US3870607A - Bearing Manufacture - Google Patents

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US3870607A
US3870607A US270355A US27035572A US3870607A US 3870607 A US3870607 A US 3870607A US 270355 A US270355 A US 270355A US 27035572 A US27035572 A US 27035572A US 3870607 A US3870607 A US 3870607A
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silver
radioactive
bearing
coating
layer
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Herbert Bardach
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Avco Corp
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Avco Corp
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    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D7/00Electroplating characterised by the article coated
    • C25D7/10Bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/12Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
    • F16C17/24Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with devices affected by abnormal or undesired positions, e.g. for preventing overheating, for safety
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/12Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
    • F16C17/24Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with devices affected by abnormal or undesired positions, e.g. for preventing overheating, for safety
    • F16C17/246Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with devices affected by abnormal or undesired positions, e.g. for preventing overheating, for safety related to wear, e.g. sensors for measuring wear
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/12Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2233/00Monitoring condition, e.g. temperature, load, vibration

Definitions

  • This invention relates to silver lined metal articles subject to wear, such as antifriction bearings, and to such articles containing radioactive atom dopants placed at a desired sub-surface layer of the silver lining wear surface.
  • the present invention is directed to an improvement over the prior art as it is exemplified in the above noted patents.
  • an extremely thin layer of the silver lining at a desired sub-surface site situated beneath a wearing surface is provided with minute amounts of radioactive silver and/or radioactive impurities without affecting the quality or bond strength of the silver lining.
  • the antifriction bearing or other silver-lined article continues to function usefully and in the same manner as it had before the overlying non-radioactive layer had worn away while the wear particles generated as a result of the wear of the radioactive layer provide an indication to a detecting device that wear of the article has reached the depth of the radioactive layer.
  • the radioactive silver film is tagged with at least one radioisotope having a much longer half-life than the half-life of the longest lived radioisotope of silver, thereby extending the useful life of the detection period for the resulting silver lined article.
  • a silver-lined bearing is produced with an extremely thin layer of the silver lining being tagged with radioactive silver-l m and cobalt-60 at a depth at which the user is to be warned of the extent of wear.
  • a layer of silver overlying the radioactive layer provides the layer to be worn away in service, and below the radioactive layer another layer of silver is provided so that the bearing can continue in service until the radioactive material worn away has been detected and until replacement of the bearing can be effected.
  • the present invention provides both technical and economic advantages over the prior art described above, especially in the manner in which it reduces the amount of radioactive material to a minimum and in the use of a radioactive material
  • Another object is to provide a novel means for depositing a radioactivated silver film on an article, said film being tagged with a radioisotope whose half-life is considerably longer than the half-life of the longest-lived radioisotope of silver, whereby the useful life of the warning layer is extended.
  • Still another object of the invention is to provide minute amounts of a secondary radioisotope species in the bearing silver lining so that the point of bearing wear can be identified, or, in the event that a plurality of bearings are tagged with radioactive material, the indi vidual bearing experiencing wearthrough of the overlying untagged silver layer can be identified by suitable detection means.
  • a further object of this invention is to provide for the electrodeposition of a layer of silver which includes at least one radioactive element in amounts which are insufficient to alter the properties or impair the quality of the silver layer, when it functions as part of the silver lining of an antifriction bearing.
  • Still a further object of the invention is to provide novel silver plating baths for accomplishing the above object.
  • FIG. 1 is a schematic view partially in perspective of a bearing embodying the invention
  • FIG. 2 is a view in section taken on plane 22 of FIG. 1;
  • FIG. 4 is a schematic view of an arrangement showing the manner in which a plurality of bearings are monitored.
  • FIG. 1 there is illustrated a bearing assembly 10 comprising an outer race 12 and a cage 14 in which balls 16 or other antifriction devices are supported.
  • An inner race 20 completes the conventional bearing structure shown by way of illustration.
  • Oil or other fluent lubricant is supplied to the bearing 10 by way of a conduit 22 and is discharged from the bearing by way of a conduit 24.
  • the oil discharged from the bearing contains particles and solid debris formed as the bearing wears away in service.
  • the dirty lubricant is conducted to a detection apparatus 30 containing a Geiger-Muller detector or other means for detecting the presence of radioactive particles when they are present in the lubricant leaving the bearing and containing a means for producing a signal 32 to signify the presence of such radioactive particles in the lubricant.
  • a detection apparatus 30 containing a Geiger-Muller detector or other means for detecting the presence of radioactive particles when they are present in the lubricant leaving the bearing and containing a means for producing a signal 32 to signify the presence of such radioactive particles in the lubricant.
  • the lubricant leaves the detector 30 by way of conduit 28 and returns to inlet 22, after being filtered or otherwise.processed to render it suitable for use in the bearing 10.
  • the annular bearing retainer or cage 14 shown in greater detail in FIGS. 2 and 3 includes an electrodeposited layer 40 of silver or silver base alloy, an extremely thin film 42 of silver deposit containing a very small amount of a radioactive material which is situated in the lands or riding surface of the bearing cage, and an overlying wear layer 44 of silver, deposited to a suitable thickness as a covering on radioactive film 42.
  • the lands are selected only by way of example. For actual applications, other surfaces may be selected as they may be deemed to be more significant wear areas.
  • layer 40 is alayer of silver approximately 0.000l to 0.0003 inch thick deposited on the retainer 14 in the usual way, e.g., in accordance with AMS 2410, which for a steel base involves the sequential application of a nickel strike, a silver strike and then the silver plate to the thickness of 0.0001 to 0.0003 inch.
  • the thickness of layer 40 is usually in proportion of the specification of the total thickness of bearing silver lining which in the above example is assumed to be 0.001 inch.
  • the nickel strike and silver strike and silver plate are deposited on the base metal in that order from conventional baths well known in the art and are not believed to require further description.
  • the silver may be present in concentrations approximately 20 grams/liter and in the plating bath silver concentrations of about 100 grams/liter are commonly used. Cyanide baths are preferred, but other baths may be used at this stage of the process without affecting the results.
  • the unmasked area, or layer 42 was plated from a cyanide bath containing radioactive cobalt-6O as a cobalt ammonium complex and radioactive silver-110m as silver cyanide whereby a radioactive material comprising approximately 99% Ag and 1% Co was electrodeposited on the silver plate to a thickness of 0.000005 inch, after which a layer of nonradioactive silver of 0.000005 inch thickness was flashed onto the radioactive layer to serve as a protective and buffer coating of the radioactive layer against the subsequent demasking and cleaning procedures, after which a 0.0005 inch thick layer of silver was deposited by electroplating from a conventional silver cyanide bath onto the entire bearing retainer surface, thus covering the radioactive material, and bringing the silver plate thickness to 0.00l inch.
  • the bath from which the radioactive cobalt-60 tagged silver layer 42 was deposited on the unmasked areas of the bearing was prepared as follows:
  • An auxiliary bath of radioactive silver-l 10m was prepared in similar fashion by neutron activation of the silver in AgCN.
  • a plating bath was now prepared by mixing 1 ml (0.7 mg of silver) of the Ag-l 10 In stock solution and 20 ml of a AgCN solution (containing 60 mg Ag) into the 1,050 ml solution containing the cobalt ammonium ions.
  • concentrations of silver, cobalt, and potassium cyanide with appertinent specific activities within the following ranges have been found to be suitable for producing radioactive films having a radioisotope constituency of about 0.5 p.c Co-60 and 0.5 uc Ag-l 10m.
  • electrodeposits of silver will contain small amounts of metallic impurities.
  • the usual impurities are iron, copper or lead. It is well known that the presence of these metals in minute amounts do not disqualify the silver electrodeposit from normal service as a bearing silver lining. This prior art knowledge is the basis for a further embodiment of the present invention.
  • each of the bearings or individual wear sites is tagged with radioisotopes which can be electrocodeposited with silver as impurity traces in amounts sufficiently small so as not to affect the quality or bond strength of the silver lining when it functions as an antifriction bearing silver lining.
  • radioisotopes which can be electrocodeposited with silver as impurity traces in amounts sufficiently small so as not to affect the quality or bond strength of the silver lining when it functions as an antifriction bearing silver lining.
  • This tag can consist of longlived cobalt-6O (5.3 year halflife), which extends the useful detection period of the radioactively tagged silver lined article, and a radioisotope such as silver-l 10m, gold-195, zinc-65, antimonyl 25, cadmium-109, or ruthenium-106, which serves to identify the radioactively tagged silver lined article. Further, this dual radioisotope tag permits eclectic utilization of the best properties of available nuclear radiation detectors.
  • a duo-detection system is established corresponding to the dual radioisotope tag whereby the simple, portable, and environmentally rugged Geiger-Mueller detector which is not capable of discriminating between radioactive species can be used, by virtue of the presence of cobalt-60, to monitor in-situ over an extended period of time the wear efflux from silver lined articles such monitoring would be frustrated were the shorter-lived identifier radioisotopes used singly while a scintillation crystal detector which is unsuitable for in-situ monitoring because of its fragility and environmental sensitivity is used as a secondary detector in the laboratory to corroborate the Geiger-Mueller signal as well as identify the secondary radioisotope such as silver-1 10m, gold-195, or other suitable radioisotopes, even after 5 years, being able to do so by virtue of its vastly superior detector sensitivity and the fact that the exigency of a rapid detection period as is requisite for in-situ monitoring is obviated by the need to corroborate
  • the detection system shown schematically detects wear from six bearings tagged with the following combinations of radioisotopes:
  • used lubricant or the oil filter may be sampled and sent to a scintillation crystal detector which will analyze the sample for radioisotope constituency, identify the radioisotope and thus identify the specific bearing indicating distress.
  • the general plating process for incorporating a dual radioisotope tag of cobalt-6O and Radioisotope A which is any of the acceptable identifier radioisotopes such as gold-165, zinc-65 or others noted above is as follows:
  • Step 1 Bearing retainers silver plate is electrochemically stripped clean without removing base metal.
  • Step 3 Retainer is masked and selectively cleaned of mask at bearing surface sites; preferred mask is beeswax.
  • Step 4 Retainer is mechanically scrubbed at the exposed surfaces to remove the superficial surface layers. This is done immediately prior to its immersion in the silver strike solutions. A quick jet stream wash precedes immersion. (Nylon wool is excellent for the mechanical scrubbing operation.)
  • Step 5 Retainer is immersed in cobalt-6O tagged cobalt-doped silver strike solution for 30 minutes.
  • Step 6 Retainer is withdrawn and immersed in radioisotope A tagged silver strike solution for 30 minutes. There is no rinse between withdrawal and immersion. Voltage and amperage requirements will be the same as those in Step 5. (This silver strike infinite dilution solution is similar to that for the cobalt, except that a cyanic compound of radioisotope A is substituted in lieu of the cobalt salts.)
  • Step 7 Retainer is withdrawn and immersed in a nonradioactive silver strike solution for 30 minutes. Voltage and amperage requirements will be the same as those in Step 5. The purpose of this step is to provide the radioactive layer with a protective coating for the rigorous demasking and cleaning operations that follow.
  • Step 9 Retainer is vapor degreased and cleaned.
  • Step 10 Retainer is overplated over entire surface with silver to thickness of 0.001 inch (layer 44).
  • Step 11 Retainer is heat-treated and tested in conformance with AMS 2410 or AMS 2412, depending on whether the base metal is steel or bronze, and is either accepted or rejected. If retainer is rejected, the cycle is repeated.
  • a method of manufacturing a bearing said bearing being coated with silver with at least one radioactive atom species embedded in the coating at a particular depth, the amount of radioactive species in said coating being insufficient to affect the properties of the silver coating when it functions as an' antifriction bearing silver coating and yet being an amount sufficient to be detected in the silver coating wear particles carried away by lubricant when the radioactivated silver incorporated in the silver coating is being worn away, said method comprising:

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  • Mechanical Engineering (AREA)
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  • Chemical Kinetics & Catalysis (AREA)
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  • Rolling Contact Bearings (AREA)

Abstract

A bearing lined with silver, there being radioactive atom dopants of two species, neither of which need be silver, at a particular depth of the silver lining and a method of placing these radioactive atom dopants in said bearing by electrodeposition without altering the quality or bond strength of the silver lining.

Description

United States Patent 1191 Bardach Mar. 11, 1975 BEARING MANUFACTURE OTHER PUBLICATIONS [75] Inventor: Herbert Bardach Danbury Radiochromium Plating for Friction Studies, by John [73] Assignee: Avco Corporation, Stratford, Conn. BUfWel], 6t Nucleonics 3 1 5 Modern Electro latin b Fred Low h 2 d d- 72 P g Y n e 1 [22] Wed July 19 tion (1963) 118, 136, 326441. [21] Appl. No.: 270,355
Related U.S. Application Data i 'y gr g g H I P ttorney, gent, 0r irmar es ogan; rwin [62] Division of Ser. No, l36,083, Aprll 21, 197]. Ga n e; Lawrence Field [52] U.S. Cl 204/15, 204/40, 308/237 R [51] Int. Cl. C23b 5/48, C23b 5/46, C23b 5/50 [57] ABSTRACT [58] F'eld Search 204/40 A bearing lined with silver, there being radioactive atom dopants of two species, neither of which need be silver, at a particular depth of the silver lining and a [56] References C'ted method of placing these radioactive atom dopants in UNITED STATES PATENTS said bearing by electrodeposition without altering the 2,315,845 4/1943 Ferris 250/836 quality or bond strength of the silver lining. 2,468,905 5/1949 Warren... 175/39 2,938,125 3/1960 Marak 250/106 6 Clalms, 4 Drawmg Flgures Will/712717717;
BEARING MANUFACTURE This is a division of application Ser. No. 136,083, filed Apr. 21, 1971.
This invention relates to silver lined metal articles subject to wear, such as antifriction bearings, and to such articles containing radioactive atom dopants placed at a desired sub-surface layer of the silver lining wear surface.
The provision of a radioactive material in a surface layer of bearings, pistons, cylinders, gears and other similar metal surfaces is disclosed in Ferris U.S. Pat. No. 2,315,845, as a means for determining wear in such surfaces in test apparatus.
Another means for detecting wear in tools, such as bits, is described in Warren U.S. Pat. No. 2,468,905. In that disclosure, a pocket or recess is provided in the tool and a radioactive capsule is inserted in the recess. When the tool face has worn down to the capsule, radioactive material begins to wear away and is detected as in the Ferris patent or by other suitable means.
Still another method for determining wear is described in Marak U.S. Pat. No. 2,938,125 in which a bearing surface is coated with a radioactive layer and this in turn is overlaid with a wear resistant layer.
The present invention is directed to an improvement over the prior art as it is exemplified in the above noted patents. In the present invention, an extremely thin layer of the silver lining at a desired sub-surface site situated beneath a wearing surface is provided with minute amounts of radioactive silver and/or radioactive impurities without affecting the quality or bond strength of the silver lining. As a result, the antifriction bearing or other silver-lined article continues to function usefully and in the same manner as it had before the overlying non-radioactive layer had worn away while the wear particles generated as a result of the wear of the radioactive layer provide an indication to a detecting device that wear of the article has reached the depth of the radioactive layer.
In a preferred embodiment of the invention, the radioactive silver film is tagged with at least one radioisotope having a much longer half-life than the half-life of the longest lived radioisotope of silver, thereby extending the useful life of the detection period for the resulting silver lined article.
For example, a silver-lined bearing is produced with an extremely thin layer of the silver lining being tagged with radioactive silver-l m and cobalt-60 at a depth at which the user is to be warned of the extent of wear. A layer of silver overlying the radioactive layer provides the layer to be worn away in service, and below the radioactive layer another layer of silver is provided so that the bearing can continue in service until the radioactive material worn away has been detected and until replacement of the bearing can be effected.
It will be seen that the present invention provides both technical and economic advantages over the prior art described above, especially in the manner in which it reduces the amount of radioactive material to a minimum and in the use of a radioactive material which Another object is to provide a novel means for depositing a radioactivated silver film on an article, said film being tagged with a radioisotope whose half-life is considerably longer than the half-life of the longest-lived radioisotope of silver, whereby the useful life of the warning layer is extended.
Still another object of the invention is to provide minute amounts of a secondary radioisotope species in the bearing silver lining so that the point of bearing wear can be identified, or, in the event that a plurality of bearings are tagged with radioactive material, the indi vidual bearing experiencing wearthrough of the overlying untagged silver layer can be identified by suitable detection means.
A further object of this invention is to provide for the electrodeposition of a layer of silver which includes at least one radioactive element in amounts which are insufficient to alter the properties or impair the quality of the silver layer, when it functions as part of the silver lining of an antifriction bearing.
Still a further object of the invention is to provide novel silver plating baths for accomplishing the above object.
Other and more specific related objects of the invention will be apparent from a study of the accompanying drawings and their description, it being understood that these are offered by way of example only and not in limitation of the invention, the scope of which is defined by the appended claims rather than by any preceding description.
IN THE DRAWINGS FIG. 1 is a schematic view partially in perspective of a bearing embodying the invention;
FIG. 2 is a view in section taken on plane 22 of FIG. 1;
FIG. 3 is an enlarged view of a portion of FIG. 2; and
FIG. 4 is a schematic view of an arrangement showing the manner in which a plurality of bearings are monitored.
Referring first to FIG. 1, there is illustrated a bearing assembly 10 comprising an outer race 12 and a cage 14 in which balls 16 or other antifriction devices are supported. An inner race 20 completes the conventional bearing structure shown by way of illustration. Oil or other fluent lubricant is supplied to the bearing 10 by way of a conduit 22 and is discharged from the bearing by way of a conduit 24. The oil discharged from the bearing contains particles and solid debris formed as the bearing wears away in service. The dirty lubricant is conducted to a detection apparatus 30 containing a Geiger-Muller detector or other means for detecting the presence of radioactive particles when they are present in the lubricant leaving the bearing and containing a means for producing a signal 32 to signify the presence of such radioactive particles in the lubricant.
The lubricant leaves the detector 30 by way of conduit 28 and returns to inlet 22, after being filtered or otherwise.processed to render it suitable for use in the bearing 10.
The annular bearing retainer or cage 14 shown in greater detail in FIGS. 2 and 3 includes an electrodeposited layer 40 of silver or silver base alloy, an extremely thin film 42 of silver deposit containing a very small amount of a radioactive material which is situated in the lands or riding surface of the bearing cage, and an overlying wear layer 44 of silver, deposited to a suitable thickness as a covering on radioactive film 42. The lands are selected only by way of example. For actual applications, other surfaces may be selected as they may be deemed to be more significant wear areas.
In service, layer 44 wears away and the wear particles being non-radioactive do not cause detector 30 and signal producing means 32 to issue any alarm.
When layer 44 has completely worn away, the particles worn from film 42 are detected by detector 30 and a signal is produced alerting the user to the fact that wear has proceeded through layer 44.
Continued use of the bearing in service leads to wear of layer 40, until such time as the bearing is replaced.
By way of illustration, layer 40 is alayer of silver approximately 0.000l to 0.0003 inch thick deposited on the retainer 14 in the usual way, e.g., in accordance with AMS 2410, which for a steel base involves the sequential application of a nickel strike, a silver strike and then the silver plate to the thickness of 0.0001 to 0.0003 inch. The thickness of layer 40 is usually in proportion of the specification of the total thickness of bearing silver lining which in the above example is assumed to be 0.001 inch.
The nickel strike and silver strike and silver plate are deposited on the base metal in that order from conventional baths well known in the art and are not believed to require further description. In the silver strike bath, the silver may be present in concentrations approximately 20 grams/liter and in the plating bath silver concentrations of about 100 grams/liter are commonly used. Cyanide baths are preferred, but other baths may be used at this stage of the process without affecting the results.
These concentrations are considerably larger than those utilized in the infinite dilution" solution from which the thin radioactive layer 42 of silver is deposited onto the lands of the silver-plated retainer 14.
After deposition of layer 40, and subsequent selective masking, the unmasked area, or layer 42, was plated from a cyanide bath containing radioactive cobalt-6O as a cobalt ammonium complex and radioactive silver-110m as silver cyanide whereby a radioactive material comprising approximately 99% Ag and 1% Co was electrodeposited on the silver plate to a thickness of 0.000005 inch, after which a layer of nonradioactive silver of 0.000005 inch thickness was flashed onto the radioactive layer to serve as a protective and buffer coating of the radioactive layer against the subsequent demasking and cleaning procedures, after which a 0.0005 inch thick layer of silver was deposited by electroplating from a conventional silver cyanide bath onto the entire bearing retainer surface, thus covering the radioactive material, and bringing the silver plate thickness to 0.00l inch.
The bath from which the radioactive cobalt-60 tagged silver layer 42 was deposited on the unmasked areas of the bearing was prepared as follows:
One liter of deionized water was poured into a beaker. Twenty grams of KCN was added to the water and the mixture was stirred until dissolved with gentle heat (l20-l80F). While maintaining the heat, 7.4 grams of finely powdered cobaltous carbonate was added to the solution and dissolved therein. The liquidturned dark green and some sediment formed on the bottom of the beaker. To the resulting solution a solution of 10 milliliters of NH OH, 1 gram of benzoic acid and 2 grams of salicylic acid were added in order to form cobalt ammonium complex ions, in situ. The formation of these ions was evidenced by a color change from greenish to reddish hue. The yield of cobalt as complexed cobalt ammonium was about 3.8 grams.
After repeated filtration, a 50 ml aliquot was withdrawn from the filtrate and run into a large evaporating pan, maintained at 180 to 200F, until the liquid was removed. The dessicated, dried salts were then packaged in a quartz tube and subjected to neutron bombardment to convert a portion of the cobalt to Co-60. The resulting cobalt ammonium compound, now tagged with Co-60, was readily redissolved in 1,050 ml of water in which it redissociated to the complex cobalt ammonium ion.
An auxiliary bath of radioactive silver-l 10m was prepared in similar fashion by neutron activation of the silver in AgCN.
A plating bath was now prepared by mixing 1 ml (0.7 mg of silver) of the Ag-l 10 In stock solution and 20 ml of a AgCN solution (containing 60 mg Ag) into the 1,050 ml solution containing the cobalt ammonium ions.
After the usual silver strike had been deposited on the base material, the cobalt-60 tagged silver-l 10m tagged bath was used as the electrolyte and a radioactive layer of between 0.0000002 and 0.000005 inch was deposited on the non-radioactive (0.0001 0.0003 inch) silver layer.
Thereafter a layer of non-radioactive silver was plated over the entire surface to the depth desired for wear purposes (e.g., about 0.001 inch).
For the radioactive bath, concentrations of silver, cobalt, and potassium cyanide with appertinent specific activities within the following ranges have been found to be suitable for producing radioactive films having a radioisotope constituency of about 0.5 p.c Co-60 and 0.5 uc Ag-l 10m.
Concentration Specific Activity Ag (as CN) 30-50 mg/liter l Lc/mg Co (as Co(NH 150-250 mg/liter -l 50 #c/mg com lex) KCBF 50-100 mg/liter In the accompanying table, results are tabulated for eight bearings prepared according to the method described above, each of which is representative of the bearings of this invention.
TABLE I Specimen Bath Unmasked Anode Composition Bath Bath Surface Area Plating to Cathode (mg) Vol- Activity Voltage Amper- (Cathode) Time Surface I ume age Spemmen Co CN Ag (ml) Co Ag (Volts) (ma) (Sq. inch) (min) Area Radius A 190 100 60.7 1050 20.8mc 37.5 1c 5.0 65 .90 40 10:1 B 190 100 60.7 1050 20.8mc 37.5 5.0 65 .90 60 10;] D 190 1000 61.1 1060 20.8mc 59.0 3.2 70 .90 30 1011 E 190 1000 61.1 1060 20.8mc 59.0,: 3.0 30 .90 30 1 F 190 1000 61.1 1060 20.8mc 59.0}LC 5.0 200 .90 30 10;] G 190 1000 61.1 1060 20.8mc $9.0m 4.3 200 .90 3O 10;1
Relative Activity te i) at Ag at Plate Activity Plate Composition Hydrogen 1.17 Mev .657 Mev (pic) ("/0 weight) Plate Weight Plate Thickness Specimen Evolution Peak Peak Co Ag Co Ag (micrograms) (inches) A Moderate 8000 27000 0.6 0.5 0.9 99.1 735 5 X B Moderate 7000 31000 0.5 0.6 0.7 99.3 841 5 X 10 D Brisk 1600 52000 Very Slight 500 1500 0.03 0.03 2.0 98.0 27 Z X 10* F Moderate 2000 50000 0.15 0.92 0.2 99.8 867 S X 10" G Brisk 2000 50000 0.15 0.92 0.2 99.8 867 5 X 10 (The anode material used was stainless steel.)
As is known, unless elaborate precautions are taken and ultrapure reagents and silver electrodes are utilized, electrodeposits of silver will contain small amounts of metallic impurities. The usual impurities are iron, copper or lead. It is well known that the presence of these metals in minute amounts do not disqualify the silver electrodeposit from normal service as a bearing silver lining. This prior art knowledge is the basis for a further embodiment of the present invention.
In a wear detection system applied to a plurality of bearings or a plurality of wear sites in a single bearing, each of the bearings or individual wear sites is tagged with radioisotopes which can be electrocodeposited with silver as impurity traces in amounts sufficiently small so as not to affect the quality or bond strength of the silver lining when it functions as an antifriction bearing silver lining. As there is a paucity of long-lived radioisotopes satisfying these requirements and as there is a need for distinguishing the silver wear from amongst a plurality of silver-lined articles assembled in a system, it is advantageous to have the tag invested in the silver lining comprise a dual radioisotope tag. This tag can consist of longlived cobalt-6O (5.3 year halflife), which extends the useful detection period of the radioactively tagged silver lined article, and a radioisotope such as silver-l 10m, gold-195, zinc-65, antimonyl 25, cadmium-109, or ruthenium-106, which serves to identify the radioactively tagged silver lined article. Further, this dual radioisotope tag permits eclectic utilization of the best properties of available nuclear radiation detectors. Thus, a duo-detection system is established corresponding to the dual radioisotope tag whereby the simple, portable, and environmentally rugged Geiger-Mueller detector which is not capable of discriminating between radioactive species can be used, by virtue of the presence of cobalt-60, to monitor in-situ over an extended period of time the wear efflux from silver lined articles such monitoring would be frustrated were the shorter-lived identifier radioisotopes used singly while a scintillation crystal detector which is unsuitable for in-situ monitoring because of its fragility and environmental sensitivity is used as a secondary detector in the laboratory to corroborate the Geiger-Mueller signal as well as identify the secondary radioisotope such as silver-1 10m, gold-195, or other suitable radioisotopes, even after 5 years, being able to do so by virtue of its vastly superior detector sensitivity and the fact that the exigency of a rapid detection period as is requisite for in-situ monitoring is obviated by the need to corroborate the first signal as well as to identify the particular silver-lined bearing in distress.
In FIG. 4, the detection system shown schematically detects wear from six bearings tagged with the following combinations of radioisotopes:
cobalt-60, silver-m cobalt-60, gold-195 cobalt-60, zinc-65 cobalt-60, antimonycobalt-60, cadmium-109 cobalt-60, ruthenium-106 After the wear to the radioactively tagged silver layer has been detected by a Geiger-Mueller detector, used lubricant or the oil filter may be sampled and sent to a scintillation crystal detector which will analyze the sample for radioisotope constituency, identify the radioisotope and thus identify the specific bearing indicating distress.
The general plating process for incorporating a dual radioisotope tag of cobalt-6O and Radioisotope A, which is any of the acceptable identifier radioisotopes such as gold-165, zinc-65 or others noted above is as follows:
Step 1. Bearing retainers silver plate is electrochemically stripped clean without removing base metal.
Step 2. Entire retainer surface is preliminarily preplated with silver layer 40 to desired depth or thickness.
Step 3. Retainer is masked and selectively cleaned of mask at bearing surface sites; preferred mask is beeswax.
Step 4. Retainer is mechanically scrubbed at the exposed surfaces to remove the superficial surface layers. This is done immediately prior to its immersion in the silver strike solutions. A quick jet stream wash precedes immersion. (Nylon wool is excellent for the mechanical scrubbing operation.)
Step 5. Retainer is immersed in cobalt-6O tagged cobalt-doped silver strike solution for 30 minutes.
2-6 volts Amperage setting:
Step 6. Retainer is withdrawn and immersed in radioisotope A tagged silver strike solution for 30 minutes. There is no rinse between withdrawal and immersion. Voltage and amperage requirements will be the same as those in Step 5. (This silver strike infinite dilution solution is similar to that for the cobalt, except that a cyanic compound of radioisotope A is substituted in lieu of the cobalt salts.)
Step 7. Retainer is withdrawn and immersed in a nonradioactive silver strike solution for 30 minutes. Voltage and amperage requirements will be the same as those in Step 5. The purpose of this step is to provide the radioactive layer with a protective coating for the rigorous demasking and cleaning operations that follow.
Step 8. Retainer is withdrawn by remote handling equipment and vigorously rinsed, then dried by a jet of inert gas.
Step 9. Retainer is vapor degreased and cleaned.
Step 10. Retainer is overplated over entire surface with silver to thickness of 0.001 inch (layer 44).
Step 11. Retainer is heat-treated and tested in conformance with AMS 2410 or AMS 2412, depending on whether the base metal is steel or bronze, and is either accepted or rejected. If retainer is rejected, the cycle is repeated.
I claim:
1. A method of manufacturing a bearing, said bearing being coated with silver with at least one radioactive atom species embedded in the coating at a particular depth, the amount of radioactive species in said coating being insufficient to affect the properties of the silver coating when it functions as an' antifriction bearing silver coating and yet being an amount sufficient to be detected in the silver coating wear particles carried away by lubricant when the radioactivated silver incorporated in the silver coating is being worn away, said method comprising:
depositing a relatively thin layer of non-radioactive silver on a base metal; masking portions of said layer thereby defining at least one wear receiving surface;
electrodepositing an extremely thin layer of silver doped with at least one radioactive atom species to said wear receiving surface;
removing the mask from the resulting article; and
thereafter depositing a relatively thick layer of silver on said article.
2. The method of claim 1 wherein the silver layers are applied to said article by electrodeposition.
3. The method of claim 2 wherein said extremely thin layer is electrodeposited from an infinite dilution silver strike solution:
4. The method of manufacturing an article coated with silver, said method comprising:
depositing a relatively thin layer of non-radioactive silver on a base metal;
electrodepositing an extremely thin layer of silver doped with at least one radioactive atom species to at least a portion of the surface of said relatively thin layer; and
thereafter depositing a relatively thick layer of silver on the aforesaid deposits.
5. The method of claim 4 wherein said silver layers are applied by electrodeposition.
6. The invention as defined in claim 5 wherein said dilu ti on silver strike solution.

Claims (6)

1. A METHOD OF MANUFACTURING A BEARING, SAID BEARING BEING COATED WITH SILVER WITH AT LEAST ONE RADIOACTIVE ATOM SPECIES EMBEDDED IN THE COATING AT A PARTICULAR DEPTH, THE AMOUNT OF RADIOACTIVE SPECIES IN SAID COATING BEING INSUFFICIENT TO AFFECT THE PROPERTIES OF THE SILVER COATING WHEN IT FUNCTIONS AS AN ANTIFRICTION BEARING SILVER COATING AND YET BEING AN AMOUNT SUFFICIENT TO BE DETECTED IN THE SILVER COATING WEAR PARTICLES CARRIED AWAY BY LUBRICANT WHEN THE RADIOACTIVATED SILVER INCORPORATED IN THE SILVER COATING IS BEING WORN AWAY, SAID METHOD COMPRISING: DEPOSITING A RELATIVELY THIN LAYER OF NON-RADIOACTIVE SILVER ON A BASE METAL; MASKING PORTIONS OF SAID LAYER THEREBY DEFINING AT LEAST ONE WEAR RECEIVING SURFACE; ELECTRODEPOSITING AN EXTREMELY THIN LAYER OF SILVER DOPED WITH AT LEAST ONE RADIOACTIVE ATOM SPECIES TO SAID WEAR RECEIVING SURFACE; REMOVING THE MASK FROM THE RESULTING ARTICLE, AND THEREAFTER DEPOSITING A RELATIVELY THICK LAYER OF SILVER ON SAID ARTICLE.
1. A method of manufacturing a bearing, said bearing being coated with silver with at least one radioactive atom species embedded in the coating at a particular depth, the amount of radioactive species in said coating being insufficient to affect the properties of the silver coating when it functions as an antifriction bearing silver coating and yet being an amount sufficient to be detected in the silver coating wear particles carried away by lubricant when the radioactivated silver incorporated in the silver coating is being worn away, said method comprising: depositing a relatively thin layer of non-radioactive silver on a base metal; masking portions of said layer thereby defining at least one wear receiving surface; electrodepositing an extremely thin layer of silver doped with at least one radioactive atom species to said wear receiving surface; removing the mask from the resulting article; and thereafter depositing a relatively thick layer of silver on said article.
2. The method of claim 1 wherein the silver layers are applied to said article by electrodeposition.
3. The method of claim 2 wherein said extremely thin layer is electrodeposited from an infinite dilution silver strike solution.
4. The method of manufacturing an article coated with silver, said method comprising: depositing a relatively thin layer of Non-radioactive silver on a base metal; electrodepositing an extremely thin layer of silver doped with at least one radioactive atom species to at least a portion of the surface of said relatively thin layer; and thereafter depositing a relatively thick layer of silver on the aforesaid deposits.
5. The method of claim 4 wherein said silver layers are applied by electrodeposition.
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Cited By (14)

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US4375761A (en) * 1979-10-04 1983-03-08 The British Petroleum Company Limited Monitoring internal combustion engines
US5298092A (en) * 1990-05-17 1994-03-29 The Boeing Company Non-chromated oxide coating for aluminum substrates
US5378293A (en) * 1990-05-17 1995-01-03 The Boeing Company Non-chromated oxide coating for aluminum substrates
US5411606A (en) * 1990-05-17 1995-05-02 The Boeing Company Non-chromated oxide coating for aluminum substrates
US5468307A (en) * 1990-05-17 1995-11-21 Schriever; Matthias P. Non-chromated oxide coating for aluminum substrates
US5472524A (en) * 1990-05-17 1995-12-05 The Boeing Company Non-chromated cobalt conversion coating method and coated articles
US5551994A (en) * 1990-05-17 1996-09-03 The Boeing Company Non-chromated oxide coating for aluminum substrates
US5873953A (en) * 1996-12-26 1999-02-23 The Boeing Company Non-chromated oxide coating for aluminum substrates
US6432225B1 (en) 1999-11-02 2002-08-13 The Boeing Company Non-chromated oxide coating for aluminum substrates
US20110188794A1 (en) * 2008-05-08 2011-08-04 Schaeffler Technologies Gmbh & Co. Kg Bearing module
US20140177990A1 (en) * 2011-08-23 2014-06-26 Ntn Corporation Rolling bearing
US20160178064A1 (en) * 2013-08-06 2016-06-23 Messier-Dowty Limited An apparatus comprising a sealing element
US20160201820A1 (en) * 2013-08-26 2016-07-14 Parker-Hannifin Corporation High cycle and speed valve
US20230258531A1 (en) * 2022-02-14 2023-08-17 Bell Textron Inc. Method and system for gearbox failure detection using radioactive components

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US2315845A (en) * 1941-10-25 1943-04-06 Atlantic Refining Co Wear test method and composition
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US2938125A (en) * 1955-06-06 1960-05-24 Phillips Petroleum Co Wear determination method

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US2315845A (en) * 1941-10-25 1943-04-06 Atlantic Refining Co Wear test method and composition
US2468905A (en) * 1943-06-11 1949-05-03 Jr John B Warren Means for detecting wear on bits
US2938125A (en) * 1955-06-06 1960-05-24 Phillips Petroleum Co Wear determination method

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4375761A (en) * 1979-10-04 1983-03-08 The British Petroleum Company Limited Monitoring internal combustion engines
US5298092A (en) * 1990-05-17 1994-03-29 The Boeing Company Non-chromated oxide coating for aluminum substrates
US5378293A (en) * 1990-05-17 1995-01-03 The Boeing Company Non-chromated oxide coating for aluminum substrates
US5411606A (en) * 1990-05-17 1995-05-02 The Boeing Company Non-chromated oxide coating for aluminum substrates
US5415687A (en) * 1990-05-17 1995-05-16 The Boeing Company Non-chromated oxide coating for aluminum substrates
US5468307A (en) * 1990-05-17 1995-11-21 Schriever; Matthias P. Non-chromated oxide coating for aluminum substrates
US5472524A (en) * 1990-05-17 1995-12-05 The Boeing Company Non-chromated cobalt conversion coating method and coated articles
US5551994A (en) * 1990-05-17 1996-09-03 The Boeing Company Non-chromated oxide coating for aluminum substrates
US5873953A (en) * 1996-12-26 1999-02-23 The Boeing Company Non-chromated oxide coating for aluminum substrates
US6432225B1 (en) 1999-11-02 2002-08-13 The Boeing Company Non-chromated oxide coating for aluminum substrates
US20110188794A1 (en) * 2008-05-08 2011-08-04 Schaeffler Technologies Gmbh & Co. Kg Bearing module
US9175726B2 (en) * 2008-05-08 2015-11-03 Schaeffler Technologies AG & Co. KG Bearing module
US20140177990A1 (en) * 2011-08-23 2014-06-26 Ntn Corporation Rolling bearing
US9011014B2 (en) * 2011-08-23 2015-04-21 Ntn Corporation Rolling bearing
US20160178064A1 (en) * 2013-08-06 2016-06-23 Messier-Dowty Limited An apparatus comprising a sealing element
US20160201820A1 (en) * 2013-08-26 2016-07-14 Parker-Hannifin Corporation High cycle and speed valve
US9885421B2 (en) * 2013-08-26 2018-02-06 Parker-Hannifin Corporation High cycle and speed valve
US20230258531A1 (en) * 2022-02-14 2023-08-17 Bell Textron Inc. Method and system for gearbox failure detection using radioactive components

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