US20080185074A1 - Preparation of compositions by melt spinning - Google Patents
Preparation of compositions by melt spinning Download PDFInfo
- Publication number
- US20080185074A1 US20080185074A1 US11/703,505 US70350507A US2008185074A1 US 20080185074 A1 US20080185074 A1 US 20080185074A1 US 70350507 A US70350507 A US 70350507A US 2008185074 A1 US2008185074 A1 US 2008185074A1
- Authority
- US
- United States
- Prior art keywords
- melt
- product
- composition
- lanthanum
- combinations
- 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.)
- Abandoned
Links
- 239000000203 mixture Substances 0.000 title claims abstract description 86
- 238000002074 melt spinning Methods 0.000 title abstract description 13
- 238000002360 preparation method Methods 0.000 title description 10
- 239000000843 powder Substances 0.000 claims abstract description 70
- 239000000155 melt Substances 0.000 claims abstract description 42
- 238000009987 spinning Methods 0.000 claims abstract description 26
- 239000002105 nanoparticle Substances 0.000 claims abstract description 22
- 229910052684 Cerium Inorganic materials 0.000 claims abstract description 16
- 229910052746 lanthanum Inorganic materials 0.000 claims abstract description 15
- 239000011159 matrix material Substances 0.000 claims abstract description 15
- -1 lanthanum halide Chemical class 0.000 claims abstract description 10
- 239000008247 solid mixture Substances 0.000 claims abstract 2
- XKUYOJZZLGFZTC-UHFFFAOYSA-K lanthanum(iii) bromide Chemical compound Br[La](Br)Br XKUYOJZZLGFZTC-UHFFFAOYSA-K 0.000 claims description 48
- 238000000034 method Methods 0.000 claims description 33
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 30
- ICAKDTKJOYSXGC-UHFFFAOYSA-K lanthanum(iii) chloride Chemical compound Cl[La](Cl)Cl ICAKDTKJOYSXGC-UHFFFAOYSA-K 0.000 claims description 30
- 230000008569 process Effects 0.000 claims description 23
- MOOUSOJAOQPDEH-UHFFFAOYSA-K cerium(iii) bromide Chemical compound [Br-].[Br-].[Br-].[Ce+3] MOOUSOJAOQPDEH-UHFFFAOYSA-K 0.000 claims description 22
- 229910052802 copper Inorganic materials 0.000 claims description 16
- 229910052786 argon Inorganic materials 0.000 claims description 15
- 239000000463 material Substances 0.000 claims description 14
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 12
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims description 11
- 150000002910 rare earth metals Chemical class 0.000 claims description 10
- 229910052777 Praseodymium Inorganic materials 0.000 claims description 8
- 229910052772 Samarium Inorganic materials 0.000 claims description 8
- 229910052771 Terbium Inorganic materials 0.000 claims description 8
- 229910052688 Gadolinium Inorganic materials 0.000 claims description 7
- 229910052693 Europium Inorganic materials 0.000 claims description 6
- 229910052747 lanthanoid Inorganic materials 0.000 claims description 6
- 150000002602 lanthanoids Chemical class 0.000 claims description 6
- 229910052758 niobium Inorganic materials 0.000 claims description 6
- 229910052715 tantalum Inorganic materials 0.000 claims description 6
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 claims description 5
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 claims description 5
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 claims description 5
- BYMUNNMMXKDFEZ-UHFFFAOYSA-K trifluorolanthanum Chemical compound F[La](F)F BYMUNNMMXKDFEZ-UHFFFAOYSA-K 0.000 claims description 5
- 229910052727 yttrium Inorganic materials 0.000 claims description 5
- 229910052779 Neodymium Inorganic materials 0.000 claims description 4
- 229910052775 Thulium Inorganic materials 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- 229910052787 antimony Inorganic materials 0.000 claims description 4
- 229910052793 cadmium Inorganic materials 0.000 claims description 4
- 229910052791 calcium Inorganic materials 0.000 claims description 4
- OGPBJKLSAFTDLK-UHFFFAOYSA-N europium atom Chemical compound [Eu] OGPBJKLSAFTDLK-UHFFFAOYSA-N 0.000 claims description 4
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052733 gallium Inorganic materials 0.000 claims description 4
- 150000004820 halides Chemical class 0.000 claims description 4
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 claims description 4
- 229910052749 magnesium Inorganic materials 0.000 claims description 4
- 229910052748 manganese Inorganic materials 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 229910052709 silver Inorganic materials 0.000 claims description 4
- 229910052716 thallium Inorganic materials 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- 229910052725 zinc Inorganic materials 0.000 claims description 4
- 229910052692 Dysprosium Inorganic materials 0.000 claims description 3
- 229910052785 arsenic Inorganic materials 0.000 claims description 3
- 229910052796 boron Inorganic materials 0.000 claims description 3
- 229910052794 bromium Inorganic materials 0.000 claims description 3
- 229910052792 caesium Inorganic materials 0.000 claims description 3
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 229910052744 lithium Inorganic materials 0.000 claims description 3
- 150000004767 nitrides Chemical class 0.000 claims description 3
- 150000002902 organometallic compounds Chemical class 0.000 claims description 3
- 229910052760 oxygen Inorganic materials 0.000 claims description 3
- 229910052700 potassium Inorganic materials 0.000 claims description 3
- 229910052708 sodium Inorganic materials 0.000 claims description 3
- 229910052721 tungsten Inorganic materials 0.000 claims description 3
- 229910003016 Lu2SiO5 Inorganic materials 0.000 claims description 2
- 229910001632 barium fluoride Inorganic materials 0.000 claims description 2
- WUKWITHWXAAZEY-UHFFFAOYSA-L calcium difluoride Chemical compound [F-].[F-].[Ca+2] WUKWITHWXAAZEY-UHFFFAOYSA-L 0.000 claims description 2
- 229910001634 calcium fluoride Inorganic materials 0.000 claims description 2
- 229910001635 magnesium fluoride Inorganic materials 0.000 claims description 2
- 229910052765 Lutetium Inorganic materials 0.000 claims 5
- 229910052768 actinide Inorganic materials 0.000 claims 3
- 150000001255 actinides Chemical class 0.000 claims 3
- OHSVLFRHMCKCQY-UHFFFAOYSA-N lutetium atom Chemical compound [Lu] OHSVLFRHMCKCQY-UHFFFAOYSA-N 0.000 claims 3
- 229910052757 nitrogen Inorganic materials 0.000 claims 3
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims 2
- 229910052691 Erbium Inorganic materials 0.000 claims 2
- 229910052689 Holmium Inorganic materials 0.000 claims 2
- UCKMPCXJQFINFW-UHFFFAOYSA-N Sulphide Chemical compound [S-2] UCKMPCXJQFINFW-UHFFFAOYSA-N 0.000 claims 2
- 229910052769 Ytterbium Inorganic materials 0.000 claims 2
- 229910052789 astatine Inorganic materials 0.000 claims 2
- 229910052790 beryllium Inorganic materials 0.000 claims 2
- 229910052799 carbon Inorganic materials 0.000 claims 2
- 229910052801 chlorine Inorganic materials 0.000 claims 2
- 229910052731 fluorine Inorganic materials 0.000 claims 2
- 229910052730 francium Inorganic materials 0.000 claims 2
- 229910052732 germanium Inorganic materials 0.000 claims 2
- 229910052737 gold Inorganic materials 0.000 claims 2
- 229910052738 indium Inorganic materials 0.000 claims 2
- 229910052740 iodine Inorganic materials 0.000 claims 2
- 229910052741 iridium Inorganic materials 0.000 claims 2
- 229910052745 lead Inorganic materials 0.000 claims 2
- 229910052753 mercury Inorganic materials 0.000 claims 2
- 229910052750 molybdenum Inorganic materials 0.000 claims 2
- 229910052759 nickel Inorganic materials 0.000 claims 2
- 229910052762 osmium Inorganic materials 0.000 claims 2
- 229910052763 palladium Inorganic materials 0.000 claims 2
- 229910052698 phosphorus Inorganic materials 0.000 claims 2
- 229910052697 platinum Inorganic materials 0.000 claims 2
- 229910052702 rhenium Inorganic materials 0.000 claims 2
- 229910052703 rhodium Inorganic materials 0.000 claims 2
- 229910052701 rubidium Inorganic materials 0.000 claims 2
- 229910052707 ruthenium Inorganic materials 0.000 claims 2
- 229910052706 scandium Inorganic materials 0.000 claims 2
- 150000003346 selenoethers Chemical class 0.000 claims 2
- 229910052710 silicon Inorganic materials 0.000 claims 2
- 229910052712 strontium Inorganic materials 0.000 claims 2
- 229910052717 sulfur Inorganic materials 0.000 claims 2
- 229910052713 technetium Inorganic materials 0.000 claims 2
- 229910052718 tin Inorganic materials 0.000 claims 2
- 229910052720 vanadium Inorganic materials 0.000 claims 2
- 229910052726 zirconium Inorganic materials 0.000 claims 2
- 229910004755 Cerium(III) bromide Inorganic materials 0.000 claims 1
- 229910002249 LaCl3 Inorganic materials 0.000 claims 1
- 229910016859 Lanthanum iodide Inorganic materials 0.000 claims 1
- 229910014323 Lanthanum(III) bromide Inorganic materials 0.000 claims 1
- 238000010924 continuous production Methods 0.000 claims 1
- 239000001307 helium Substances 0.000 claims 1
- 229910052734 helium Inorganic materials 0.000 claims 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims 1
- KYKBXWMMXCGRBA-UHFFFAOYSA-K lanthanum(3+);triiodide Chemical compound I[La](I)I KYKBXWMMXCGRBA-UHFFFAOYSA-K 0.000 claims 1
- 238000010438 heat treatment Methods 0.000 description 15
- 238000002156 mixing Methods 0.000 description 15
- 239000010949 copper Substances 0.000 description 14
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 13
- 239000012535 impurity Substances 0.000 description 13
- 230000006698 induction Effects 0.000 description 12
- 238000002844 melting Methods 0.000 description 11
- 230000008018 melting Effects 0.000 description 11
- 239000012768 molten material Substances 0.000 description 9
- 239000004570 mortar (masonry) Substances 0.000 description 9
- 239000002019 doping agent Substances 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 229910052582 BN Inorganic materials 0.000 description 5
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 5
- 230000008878 coupling Effects 0.000 description 5
- 238000010168 coupling process Methods 0.000 description 5
- 238000005859 coupling reaction Methods 0.000 description 5
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 5
- 239000002243 precursor Substances 0.000 description 5
- 210000004894 snout Anatomy 0.000 description 5
- 238000002441 X-ray diffraction Methods 0.000 description 4
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 239000010955 niobium Substances 0.000 description 4
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 4
- 239000004033 plastic Substances 0.000 description 4
- 229920003023 plastic Polymers 0.000 description 4
- 230000005855 radiation Effects 0.000 description 4
- 239000002994 raw material Substances 0.000 description 4
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 229910052593 corundum Inorganic materials 0.000 description 3
- 239000013078 crystal Substances 0.000 description 3
- 238000013021 overheating Methods 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 238000010926 purge Methods 0.000 description 3
- 239000010453 quartz Substances 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 3
- 229910001845 yogo sapphire Inorganic materials 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- HSJPMRKMPBAUAU-UHFFFAOYSA-N cerium(3+);trinitrate Chemical compound [Ce+3].[O-][N+]([O-])=O.[O-][N+]([O-])=O.[O-][N+]([O-])=O HSJPMRKMPBAUAU-UHFFFAOYSA-N 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000005496 eutectics Effects 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 230000001788 irregular Effects 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 238000003801 milling Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000002086 nanomaterial Substances 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 238000002601 radiography Methods 0.000 description 2
- 239000011734 sodium Substances 0.000 description 2
- 229910052714 tellurium Inorganic materials 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 238000009827 uniform distribution Methods 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- CPELXLSAUQHCOX-UHFFFAOYSA-M Bromide Chemical compound [Br-] CPELXLSAUQHCOX-UHFFFAOYSA-M 0.000 description 1
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 239000004743 Polypropylene Substances 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- 238000003917 TEM image Methods 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000000498 ball milling Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- GDTBXPJZTBHREO-UHFFFAOYSA-N bromine Substances BrBr GDTBXPJZTBHREO-UHFFFAOYSA-N 0.000 description 1
- 229910000420 cerium oxide Inorganic materials 0.000 description 1
- VYLVYHXQOHJDJL-UHFFFAOYSA-K cerium trichloride Chemical compound Cl[Ce](Cl)Cl VYLVYHXQOHJDJL-UHFFFAOYSA-K 0.000 description 1
- QCCDYNYSHILRDG-UHFFFAOYSA-K cerium(3+);trifluoride Chemical compound [F-].[F-].[F-].[Ce+3] QCCDYNYSHILRDG-UHFFFAOYSA-K 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- WEWLNOZUAAHMFS-UHFFFAOYSA-N copper gadolinium Chemical compound [Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Gd] WEWLNOZUAAHMFS-UHFFFAOYSA-N 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000002059 diagnostic imaging Methods 0.000 description 1
- KBQHZAAAGSGFKK-UHFFFAOYSA-N dysprosium atom Chemical compound [Dy] KBQHZAAAGSGFKK-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 238000010902 jet-milling Methods 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
- 238000004949 mass spectrometry Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000010309 melting process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000004377 microelectronic Methods 0.000 description 1
- 238000001000 micrograph Methods 0.000 description 1
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 description 1
- 230000005693 optoelectronics Effects 0.000 description 1
- BMMGVYCKOGBVEV-UHFFFAOYSA-N oxo(oxoceriooxy)cerium Chemical compound [Ce]=O.O=[Ce]=O BMMGVYCKOGBVEV-UHFFFAOYSA-N 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 229920001155 polypropylene Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 238000002600 positron emission tomography Methods 0.000 description 1
- BOTHRHRVFIZTGG-UHFFFAOYSA-K praseodymium(3+);trifluoride Chemical compound F[Pr](F)F BOTHRHRVFIZTGG-UHFFFAOYSA-K 0.000 description 1
- ICKYUJFKBKOPJT-UHFFFAOYSA-K samarium(3+);tribromide Chemical compound Br[Sm](Br)Br ICKYUJFKBKOPJT-UHFFFAOYSA-K 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 description 1
- GFISHBQNVWAVFU-UHFFFAOYSA-K terbium(iii) chloride Chemical compound Cl[Tb](Cl)Cl GFISHBQNVWAVFU-UHFFFAOYSA-K 0.000 description 1
- BKVIYDNLLOSFOA-UHFFFAOYSA-N thallium Chemical compound [Tl] BKVIYDNLLOSFOA-UHFFFAOYSA-N 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/5152—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on halogenides other than fluorides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B82—NANOTECHNOLOGY
- B82Y—SPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
- B82Y30/00—Nanotechnology for materials or surface science, e.g. nanocomposites
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01F—COMPOUNDS OF THE METALS BERYLLIUM, MAGNESIUM, ALUMINIUM, CALCIUM, STRONTIUM, BARIUM, RADIUM, THORIUM, OR OF THE RARE-EARTH METALS
- C01F17/00—Compounds of rare earth metals
- C01F17/20—Compounds containing only rare earth metals as the metal element
- C01F17/253—Halides
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01G—COMPOUNDS CONTAINING METALS NOT COVERED BY SUBCLASSES C01D OR C01F
- C01G1/00—Methods of preparing compounds of metals not covered by subclasses C01B, C01C, C01D, or C01F, in general
- C01G1/06—Halides
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01G—COMPOUNDS CONTAINING METALS NOT COVERED BY SUBCLASSES C01D OR C01F
- C01G41/00—Compounds of tungsten
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B37/00—Manufacture or treatment of flakes, fibres, or filaments from softened glass, minerals, or slags
- C03B37/005—Manufacture of flakes
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C14/00—Glass compositions containing a non-glass component, e.g. compositions containing fibres, filaments, whiskers, platelets, or the like, dispersed in a glass matrix
- C03C14/006—Glass compositions containing a non-glass component, e.g. compositions containing fibres, filaments, whiskers, platelets, or the like, dispersed in a glass matrix the non-glass component being in the form of microcrystallites, e.g. of optically or electrically active material
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C3/00—Glass compositions
- C03C3/32—Non-oxide glass compositions, e.g. binary or ternary halides, sulfides or nitrides of germanium, selenium or tellurium
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
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- C04B35/62605—Treating the starting powders individually or as mixtures
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Definitions
- the invention relates to the preparation of inorganic compositions by melt spinning.
- Nanostructured materials generally have different electronic, magnetic, optical, and mechanical properties than the corresponding bulk materials.
- Light output from nanophosphors can be higher than for micron-sized or larger phosphors.
- Nanophosphors have attracted interest due to their potential uses in optics, optoelectronics, lighting, displays, optical amplifiers/scintillators, lasers, microelectronics, tribology, homeland security, radiation detectors, medical imaging, and other applications.
- the present invention is concerned with a process for preparing a composition.
- the process includes sending an inorganic melt to a spinning wheel, whereby the melt cools after it contacts the wheel and is converted into a product that comprises nanoparticles embedded in a glassy matrix.
- the present invention is also concerned with a product prepared by a process that comprises sending an inorganic melt to a spinning wheel that cools the melt after the melt contacts the spinning wheel, whereby the melt is converted into a product that comprises nanoparticles of a composition embedded in a glassy matrix of essentially the same composition.
- the present invention is also concerned with a composition that consists essentially of nanoparticles of a composition embedded in a glassy matrix of essentially the same composition as that of the nanoparticles.
- FIG. 1 shows a schematic representation demonstrating operating principles of a melt spinner.
- FIG. 2 shows results from a differential scanning calorimeter (DSC) run for lanthanum bromide (LaBr 3 ) powder.
- FIG. 3 shows results from a DSC run for lanthanum chloride LaCl 3 ) powder.
- FIG. 4 shows results from a DSC run for a powder mixture having the formula La 0.95 Ce 0.05 Br 3 powder.
- FIG. 5 shows results from a DSC run for a powder mixture having the formula La 0.95 Ce 0.05 Br 2.288 Cl 0.713 powder.
- FIG. 6 shows results from a DSC run for a powder mixture having the formula La 0.95 Ce 0.05 Br 1.575 Cl 1.425 powder.
- FIG. 7 shows a transmission electron microscope (TEM) micrograph showing the microstructure of an embodiment flake of nanoparticles embedded in a glassy matrix of the invention.
- TEM transmission electron microscope
- FIG. 8 shows an x-ray diffraction (XRD) pattern of an embodiment phase of LaBr 3 :Ce nanoparticles.
- the present invention provides compositions and methods for preparing the compositions.
- the compositions are generally inorganic compositions. Some embodiments of these compositions are phosphors.
- compositions of the invention include rare earth doped lanthanum fluoride, rare earth doped lanthanum chloride, rare earth doped lanthanum bromide, and rare earth doped mixtures of lanthanum chloride and lanthanum bromide.
- rare earth dopants include cerium, neodymium, europium, thulium, terbium, samarium, gadolinium, dysprosium, and praseodymium.
- Some other non-limiting embodiment dopants include thallium, chromium, manganese, titanium, copper, silver, zinc, gallium, antimony, and tellurium.
- An embodiment method for preparing the compositions involves the use of melt spinning.
- Melt spinning involves sending a composition in the form of a melt to a spinning wheel. When the melt contacts the spinning wheel, it loses heat and solidifies.
- FIG. 1 A schematic representation showing the production of the compositions by melt spinning is shown in FIG. 1 .
- Melt spinning apparatus 10 includes crucible 12 filled with powder 14 and surrounded by induction heating coils 16 .
- Crucible 12 can be made from a material such as, but not limited to, boron nitride, and may be provided with a coupling (a tantalum coupling, for example) to facilitate the heating process.
- Melt spinning apparatus 10 also includes melt spinning chamber 18 and spinning wheel 20 (a copper wheel, for example) inside the chamber.
- the induction heating coils transfer energy to the crucible (a coupler facilitates this, depending on the choice of crucible materials), and powder 14 inside the crucible heats until it melts.
- the melt exits the crucible through opening 22 at the bottom of crucible 12 and moves into melt-spinning chamber 18 where it makes contact with spinning wheel 20 .
- the melt cools as it contacts the wheel, and is sent through snout 24 where it is collected as flakes 26 .
- a non-limiting range of speeds of the spinning wheel may be from about 1 rpm to about 5000 rpm, or from about 1000 to about 3000 rpm, or from about 1000 rpm to about 2000 rpm, or from about 1000 rpm to about 1700 rpm.
- An embodiment composition produced by sending a melt to the spinning wheel may be in the form of flakes that include crystalline nanoparticles in a glassy matrix.
- the chemical formula for the crystalline nanoparticle portion of the flakes may be essentially the same as that for the glassy matrix.
- a cerium doped lanthanum bromide (LaBr 3 :Ce) embodiment composition may be prepared from a mixture of cerium bromide (CeBr 3 ) powder and lanthanum bromide (LaBr 3 ) powder.
- a terbium doped lanthanum chloride (LaCl 3 :Tb) embodiment composition may be prepared from a mixture of terbium chloride (TbCl 3 ) powder and lanthanum chloride (LaCl 3 ).
- a samarium doped lanthanum bromide/chloride (LaBr (3-x) Cl x :Sm) embodiment composition may be prepared from a powder mixture of samarium bromide (SmBr 3 ), lanthanum bromide, and lanthanum chloride.
- a praseodymium doped lanthanum fluoride (LaF 3 :Pr) embodiment composition may be prepared from a mixture of praseodymium fluoride (PrF 3 ) and lanthanum fluoride (LaF 3 ).
- compositions include but are not limited to, CeBr 3 , YAlO 3 :Ce, LuAlO 3 :Ce, Lu 1-x Y x O 3 :Ce, Bi 4 Ge 3 O 12 , PbWO 4 , CdWO 4 , Lu 2 SiO 5 :Ce, Y 2 SiO 5 :Ce, Lu 2-x Y x SiO 5 :Ce, MgF 2 :Ce, CaF 2 :Ce, BaF 2 :Ce, LaCl 3 :Ce, K 2 LaCl 5 :Ce, LaBr 3 :Ce, RbGd 2 Br 3 :Ce, Csl:Na, Csl, Csl:Tl, Nal:Tl, ZnS:Ag, and the like.
- the amount of each powder used in preparing an embodiment composition depends on the desired amounts of dopant and other ingredients in the composition. From the formula of an embodiment composition, the amount of each ingredient can be calculated.
- any mixing device or method may be used to mix the powder.
- Mixing devices should not generate impurities that remain in a product phosphor composition, or generate only a minimal amount that does not substantially affect properties of the composition.
- Some non-limiting examples of methods and devices for mixing powder include mortar/pestle, ball milling, mixer mixing, attrition milling, and jet milling. Some or all of these methods and devices are employed in industrial operations.
- a mill containing spherical or rod-like materials, for example, may be used as the mixing device. In such a mill, the inner wall of the mill and the spherical or rod-like materials could be made of highly pure (at least 99.9 percent) alumina in order to avoid, or at least minimize impurities in a composition.
- the surface of a mixing device that contacts powder precursor could be made of plastic or coated with plastic.
- plastics include polyethylene, polypropylene, polyamides, polyesters and polyurethanes. The use of plastic tends to minimize impurities generated during a mixing operation.
- a non-limiting temperature range for heating a melt may be from about 100° C. to about 2800° C., or from about 800° C. to about 950° C.
- the melting of precursor powder can take place in a crucible having a small opening and nozzle.
- a melt once generated in the crucible can flow through the nozzle.
- the flow through the opening/nozzle can be enhanced using pressurized gas. Additional mixing action may take place as a melt moves through the opening/nozzle and out of the crucible. This type of mixing action is believed to be similar to that of a vortex, which can enhance the uniformity of the components in the melt.
- the nozzle opening should be large enough for the melt to flow through, aided with pressure from a jet of inert gas (argon, for example).
- a non-limiting range of nozzle opening sizes for a crucible may be from about 0.006 to about 0.1 inches, or from about 0.01 to about 0.03 inches, or from about 0.010 inches to about 0.020 inches. Without wishing to be bound by any explanation, it is believed that the mixing, melting and flow of melt through the nozzle of a crucible is believed to cause mixing of the precursor on an atomic scale.
- the temperature of the melt and the rate of spinning of a spinning wheel were such that the product phosphor composition produced was is in the form of nanoparticles of rare earth doped lanthanum halide embedded in a glassy matrix.
- flakes of nanoparticles of cerium-doped lanthanum bromide LaBr 3 :Ce embedded in a glassy matrix were prepared by mixing LaBr 3 powder with CeBr 3 powder using a mortar and pestle under argon in a glove box, loading the powder into a boron nitride crucible, transferring the loaded crucible to a melt spinner apparatus, melting the powder and injecting the melt through a nozzle on the crucible to a spinning copper wheel.
- the molten material was forced through the opening using pressurized gas (argon, for example). By using different pressures of the pressurized gas, the flow of the molten material through the opening in the crucible and therefore the feeding rate of the molten material to the copper spinning wheel can be adjusted.
- the viscosity of the molten material can be adjusted by adjusting the temperature of the molten material.
- the viscosity also has an effect on the flow of molten material through the opening in the crucible.
- the rotation of the spinning wheel promotes cooling of the copper wheel, which is cool before it is exposed to any new molten material.
- the molten material is cooled rapidly as it contacts the wheel. As the molten material cools, it forms flakes.
- these flakes include nanoparticles of cerium doped lanthanum bromide (i.e. LaBr 3 :Ce) having an average particle of less than about 100 nanometers (nm) embedded in a glassy LaBr 3 :Ce matrix.
- the LaBr 3 :Ce product produced according to this embodiment has good light output and energy resolution.
- melt spinning of LaBr 3 :Ce results in nanoparticles LaBr 3 :Ce of a uniform size.
- LaBr 3 :Ce nanoparticles having better light output and energy resolution than conventional methods is obtainable because impurities that typically result from an extensive milling step and from hydrate formation can be minimized or completely prevented,
- lanthanides and dopants are not limited to lanthanum (La) and cerium (Ce), and that any lanthanide capable of functioning as an inert host into which an emitting ion may be doped, may be used with the invention. These include La, Ce, Y, Nd, Cd, W, Mg, Ca, Ba, Na, K, Cs.
- the host can be any halide, oxyhalide, oxide, nitride, oxynitride, carbide, oxycarbide, or boride.
- the dopant can be Ce, Pr, Tm, Tb, Gd, Dy, Cr, Mn, Ti, Cu, Zn, Ga, Sb, Te, Eu, Sm, Y, Tl, Na, Li, B, Ag, or Nd.
- the choice of lanthanide may be tailored in order to prepare a chosen nanophosphor having desired emission properties.
- compositions may be prepared from powders. The amount of each powder can be calculated for a desired composition.
- a powder composition is one with both LaBr 3 powder and CeBr 3 powder.
- Another embodiment powder is one with LaBr 3 , LaCl 3 , and CeBr 3 .
- CeBr 3 powder is combined with LaBr 3 powder in a composition with a mole percent of cerium in a range of from 0.01 mole percent to 20 mole percent.
- a melt spun product may be one of the formula La 1-x Br 3-y Cl y :Ce x wherein x is from 0 to 1, and wherein y is from 0 to 3. Both x and y can be fractional numbers.
- cerium is not introduced as a bromide but instead it may introduced as cerium metal, as an organometallic compound of cerium as cerium oxide, as cerium fluoride, as cerium chloride, as cerium nitrate, or in any other form.
- raw materials were used for preparing some embodiment compositions that included LaBr 3 , LaCl 3 , and CeBr 3 also included some impurities.
- the amounts of the impurities were determined using Inductive Coupled Plasma-Mass Spectroscopy (ICP-MS). TABLE 1 below provides a listing of the impurities.
- a Differential Scanning Calorimeter was used to evaluate reactions between the raw material and crucible materials and to provide guidance on the melt temperature during melt spinning.
- a small batch of LaBr 3 , LaCl 3 , and CeBr 3 raw powders yielding a La 0.95 Ce 0.05 Br 1.575 Cl 1.425 composition was mixed using high purity aluminum oxide mortar and pestle. Powder mixing was performed in a glove box. The mixture powder was added into four different types of crucibles including Al 2 O 3 , BN, Pt, and quartz to investigate the possibility of reaction between crucible material and raw materials.
- the raw material was heated in the crucible to melting in an Ar environment with a heating rate of 20° C./min.
- FIG. 2 shows typical DSC result from LaBr 3 powders. As can be seem from FIG. 2 , some moisture that adsorbed on the powder surface was removed at about 91° C. In addition, some crystalline water was removed at about 372° C. The strong endothermic peak indicates that LaBr 3 starts to melt at about 788° C.
- FIG. 3 shows typical DSC result from LaCl 3 powders.
- LaCl 3 has a moisture adsorption at 125° C., however it does not have the crystalline water at about 400° C. This is an indication that LaCl 3 is less sensitive to the moisture than LaBr 3 .
- the melting point of LaCl 3 is at 877° C.
- FIG. 4 shows typical DSC results from LaBr 3 powders with 5 mole percent of CeBr 3 . From this figure, one can see that the melting is reduced slightly to about 785° C. due to the eutectic composition. In addition to the removal of moisture at about 125 and 400° C., there is additional moisture removal at about 334° C. Furthermore, the stronger peak at 334° C. might be an indication that CeBr 3 is much more sensitive to moisture.
- FIG. 5 shows typical DSC results from La 0.95 Ce 0.05 Br 2.288 Cl 0.713 with LaBr 3 /LaCl 3 of 75/25 mole ratio. This powder composition has 5 mole percent of CeBr 3 . As indicated in FIG. 5 , the melting point of the La 0.95 Ce 0.05 Br 2.288 Cl 0.713 mixture is lower because of the ternary eutectic.
- FIG. 6 shows typical DSC results from La 0.95 Ce 0.05 Br 1.575 Cl 1.425 with LaBr 3 /LaCl 3 in a 50/50 mole ratio. This powder composition has 5 mole % of CeBr 3 . As indicated in FIG. 6 , the melting point for the La 0.95 Ce 0.05 Br 1.575 Cl 1.425 composition has a higher melting point due to the higher amount of high melting point constituent LaCl 3 .
- La 0.95 Ce 0.05 Br 3 Preparation of La 0.95 Ce 0.05 Br 3 .
- a uniform powder mixture of lanthanum bromide (LaBr 3 , 40 grams) and cerium bromide (CeBr 3 , 2.11 grams) was prepared using a mortar and pestle in a glove box. The resulting mixture was transferred to a boron nitride crucible. The crucible had a nozzle with an opening of 0.019 inches. The crucible and powder were transferred from the glove box to the induction-heating coil of a melt spinner apparatus. A niobium shield was machined to serve as a coupling from the crucible/powder to the induction coil. The induction coil was water cooled to prevent the coil from overheating.
- the induction power was turned on to melt the powder.
- the peak temperature was set at 870° C. with a heating rate of about 20° C./min.
- the copper wheel was turned on and the turning speed was increased slowly to about 1000 rpm.
- a 3 psi jet of argon was used to inject the molten La 0.95 Ce 0.05 Br 3 through the nozzle opening and onto the copper wheel. As the melt contacted the wheel, it was converted to flakes that sprayed into the snout section the collecting area.
- a funnel made out of aluminum foil was made as liner for the snout to minimize exposure to moisture.
- FIG. 7 shows a TEM micrograph of the flaky product. As can be seen from FIG. 7 , the flakes include large numbers of small particles of a size on the order of about 20 nm. According to the diffused rings of the diffraction pattern, the product is a composition of La 0.95 Ce 0.05 Br 3 nanoparticles that are embedded in a glassy LaBr 3 :Ce matrix.
- La 0.95 Ce 0.05 Br 3 Preparation of La 0.95 Ce 0.05 Br 3 .
- a uniform powder mixture of LaBr 3 (40 grams), LaCl 3 (8.64 grams), and CeBr 3 (2.11 grams) was prepared inside a glove box using a mortar and pestle made of high purity aluminum oxide. The mixture was poured into a boron nitride crucible inside the glove box, and then loaded into an induction-heating coil in a melt spinner apparatus. A tantalum (Ta) shield was machined to serve as a coupling to the induction coil. The induction coil was water cooled to prevent the coil from overheating. The apparatus was evacuated and then purged with argon.
- the induction power was turned on to heat up the powder.
- the apparatus peak temperature was set at 870° C. with a heating rate of about 20° C./min.
- the copper wheel was turned on and the turning speed was increased slowly to about 2000 rpm.
- an argon jet of 1 psi was applied to inject the molten La 0.95 Ce 0.05 Br 3 through the nozzle opening and onto the copper wheel.
- the opening of the BN nozzle was about 0.019′′.
- the nozzle was lowered to toward the copper wheel, which reduced the distance between the nozzle and the copper wheel. Due to the small distance between the nozzle and the wheel, all of the melt was splashed randomly instead of going into the snout area.
- the splashed products were chunky with irregular structure.
- FIG. 8 shows an X-ray diffraction pattern of the product.
- FIG. 8 An x-ray diffraction (XRD) spectrum of the nanoparticle composition of EXAMPLE 6 is shown in FIG. 8 .
- the XRD pattern of LaX 3 :Ce shows the expected lines of the tysonite structure, and the absence of other lines indicates high phase purity.
- La 0.95 Ce 0.05 Br 2.288 Cl 0.713 A uniform powder mixture of LaBr 3 (40 g), LaCl 3 (8.64 g) and CeBr 3 (2.11 g) was prepared in a glove box using a mortar and pestle. The powder mixture was transferred to a boron nitride crucible. The crucible had a nozzle opening of 0.019 inches. The crucible and powder were transferred to the induction-heating coil of a melt spinner apparatus. A niobium shield was machined to serve as a coupling to the induction coil. The induction coil was water cooled to prevent the coil from overheating.
- the induction power was turned on to melt the powder mixture.
- the peak temperature was set at 870° C. with a heating rate of about 20° C./min.
- the copper wheel was also turned on and the turning speed was increased slowly to about 1700 rpm.
- a 1 psi jet of argon was used to inject the molten La 0.95 Ce 0.05 Br 3 through the nozzle opening and onto the copper wheel.
- the melt contacted the wheel, it was converted to solid flakes.
- the flakes were sprayed into the snout section of the collecting area.
- the flakes were collected quickly under argon in a glass container and transferred to a glove box. Yield: about 10 grams.
- Some embodiment compositions are phosphors that may be used for radiation detection.
- Large-area radiographic devices are often based on tiled mosaics of single crystals or an array of single crystal pixels. These devices suffer from disadvantages associated with non-uniform light output over the large area of the detector, and from the dark contrast lines that result from the seams between the tiles or pixels.
- Another significant problem associated with the production of pixelated detectors relates to the difficulty in producing pixels; some materials, such as the known scintillator Gd 2 SiO 5 :Ce (GSO:Ce) single crystals are micaceous and cannot be easily cut into pixels and polished for use in radiographic imaging.
- embodiment compositions of this invention are expected to have a relatively uniform light output, can be made seamless over a large area.
- compositions can be used in detectors for proton and neutron radiography, for positron emission tomography, and for medical radiography.
- Relatively inexpensive, large area detectors are possible because the process for making embodiment phosphor compositions can be scaled up to form large amounts of the compositions.
- the compositions may be used in radiation detectors for interrogation of complex and irregular shapes.
- the light emission from the radiation detector can be tailored for either a photomultiplier or a photodiode.
- the EXAMPLES described above involve preparation of a product using a batch type process on a relatively small scale. It should be understood that the process could be scaled up so that much greater amounts of product could be obtained.
- the process could be changed from a batch type to a continuous type process. This could be accomplished by using, for example, a continuous feed mechanism such as a screw feed for continuously delivering powder at a controlled rate into the melt crucible. Such a feeder would be used with an airlock system for delivering powder without opening the melt spinner to the atmosphere.
- a larger crucible with multiple ejection nozzles would be used.
- the crucible could be heated by induction heating, resistance heating, or by using radiant heat.
- a wheel large enough to accommodate the multiple ejection nozzles would be used. The wheel would be actively cooled using, for example, water or gas.
- a continuous or batch removal system that allows product to exit the melt spinner without letting air into it would also be used.
- inorganic compositions were prepared by sending an inorganic melt to a spinning wheel. Some of the products were shown to be nanostructured, having nanoparticles embedded in a glassy matrix.
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Abstract
Description
- This invention was made with government support under Contract No. DE-AC51-06NA25396 awarded by the U.S. Department of Energy. The government has certain rights in the invention.
- The invention relates to the preparation of inorganic compositions by melt spinning.
- Nanostructured materials generally have different electronic, magnetic, optical, and mechanical properties than the corresponding bulk materials. Light output from nanophosphors, for example, can be higher than for micron-sized or larger phosphors. Nanophosphors have attracted interest due to their potential uses in optics, optoelectronics, lighting, displays, optical amplifiers/scintillators, lasers, microelectronics, tribology, homeland security, radiation detectors, medical imaging, and other applications.
- There remains a need for better methods for preparing nanostructured materials.
- In accordance with the purposes of the present invention, as embodied and broadly described herein, the present invention is concerned with a process for preparing a composition. The process includes sending an inorganic melt to a spinning wheel, whereby the melt cools after it contacts the wheel and is converted into a product that comprises nanoparticles embedded in a glassy matrix.
- The present invention is also concerned with a product prepared by a process that comprises sending an inorganic melt to a spinning wheel that cools the melt after the melt contacts the spinning wheel, whereby the melt is converted into a product that comprises nanoparticles of a composition embedded in a glassy matrix of essentially the same composition.
- The present invention is also concerned with a composition that consists essentially of nanoparticles of a composition embedded in a glassy matrix of essentially the same composition as that of the nanoparticles.
- The accompanying drawings, which are incorporated in and form a part of the specification, illustrate embodiments of the present invention and, together with the description, serve to explain the principles of the invention. In the drawings:
-
FIG. 1 shows a schematic representation demonstrating operating principles of a melt spinner. -
FIG. 2 shows results from a differential scanning calorimeter (DSC) run for lanthanum bromide (LaBr3) powder. -
FIG. 3 shows results from a DSC run for lanthanum chloride LaCl3) powder. -
FIG. 4 shows results from a DSC run for a powder mixture having the formula La0.95Ce0.05Br3 powder. -
FIG. 5 shows results from a DSC run for a powder mixture having the formula La0.95Ce0.05Br2.288Cl0.713 powder. -
FIG. 6 shows results from a DSC run for a powder mixture having the formula La0.95Ce0.05Br1.575Cl1.425 powder. -
FIG. 7 shows a transmission electron microscope (TEM) micrograph showing the microstructure of an embodiment flake of nanoparticles embedded in a glassy matrix of the invention. -
FIG. 8 shows an x-ray diffraction (XRD) pattern of an embodiment phase of LaBr3:Ce nanoparticles. - The present invention provides compositions and methods for preparing the compositions. The compositions are generally inorganic compositions. Some embodiments of these compositions are phosphors.
- Some non-limiting embodiment compositions of the invention include rare earth doped lanthanum fluoride, rare earth doped lanthanum chloride, rare earth doped lanthanum bromide, and rare earth doped mixtures of lanthanum chloride and lanthanum bromide. Some non-limiting embodiment rare earth dopants include cerium, neodymium, europium, thulium, terbium, samarium, gadolinium, dysprosium, and praseodymium. Some other non-limiting embodiment dopants include thallium, chromium, manganese, titanium, copper, silver, zinc, gallium, antimony, and tellurium.
- An embodiment method for preparing the compositions involves the use of melt spinning. Melt spinning involves sending a composition in the form of a melt to a spinning wheel. When the melt contacts the spinning wheel, it loses heat and solidifies. A schematic representation showing the production of the compositions by melt spinning is shown in
FIG. 1 .Melt spinning apparatus 10 includescrucible 12 filled withpowder 14 and surrounded byinduction heating coils 16. Crucible 12 can be made from a material such as, but not limited to, boron nitride, and may be provided with a coupling (a tantalum coupling, for example) to facilitate the heating process.Melt spinning apparatus 10 also includesmelt spinning chamber 18 and spinning wheel 20 (a copper wheel, for example) inside the chamber. During operation, the induction heating coils transfer energy to the crucible (a coupler facilitates this, depending on the choice of crucible materials), andpowder 14 inside the crucible heats until it melts. The melt exits the crucible through opening 22 at the bottom ofcrucible 12 and moves into melt-spinningchamber 18 where it makes contact withspinning wheel 20. The melt cools as it contacts the wheel, and is sent throughsnout 24 where it is collected asflakes 26. A non-limiting range of speeds of the spinning wheel may be from about 1 rpm to about 5000 rpm, or from about 1000 to about 3000 rpm, or from about 1000 rpm to about 2000 rpm, or from about 1000 rpm to about 1700 rpm. An embodiment composition produced by sending a melt to the spinning wheel may be in the form of flakes that include crystalline nanoparticles in a glassy matrix. The chemical formula for the crystalline nanoparticle portion of the flakes may be essentially the same as that for the glassy matrix. - Powders may be used as starting materials. A cerium doped lanthanum bromide (LaBr3:Ce) embodiment composition, for example, may be prepared from a mixture of cerium bromide (CeBr3) powder and lanthanum bromide (LaBr3) powder. A terbium doped lanthanum chloride (LaCl3:Tb) embodiment composition may be prepared from a mixture of terbium chloride (TbCl3) powder and lanthanum chloride (LaCl3). A samarium doped lanthanum bromide/chloride (LaBr(3-x)Clx:Sm) embodiment composition may be prepared from a powder mixture of samarium bromide (SmBr3), lanthanum bromide, and lanthanum chloride. A praseodymium doped lanthanum fluoride (LaF3:Pr) embodiment composition may be prepared from a mixture of praseodymium fluoride (PrF3) and lanthanum fluoride (LaF3). Other embodiment compositions include but are not limited to, CeBr3, YAlO3:Ce, LuAlO3:Ce, Lu1-xYxO3:Ce, Bi4Ge3O12, PbWO4, CdWO4, Lu2SiO5:Ce, Y2SiO5:Ce, Lu2-xYxSiO5:Ce, MgF2:Ce, CaF2:Ce, BaF2:Ce, LaCl3:Ce, K2LaCl5:Ce, LaBr3:Ce, RbGd2Br3:Ce, Csl:Na, Csl, Csl:Tl, Nal:Tl, ZnS:Ag, and the like.
- The amount of each powder used in preparing an embodiment composition depends on the desired amounts of dopant and other ingredients in the composition. From the formula of an embodiment composition, the amount of each ingredient can be calculated.
- When powders are used, any mixing device or method may be used to mix the powder. Mixing devices should not generate impurities that remain in a product phosphor composition, or generate only a minimal amount that does not substantially affect properties of the composition. Some non-limiting examples of methods and devices for mixing powder include mortar/pestle, ball milling, mixer mixing, attrition milling, and jet milling. Some or all of these methods and devices are employed in industrial operations. A mill containing spherical or rod-like materials, for example, may be used as the mixing device. In such a mill, the inner wall of the mill and the spherical or rod-like materials could be made of highly pure (at least 99.9 percent) alumina in order to avoid, or at least minimize impurities in a composition. The surface of a mixing device that contacts powder precursor could be made of plastic or coated with plastic. Some non-limiting examples of plastics include polyethylene, polypropylene, polyamides, polyesters and polyurethanes. The use of plastic tends to minimize impurities generated during a mixing operation.
- After a mixing operation, precursor powder is heated to form a melt. The melting process can enhance the mixing significantly, and therefore an extensive grinding of powder prior to melting may not be necessary, which may avoid or minimize impurities that tend to result from grinding powder. When lanthanum halide precursor powder is used, for example, a non-limiting temperature range for heating a melt may be from about 100° C. to about 2800° C., or from about 800° C. to about 950° C.
- The melting of precursor powder can take place in a crucible having a small opening and nozzle. A melt once generated in the crucible can flow through the nozzle. The flow through the opening/nozzle can be enhanced using pressurized gas. Additional mixing action may take place as a melt moves through the opening/nozzle and out of the crucible. This type of mixing action is believed to be similar to that of a vortex, which can enhance the uniformity of the components in the melt. The nozzle opening should be large enough for the melt to flow through, aided with pressure from a jet of inert gas (argon, for example). A non-limiting range of nozzle opening sizes for a crucible may be from about 0.006 to about 0.1 inches, or from about 0.01 to about 0.03 inches, or from about 0.010 inches to about 0.020 inches. Without wishing to be bound by any explanation, it is believed that the mixing, melting and flow of melt through the nozzle of a crucible is believed to cause mixing of the precursor on an atomic scale.
- It should be understood that there is no particular restriction on the size and shape of the crucible. A tube shape with a small opening at the bottom of the crucible, for example, could be used. A crucible with a continuous feeding device could be used.
- It is believed that a uniform distribution of components is formed in the melt, and that this uniform distribution does not change when the melt contacts the spinning wheel, loses heat, and solidifies. The cooling provided by the spinning wheel is believed to prevent segregation of a component as particles form after the melt contacts the spinning wheel.
- In some embodiments for preparing rare earth doped lanthanum halide compositions, the temperature of the melt and the rate of spinning of a spinning wheel were such that the product phosphor composition produced was is in the form of nanoparticles of rare earth doped lanthanum halide embedded in a glassy matrix. In one of these embodiments, flakes of nanoparticles of cerium-doped lanthanum bromide LaBr3:Ce embedded in a glassy matrix were prepared by mixing LaBr3 powder with CeBr3 powder using a mortar and pestle under argon in a glove box, loading the powder into a boron nitride crucible, transferring the loaded crucible to a melt spinner apparatus, melting the powder and injecting the melt through a nozzle on the crucible to a spinning copper wheel. The molten material was forced through the opening using pressurized gas (argon, for example). By using different pressures of the pressurized gas, the flow of the molten material through the opening in the crucible and therefore the feeding rate of the molten material to the copper spinning wheel can be adjusted.
- The viscosity of the molten material can be adjusted by adjusting the temperature of the molten material. The viscosity also has an effect on the flow of molten material through the opening in the crucible. The rotation of the spinning wheel promotes cooling of the copper wheel, which is cool before it is exposed to any new molten material. The molten material is cooled rapidly as it contacts the wheel. As the molten material cools, it forms flakes. In an embodiment, these flakes include nanoparticles of cerium doped lanthanum bromide (i.e. LaBr3:Ce) having an average particle of less than about 100 nanometers (nm) embedded in a glassy LaBr3:Ce matrix. The LaBr3:Ce product produced according to this embodiment has good light output and energy resolution.
- In an embodiment, melt spinning of LaBr3:Ce results in nanoparticles LaBr3:Ce of a uniform size.
- In an aspect of the invention related to LaBr3:Ce formation, LaBr3:Ce nanoparticles having better light output and energy resolution than conventional methods is obtainable because impurities that typically result from an extensive milling step and from hydrate formation can be minimized or completely prevented,
- It should be understood that the choice of lanthanides and dopants are not limited to lanthanum (La) and cerium (Ce), and that any lanthanide capable of functioning as an inert host into which an emitting ion may be doped, may be used with the invention. These include La, Ce, Y, Nd, Cd, W, Mg, Ca, Ba, Na, K, Cs. The host can be any halide, oxyhalide, oxide, nitride, oxynitride, carbide, oxycarbide, or boride. The dopant can be Ce, Pr, Tm, Tb, Gd, Dy, Cr, Mn, Ti, Cu, Zn, Ga, Sb, Te, Eu, Sm, Y, Tl, Na, Li, B, Ag, or Nd. The choice of lanthanide may be tailored in order to prepare a chosen nanophosphor having desired emission properties.
- Some embodiment compositions may be prepared from powders. The amount of each powder can be calculated for a desired composition. One example of a powder composition is one with both LaBr3 powder and CeBr3 powder. Another embodiment powder is one with LaBr3, LaCl3, and CeBr3. In some of these, CeBr3 powder is combined with LaBr3 powder in a composition with a mole percent of cerium in a range of from 0.01 mole percent to 20 mole percent. A melt spun product may be one of the formula La1-xBr3-yCly:Cex wherein x is from 0 to 1, and wherein y is from 0 to 3. Both x and y can be fractional numbers. In some embodiments, cerium is not introduced as a bromide but instead it may introduced as cerium metal, as an organometallic compound of cerium as cerium oxide, as cerium fluoride, as cerium chloride, as cerium nitrate, or in any other form.
- In demonstrating the operability of the invention, raw materials were used for preparing some embodiment compositions that included LaBr3, LaCl3, and CeBr3 also included some impurities. The amounts of the impurities were determined using Inductive Coupled Plasma-Mass Spectroscopy (ICP-MS). TABLE 1 below provides a listing of the impurities.
-
TABLE 1 Impurity LaBr3 (ppm) LaCl3 (ppm) CeBr3 (ppm) Aluminum 21 — — Arsenic 31 — — Barium — — — Boron — — — Bromine — 410 — Cadmium — — — Calcium — 77 67 Copper — — — Gadolinium — — — Iron 16 — — Lanthanum — — 21 Magnesium 6 — — Manganese 27 — — Lithium — — — Potassium — — — Sodium — — — Tellurium — — — Thorium 6 — — Titanium — — — Uranium — — — Total 107 487 88
According to TABLE 1, CeBr3 has the lowest content of impurities (total of less than 100 ppm). Although LaCl3 had a high impurity content, most of the impurity is Br, which is a major component of LaBr3 and so can be used to form a melt with LaBr3 without contributing to the overall impurity content. - A Differential Scanning Calorimeter (DSC) was used to evaluate reactions between the raw material and crucible materials and to provide guidance on the melt temperature during melt spinning. A small batch of LaBr3, LaCl3, and CeBr3 raw powders yielding a La0.95Ce0.05Br1.575Cl1.425 composition was mixed using high purity aluminum oxide mortar and pestle. Powder mixing was performed in a glove box. The mixture powder was added into four different types of crucibles including Al2O3, BN, Pt, and quartz to investigate the possibility of reaction between crucible material and raw materials. The raw material was heated in the crucible to melting in an Ar environment with a heating rate of 20° C./min. The results indicate that there is no reaction with any crucible materials including Al2O3, BN, Pt, and quartz. These results confirm that Al2O3, BN, Pt, and quartz can be used as crucible materials for melt spinning an inorganic composition.
- DSC was performed on the as-received LaBr3 material (TABLE 1). LaBr3 powders were loaded into the BN crucible inside a glove box, and moisture content was maintained at less than 50 ppm. The crucible with LaBr3 powder was quickly transferred to the DSC with BN lid protection. The test was performed with a heating rate of 20° C./min in an Ar environment.
FIG. 2 shows typical DSC result from LaBr3 powders. As can be seem fromFIG. 2 , some moisture that adsorbed on the powder surface was removed at about 91° C. In addition, some crystalline water was removed at about 372° C. The strong endothermic peak indicates that LaBr3 starts to melt at about 788° C. - DSC was performed on the as-received LaCl3 materials. LaCl3 powders were loaded into the BN crucible inside a glove box, and moisture content was maintained at less than 50 ppm. The crucible with LaCl3 powder was quickly transferred to the DSC with BN lid protection. The test was performed with a heating rate of 20° C./min in an Ar environment.
FIG. 3 shows typical DSC result from LaCl3 powders. As can be seem fromFIG. 3 , LaCl3 has a moisture adsorption at 125° C., however it does not have the crystalline water at about 400° C. This is an indication that LaCl3 is less sensitive to the moisture than LaBr3. The melting point of LaCl3 is at 877° C. - A small batch of LaBr3 and CeBr3 raw powders yielding La0.95Ce0.05Br3 composition was mixed using high purity aluminum oxide mortar and pestle. The mixture powders were also analyzed using DSC.
FIG. 4 shows typical DSC results from LaBr3 powders with 5 mole percent of CeBr3. From this figure, one can see that the melting is reduced slightly to about 785° C. due to the eutectic composition. In addition to the removal of moisture at about 125 and 400° C., there is additional moisture removal at about 334° C. Furthermore, the stronger peak at 334° C. might be an indication that CeBr3 is much more sensitive to moisture. - A small batch of LaBr3, LaCl3, and CeBr3 raw powders yielding a La0.95Ce0.05Br2.288Cl0.713 composition was mixed using high purity aluminum oxide mortar and pestle.
FIG. 5 shows typical DSC results from La0.95Ce0.05Br2.288Cl0.713 with LaBr3/LaCl3 of 75/25 mole ratio. This powder composition has 5 mole percent of CeBr3. As indicated inFIG. 5 , the melting point of the La0.95Ce0.05Br2.288Cl0.713 mixture is lower because of the ternary eutectic. - A small batch of LaBr3, LaCl3, and CeBr3 raw powders yielding a La0.95Ce0.05Br1.575Cl1.425 composition was mixed using high purity aluminum oxide mortar and pestle.
FIG. 6 shows typical DSC results from La0.95Ce0.05Br1.575Cl1.425 with LaBr3/LaCl3 in a 50/50 mole ratio. This powder composition has 5 mole % of CeBr3. As indicated inFIG. 6 , the melting point for the La0.95Ce0.05Br1.575Cl1.425 composition has a higher melting point due to the higher amount of high melting point constituent LaCl3. - The following non-limiting EXAMPLES provide detailed procedures for the preparation of some embodiment inorganic compositions that are also scintillators.
- Preparation of La0.95Ce0.05Br3. A uniform powder mixture of lanthanum bromide (LaBr3, 40 grams) and cerium bromide (CeBr3, 2.11 grams) was prepared using a mortar and pestle in a glove box. The resulting mixture was transferred to a boron nitride crucible. The crucible had a nozzle with an opening of 0.019 inches. The crucible and powder were transferred from the glove box to the induction-heating coil of a melt spinner apparatus. A niobium shield was machined to serve as a coupling from the crucible/powder to the induction coil. The induction coil was water cooled to prevent the coil from overheating. After twice evacuating and purging the system with argon, the induction power was turned on to melt the powder. The peak temperature was set at 870° C. with a heating rate of about 20° C./min. The copper wheel was turned on and the turning speed was increased slowly to about 1000 rpm. After the temperature had stabilized for about 2 minutes, a 3 psi jet of argon was used to inject the molten La0.95Ce0.05Br3 through the nozzle opening and onto the copper wheel. As the melt contacted the wheel, it was converted to flakes that sprayed into the snout section the collecting area. A funnel made out of aluminum foil was made as liner for the snout to minimize exposure to moisture. The translucent flakes were collected quickly under argon in a glass container and transferred to a glove box. Yield: about 4 grams. The flakes appear to be agglomerates held loosely together because they break up easily.
FIG. 7 shows a TEM micrograph of the flaky product. As can be seen fromFIG. 7 , the flakes include large numbers of small particles of a size on the order of about 20 nm. According to the diffused rings of the diffraction pattern, the product is a composition of La0.95Ce0.05Br3 nanoparticles that are embedded in a glassy LaBr3:Ce matrix. - Preparation of La0.95Ce0.05Br3. A uniform powder mixture of LaBr3 (40 grams), LaCl3 (8.64 grams), and CeBr3 (2.11 grams) was prepared inside a glove box using a mortar and pestle made of high purity aluminum oxide. The mixture was poured into a boron nitride crucible inside the glove box, and then loaded into an induction-heating coil in a melt spinner apparatus. A tantalum (Ta) shield was machined to serve as a coupling to the induction coil. The induction coil was water cooled to prevent the coil from overheating. The apparatus was evacuated and then purged with argon. After repeating the evacuation/purging process to minimize the presence of oxygen and moisture, the induction power was turned on to heat up the powder. The apparatus peak temperature was set at 870° C. with a heating rate of about 20° C./min. The copper wheel was turned on and the turning speed was increased slowly to about 2000 rpm. After the temperature had stabilized for about 2 minutes, an argon jet of 1 psi was applied to inject the molten La0.95Ce0.05Br3 through the nozzle opening and onto the copper wheel. The opening of the BN nozzle was about 0.019″. The nozzle was lowered to toward the copper wheel, which reduced the distance between the nozzle and the copper wheel. Due to the small distance between the nozzle and the wheel, all of the melt was splashed randomly instead of going into the snout area. The splashed products were chunky with irregular structure.
FIG. 8 shows an X-ray diffraction pattern of the product. - An x-ray diffraction (XRD) spectrum of the nanoparticle composition of EXAMPLE 6 is shown in
FIG. 8 . The XRD pattern of LaX3:Ce shows the expected lines of the tysonite structure, and the absence of other lines indicates high phase purity. - Preparation of La0.95Ce0.05Br2.288Cl0.713. A uniform powder mixture of LaBr3 (40 g), LaCl3 (8.64 g) and CeBr3 (2.11 g) was prepared in a glove box using a mortar and pestle. The powder mixture was transferred to a boron nitride crucible. The crucible had a nozzle opening of 0.019 inches. The crucible and powder were transferred to the induction-heating coil of a melt spinner apparatus. A niobium shield was machined to serve as a coupling to the induction coil. The induction coil was water cooled to prevent the coil from overheating. After twice evacuating and purging the system with argon, the induction power was turned on to melt the powder mixture. The peak temperature was set at 870° C. with a heating rate of about 20° C./min. The copper wheel was also turned on and the turning speed was increased slowly to about 1700 rpm. After the temperature had stabilized for about 2 minutes, a 1 psi jet of argon was used to inject the molten La0.95Ce0.05Br3 through the nozzle opening and onto the copper wheel. As the melt contacted the wheel, it was converted to solid flakes. The flakes were sprayed into the snout section of the collecting area. The flakes were collected quickly under argon in a glass container and transferred to a glove box. Yield: about 10 grams.
- Preparation of La0.95Ce0.05Br2.288Cl0.713. The procedure of EXAMPLE 3 was followed with the exception that a tantalum shield was used instead of a niobium shield, and the speed of the rotating wheel was about 2000 rpm instead of 1700 rpm. Yield: about 12 grams.
- Preparation of La0.95Ce0.05Br2.288Cl0.713. The procedure of EXAMPLE 3 was followed with the exception that a tantalum shield was used instead of a niobium shield, the speed of the rotating wheel was about 2000 rpm instead of 1700 rpm, and the nozzle opening of the crucible was 0.010 inches instead of 0.019 inches. The melt-spun flakes were much smaller and had a finer texture than those of EXAMPLE 3 or EXAMPLE 4.
- Attempted preparation of La0.95Ce0.05Br2.288Cl0.713 using a crucible with a very small nozzle opening. The procedure of EXAMPLE 4 was repeated with the exception that the nozzle opening was 0.005 inches. At a peak temperature of 870° C. and an argon jet pressure of about 1 psi, no melt could be injected out of the nozzle. When the argon jet pressure was increased to about 12 psi, still no melt could be injected. When the melt temperature was increased to about 1300° C. with an argon jet pressure of 12 psi, still no melt could be injected through the nozzle.
- Some embodiment compositions are phosphors that may be used for radiation detection. Large-area radiographic devices are often based on tiled mosaics of single crystals or an array of single crystal pixels. These devices suffer from disadvantages associated with non-uniform light output over the large area of the detector, and from the dark contrast lines that result from the seams between the tiles or pixels. Another significant problem associated with the production of pixelated detectors relates to the difficulty in producing pixels; some materials, such as the known scintillator Gd2SiO5:Ce (GSO:Ce) single crystals are micaceous and cannot be easily cut into pixels and polished for use in radiographic imaging. By contrast, embodiment compositions of this invention are expected to have a relatively uniform light output, can be made seamless over a large area. They can be used in detectors for proton and neutron radiography, for positron emission tomography, and for medical radiography. Relatively inexpensive, large area detectors (portal monitors, shipping containers, medical imagers, and the like) are possible because the process for making embodiment phosphor compositions can be scaled up to form large amounts of the compositions. The compositions may be used in radiation detectors for interrogation of complex and irregular shapes.
- By selecting the appropriate rare earth dopant, the light emission from the radiation detector can be tailored for either a photomultiplier or a photodiode.
- The EXAMPLES described above involve preparation of a product using a batch type process on a relatively small scale. It should be understood that the process could be scaled up so that much greater amounts of product could be obtained. In addition, the process could be changed from a batch type to a continuous type process. This could be accomplished by using, for example, a continuous feed mechanism such as a screw feed for continuously delivering powder at a controlled rate into the melt crucible. Such a feeder would be used with an airlock system for delivering powder without opening the melt spinner to the atmosphere. A larger crucible with multiple ejection nozzles would be used. The crucible could be heated by induction heating, resistance heating, or by using radiant heat. A wheel large enough to accommodate the multiple ejection nozzles would be used. The wheel would be actively cooled using, for example, water or gas. A continuous or batch removal system that allows product to exit the melt spinner without letting air into it would also be used.
- In summary, inorganic compositions were prepared by sending an inorganic melt to a spinning wheel. Some of the products were shown to be nanostructured, having nanoparticles embedded in a glassy matrix.
- The foregoing description of the invention has been presented for purposes of illustration and description and is not intended to be exhaustive or to limit the invention to the precise form disclosed, and obviously many modifications and variations are possible in light of the above teaching.
- The embodiments were chosen and described in order to best explain the principles of the invention and its practical application to thereby enable others skilled in the art to best utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the claims appended hereto.
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2014019318A1 (en) * | 2012-07-30 | 2014-02-06 | 江苏巨鑫磁业有限公司 | A method for industrialized cryogenic production of a rapidly-quenched nanocrystalline permanent magnetic neodymium powder |
CN103785827A (en) * | 2014-03-04 | 2014-05-14 | 南京信息工程大学 | Ferrocobalt-base alloy magnetic powder material for paint and preparation method |
US9848634B2 (en) * | 2009-06-30 | 2017-12-26 | Philip Morris Products S.A. | Smokeless tobacco product |
US20180112326A1 (en) * | 2015-03-27 | 2018-04-26 | Board Of Regents Of The Nevada System Of Higher Education, On Behalf Of The University Of Nevada, | Thin silicon substrate fabrication directly from silicon melt |
CN107988542A (en) * | 2017-11-15 | 2018-05-04 | 重庆嘉萌鸿业科技有限公司 | A kind of formula and its preparation process of lightization type automotive wheel wheel hub |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040180203A1 (en) * | 1996-09-03 | 2004-09-16 | Tapesh Yadav | Nanomaterial compositions with distinctive shape and morphology |
US20050214967A1 (en) * | 2002-09-05 | 2005-09-29 | Nanosys, Inc. | Nanostructure and nanocomposite based compositions and photovoltaic devices |
US20080093557A1 (en) * | 2005-12-21 | 2008-04-24 | Cooke D W | Nanocomposite scintillator, detector, and method |
-
2007
- 2007-02-06 US US11/703,505 patent/US20080185074A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040180203A1 (en) * | 1996-09-03 | 2004-09-16 | Tapesh Yadav | Nanomaterial compositions with distinctive shape and morphology |
US20050214967A1 (en) * | 2002-09-05 | 2005-09-29 | Nanosys, Inc. | Nanostructure and nanocomposite based compositions and photovoltaic devices |
US20080093557A1 (en) * | 2005-12-21 | 2008-04-24 | Cooke D W | Nanocomposite scintillator, detector, and method |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9848634B2 (en) * | 2009-06-30 | 2017-12-26 | Philip Morris Products S.A. | Smokeless tobacco product |
US10602769B2 (en) | 2009-06-30 | 2020-03-31 | Philip Morris Products S.A. | Smokeless tobacco product |
WO2014019318A1 (en) * | 2012-07-30 | 2014-02-06 | 江苏巨鑫磁业有限公司 | A method for industrialized cryogenic production of a rapidly-quenched nanocrystalline permanent magnetic neodymium powder |
CN103785827A (en) * | 2014-03-04 | 2014-05-14 | 南京信息工程大学 | Ferrocobalt-base alloy magnetic powder material for paint and preparation method |
US20180112326A1 (en) * | 2015-03-27 | 2018-04-26 | Board Of Regents Of The Nevada System Of Higher Education, On Behalf Of The University Of Nevada, | Thin silicon substrate fabrication directly from silicon melt |
CN107988542A (en) * | 2017-11-15 | 2018-05-04 | 重庆嘉萌鸿业科技有限公司 | A kind of formula and its preparation process of lightization type automotive wheel wheel hub |
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