GB987155A - Bearings - Google Patents
BearingsInfo
- Publication number
- GB987155A GB987155A GB9746/63A GB974663A GB987155A GB 987155 A GB987155 A GB 987155A GB 9746/63 A GB9746/63 A GB 9746/63A GB 974663 A GB974663 A GB 974663A GB 987155 A GB987155 A GB 987155A
- Authority
- GB
- United Kingdom
- Prior art keywords
- inch
- powder
- bearing surface
- cobalt
- nickel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/043—Sliding surface consisting mainly of ceramics, cermets or hard carbon, e.g. diamond like carbon [DLC]
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/122—Multilayer structures of sleeves, washers or liners
- F16C33/125—Details of bearing layers, i.e. the lining
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2206/00—Materials with ceramics, cermets, hard carbon or similar non-metallic hard materials as main constituents
- F16C2206/40—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal
- F16C2206/42—Ceramics, e.g. carbides, nitrides, oxides, borides of a metal based on ceramic oxides
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/30—Coating surfaces
- F16C2223/42—Coating surfaces by spraying the coating material, e.g. plasma spraying
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2240/00—Specified values or numerical ranges of parameters; Relations between them
- F16C2240/40—Linear dimensions, e.g. length, radius, thickness, gap
- F16C2240/60—Thickness, e.g. thickness of coatings
Abstract
A bearing surface is formed of material containing nickel oxide and/or cobalt oxide applied by projecting at least superficially molten particles of nickel oxide and/or cobalt oxide on to a substrate or by projecting at least superficially molten particles of nickel or cobalt on to a substrate and subsequently oxidizing them. In addition to the use of either or both of nickel and cobalt oxides, the bearing surface can be modified by including in addition nickel and/or cobalt metals (which may if desired be subsequently oxidized) or other additives and coadjutants. The substrate can be made of various materials such as stainless steel, mild steel, aluminium, ceramics and thermosetting plastics. The thickness of the bearing surface can be varied over a wide range, at least from 0.005 to 0.025 inch and suitably up to 0.085 inch. The following materials were charged into an 8-inch diameter rubber-lined ball mill:- .Green nickel oxide (200 B.S. mesh).2000 gm .Calcined alumina (200 B.S. mesh).160 gm . 1/2 -inch Alorite cylinders.2160 gm .Distilled water.1000 ml The mill was then rotated at 60 r.p.m. for six hours. After milling, the water was removed by drying at 105-110 DEG C. in an oven until the powder was almost dry. The damp powder was passed through a 22 B.S. sieve and pressed into a compact 1 1/2 inches x 1 inch x 1/2 inch at 2 tons per square inch. The compact was placed on coarse fused magnesia powder on an alumina tile and fired to 1500 DEG C. in an oxidizing atmosphere. After sintering, the compact was powdered by passing it through a jaw crusher and hammer mill. The powder was sieved into the following fractions:- .A..On 100 B.S.S .B..Through 100 B.S.S. on 200 B.S.S .C..Through 200 B.S.S. on 350 B.S.S .D..Through 350 B.S.S The (A) and (D) fractions were rejected and the (B) and (C) fractions were re-blended in the weight ratio of 1:4. The resultant powder was flame-sprayed on to a prepared stainless steel surface by the usual techniques and formed a bearing surface having a thickness of 0.02 inch. Alternatively the powder, after milling and drying, can be extruded into rod form after the addition of a suitable extrusion binder such as 20% by weight of a cellulose material in water. The extruded rods are dried for several hours, then fired to say 1450 DEG C. in air whilst supported on an inert material such as magnesia powder. These rods can then be used in a rod type of flame spraying gun to apply coatings as before.ALSO:A bearing surface is formed of material containing nickel oxide and/or cobalt oxide applied by projecting at least superficially molten particles of nickel oxide and/or cobalt oxide on to a substrate. In addition to the use of either or both of nickel and cobalt oxides, the bearing surface can be modified by including in addition nickel and/or cobalt metals (which may if desired be subsequently oxidized) or other additives and coadjutants. The substrate can be made of various materials such as stainless steel, mild steel, aluminium, ceramics and thermosetting plastics. The thickness of the bearing surface can be varied over a wide range, at least from 0,005-0,025 inch and suitably up to 0,085 inch. The powder may be flame-sprayed on to a prepared stainless steel surface by the usual techniques and form a bearing surface having a thickness of 0,02 inch. Alternatively the powder, after milling and drying, can be extruded into rod form after the addition of a suitable extrusion binder such as 20% by weight of a cellulose material in water. The extruded rods are dried for several hours, then fired to say 1450 DEG C. in air whilst supported on an inert material such as magnesia powder. These rods can then be used in a rod type of flame spraying gun to apply coatings as before.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9746/63A GB987155A (en) | 1963-03-12 | 1963-03-12 | Bearings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9746/63A GB987155A (en) | 1963-03-12 | 1963-03-12 | Bearings |
Publications (1)
Publication Number | Publication Date |
---|---|
GB987155A true GB987155A (en) | 1965-03-24 |
Family
ID=9877973
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9746/63A Expired GB987155A (en) | 1963-03-12 | 1963-03-12 | Bearings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB987155A (en) |
-
1963
- 1963-03-12 GB GB9746/63A patent/GB987155A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3296002A (en) | Refractory shapes | |
US2707691A (en) | Coating metals and other materials with oxide and articles made thereby | |
KR910009192B1 (en) | Burnable neutron absorbers | |
JP2002527334A5 (en) | ||
DE966860C (en) | Compounds and bodies containing boron nitride and processes for their production | |
WO1994018140A1 (en) | Method of producing ceramic moldings containing fine-grained alumina, using powdered aluminum metal | |
US3244539A (en) | Bonded alumina refractory | |
US2882174A (en) | Alumina rods for coating articles | |
GB987155A (en) | Bearings | |
US2899323A (en) | Heat exchange pebbles | |
JPS5757804A (en) | Production of honeycomb-shaped molding made of metal | |
US2801590A (en) | Pyrophoric element | |
ES8609179A1 (en) | Process for producing a sintered silicon carbide/carbon composite ceramic body having ultrafine grain microstructure. | |
US5320989A (en) | Boron nitride-containing bodies and method of making the same | |
US3679383A (en) | Process for the manufacture of shaped articles of zirconium corundum | |
GB954948A (en) | Rods for flame-spraying | |
DE1471032C3 (en) | Mixture for the production of a refractory body, mortar and the like | |
GB949727A (en) | Improvements in or relating to nuclear fuel | |
JPS59207873A (en) | Manufacture of high density silicon carbide sintered body | |
US3244540A (en) | High alumina refractory bodies | |
DE959423C (en) | Device for burning liquid and solid fuels, especially in jet engines or the like. | |
DE1902085B2 (en) | Process for flame spraying and a suitable sintered rod | |
US2687364A (en) | Process for cementing plastically deformable bodies and products thereof | |
GEORGIA INST OF TECH ATLANTA ENGINEERING EXPERIMENT STATION | CERAMIC SYSTEMS FOR MISSILE STRUCTURAL APPLICATIONS. | |
SU781190A1 (en) | Charge for producing ceramic materials |