US3871840A - Abrasive particles encapsulated with a metal envelope of allotriomorphic dentrites - Google Patents
Abrasive particles encapsulated with a metal envelope of allotriomorphic dentrites Download PDFInfo
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- US3871840A US3871840A US219973A US21997372A US3871840A US 3871840 A US3871840 A US 3871840A US 219973 A US219973 A US 219973A US 21997372 A US21997372 A US 21997372A US 3871840 A US3871840 A US 3871840A
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- US
- United States
- Prior art keywords
- metal
- abrasive
- tungsten
- article
- encapsulated
- Prior art date
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- Expired - Lifetime
Links
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 183
- 239000002184 metal Substances 0.000 title claims abstract description 183
- 239000002245 particle Substances 0.000 title claims abstract description 140
- 239000010432 diamond Substances 0.000 claims abstract description 76
- 238000000034 method Methods 0.000 claims abstract description 52
- 239000011159 matrix material Substances 0.000 claims abstract description 47
- 229910003460 diamond Inorganic materials 0.000 claims abstract description 34
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 52
- 229910052721 tungsten Inorganic materials 0.000 claims description 52
- 239000010937 tungsten Substances 0.000 claims description 52
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims description 45
- 230000008569 process Effects 0.000 claims description 25
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 22
- 239000010955 niobium Substances 0.000 claims description 21
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 19
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 14
- 239000001257 hydrogen Substances 0.000 claims description 14
- 229910052739 hydrogen Inorganic materials 0.000 claims description 14
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 14
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 14
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 11
- 229910052750 molybdenum Inorganic materials 0.000 claims description 11
- 239000011733 molybdenum Substances 0.000 claims description 11
- 229910052715 tantalum Inorganic materials 0.000 claims description 11
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 11
- 229910052758 niobium Inorganic materials 0.000 claims description 10
- 210000001787 dendrite Anatomy 0.000 claims description 9
- 238000000151 deposition Methods 0.000 claims description 9
- 238000004519 manufacturing process Methods 0.000 claims description 9
- 150000002736 metal compounds Chemical class 0.000 claims description 7
- 229910002651 NO3 Inorganic materials 0.000 claims description 5
- NHNBFGGVMKEFGY-UHFFFAOYSA-N Nitrate Chemical compound [O-][N+]([O-])=O NHNBFGGVMKEFGY-UHFFFAOYSA-N 0.000 claims description 5
- 238000000354 decomposition reaction Methods 0.000 claims description 4
- 239000007789 gas Substances 0.000 claims description 4
- 229910001963 alkali metal nitrate Inorganic materials 0.000 claims description 3
- 239000003513 alkali Substances 0.000 claims description 2
- 239000000758 substrate Substances 0.000 abstract description 45
- 239000003082 abrasive agent Substances 0.000 abstract description 16
- 239000011230 binding agent Substances 0.000 abstract description 13
- 238000000576 coating method Methods 0.000 abstract description 10
- 239000011248 coating agent Substances 0.000 abstract description 9
- 230000008602 contraction Effects 0.000 abstract description 3
- 229910000765 intermetallic Inorganic materials 0.000 abstract description 3
- 150000002739 metals Chemical class 0.000 description 19
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 17
- 238000002844 melting Methods 0.000 description 16
- 230000008018 melting Effects 0.000 description 15
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 13
- 239000000203 mixture Substances 0.000 description 13
- 239000012071 phase Substances 0.000 description 12
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 10
- 230000005484 gravity Effects 0.000 description 10
- 238000005538 encapsulation Methods 0.000 description 9
- 229910045601 alloy Inorganic materials 0.000 description 8
- 239000000956 alloy Substances 0.000 description 8
- 230000008901 benefit Effects 0.000 description 8
- 238000006243 chemical reaction Methods 0.000 description 8
- 239000010941 cobalt Substances 0.000 description 8
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 8
- 229910052759 nickel Inorganic materials 0.000 description 8
- 229910017052 cobalt Inorganic materials 0.000 description 7
- 239000000463 material Substances 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 239000007767 bonding agent Substances 0.000 description 6
- 229910052742 iron Inorganic materials 0.000 description 6
- 239000000047 product Substances 0.000 description 6
- 229910052786 argon Inorganic materials 0.000 description 5
- 150000001875 compounds Chemical class 0.000 description 5
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 239000013078 crystal Substances 0.000 description 4
- 238000005520 cutting process Methods 0.000 description 4
- -1 masonry Substances 0.000 description 4
- 230000000704 physical effect Effects 0.000 description 4
- FGIUAXJPYTZDNR-UHFFFAOYSA-N potassium nitrate Chemical compound [K+].[O-][N+]([O-])=O FGIUAXJPYTZDNR-UHFFFAOYSA-N 0.000 description 4
- 239000011347 resin Substances 0.000 description 4
- 229920005989 resin Polymers 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000009835 boiling Methods 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 239000011651 chromium Substances 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 229910052802 copper Inorganic materials 0.000 description 3
- 230000008021 deposition Effects 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 229910002804 graphite Inorganic materials 0.000 description 3
- 239000010439 graphite Substances 0.000 description 3
- 238000001465 metallisation Methods 0.000 description 3
- 239000003129 oil well Substances 0.000 description 3
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- NXHILIPIEUBEPD-UHFFFAOYSA-H tungsten hexafluoride Chemical compound F[W](F)(F)(F)(F)F NXHILIPIEUBEPD-UHFFFAOYSA-H 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 2
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 229910007948 ZrB2 Inorganic materials 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 2
- 230000009471 action Effects 0.000 description 2
- IWOUKMZUPDVPGQ-UHFFFAOYSA-N barium nitrate Chemical compound [Ba+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O IWOUKMZUPDVPGQ-UHFFFAOYSA-N 0.000 description 2
- 239000002585 base Substances 0.000 description 2
- VWZIXVXBCBBRGP-UHFFFAOYSA-N boron;zirconium Chemical compound B#[Zr]#B VWZIXVXBCBBRGP-UHFFFAOYSA-N 0.000 description 2
- 125000002915 carbonyl group Chemical group [*:2]C([*:1])=O 0.000 description 2
- 239000012159 carrier gas Substances 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 2
- 239000007795 chemical reaction product Substances 0.000 description 2
- 238000005229 chemical vapour deposition Methods 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000005530 etching Methods 0.000 description 2
- 239000012634 fragment Substances 0.000 description 2
- 238000013467 fragmentation Methods 0.000 description 2
- 238000006062 fragmentation reaction Methods 0.000 description 2
- MELCCCHYSRGEEL-UHFFFAOYSA-N hafnium diboride Chemical compound [Hf]1B=B1 MELCCCHYSRGEEL-UHFFFAOYSA-N 0.000 description 2
- 150000004820 halides Chemical class 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- NFFIWVVINABMKP-UHFFFAOYSA-N methylidynetantalum Chemical compound [Ta]#C NFFIWVVINABMKP-UHFFFAOYSA-N 0.000 description 2
- 235000010333 potassium nitrate Nutrition 0.000 description 2
- 239000004323 potassium nitrate Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 239000012255 powdered metal Substances 0.000 description 2
- PUZPDOWCWNUUKD-UHFFFAOYSA-M sodium fluoride Chemical compound [F-].[Na+] PUZPDOWCWNUUKD-UHFFFAOYSA-M 0.000 description 2
- VWDWKYIASSYTQR-UHFFFAOYSA-N sodium nitrate Chemical compound [Na+].[O-][N+]([O-])=O VWDWKYIASSYTQR-UHFFFAOYSA-N 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 229910003468 tantalcarbide Inorganic materials 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 239000003039 volatile agent Substances 0.000 description 2
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 description 1
- 229910052582 BN Inorganic materials 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- 229910001369 Brass Inorganic materials 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 1
- KRHYYFGTRYWZRS-UHFFFAOYSA-M Fluoride anion Chemical compound [F-] KRHYYFGTRYWZRS-UHFFFAOYSA-M 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 229910001128 Sn alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910033181 TiB2 Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 229910001080 W alloy Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- DBNPLCUZNLSUCT-UHFFFAOYSA-N [B].[B].[B].[B].[B].[B].[Ba] Chemical compound [B].[B].[B].[B].[B].[B].[Ba] DBNPLCUZNLSUCT-UHFFFAOYSA-N 0.000 description 1
- YTPZWYPLOCEZIX-UHFFFAOYSA-N [Nb]#[Nb] Chemical compound [Nb]#[Nb] YTPZWYPLOCEZIX-UHFFFAOYSA-N 0.000 description 1
- KOMIMHZRQFFCOR-UHFFFAOYSA-N [Ni].[Cu].[Zn] Chemical compound [Ni].[Cu].[Zn] KOMIMHZRQFFCOR-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000013019 agitation Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 239000011449 brick Substances 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 239000002775 capsule Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000011195 cermet Substances 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 239000004567 concrete Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000006023 eutectic alloy Substances 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 229910000040 hydrogen fluoride Inorganic materials 0.000 description 1
- 229910000039 hydrogen halide Inorganic materials 0.000 description 1
- 239000012433 hydrogen halide Substances 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229910001507 metal halide Inorganic materials 0.000 description 1
- 150000005309 metal halides Chemical class 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- AYOOGWWGECJQPI-NSHDSACASA-N n-[(1s)-1-(5-fluoropyrimidin-2-yl)ethyl]-3-(3-propan-2-yloxy-1h-pyrazol-5-yl)imidazo[4,5-b]pyridin-5-amine Chemical compound N1C(OC(C)C)=CC(N2C3=NC(N[C@@H](C)C=4N=CC(F)=CN=4)=CC=C3N=C2)=N1 AYOOGWWGECJQPI-NSHDSACASA-N 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 239000000376 reactant Substances 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- VSZWPYCFIRKVQL-UHFFFAOYSA-N selanylidenegallium;selenium Chemical compound [Se].[Se]=[Ga].[Se]=[Ga] VSZWPYCFIRKVQL-UHFFFAOYSA-N 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 235000013024 sodium fluoride Nutrition 0.000 description 1
- 239000011775 sodium fluoride Substances 0.000 description 1
- 235000010344 sodium nitrate Nutrition 0.000 description 1
- 239000004317 sodium nitrate Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000011135 tin Substances 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 238000005292 vacuum distillation Methods 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 238000007740 vapor deposition Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24D—TOOLS FOR GRINDING, BUFFING OR SHARPENING
- B24D7/00—Bonded abrasive wheels, or wheels with inserted abrasive blocks, designed for acting otherwise than only by their periphery, e.g. by the front face; Bushings or mountings therefor
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K3/00—Materials not provided for elsewhere
- C09K3/14—Anti-slip materials; Abrasives
- C09K3/1436—Composite particles, e.g. coated particles
- C09K3/1445—Composite particles, e.g. coated particles the coating consisting exclusively of metals
Definitions
- ABSTRACT Abrasive particles are improved in function by encapsulating them with a metallic envelope; preferably the envelope is made of a pure metal in dendritic crystalline form. Desirably the abrasive substrate is placed in contraction by the envelope which is heat shrunk onto the abrasive substrate. The preferred method is to deposit the metal on the substrate at an elevated temperature by contacting a vapor of the metallic compound with the substrate particle under reducing conditions.
- the preferred primary abrasive is a diamond, and it is preferably etched before coating.
- Superior formed abraders may be formed by metal bonding such encapsulated abrasives with a metal matrix which forms a continuous phase in which the abrasive particles may be positioned.
- the encapsulated abrasive particle may form the primary abrasive together with a secondary abrasive which is not as hard as the primary abrasive and which may or may not be encapsulated with a metal.
- the primary and secondary abrasive may in one form of the abrader be distributed in the continuous phase metal binder forming the matrix.
- IZEACTolZ T T is 2 [1% ..I If
- PATENIEDHARI 3 87 1 ,840
- abraders have bound abrasive particles into an abrader structure, using a binder such as a resin and, in some cases, metal, which acts as the matrix to hold the abrasive particles in the abrader structure.
- the metal in the envelope when the encapsulated particle is to be used with the metal matrix acting as a bonding agent, it is desirable that the metal in the envelope have a suitably higher melting point than the metal matrix.
- the third advantage of the encapsulated abrasive particle of our invention when used together with a metal matrix resides in the increased rate of heat transfer from the abrasive particle resulting from the more intimate contact surface between the envelope and the substrate particle and the envelope and the metal matrix. Heat generated at the abrading surfaces, if not readily transmitted to and absorbed in the metal matrix, acting as a heat mass, will cause a local rise in temperature which may have a deleterious effect upon the life of the abrasive particle.
- the metallic envelopes which constitute the abrasive particles of our invention employed in the novel abrader structure of our invention differ from the foregoing coatings in composition and crystalline nature.
- the deposits of our invention are substantially pure metal envelopes, substantially free of intergranular inclusions.
- aforesaid encapsulated abrasive of our invention by a process of chemical vapor deposition, by subjecting the abrasive particles to contact with a volatile metal compound at an elevated temperature sufficient to maintain the metal compound in vapor form and contact the vapor with a solid substrate under metal deposition conditions.
- the coefficient of linear expansion of the metal is substantially greater than that of diamond, and their use would also have the advantage of adding a compressive force upon the diamonds to help in overcoming the tensile forces which would tend to fracture the diamond when used in an abrader structure as the abrasive particle.
- metals may be selected, depending on the stress desired to be imparted.
- metals listed in Table 2 and the abrasives of Table l metals having a coefficient greater than the substrate coefficient by about 5 to percent or more of the value of the coefficient of the substrate. That is, the coefficient of the metal should be about 1.05 or more, for example, up to about 7 times the coefficient of the substrate.
- metal encapsulating materials when employing diamonds as a substrate, when we employ carbide-forming metals, we prefer to employ those which have only a limited reaction rate at the temperatures of deposition, as hereinafter described.
- molybdenum, tungsten, tantalum, titanium, and niobium all of which are carbide formers but are unlike iron which under the conditions of deposition or the production of the abrader may result in excessive attack on the diamond forming carbides or graphite.
- tungsten, tantalum, niobium (columbium) and molybdenum we prefer to employ diamonds, either the natural or synthetic forms, and prefer to employ tungsten as the encapsulating material, deposited under conditions to produce pure tungsten of the crystal form as described herein.
- the metal encapsulated abrasive in abrader structures formed by metal bonding the encapsulated abrasive in a metal continuous phase matrix
- a metal having a significantly lower melting point than the metal sheath of the abrasive substrate we prefer to limit the melting point of the metal matrix to a temperature below about 2,800 F. in order not to expose the diamonds to excessive temperature which may impair the mechanical strength of the diamonds.
- the coefficient of thermal expansion of the metal matrix used as bonding agent is the coefficient of thermal expansion of the metal matrix used as bonding agent. Since, in general, the low melting metals and materials have high thermal expansion, in the absence of an encapsulating metal which is wetted by the molten metal, the mass of matrix on cooling would tend to pull away from the abrasive material, thus impairing the bond. It is one advantage of the encapsulating metal that the thermal expansion of the metal sheath matches more closely the thermal expansion of the metal matrix and that the interfacial tensions will tend to prevent the pulling away of the metal matrix from the metal sheath. Such metals having melting points so as to be fluid in the formation of the abrader structure, for example at temperatures below about 2,800 F. when employing diamonds are suitable.
- the metal chosen should be fluid at the temperature at which it is desired to employ the molten metal in forming the composite abrader structure and desirably should have, when solid, ductility as measured in the terms of microhardness of below about 400 kg/mm Desirably, also, it should have a compressive strength above about 90,000 psi. and an impact strength above about 5 foot pounds.
- the abrasive particle is a tungsten carbide or diamond particle which is attacked by nickel, cobalt or iron or alloys of these metals
- the encapsulation of the tungsten carbide by a metal envelope of substantially higher melting point according to our invention will prevent the attack which the unencapsulated particle would otherwise suffer under the conditions of fabrication of the abrader structure.
- unencapsulated cast tungsten carbide is attacked by iron-based or nickel-based alloys.
- the W C tungsten carbide is attacked or dissolved in the binder, and on freezing precipitates a new phase called eta.
- This phase is M C type carbide, and in the case of nickel binders will have the composition Ni W C.
- Eta phase is more brittle than the original particle.
- the particle is said to be haloed.
- the haloed portion of particle will have a hardness 'only of about 1,500 kilograms per square millimeter, compared for example to 1,950 to 2,100 kilograms per square millimeter (Knoop) for the core of the particle.
- a plurality of different abrasive particles are employed.
- particles of high hardness values for example, diamonds which act on the primary abrasives
- there is distributed in the continuous phase of the metal matrix binder a secondary abrasive of lower hardness value for example, those shown in Table l.
- this secondary abrasive particle is to wear away preferentially thus exposing new abrasive faces of the primary abrasive particle.
- the abrader structures thus formed are deemed selfsharpening. That is, the matrixincluding the secondary abrasive should wear away preferentially and uniformally exposing new primary abrasive cutting surfaces. This tends to reduce the area of the interfacial surfaces between the bonding metal of the matrix and the primary and secondary abrasive particles. Where the bond isweak, the particles are torn out of the metal matrix, causing excessive wear.
- the intermetallic bond between the metal matrix and the encapsulated primary or secondary abrasive increases the retention of the abrasive particle until its cutting life is ended by wearing away of the particle or breaking away of fragments thereof from the portion of the abrasive particle which has become free of the encapsulation at the abrading surface during the abrading action.
- the secondary abrasive we may, in order to add mass to the abrader select from the abrasive particles having suitable hardness and other desirable physical properties those having a specific gravity to give mass to the abrader; i.e., those with specific gravities substantially in excess of the abrasive substrate.
- tungsten carbide or hafnium diboride or those of somewhat lower specific gravity, i.e. 6 or more as set forth in Table 1.
- encapsulated secondary abrasive of suitable hardness chosen for example from the list of Table l and encapsulate the secondary abrasive with a metal of suitable specific gravity to increase the apparent density of the particle. This will permit the fabrication of an abrader having the required volume percent of secondary abrasive but impart a greater weight to the abrader structure as compared with one of like composition and volume but employing the unencapsulated secondary abrasive particle.
- halides or the carbonyls of the metals Preferably for convenience of operation, we prefer to employ those compounds having a boiling point at atmospheric pressure below the reaction temperature.
- encapsulated diamond in place of or in addition to the encapsulated diamond, we may use the other abrasives as described above, preferring among them encapsulated alumina but may also use the other abrasives described above, particularly encapsulated tungsten carbide or silicon carbide as is more fully described below.
- FIG. 5 is a section taken on 55 of FIG. 2.
- FIG. 7 is a section through a mold for the core bit shown in FIG. 8.
- FIGS. 9-14 are photomicrographs of etched sections of metal abrasive particles contained in a metal matrix according to our invention.
- FIG. 1 illustrated a flow sheet of our preferred process for producing the novel encapsulated abrasive of our invention.
- the particles to be coated are placed in the reactor 1, whose cap 2 has been removed.
- the reactor has a perforated bottom to support the particles of selected mesh size.
- the vacuum pump is started to de-aerate the system.
- Valve 7 is closed and the system filled with hydrogen from hydrogen storage 11, valve 5 being open.
- the reactor is heated by the furnace 9 to the reaction temperature, for example, from about 1,000 to about 1,200 F. while purging slowly with hydrogen.
- the hydrogen flow rate is increased until a fluidized bed is established.
- Hydrogen prior to introduction into the reactor passes through a conventional palladium catalyst to remove any impurities, such as oxygen in the hydrogen.
- Vaporized metallic compound is discharged from the vaporizing chamber 10, which may if necessary be heated by furnace 14, together with an inert gas, for example, argon from argon storage 6 into the reactionv chamber.
- the reaction forms hydrogen halide, which is passed through the bubble traps and is absorbed in the absorber.
- the volatile compound employed is a fluoride
- the product formed is a hydrogen fluoride, and we may use sodium fluoride for that absorption.
- the reaction deposits metal on the substrate and the effluent material, being in the vapor state is discharged, leaving no contaminants on or in the metal.
- the metal is formed in its pure state.
- the rate of metal deposition depends on the temperature, and flow rate of the reactants, being the greater the higher the temperature and the greater the flow rate of the hydrogen and volatile metals compound.
- valves 4 and 5 are closed and argon is continued to pass into the reactor and the metal encapsulated abrasive is allowed to cool to room temperature in the non-oxidizing condition of the argon environment.
- reaction products and the carrier gases and excess hydrogen enter the upper space termed the disengaging space where they are separated from any entrained particles.
- the diamond particle is smooth as for example in the case of synthetic diamonds
- the etching of the diamonds will also have an advantage where the metal envelope is produced by other processes such as electrochemical or electrolytic deposition methods.
- the product produced by the process of vapor deposition described above is superior and is preferred by us.
- hydrogen flow is established at a low flow rate of about 100 ml/min and as described above, the temperatures in the reactor 1 having been adjusted to 1,l50 F., as measured by the thermocouples, the hydrogen flow is increased to about l,250-l ,350 ml/min, and the flow of the tungsten fluoride vapor to about ml/min and the argon gas is adjusted. to about 285 ml/min, all as measured by the flow meters as indicated in FIG. 1, the hydrogen being in stoichiometric excess over the tungsten hexafluoride.
- the thickness of the coat of the tungsten on the diamond depends on the duration of the treatment and suitably for the 40 to 50 mesh diamonds described above, the coat will be 1 mil. thick in about 1 hour. Suitable thickness deposit will run from about 0.1 to about 1.5 mils thick.
- the substrate surface is completely coated, indicating that the process of vacuum chemical vapor deposition has great throwing power.
- the metal coated particles may be employed in producing improved abrader structures by any of the techniques previously used with unencapsulated abrasive particles. These include what have become known as surface set, infiltration, hot pressing, and flame metalizing procedures.
- a surface set oil well drill (see FIGS. 7 and 8) (such as described in the Austin Pat. No. 2,838,284) may be formed in a graphite mold which is formed with sockets positioned in the interior surface of the mold adjacent to the boring surface of the drill to be formed in the mold.
- a steel shank is positioned in the mold spaced from the interior surfaces of the mold.
- a matrix composed of a mixture of sized particles of cast tungsten carbide as the secondary abrasive and a powdered metal such as nickel or tungsten. This mixture extends in the mold above the surface on which the diamonds are deposited.
- the grain size of the tungsten carbide is chosen to give the proper compaction and void volume; for example, in the range of 35 to 75 percent of the total volume, e.g., -30 60 mesh such as described abovefThe mold is vibrated to compact the tungsten carbide particles.
- tungsten coated diamonds prepared according to the process previously described, having a coating, for example, of about half a mil or more, e.g. l to 1.5 mils.
- tungsten carbide we may employ as the secondary abrasive any of the other abrasives other than diamonds listed in Table l, or the aforesaid second abrasive particles encapsulated in a metal capsule, as described above, for example, alumina coated with tungsten according to the above procedure.
- Abrader elements may also be produced by an impregnation technique by mixing the primary and secondary abrasive materials in powder form, vibrating or packing the mixture in a suitable mold, and infiltrating the mixture with a low-melting binder metal alloy as described above.
- FIGS. 2 and 5 show a suitable graphite mold for use in such techniques for producing saw blade segments to be brazed to a saw blade.
- the mold is composed of a base 101, the mold proper 102, with an anchor 103, carrying a funnel 104, clamped by clamp bolt 105, and covered with a furnace cap 106.
- the mold proper consists of circumferentially space mold cavities having substantially smaller circumferential extension than their radial length.
- the primary abrasive for example, a mix of diamond particles 20 45 or 45 60 mesh screen and powdered tungsten carbide is tamped into the mold 102.
- the funnel contains a bronze-copper-tinalloy powder through a 200 mesh screen.
- Example 8 The process of Example 7 and the product then produced may also be carried out by replacing the tungsten carbide with a metal coatedtungsten carbide for example tungsten carbide coated with tungsten metal or other tungsten coated secondary abrasive such as alumina or silicon carbide.
- a metal coatedtungsten carbide for example tungsten carbide coated with tungsten metal or other tungsten coated secondary abrasive such as alumina or silicon carbide.
- sections of about 1 /8 inches long, one-eighth inch wide, and about five thirty-seconds inch thick may be formed suitably by introducing about 3,500 stones of mesh size 45 60 grit or about 1.1 carats of diamonds grit. (See FIG.
- Example 9 The mold employed is shown in FIGS. 4 and 3. The mold is similar to that of FIG. 2 except that no funnel is employed and the nut 105 is now a plug 107 and the funnel 104 is replaced by the cap 108 in place of cap 106. The mold is formed for the insertion of the cap as shown. The mold is placed in a press and heated for example in an induction furnace.
- a mixture of tungsten metal power, powdered tungsten carbide 35 50 mesh diamond grit which has been coated with a 10 micron tungsten metal envelope as described above is mixed with a 200 mesh bronze-tin alloy and tamped into the mold of FIG. 4.
- Theconcentration of diamonds in the mix may be suitably about 25 percent.
- the mold is heated to about 1,600 F. at about 3,000 p.s.i. pressure to produce the saw blade element.
- tungsten carbide instead of tungsten carbide, we may use tungsten coated tungsten carbide or other metal coated secondary abrasive described above, for example, tungsten coated alumina or silicon carbide.
- the higher melting metals as binder matrix such as iron, cobalt, nickel or alloys of these metals and heat the hot press mold to temperatures as high as above l,535 F. depending on the melting point of the metal selected to form the binder.
- FIG. 9 which shows a 0.025 inch tungsten coat on an aluminum oxide particle in the metal matrix at 140 X magnification and having an apparent density of 9.3 grams per cubic centimeter.
- FIG. 10 shows a similar tungsten coated alumina particle in a metal matrix at 280 X magnification.
- FIG. 11 shows a tungsten coated diamond particle hot pressed into a metal matrix at 210 X magnification.
- FIG. 12 shows a portion of the particle at 840 X magnification.
- FIG. 13 shows mesh silicon carbide particle coated with tungsten hot pressed into a metal matrix at 280 X magnification.
- FIG. 14 shows tungsten coated A1 0 hot pressed in a metal matrix at 1700 F., polished and etched at 560 X magnification to show the allotriomorphic dendrite crystal structure.
- An article of manufacture consisting of abrasive particles having a hardness of above about 2000 kg/mm encapsulated with a metal envelope formed of allotriomorphic dendrites.
- abrasive particles are chosen from the group consisting of diamonds, tungsten carbide, alumina and silicon carbide.
- the encapsulated metal is chosen from the group consisting of tungsten, tantalum, columbium (niobium) and molybdenum.
- the abrasive has a coefficient of linear expansion in the range of about 1 X 10 inches per inch per degree Fahrenheit to about 5 X 10" inches per inch per degree Fahrenheit and said metal has a linear coefficient of expansion in the range of from about 2 X 10 to about 10 inches per inch per degree Fahrenheit and in which the linear coefficient of expansion of said metal is in the range of from about 1.05 to about 7 times the linear coefficient of expansion of said unencapsulated particle.
- abrasive particles are chosen from the group consisting of diamonds, tungsten carbide, alumina and silicon carbide.
- the encapsulated metal is chosen from the group consisting of tungsten, tantalum, columbium (niobium) and molybdenum.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Polishing Bodies And Polishing Tools (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US219973A US3871840A (en) | 1972-01-24 | 1972-01-24 | Abrasive particles encapsulated with a metal envelope of allotriomorphic dentrites |
JP11019072A JPS5337599B2 (pt) | 1972-01-24 | 1972-11-02 | |
FR7241531A FR2169573A5 (pt) | 1972-01-24 | 1972-11-22 | |
DE2302574A DE2302574C3 (de) | 1972-01-24 | 1973-01-19 | Schleifmittel und Verfahren zu seiner Herstellung |
JP14915477A JPS54108994A (en) | 1972-01-24 | 1977-12-12 | Polishing instrument |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US219973A US3871840A (en) | 1972-01-24 | 1972-01-24 | Abrasive particles encapsulated with a metal envelope of allotriomorphic dentrites |
Publications (1)
Publication Number | Publication Date |
---|---|
US3871840A true US3871840A (en) | 1975-03-18 |
Family
ID=22821507
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US219973A Expired - Lifetime US3871840A (en) | 1972-01-24 | 1972-01-24 | Abrasive particles encapsulated with a metal envelope of allotriomorphic dentrites |
Country Status (4)
Country | Link |
---|---|
US (1) | US3871840A (pt) |
JP (2) | JPS5337599B2 (pt) |
DE (1) | DE2302574C3 (pt) |
FR (1) | FR2169573A5 (pt) |
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US3929432A (en) * | 1970-05-29 | 1975-12-30 | De Beers Ind Diamond | Diamond particle having a composite coating of titanium and a metal layer |
US4063909A (en) * | 1974-09-18 | 1977-12-20 | Robert Dennis Mitchell | Abrasive compact brazed to a backing |
US4108614A (en) * | 1976-04-14 | 1978-08-22 | Robert Dennis Mitchell | Zirconium layer for bonding diamond compact to cemented carbide backing |
US4110084A (en) * | 1977-04-15 | 1978-08-29 | General Electric Company | Composite of bonded cubic boron nitride crystals on a silicon carbide substrate |
US4142869A (en) * | 1973-12-29 | 1979-03-06 | Vereschagin Leonid F | Compact-grained diamond material |
US4164527A (en) * | 1974-11-01 | 1979-08-14 | Bakul Valentin N | Method of making superhard articles |
USRE30503E (en) * | 1979-04-16 | 1981-02-03 | General Electric Company | Composite of bonded cubic boron nitride crystals on a silicon carbide substrate |
US4610698A (en) * | 1984-06-25 | 1986-09-09 | United Technologies Corporation | Abrasive surface coating process for superalloys |
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US4943488A (en) * | 1986-10-20 | 1990-07-24 | Norton Company | Low pressure bonding of PCD bodies and method for drill bits and the like |
US5011514A (en) * | 1988-07-29 | 1991-04-30 | Norton Company | Cemented and cemented/sintered superabrasive polycrystalline bodies and methods of manufacture thereof |
US5030276A (en) * | 1986-10-20 | 1991-07-09 | Norton Company | Low pressure bonding of PCD bodies and method |
US5062865A (en) * | 1987-12-04 | 1991-11-05 | Norton Company | Chemically bonded superabrasive grit |
US5074970A (en) * | 1989-07-03 | 1991-12-24 | Kostas Routsis | Method for applying an abrasive layer to titanium alloy compressor airfoils |
US5096465A (en) * | 1989-12-13 | 1992-03-17 | Norton Company | Diamond metal composite cutter and method for making same |
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US5116568A (en) * | 1986-10-20 | 1992-05-26 | Norton Company | Method for low pressure bonding of PCD bodies |
US5126207A (en) * | 1990-07-20 | 1992-06-30 | Norton Company | Diamond having multiple coatings and methods for their manufacture |
US5489449A (en) * | 1990-03-28 | 1996-02-06 | Nisshin Flour Milling Co., Ltd. | Coated particles of inorganic or metallic materials and processes of producing the same |
WO1996004862A1 (en) | 1994-08-12 | 1996-02-22 | U.S. Synthetic | Prosthetic joint with diamond coated interfaces |
WO1997006339A1 (en) * | 1995-08-03 | 1997-02-20 | Dresser Industries, Inc. | Hardfacing with coated diamond particles |
US5733350A (en) * | 1996-08-13 | 1998-03-31 | Purafil, Inc. | Container for solid filtration media and filtration system utilizing same |
US5871060A (en) * | 1997-02-20 | 1999-02-16 | Jensen; Kenneth M. | Attachment geometry for non-planar drill inserts |
US5979579A (en) * | 1997-07-11 | 1999-11-09 | U.S. Synthetic Corporation | Polycrystalline diamond cutter with enhanced durability |
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US6098730A (en) * | 1996-04-17 | 2000-08-08 | Baker Hughes Incorporated | Earth-boring bit with super-hard cutting elements |
US6102140A (en) * | 1998-01-16 | 2000-08-15 | Dresser Industries, Inc. | Inserts and compacts having coated or encrusted diamond particles |
US6138779A (en) * | 1998-01-16 | 2000-10-31 | Dresser Industries, Inc. | Hardfacing having coated ceramic particles or coated particles of other hard materials placed on a rotary cone cutter |
US6170583B1 (en) | 1998-01-16 | 2001-01-09 | Dresser Industries, Inc. | Inserts and compacts having coated or encrusted cubic boron nitride particles |
US6241036B1 (en) | 1998-09-16 | 2001-06-05 | Baker Hughes Incorporated | Reinforced abrasive-impregnated cutting elements, drill bits including same |
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US6524357B2 (en) | 2000-06-30 | 2003-02-25 | Saint-Gobain Abrasives Technology Company | Process for coating superabrasive with metal |
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US20050108948A1 (en) * | 2002-09-24 | 2005-05-26 | Chien-Min Sung | Molten braze-coated superabrasive particles and associated methods |
US20060059785A1 (en) * | 2002-09-24 | 2006-03-23 | Chien-Min Sung | Methods of maximizing retention of superabrasive particles in a metal matrix |
US20060213128A1 (en) * | 2002-09-24 | 2006-09-28 | Chien-Min Sung | Methods of maximizing retention of superabrasive particles in a metal matrix |
US20070032877A1 (en) * | 2005-08-05 | 2007-02-08 | Whiteside Leo A | Coated ceramic total joint arthroplasty and method of making same |
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US20070267820A1 (en) * | 2006-05-16 | 2007-11-22 | Skf Usa Inc. | Mechanical end face seal with ultrahard face material |
US20080096479A1 (en) * | 2006-10-18 | 2008-04-24 | Chien-Min Sung | Low-melting point superabrasive tools and associated methods |
US20080187769A1 (en) * | 2006-04-13 | 2008-08-07 | 3M Innovative Properties | Metal-coated superabrasive material and methods of making the same |
US20080202821A1 (en) * | 2007-02-23 | 2008-08-28 | Mcclain Eric E | Multi-Layer Encapsulation of Diamond Grit for Use in Earth-Boring Bits |
EP2009124A3 (en) * | 1997-05-13 | 2009-04-22 | Richard Edmund Toth | Tough-coated hard powders and sintered articles thereof |
US7632355B2 (en) | 1997-05-13 | 2009-12-15 | Allomet | Apparatus and method of treating fine powders |
US20100193255A1 (en) * | 2008-08-21 | 2010-08-05 | Stevens John H | Earth-boring metal matrix rotary drill bit |
US20110030440A1 (en) * | 2009-08-04 | 2011-02-10 | Allomet Corporation | Tough coated hard particles consolidated in a tough matrix material |
WO2011049479A1 (en) * | 2009-10-21 | 2011-04-28 | Andrey Mikhailovich Abyzov | Composite material having high thermal conductivity and process of fabricating same |
US20130081334A1 (en) * | 2011-09-29 | 2013-04-04 | Marc Linh Hoang | Bonded abrasives formed by uniaxial hot pressing |
US20140000579A1 (en) * | 2011-03-04 | 2014-01-02 | Nv Bekaert Sa | Sawing bead |
US8672634B2 (en) | 2010-08-30 | 2014-03-18 | United Technologies Corporation | Electroformed conforming rubstrip |
US8778259B2 (en) | 2011-05-25 | 2014-07-15 | Gerhard B. Beckmann | Self-renewing cutting surface, tool and method for making same using powder metallurgy and densification techniques |
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US10246335B2 (en) * | 2016-05-27 | 2019-04-02 | Baker Hughes, A Ge Company, Llc | Methods of modifying surfaces of diamond particles, and related diamond particles and earth-boring tools |
US10723041B2 (en) * | 2016-10-28 | 2020-07-28 | Saint-Gobain Abrasives, Inc./Saint-Gobain Abrasifs | Core drill bit |
US12064850B2 (en) | 2021-12-30 | 2024-08-20 | Saint-Gobain Abrasives, Inc. | Abrasive articles and methods for forming same |
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3929432A (en) * | 1970-05-29 | 1975-12-30 | De Beers Ind Diamond | Diamond particle having a composite coating of titanium and a metal layer |
US4142869A (en) * | 1973-12-29 | 1979-03-06 | Vereschagin Leonid F | Compact-grained diamond material |
US4063909A (en) * | 1974-09-18 | 1977-12-20 | Robert Dennis Mitchell | Abrasive compact brazed to a backing |
US4164527A (en) * | 1974-11-01 | 1979-08-14 | Bakul Valentin N | Method of making superhard articles |
US4108614A (en) * | 1976-04-14 | 1978-08-22 | Robert Dennis Mitchell | Zirconium layer for bonding diamond compact to cemented carbide backing |
US4110084A (en) * | 1977-04-15 | 1978-08-29 | General Electric Company | Composite of bonded cubic boron nitride crystals on a silicon carbide substrate |
USRE30503E (en) * | 1979-04-16 | 1981-02-03 | General Electric Company | Composite of bonded cubic boron nitride crystals on a silicon carbide substrate |
US4744725A (en) * | 1984-06-25 | 1988-05-17 | United Technologies Corporation | Abrasive surfaced article for high temperature service |
US4610698A (en) * | 1984-06-25 | 1986-09-09 | United Technologies Corporation | Abrasive surface coating process for superalloys |
US4943488A (en) * | 1986-10-20 | 1990-07-24 | Norton Company | Low pressure bonding of PCD bodies and method for drill bits and the like |
US5030276A (en) * | 1986-10-20 | 1991-07-09 | Norton Company | Low pressure bonding of PCD bodies and method |
US5116568A (en) * | 1986-10-20 | 1992-05-26 | Norton Company | Method for low pressure bonding of PCD bodies |
US5062865A (en) * | 1987-12-04 | 1991-11-05 | Norton Company | Chemically bonded superabrasive grit |
US5011514A (en) * | 1988-07-29 | 1991-04-30 | Norton Company | Cemented and cemented/sintered superabrasive polycrystalline bodies and methods of manufacture thereof |
US5074970A (en) * | 1989-07-03 | 1991-12-24 | Kostas Routsis | Method for applying an abrasive layer to titanium alloy compressor airfoils |
US5096465A (en) * | 1989-12-13 | 1992-03-17 | Norton Company | Diamond metal composite cutter and method for making same |
US5489449A (en) * | 1990-03-28 | 1996-02-06 | Nisshin Flour Milling Co., Ltd. | Coated particles of inorganic or metallic materials and processes of producing the same |
US5224969A (en) * | 1990-07-20 | 1993-07-06 | Norton Company | Diamond having multiple coatings and methods for their manufacture |
US5126207A (en) * | 1990-07-20 | 1992-06-30 | Norton Company | Diamond having multiple coatings and methods for their manufacture |
US5164220A (en) * | 1990-10-29 | 1992-11-17 | Diamond Technologies Company | Method for treating diamonds to produce bondable diamonds for depositing same on a substrate |
WO1992007664A1 (en) * | 1990-10-29 | 1992-05-14 | Diamond Technologies Company | Method of treating and depositing diamonds |
US5277940A (en) * | 1990-10-29 | 1994-01-11 | Diamond Technologies Company | Method for treating diamonds to produce bondable diamonds for depositing same on a substrate |
WO1996004862A1 (en) | 1994-08-12 | 1996-02-22 | U.S. Synthetic | Prosthetic joint with diamond coated interfaces |
WO1997006339A1 (en) * | 1995-08-03 | 1997-02-20 | Dresser Industries, Inc. | Hardfacing with coated diamond particles |
US5755299A (en) * | 1995-08-03 | 1998-05-26 | Dresser Industries, Inc. | Hardfacing with coated diamond particles |
US5755298A (en) * | 1995-08-03 | 1998-05-26 | Dresser Industries, Inc. | Hardfacing with coated diamond particles |
AU702263B2 (en) * | 1995-08-03 | 1999-02-18 | Halliburton Energy Services, Inc. | Hardfacing with coated diamond particles |
US6098730A (en) * | 1996-04-17 | 2000-08-08 | Baker Hughes Incorporated | Earth-boring bit with super-hard cutting elements |
US6068071A (en) * | 1996-05-23 | 2000-05-30 | U.S. Synthetic Corporation | Cutter with polycrystalline diamond layer and conic section profile |
US5733350A (en) * | 1996-08-13 | 1998-03-31 | Purafil, Inc. | Container for solid filtration media and filtration system utilizing same |
US5871060A (en) * | 1997-02-20 | 1999-02-16 | Jensen; Kenneth M. | Attachment geometry for non-planar drill inserts |
US7632355B2 (en) | 1997-05-13 | 2009-12-15 | Allomet | Apparatus and method of treating fine powders |
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Also Published As
Publication number | Publication date |
---|---|
DE2302574B2 (de) | 1979-10-31 |
DE2302574C3 (de) | 1980-07-10 |
JPS5337599B2 (pt) | 1978-10-09 |
JPS4886189A (pt) | 1973-11-14 |
JPS54108994A (en) | 1979-08-27 |
FR2169573A5 (pt) | 1973-09-07 |
DE2302574A1 (de) | 1973-08-02 |
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