact surface were 1.95 ⁇ in. and 45.4 ⁇ in., respectively.
  • Example 1 shows that two mating workpieces fabricated from a hardened metal can be surface finished and even superfinished, and/or sized and/or shaped by wetting the surfaces with an appropriate active chemistry while lightly rubbing them together. No abrasives, high temperatures or high pressures are needed in this embodiment of the invention.
  • the surface is shaped and/or sized and/or surface finished only where there is metal-to-metal contact.
  • bearings can be shaped, sized and/or surface finished by the addition of active chemistry to the workpieces while running under very light loading. No metallurgical damage can occur as in conventional machining that uses abrasives or forces that generate high localized temperatures resulting in stress raisers or tempering leading to premature workpiece failure from friction, wear, scuffing, contact fatigue and dynamic fatigue.
  • the present invention is not limited to bearings or gears, but can be applied to any hard metal-to-metal contact that would benefit from surface finishing and/or sizing and/or shaping.
  • the ability to shape and/or size and/or surface finish in one step increases the manufacturing efficiency for a variety of workpieces.
  • a Falex Corporation FLC Lubricity Tester is used to rotate the ring at a set RPM while a hard plastic mold (Facsimile®) of the outer ring surface holds a piece of 600 grit silicon carbide wet/dry paper against it.
  • the Falex supplied 0-150 foot-pound Sears Craftsman torque wrench with gravity acting on it is the only load applied to the traditional mechanical grinding process.
  • the ring is partially submerged in a reservoir of SAE 30 weight detergent free motor oil throughout the test.
  • FIG. 1 illustrates the test apparatus.
  • test ring is cleaned, dried and weighed before and after processing on an analytical balance to determine metal removal.
  • the test ring has a weight of 22.0951 grams before processing. After a period of 1.0 hour of processing at 460 RPM the weight is 22.0934 grams. This is a loss of 0.0017 grams per hour that calculates to an 8.9 ⁇ in. change in dimension.
  • a Falex Corporation FLC Lubricity Tester is used to rotate the ring at a set RPM while a hard plastic mold (Facsimile®) of the outer ring surface holds a piece of 600 grit Silicon Carbide wet/dry paper against it.
  • the Falex supplied 0-150 foot-pound Sears Craftsman torque wrench with gravity acting on it is the only load applied to the chemical mechanical process.
  • the ring is partially submerged in FERROMIL® FML-575 IFP that is flowing through the reservoir at 6.5 milliliter/minute at ambient room temperature. See FIG. 1 for image of test apparatus.
  • test ring is cleaned, dried and weighed before and after processing on an analytical balance to determine metal removal.
  • the test ring has a weight of 22.1827 grams before processing. After a period of 1.0 hour of processing at 460 RPM the weight is 22.1550 grams. This is a loss of 0.0277 grams per hour that calculates to a 145.6 ⁇ in. change in dimension. These results show that the metal removal rate is 16 times that of Example 2.
  • Examples 2 and 3 demonstrate that chemical mechanical machining on hard workpieces increases the rate of metal removal dramatically. Therefore, it is possible to shape and/or size and/or surface finish hardened metal workpieces using a slightly abrasive tool in conjunction with active chemistry.
  • the hardness of the workpiece is inconsequential for as long as the active chemistry reacts with the surface. In fact, the rate of metal removal stays approximately the same no matter how high the hardness of the metal.
  • conventional machining e.g., grinding, honing, polishing, etc.
  • tool wear increases while metal removal rates decrease.
  • the embodiment of the invention of Examples 2 and 3 demonstrates that it is possible to shape and/or size and/or surface finish extremely hard metal surfaces using a slightly abrasive tool.
  • a small rotating and/or vibrating tool with a light abrasive would be placed in contact with the gear flank of a gear that is continually wetted with an appropriate active chemistry. This would remove the machine and/or grind lines and be used to shape the tooth to the ideal gear geometry. This would significantly increase the service life of gears that experience bending fatigue, scuffing, and other failures while reducing gear noise and allowing for increased operating power densities.
  • the present invention is not limited to gears, but can be applied to any hard metal surface that would benefit from shaping and/or sizing and/or surface finishing.
  • the ability to shape and surface finish in one step will increase the manufacturing efficiency of a variety of workpieces.
  • a Falex Corporation FLC Lubricity Tester is used to rotate the ring at a set RPM while a piece of fixtured FERROMIL® Media #NA (Pure plastic (polyester resin) without any abrasive particles) contacts the outer ring.
  • the plastic media was shaped to the contour of the ring to provide adequate surface contact.
  • the Falex supplied 0-150 foot-pound Sears Craftsman torque wrench with gravity acting on it is the only load applied to the traditional mechanical process.
  • the ring is partially submerged in 1% by volume REM® FBC-50 that is flowing through the reservoir at 6.5 milliliter/minute. See FIG. 2 for image of test apparatus.
  • test ring is cleaned, dried and weighed before and after processing on an analytical balance to determine metal removal.
  • the test ring has a weight of 22.3125 grams before processing. After a period of 3.0 hours at 460 RPM the weight is 22.3120 grams. This is a loss of 0.0005 grams total or 0.00017 grams per hour. Calculations show this to be a 0.9 ⁇ in. per hour change in dimension.
  • a Falex Corporation FLC Lubricity Tester is used to rotate the ring at a set RPM while a piece of fixtured FERROMIL® Media #NA (Pure plastic (polyester resin) without any abrasive particles) contacts the outer ring.
  • the plastic media was shaped to the contour of the ring to provide adequate surface contact.
  • the Falex supplied 0-150 foot-pound Sears Craftsman torque wrench with gravity acting on it is the only load applied to the chemical mechanical machining process.
  • the ring is partially submerged in FERROMIL® VII Aero-700 at 12.5% by volume that is flowing through the reservoir at 6.5 milliliter/minute. See FIG. 2 for image of test apparatus.
  • test ring is cleaned, dried and weighed before and after processing on an analytical balance to determine metal removal.
  • the test ring has a weight of 22.1059 grams before processing. After a period of 3.0 hours at 460 RPM the weight is 22.0808 grams. This is a loss of 0.0251 grams total or 0.00837 grams per hour. Calculations show this to be a 44.0 ⁇ in. per hour change in dimension. This translates too more than 49 times the metal removal of Example 4 using non-abrasive tooling that is softer than the basis metal, and, thus, not capable of exceeding plastic deformation, shear strength or tensile strength of the basis metal.
  • Examples 4 and 5 demonstrate that significant amounts of metal can be removed from hardened steel even using a non-abrasive plastic.
  • a tool fashioned from plastic then can be used to shape and/or size and/or surface finish a hardened steel surface when active chemistry is used. It is reasonable then that tools fashioned from harder materials will have greatly extended lives because they do not have to exert high forces or experience high localized temperatures. The tool will last longer since it can remove metal by exerting only the force needed to remove the soft conversion coating.
  • the root fillet area of a gear tooth was chemically mechanically surface finished to remove the axial grind lines.
  • a tool was created by using a section of high-speed steel wire with a diameter of 0.067 in. wrapped with 600 grit wet/dry silicon carbide paper. The tool was rotated at approximately 80 RPM. The tool was held against the root fillet area of a gear tooth (Webster, AISI 8620 carburized steel, 17-tooth gear, 8-diametral pitch and 25° pressure angle, fillet radius of approximately 0.0469 inches) with very light pressure.
  • a gear tooth Webster, AISI 8620 carburized steel, 17-tooth gear, 8-diametral pitch and 25° pressure angle, fillet radius of approximately 0.0469 inches
  • a solution of 60 g/L oxalic acid and 20 g/L sodium metanitrobenzene sulfonate was introduced to the contact surface drop-wise (1-2 drops per 10 seconds). This was done for a period of 15 minutes.
  • the silicon carbide paper was changed once after surface finishing for 10 minutes.
  • the present invention is not limited to gears, but can be applied to any hard metal surface that experiences dynamic fatigue.
  • the ability to shape and surface finish in one step will increase the manufacturing efficiency of a variety of workpieces.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)
  • ing And Chemical Polishing (AREA)
  • Polishing Bodies And Polishing Tools (AREA)
  • Chemical Treatment Of Metals (AREA)
  • Dental Preparations (AREA)
  • Milling Processes (AREA)
  • Grinding And Polishing Of Tertiary Curved Surfaces And Surfaces With Complex Shapes (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Gear Processing (AREA)
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US20050202921A1 (en) * 2004-03-09 2005-09-15 Ford Global Technologies, Llc Application of novel surface finishing technique for improving rear axle efficiency
US20050218117A1 (en) * 2004-04-05 2005-10-06 Jaworowski Mark R Chemically assisted surface finishing process
US20050268809A1 (en) * 2004-06-02 2005-12-08 Continuous Metal Technology Inc. Tungsten-iron projectile
US20060084367A1 (en) * 2004-10-19 2006-04-20 Cabot Microelectronics Corporation Method of sharpening cutting edges
US20080108470A1 (en) * 2003-05-30 2008-05-08 Mark Michaud Superfinishing Large Planetary Gear Systems
WO2009032221A1 (fr) 2007-08-28 2009-03-12 Rem Technologies Inc Procédé pour inspecter et remettre en état des composants mécaniques
EP2267338A1 (fr) 2009-06-25 2010-12-29 United Technologies Corporation Système d'engrenage épicycloidal ayant un revêtement de journal superfini
WO2013087429A1 (fr) * 2011-12-13 2013-06-20 Aktiebolaget Skf Procédé permettant de préparer une couche de protection sur une surface tribologique d'un composant mécanique
CN103454394A (zh) * 2013-09-11 2013-12-18 西安航空动力股份有限公司 一种航空发动机正齿轮硬化面缺陷的判定方法
CN107735218A (zh) * 2015-07-08 2018-02-23 斯堪尼亚商用车有限公司 研磨具有柱形支承面的工件的方法和用于确定工艺参数的方法
US10792781B2 (en) 2018-04-13 2020-10-06 Bell Helicopter Textron Inc. Masking tool system and method
US10927959B2 (en) 2019-02-27 2021-02-23 Caterpillar Inc. Method and appliance for making isotropically finished seal ring of seal assembly for machine
US20220096114A1 (en) * 2020-09-30 2022-03-31 Entrepix Medical, Llc Cutting instrument with improved surface topography
CN114728355A (zh) * 2019-10-02 2022-07-08 普罗费雷特两合公司 对已制齿的工件的齿的齿面进行整平的方法和装置以及用于实施该方法的刀具
US11518960B2 (en) 2016-08-24 2022-12-06 Ppg Industries Ohio, Inc. Alkaline molybdenum cation and phosphonate-containing cleaning composition
KR102669076B1 (ko) * 2023-01-11 2024-05-24 (주) 시에스텍 이종접합금속 부스바 제조방법

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US10179388B2 (en) * 2009-05-12 2019-01-15 Rem Technologies, Inc. High throughput finishing of metal components
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CN103567848A (zh) * 2013-10-10 2014-02-12 广东电网公司东莞供电局 一种清除硅橡胶互感器硅伞套表面老化层的方法
DE102014220976A1 (de) * 2013-10-17 2015-04-23 Chemetall Gmbh Verfahren zur Vorbereitung von metallischen Formkörpern für die Kaltumformung
DK3417090T3 (da) * 2016-02-15 2021-09-06 Rem Tech Inc Kemisk bearbejdning af additivt fremstillede arbejdsemner
CN110512200B (zh) * 2019-10-10 2020-09-15 黄鸿珊 一种五金件磷化发黑设备
CN113211006B (zh) * 2021-04-08 2022-04-22 浙江先导精密机械有限公司 一种机械手臂的凸台倾角加工方法

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US7730618B2 (en) * 2001-11-15 2010-06-08 Arkema France Method for working or forming metals in the presence of aqueous lubricants based on methanesulfonic acid
US20050044912A1 (en) * 2001-11-15 2005-03-03 Gilles Darvaux-Hubert Method for working or forming metals in the presence of aqueous lubricants based on methanesulfonic acid
EP2106881B2 (fr) † 2003-05-30 2016-02-24 REM Technologies, Inc. Procédé de superfinition d'une roue dentée creuse
US8858734B2 (en) * 2003-05-30 2014-10-14 Rem Technologies, Inc. Superfinishing large planetary gear systems
US20080108470A1 (en) * 2003-05-30 2008-05-08 Mark Michaud Superfinishing Large Planetary Gear Systems
US20050202921A1 (en) * 2004-03-09 2005-09-15 Ford Global Technologies, Llc Application of novel surface finishing technique for improving rear axle efficiency
US20050218117A1 (en) * 2004-04-05 2005-10-06 Jaworowski Mark R Chemically assisted surface finishing process
US7229565B2 (en) * 2004-04-05 2007-06-12 Sikorsky Aircraft Corporation Chemically assisted surface finishing process
US7950330B2 (en) 2004-06-02 2011-05-31 Continuous Metal Technology, Inc. Tungsten-iron projectile
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US7037175B1 (en) 2004-10-19 2006-05-02 Cabot Microelectronics Corporation Method of sharpening cutting edges
US20060084367A1 (en) * 2004-10-19 2006-04-20 Cabot Microelectronics Corporation Method of sharpening cutting edges
WO2009032221A1 (fr) 2007-08-28 2009-03-12 Rem Technologies Inc Procédé pour inspecter et remettre en état des composants mécaniques
US20100331139A1 (en) * 2009-06-25 2010-12-30 United Technologies Corporation Epicyclic gear system with superfinished journal bearing
EP2267338A1 (fr) 2009-06-25 2010-12-29 United Technologies Corporation Système d'engrenage épicycloidal ayant un revêtement de journal superfini
US8172716B2 (en) 2009-06-25 2012-05-08 United Technologies Corporation Epicyclic gear system with superfinished journal bearing
WO2013087429A1 (fr) * 2011-12-13 2013-06-20 Aktiebolaget Skf Procédé permettant de préparer une couche de protection sur une surface tribologique d'un composant mécanique
US9784316B2 (en) 2011-12-13 2017-10-10 Aktiebolaget Skf Process for preparing a protective layer on a tribological surface of a mechanical component
CN103454394A (zh) * 2013-09-11 2013-12-18 西安航空动力股份有限公司 一种航空发动机正齿轮硬化面缺陷的判定方法
CN107735218A (zh) * 2015-07-08 2018-02-23 斯堪尼亚商用车有限公司 研磨具有柱形支承面的工件的方法和用于确定工艺参数的方法
US11518960B2 (en) 2016-08-24 2022-12-06 Ppg Industries Ohio, Inc. Alkaline molybdenum cation and phosphonate-containing cleaning composition
US10792781B2 (en) 2018-04-13 2020-10-06 Bell Helicopter Textron Inc. Masking tool system and method
US10927959B2 (en) 2019-02-27 2021-02-23 Caterpillar Inc. Method and appliance for making isotropically finished seal ring of seal assembly for machine
US11149857B2 (en) 2019-02-27 2021-10-19 Caterpillar Inc. Appliance for making isotropically finished seal ring of seal assembly for machine
CN114728355A (zh) * 2019-10-02 2022-07-08 普罗费雷特两合公司 对已制齿的工件的齿的齿面进行整平的方法和装置以及用于实施该方法的刀具
US20220096114A1 (en) * 2020-09-30 2022-03-31 Entrepix Medical, Llc Cutting instrument with improved surface topography
KR102669076B1 (ko) * 2023-01-11 2024-05-24 (주) 시에스텍 이종접합금속 부스바 제조방법

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JP2004530040A (ja) 2004-09-30
ZA200305319B (en) 2004-10-18
HUP0303188A2 (hu) 2003-12-29
PL363342A1 (en) 2004-11-15
RU2003127071A (ru) 2005-03-10
BR0206813A (pt) 2004-02-03
DE60230114D1 (de) 2009-01-15
ES2317993T3 (es) 2009-05-01
EP1358044B1 (fr) 2008-12-03
CN1491146A (zh) 2004-04-21
CZ20032027A3 (cs) 2004-03-17
KR20030085529A (ko) 2003-11-05
IL157290A0 (en) 2004-02-19
WO2002062528A2 (fr) 2002-08-15
EP1358044A2 (fr) 2003-11-05
US20050164610A1 (en) 2005-07-28
ATE416065T1 (de) 2008-12-15
WO2002062528A3 (fr) 2003-02-27
CA2435732A1 (fr) 2002-08-15
SK8982003A3 (en) 2004-05-04
IL157290A (en) 2007-06-03
MXPA03007106A (es) 2004-10-15

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