US3403008A - Process for producing metal carbide fibers, textiles and shapes - Google Patents
Process for producing metal carbide fibers, textiles and shapes Download PDFInfo
- Publication number
- US3403008A US3403008A US602571A US60257166A US3403008A US 3403008 A US3403008 A US 3403008A US 602571 A US602571 A US 602571A US 60257166 A US60257166 A US 60257166A US 3403008 A US3403008 A US 3403008A
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- US
- United States
- Prior art keywords
- fibers
- metal
- fiber
- organic
- carbide
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000835 fiber Substances 0.000 title description 115
- 229910052751 metal Inorganic materials 0.000 title description 76
- 239000002184 metal Substances 0.000 title description 76
- 238000000034 method Methods 0.000 title description 43
- 230000008569 process Effects 0.000 title description 22
- 239000004753 textile Substances 0.000 title description 13
- 150000002736 metal compounds Chemical class 0.000 description 39
- 229920000297 Rayon Polymers 0.000 description 35
- 229920000642 polymer Polymers 0.000 description 30
- 239000002964 rayon Substances 0.000 description 29
- 239000000243 solution Substances 0.000 description 27
- 238000010438 heat treatment Methods 0.000 description 21
- 238000006243 chemical reaction Methods 0.000 description 20
- 229920000620 organic polymer Polymers 0.000 description 20
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 20
- 239000000463 material Substances 0.000 description 19
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 18
- 239000004744 fabric Substances 0.000 description 17
- 239000012298 atmosphere Substances 0.000 description 16
- 229910052799 carbon Inorganic materials 0.000 description 15
- 150000003839 salts Chemical class 0.000 description 15
- 239000007788 liquid Substances 0.000 description 13
- 239000002904 solvent Substances 0.000 description 13
- 238000007654 immersion Methods 0.000 description 12
- 230000001590 oxidative effect Effects 0.000 description 12
- 239000007789 gas Substances 0.000 description 11
- 238000005213 imbibition Methods 0.000 description 11
- 238000000197 pyrolysis Methods 0.000 description 10
- 238000006460 hydrolysis reaction Methods 0.000 description 8
- 239000011368 organic material Substances 0.000 description 8
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 7
- 229910052770 Uranium Inorganic materials 0.000 description 7
- 239000007864 aqueous solution Substances 0.000 description 7
- 239000013078 crystal Substances 0.000 description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- 229910026551 ZrC Inorganic materials 0.000 description 6
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 6
- 238000001035 drying Methods 0.000 description 6
- 230000007062 hydrolysis Effects 0.000 description 6
- 150000001247 metal acetylides Chemical class 0.000 description 6
- 239000001301 oxygen Substances 0.000 description 6
- 229910052760 oxygen Inorganic materials 0.000 description 6
- 230000008961 swelling Effects 0.000 description 6
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 description 6
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 5
- 229920002678 cellulose Polymers 0.000 description 5
- 239000001913 cellulose Substances 0.000 description 5
- 238000000354 decomposition reaction Methods 0.000 description 5
- 239000001257 hydrogen Substances 0.000 description 5
- 229910052739 hydrogen Inorganic materials 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- -1 polyethylene Polymers 0.000 description 5
- 239000007858 starting material Substances 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- 238000002441 X-ray diffraction Methods 0.000 description 4
- OTCHGXYCWNXDOA-UHFFFAOYSA-N [C].[Zr] Chemical compound [C].[Zr] OTCHGXYCWNXDOA-UHFFFAOYSA-N 0.000 description 4
- 238000004458 analytical method Methods 0.000 description 4
- DIKBFYAXUHHXCS-UHFFFAOYSA-N bromoform Chemical compound BrC(Br)Br DIKBFYAXUHHXCS-UHFFFAOYSA-N 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 4
- 238000005470 impregnation Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 229910044991 metal oxide Inorganic materials 0.000 description 4
- 150000004706 metal oxides Chemical class 0.000 description 4
- 150000002739 metals Chemical class 0.000 description 4
- VZGDMQKNWNREIO-UHFFFAOYSA-N tetrachloromethane Chemical compound ClC(Cl)(Cl)Cl VZGDMQKNWNREIO-UHFFFAOYSA-N 0.000 description 4
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 4
- 229910052721 tungsten Inorganic materials 0.000 description 4
- 239000010937 tungsten Substances 0.000 description 4
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 4
- ZWEHNKRNPOVVGH-UHFFFAOYSA-N 2-Butanone Chemical compound CCC(C)=O ZWEHNKRNPOVVGH-UHFFFAOYSA-N 0.000 description 3
- VXEGSRKPIUDPQT-UHFFFAOYSA-N 4-[4-(4-methoxyphenyl)piperazin-1-yl]aniline Chemical compound C1=CC(OC)=CC=C1N1CCN(C=2C=CC(N)=CC=2)CC1 VXEGSRKPIUDPQT-UHFFFAOYSA-N 0.000 description 3
- 229910052580 B4C Inorganic materials 0.000 description 3
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 3
- MHAJPDPJQMAIIY-UHFFFAOYSA-N Hydrogen peroxide Chemical compound OO MHAJPDPJQMAIIY-UHFFFAOYSA-N 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 3
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 3
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 description 3
- 239000004327 boric acid Substances 0.000 description 3
- 229910052796 boron Inorganic materials 0.000 description 3
- 239000006260 foam Substances 0.000 description 3
- 229910002804 graphite Inorganic materials 0.000 description 3
- 239000010439 graphite Substances 0.000 description 3
- 239000011261 inert gas Substances 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- VLKZOEOYAKHREP-UHFFFAOYSA-N n-Hexane Chemical compound CCCCCC VLKZOEOYAKHREP-UHFFFAOYSA-N 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 229920000728 polyester Polymers 0.000 description 3
- 229920002635 polyurethane Polymers 0.000 description 3
- 239000004814 polyurethane Substances 0.000 description 3
- 108090000623 proteins and genes Proteins 0.000 description 3
- 102000004169 proteins and genes Human genes 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 3
- 229910010271 silicon carbide Inorganic materials 0.000 description 3
- 239000005049 silicon tetrachloride Substances 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 description 3
- 229920002554 vinyl polymer Polymers 0.000 description 3
- 238000005303 weighing Methods 0.000 description 3
- 229910052726 zirconium Inorganic materials 0.000 description 3
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 description 2
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- PAYRUJLWNCNPSJ-UHFFFAOYSA-N Aniline Chemical compound NC1=CC=CC=C1 PAYRUJLWNCNPSJ-UHFFFAOYSA-N 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 2
- HEDRZPFGACZZDS-UHFFFAOYSA-N Chloroform Chemical compound ClC(Cl)Cl HEDRZPFGACZZDS-UHFFFAOYSA-N 0.000 description 2
- 229910052778 Plutonium Inorganic materials 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 229910052776 Thorium Inorganic materials 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- 239000002253 acid Substances 0.000 description 2
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 2
- 229950005228 bromoform Drugs 0.000 description 2
- 238000005119 centrifugation Methods 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000002425 crystallisation Methods 0.000 description 2
- 230000008025 crystallization Effects 0.000 description 2
- 239000003085 diluting agent Substances 0.000 description 2
- 238000001704 evaporation Methods 0.000 description 2
- 230000008020 evaporation Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000001307 helium Substances 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 2
- 229930195733 hydrocarbon Natural products 0.000 description 2
- 150000002430 hydrocarbons Chemical class 0.000 description 2
- 150000002576 ketones Chemical class 0.000 description 2
- 238000011068 loading method Methods 0.000 description 2
- 239000002932 luster Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- LQNUZADURLCDLV-UHFFFAOYSA-N nitrobenzene Chemical compound [O-][N+](=O)C1=CC=CC=C1 LQNUZADURLCDLV-UHFFFAOYSA-N 0.000 description 2
- 230000000737 periodic effect Effects 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- OYEHPCDNVJXUIW-UHFFFAOYSA-N plutonium atom Chemical compound [Pu] OYEHPCDNVJXUIW-UHFFFAOYSA-N 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 239000012266 salt solution Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- AKEJUJNQAAGONA-UHFFFAOYSA-N sulfur trioxide Chemical compound O=S(=O)=O AKEJUJNQAAGONA-UHFFFAOYSA-N 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 238000003828 vacuum filtration Methods 0.000 description 2
- 210000002268 wool Anatomy 0.000 description 2
- 239000002759 woven fabric Substances 0.000 description 2
- IQUPABOKLQSFBK-UHFFFAOYSA-N 2-nitrophenol Chemical compound OC1=CC=CC=C1[N+]([O-])=O IQUPABOKLQSFBK-UHFFFAOYSA-N 0.000 description 1
- MGWGWNFMUOTEHG-UHFFFAOYSA-N 4-(3,5-dimethylphenyl)-1,3-thiazol-2-amine Chemical compound CC1=CC(C)=CC(C=2N=C(N)SC=2)=C1 MGWGWNFMUOTEHG-UHFFFAOYSA-N 0.000 description 1
- 239000004604 Blowing Agent Substances 0.000 description 1
- 240000008564 Boehmeria nivea Species 0.000 description 1
- 101100368700 Caenorhabditis elegans tac-1 gene Proteins 0.000 description 1
- 229920000298 Cellophane Polymers 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910019704 Nb2O Inorganic materials 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 239000004743 Polypropylene Substances 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000002745 absorbent Effects 0.000 description 1
- 239000002250 absorbent Substances 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 229920006397 acrylic thermoplastic Polymers 0.000 description 1
- 238000007605 air drying Methods 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 150000001412 amines Chemical class 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
- 125000004429 atom Chemical group 0.000 description 1
- 238000010923 batch production Methods 0.000 description 1
- YXVFYQXJAXKLAK-UHFFFAOYSA-N biphenyl-4-ol Chemical compound C1=CC(O)=CC=C1C1=CC=CC=C1 YXVFYQXJAXKLAK-UHFFFAOYSA-N 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- DKPFZGUDAPQIHT-UHFFFAOYSA-N butyl acetate Chemical compound CCCCOC(C)=O DKPFZGUDAPQIHT-UHFFFAOYSA-N 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 229920002301 cellulose acetate Polymers 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 238000000975 co-precipitation Methods 0.000 description 1
- 238000010924 continuous production Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- XAYGUHUYDMLJJV-UHFFFAOYSA-Z decaazanium;dioxido(dioxo)tungsten;hydron;trioxotungsten Chemical compound [H+].[H+].[NH4+].[NH4+].[NH4+].[NH4+].[NH4+].[NH4+].[NH4+].[NH4+].[NH4+].[NH4+].O=[W](=O)=O.O=[W](=O)=O.O=[W](=O)=O.O=[W](=O)=O.O=[W](=O)=O.O=[W](=O)=O.[O-][W]([O-])(=O)=O.[O-][W]([O-])(=O)=O.[O-][W]([O-])(=O)=O.[O-][W]([O-])(=O)=O.[O-][W]([O-])(=O)=O.[O-][W]([O-])(=O)=O XAYGUHUYDMLJJV-UHFFFAOYSA-Z 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000005868 electrolysis reaction Methods 0.000 description 1
- 150000002148 esters Chemical class 0.000 description 1
- 239000011151 fibre-reinforced plastic Substances 0.000 description 1
- 238000009730 filament winding Methods 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- GPRLSGONYQIRFK-UHFFFAOYSA-N hydron Chemical compound [H+] GPRLSGONYQIRFK-UHFFFAOYSA-N 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- RLSSMJSEOOYNOY-UHFFFAOYSA-N m-cresol Chemical compound CC1=CC=CC(O)=C1 RLSSMJSEOOYNOY-UHFFFAOYSA-N 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229940100630 metacresol Drugs 0.000 description 1
- 229910001507 metal halide Inorganic materials 0.000 description 1
- 150000005309 metal halides Chemical class 0.000 description 1
- 229910021645 metal ion Inorganic materials 0.000 description 1
- 239000000693 micelle Substances 0.000 description 1
- 210000001724 microfibril Anatomy 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052754 neon Inorganic materials 0.000 description 1
- GKAOGPIIYCISHV-UHFFFAOYSA-N neon atom Chemical compound [Ne] GKAOGPIIYCISHV-UHFFFAOYSA-N 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- UJVRJBAUJYZFIX-UHFFFAOYSA-N nitric acid;oxozirconium Chemical compound [Zr]=O.O[N+]([O-])=O.O[N+]([O-])=O UJVRJBAUJYZFIX-UHFFFAOYSA-N 0.000 description 1
- JCXJVPUVTGWSNB-UHFFFAOYSA-N nitrogen dioxide Inorganic materials O=[N]=O JCXJVPUVTGWSNB-UHFFFAOYSA-N 0.000 description 1
- 150000002894 organic compounds Chemical class 0.000 description 1
- 239000012071 phase Substances 0.000 description 1
- 229920003229 poly(methyl methacrylate) Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 229920001155 polypropylene Polymers 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000000634 powder X-ray diffraction Methods 0.000 description 1
- 238000009725 powder blending Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 229910052814 silicon oxide Inorganic materials 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- ISXSCDLOGDJUNJ-UHFFFAOYSA-N tert-butyl prop-2-enoate Chemical compound CC(C)(C)OC(=O)C=C ISXSCDLOGDJUNJ-UHFFFAOYSA-N 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 150000003657 tungsten Chemical class 0.000 description 1
- 210000001170 unmyelinated nerve fiber Anatomy 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 1
- 239000012808 vapor phase Substances 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
- 150000003754 zirconium Chemical class 0.000 description 1
- IPCAPQRVQMIMAN-UHFFFAOYSA-L zirconyl chloride Chemical compound Cl[Zr](Cl)=O IPCAPQRVQMIMAN-UHFFFAOYSA-L 0.000 description 1
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
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/62227—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining fibres
- C04B35/62272—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining fibres based on non-oxide ceramics
- C04B35/62277—Fibres based on carbides
- C04B35/62281—Fibres based on carbides based on silicon carbide
-
- C—CHEMISTRY; METALLURGY
- C01—INORGANIC CHEMISTRY
- C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
- C01B32/00—Carbon; Compounds thereof
- C01B32/90—Carbides
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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
- C04B35/5158—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 actinide compounds
-
- 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
- C04B35/56—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 carbides or oxycarbides
-
- 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
- C04B35/56—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 carbides or oxycarbides
- C04B35/5607—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 carbides or oxycarbides based on refractory metal carbides
-
- C—CHEMISTRY; METALLURGY
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Definitions
- This invention relates to fibers, textiles, and shaped articles composed of metal carbides and to a process for producing such fibers, textiles, and shaped articles.
- the prior art has prepared certain metal carbide fibers by a number of methods, but each is characterized by important limitations.
- silicon carbide has been crystallized in a liquid system, but this procedure requires high pressures and/or high temperatures.
- the whisker method fibers are formed from the vapor phase or by electrolysis of molten salt. This method produces fibers which are often irregularly matted, kinked and very closely spaced.
- metal carbide fibers made by the whisker method are characterized by distortions, and relatively short (below 0.25 inch). It has heretofore been impossible to reproduceably prepare flexible metal carbide fibers having a length-to-diameter ratio over 400, characterized by high strength at high temperatures.
- Another object of the invention nited States Patent O is to provide a method for producing such articles from non-fibrous organic material.
- Still another object is to provide a variety of films, tubes, cups and other shapes which are composed of microcrystallinemetal carbides.
- Another object is to provide'such a method in'which the metal carbide fibers are of uniform diameter, straight, smooth surfaced and free of distortions.
- a further obpect is to provide metal carbide fibers of less than about 30 microns diameter having a length-todiameter ratio over 400, which are flexible and charac terized by high strength at high temperatures.
- a still further object is to provide a variety of textile forms, including staple fibers, continuous tow and yarns, woven fabrics, batting and felts, composed of metal carbide fibers.
- One aspect of the novel process comprises first providing a compound of a metal dissolved in a solvent, and immersing a preformed organic polymeric material in the resulting solution thereby swelling and opening the organic material interstices such that the metal compound is imbibed or absorbed in the interstices.
- the unimbibed metal compound is then removed from the organic material outer surfaces and the metal compoundim-bibed material is dried.
- the latter is first heated to temperature of at least 250 C. at a rate sufliciently low to evolve volatile decomposition products of the organic material without destroying the intergrity of this polymeric material.
- This pyrolysis step is continued for a sufficient duration to decompose the organic structure of the polymeric material and form a carbonaceous relic containing the metal in finely dispersed form.
- the relic is further heated from the pyrolysis step to temperature of about 1000-2000 C. in a non-oxidizing atmosphere to react the imbibed metal with the carbonaceous organic polymer relic to form a metal carbide shape, fiber, or textile.
- the non-oxidizing atmosphere of the carburization step may for example be that of an inert gas, hydrogen, or hydrocarbon reducing gas, vacuum or a combination of any of these atmospheres,
- an inert gas, hydrogen, or hydrocarbon reducing gas, vacuum or a combination of any of these atmospheres There results a metal carbide shaped article which has essentially the same physical shape as the original preformed organic polymeric material, although the dimensions may be reduced by as much as about 40 to 6 percent.
- organic polymers such as rayon fiber are composed of extremely small crystallites of cellulosic chains (micelles or microfibrils) held together in a matrix of amorphous cellulose.
- the crystallites approximately 40 Angstrom units (A.) in diameter and 250 A. long in high tenacity rayon yarns, are parallel to the axis of the rayon fiber and are spaced approximately 20 A. apart in the dry state.
- a one-denier fiber (1 gram weight per 9000 meters of length) has several million crystallites in its cross-section.
- the fiber When the fiber is immersed in a solvent such as water or aqueous solutions, it swells laterally opening the interstices, the amorphous regions enlarge and the crystallite spacing becomes approximately 50 A. (in the case of rayon).
- the dissolved selected metal compound such as a salt enters the swollen amorphous regions, which is about of the volume of the swollen rayon, and becomes trapped in the amorphous regions between the crystallites when the solvent is evaporated from the fibers.
- the metal compounds do not crystallize upon drying of theorganic polymer, as would normally occur upon drying a solution, since they are effectively suspended and separated as islands about 50 A. in size between the crystallites.
- the organic polymers may be imbibed with two or more metal compounds from the same solvent solution, so that carbides of more than one metal may be prepared, e.g. tungsten carbide and zirconium carbide.
- carbides of more than one metal e.g. tungsten carbide and zirconium carbide.
- most metal compounds enter the polymer interstices in direct, proportion to their solution concentration, allowing ready control of the relative loadings of metal compounds in the preformed organic polymer. Due to the blocking action of the organic crystallites, the metal compounds cannot segregate from each other nor crystallize during the drying and heat conversion steps.
- the metal compounds and later the oxides and carbides are extremely reactive and can be made to undergo the necessary chemical reactions to form the desired metal carbide alloy product at lower temperatures than normally required by conventional coprecipitation or powder blending methods for preparing such mixtures.
- Any organic polymeric material can be employed as a starting material in the process of this invention providing it is characterized by the above-described sequence of extremely small crystallites held together in a matrix of amorphous regions which enlarge and admit the metal compounds on immersion in the solvent.
- Any class of materials which are composed of long-chain molecules held together by chemical cross-links may also be used.
- Any cellulosic material can be employed including rayon, cellophane, saponified cellulose acetate, cotton, wood and ramie.
- Other suitable organic materials include the protein fibers (wool and silk) and the man-made acrylics, polyesters, vinyls and polyurethanes.
- Certain organic materials such as polyethylene and polypropylene are not suitable for practicing the instant process because they cannot be swollen for imbibition of the metal compounds and/or the materials melt and lose their structure during pyrolysis.
- a preferred cellulosic material is rayon due to its structural uniformity, good imbibition characteristics and low impurity content.
- the physical form of the elemental metal carbide composition is essentially the same as and is determined by the physical form of the organic polymer starting material.
- the length of the fiber shrinks to approximately 40 to 60 percent and the diameter to 25 to 35 percent of the original dimensions. Similar shrinkage in all dimensions also occurs with the non-fibrous shapes.
- a yarn composed of a multiplicity of continuous-length metal carbide fibers is desired, a continuous-filament organic yarn is employed as the starting material in the process of this invention.
- a woven fabric or felt composed of metal carbide fibers is desired, a woven organic fiber cloth or felt can be used as the starting material.
- metal carbide woven textiles can be made using conventional textile equipment and techniques starting with metal carbide staple fibers or yarns made by the process of this invention.
- cellulosic materials are imbibed with the metal compounds to the extent of at least one-quarter mole and preferably 1.0-2.0 moles of the metal compound(s) in each base mole of cellulose.
- base mole refers to the molecular weight of a glycosidic unit of the cellulose chain (molecular weight of 162).
- the degree of imbibition should be at least 0.1 and preferably 0.5-1.0 gram-equivalent metal ion in the metal compound imbibing solution per gram organic polymer.
- metal compound(s) With lower concentrations of metal compound(s), insufficient metal salt is available in the relic to form a strong article and the process becomes less efficient in terms of metal carbide yield per unit weight of preformed organic polymer starting material.
- Another disadvantage of low metal compound concentrations is that more drastic oxidation conditions are necessary to achieve pyrolysis.
- Imbibition or impregnation of the organic material can be carried out by several methods.
- the imbibition step can be carried out by immersing the organic material in a concentrated aqueous solution of such salt.
- the organic fiber can be imbibed by immersion in an aqueous solution of zirconyl chloride or zirconyl nitrate having concentrations in the range of 2.5 to 3.0 moles per liter.
- the acidity of the impregnating solution is preferably not greater than 1.0 molar (in hydrogen ion) in order to prevent degradation of the organic fiber during immersion.
- the acid may be neutralized with ammonia, if desired.
- Pre-swelling the cellulosic organic polymers in water prior to immersion in concentrated imbibing solutions is preferably employed to increase both the rate and extent of salt imbibition.
- Water is also suitable for swelling protein materials.
- acrylic and polyester polymers aromatic alcohols are suitable swelling agents, and the ketones are useful in swelling vinyl and polyurethane polymers for the same purpose.
- Water is the preferred solvent for metal compoundimbibing of cellulosic and protein materials such as wool and silk.
- Other solvents such as alcohols do not afford as efficient swelling of the polymers nor solubility of the selected metal compound for a high degree of imbibing.
- esters and ketones are appropriate solvents, as for example normal butyl acetate or methyl ethyl ketone.
- suitable solvents for the metal compound imbibition include aromatic alcohols and amines such as aniline, nitro-phenol, meta-cresol and paraphenylphenol.
- Immersion times at normal temperatures (2l23 C.) required to give adequate imbibition vary from 30 minutes to several days depending on the salt(s) employed and the type of organic polymer employed. Immersion times greater than about 3 days in concentrated salt solutions are undesirable for fibers since the organic fiber may degrade, resulting in a decrease in amount of metal compound absorbed and causing the polymers to bond to each other.
- the metal compound solution may be heated to as high as C.
- One method of impregnating rayon fibers and other cellulosic fibers and films with certain important metals is to absorb water into rayon and then contact the rayon with a compound of the metal so that it penetrates the fiber and hydrolyzes or reacts with the absorbed water to form insoluble metal oxide products.
- the metal oxide product remains in the fiber matrix without greatly disturbing the fibrous character of the rayon.
- the extent or amount of metal deposited within the fiber is directly a function of the amount of water absorbed in the rayon.
- the amount of water absorbed in the rayon fibers is readily controlled by exposing the fibers to air containing the desired amount of moisture. For maximum water absorption the rayon fibers may be immersed directly in liquid water. The amount of water absorbed in textilegrade viscose rayon in equilibrium with moisture in air and liquid water at 75 F. is shown below:
- Some hydrolyzable metal compounds are liquid at nor mal conditions and the H O-laden rayon may be immersed directly in the metal compound to cause the hydrolysis product to be formed in the fiber.
- Examples of liquids are SiC1 TiC1 VOCl VC1
- many of the hydrolysis reactions proceed very rapidly with the evolution of heat. The resulting severe conditions may degrade or break up the fibers; in this event the metal compound is preferably diluted with a non-reactive, miscible liquid to avoid such conditions.
- non-polar organic liquids such as benzene, toluene, hexane, carbon tetrachloride, chloroform
- these organic liquids when used as diluents for the metal compounds, slow the rates of hydrolysis and help to dissipate the heat of reaction. Unreacted metal compound liquid (as well as any diluent) may be removed from between the fibers by evaporation, since they have high vapor pressures.
- metal compounds which can be incorporated in fibers, films, and the like, by hydrolysis reaction but are not normally liquids are best utilized When dissolved in a non-reactive liquid, which is immiscible with water.
- metal compounds for example, include TaC1 NbCl ZrC1 UC1 Suitable solvents are bromoform, carbon tetrachloride, diethyl ether, and nitrobenzene.
- the metal compound-imbibed organic polymer is then thoroughly dried by any convenient means, such as air drying or heating in a stream of warm gas at a temperature not exceeding 70 C. It is desirable to dry the ploymer rapidly (in about one hour or less) to prevent expulsion of the metal compound from the interior of the organic polymer to its surface.
- the organic polymer is imbibed with compounds containing all of thedesired metals.
- the imbibition can be carried out by a single immersion in an aqueous solution containing both salts.
- a preferred method is to imbibe first with the hydrolysis product and then with the water soluble salt.
- the metal compound-imbibed organic polymer is heated under controlled conditions, namely: (1) to a temperature of at least 250 C., (2) at a rate sutficiently low to evolve volatile decomposition products of the polymer without destroying the polymer integrity, (3) for a sutficient duration to decompose the organic structure of said polymer and form a carbonaceous relic containing the metal compound in finely dispersed form.
- the metal compound-imbibed polymer It is necessary to heat the metal compound-imbibed polymer at a rate sutficiently low to avoid ignition of the polymer. If the organic polymer burns instead of carbonizes, the metal compound temperature rises execessively, due to its contiguous relation to the organic structure. Under such circumstances it is impossible to control the temperature, and the melting point of intermediate metal compounds formed may be exceeded or excessive crystallization and grain growth occurs. Also, the metal compound may be suspended in the organic compound vapors, and thus lost from the environment and unavailable to form the desired relic. Also, when ignition is avoided the product shaped articles, fibers, and textiles have smoother surfaces, are more free to bend, and are stronger.
- the first heating step is normally performed in a nonoxidizing inert atmosphere, as for example that provided by nitrogen, helium, argon, neon and the like, or a vacuum. However, if it is desirable to reduce the quantity of carbon remaining from the polymer pyrolysis step, a portion or all of this first heating step may be performed in an oxygen-containing atmosphere, perferably with between about 5 and about 25 volume percent oxidizinggas.
- the balance of the gaseous atmosphere comprises gasses which are chemically non-reactive with the environment, as for example the previously mentioned inert gases. In the event that an oxygen-containing gas is used, a portion of the carbon is removed as a carbon-containing gas through reaction with the oxidizing gas (volatilized).
- Oxidation provides a method for reducing the carbon content of the polymer relic, and controlling the molar ratio of carbon-to-metal for the ensuing carburization reaction.
- pyrolysis of cellulose yields about four moles of carbon per mole cellulose as a residue, and the molar ratio of carbon to metal needed for a stoichimetric carburization reaction is between about 3/1 and 7/4.
- the heating rate is affected by the environment whether inert or oxidizing, the latter being more diflicult to control.
- the heating rate may be at least C. per hour or higher, as long as polymer ignition is avoided. It is preferred to heat the polymer at a rate between 10 C. per hour and 100 C. per hour in an atmosphere containing from 5 to 25 volume percent oxygen, although higher heating rates may be satisfactory with effective means for venting the carboncontaining gas. Higher oxygen concentrations may be suitable, particularly during the later portion of the first heating step.
- the preferred oxidizing gas is oxygen, although other oxidizing gases such as nitrogen dioxide and sulphur trioXide can be used if desired.
- the carbonized organic polymer comprises predominantly carbon but also can include small amounts of residual oxygen and hydrogen. If the heating continues and in an oxidizing atmosphere, oxidation of the carbon becomes the predominant reaction.
- the relic from the first heating-pyrolysis step is further heated to a temperature between about 1000 C. and 2000 C. in a non-oxidizing atmosphere to react the metal with the carbonaceous relic to form a metal carbide fiber, textile, or shaped article.
- the non-oxidizing atmosphere may be a vacuum, an inert gas as for example nitrogen, helium, or argon, or alternatively a reducing gas such as hydrogen or a hydrocarbon.
- a carburization temperature of at least about 1000. C. is necessary to form a crystalline structure, which in turn provides a high-strength product. That is, the tensile strength of the metal carbide products of this invention is greater than 100,000 lbs. per square inch. It is desirable to limit the carburization temperature and time duration to achieve minimum grain size wihin the article. When producing fibers, crystal grain sizes of less than 0.2 of the fiber diameter are preferred. Larger crystal grain sizes reduce the fiber strength and flexibility.
- the rate of heating in the carburization step is not critical; rates of between about 200 C. per hour and 1000 C. per hour have been found suitable, although higher rates canbe em ployed. Similarly the overall duration of the carburization step is not critical, and periods of between about 1 and 4 hours may be employed for a batch process, while much shorter times can be employed in a continuous process.
- any metal forming a stable carbide may be used to practice the invention.
- the preferred carburization conditions in terms of reaction temperature and molar ratios will of course very somewhat depending on the selected metal. It has been pointed out that in general the molar ratio of carbon to metal for a stoichiometric reaction is between about 3/1 and 7/4.
- the fibers should be either on and/or continuous within the geometrical shape of the structure because the loading to the embedded fibers is accomplished via a shear transfer process at the matrix-fiber interface. Since the shear strength of polymers is low, a greater transfer length (i.e., on fibers) is necessary if the fibers are to carry the major portion of the load.
- Short fiber-reinforced plastics generally show tensile strengths of about 50,000 p.s.i., whereas thesame polymers reinforced with continuous fibers may exhibit strengths of 250,000 p.s.i. or greater.
- Boron carbide (B C) and silicon carbide (SiC) continuous filament yarns prepared by the present invention are particularly suitable for composite reinforcement.
- these metal carbide fibers may be prepared in the form of cloth and continuous .yarn, they may be used in filament winding of composite structures.
- the metal carbide fibers, textiles, and shaped articles of the invention are generally useful in high temperature insulation, corrosion-resistant articles, and the like.
- the process of the invention employs a preformed? organic polymeric material.
- preformed means that the organic polymeric material has been fabricated into a fibrous or non-fibrous shape prior to impregnation with the metal compound.
- the metal carbide fibers of this invention have numer- I-Iydrolysis of 81014 SiOz+3C- S1C+2CO
- the metal carbide shapes of this invention have a wide variety of uses. Metal carbide shapes prepared from,organic foams or sponges are also useful as filters.
- the metal carbide shapes of this invention be prepared from cellulosic foams or sponges characterized by open porosity, uniform pore size and low density.
- the metal carbide films of this invention are sheets which are highly uniform in thickness and which can be as 10 microns. 1
- Example L+UC fibers 100ml. of 4.2 molar'UO Cl solution. After ten minutes immersion in the solution, the fibers were removed and centrifuged toremove excess solution. The fibers contained 3.3 grams of solution per gram of rayon. They were dried in a warm air stream and after drying weighed 22.2 grams, including 1.57 grams imbided uranium per gram rayon. These fibers were next placed in a tube-type furnace and heated in a vacuum of about 1 micron Hg at a rate of C./hour to 900 C. The furnace was then allowed to cool to room temperature under the vacuum. The resulting carbonaceous fiber relic weighed 14.9 grams and contained finely dispersed uranium with a carbon-to-uranium atom ratio of 3.7. The fibers were black lustrous and strong; there was no fiber breakage.
- These carbonaceous fiber relics had approximately the correct carbon-to-uranium ratio for producing monouranium carbide fibers by heating to temperatures of about 1500-2000 C. in a nonoxidizing atmosphere.
- UC fibers by the reaction UO +3C UC+2CO can be prepared by heating uranium impregnated rayon fibers to about 1700 C. and maintaining this temperature level for a period of 1 hour in an argon atmosphere.
- Example 2.WC fiber cloth The solution used for imbibing was made by dissolving 400 grams ofammonium paratungstate in 400 ml. of 30% hydrogen peroxide solution. The solution was heated to 6070 C. at which temperature the ammonium paratungstate reacted with the hydrogen peroxide and dissolved in 510 minutes. The clear solution was then rapidly cooled to room temperature and contained 655 grams of tungsten per liter, with a specific gravity of 1.82 gms./cc. and a pH of 1.1. The rayon cloth was of 5 harness satin weave in both fill and warp directions using a textile grade viscose rayon yarn (1650 denier/ 720 filament), the cloth weight being ounces per square yard.
- the cloth was converted to the tungsten carbide form by first heating in air at a rate of C./hour to 300 C. and maintaining this temperature for four hours. The cloth was then further heated at a rate of 50 C./ hour until 350 C. was reached and this temperature was maintained for four hours, thereby forming the carbonaceous fiber relic containing finely divided tungstein in dispersed form. The air in the tube furnace was then purged with nitrogen before the carburization reaction commenced. Dry hydrogen gas was passed through the furnace at a rate of 4 liters/minute (SPT) as the cloth was heated to 600 C. within 30 minutes and held at 600 C. for one hour, then heated to 1000 C. and held there for an hour. During the pyrolysis and carburization steps the cloth shrank from 6 inches x 18 inches to 3 inches x 10 inches. The weight of the tungsten carbide cloth was 73% of the weight of the starting rayon cloth.
- SPT 4 liters/minute
- the cloth was composed chiefly of highly crystalline tungsten carbide (WC), (i.e. at least 80 wt. percent) and a trace of tungsten metal.
- WC highly crystalline tungsten carbide
- Fiber diameter 5-6 microns.
- Example 3 ZrC fibers
- the starting rayorrfibers were 1.5 denier viscose tow (133,000 continuous filaments in the tow).
- the tow weighing 6.8 grams was preswol len in water for 15 minutes prior to immersion in 2.84 molar ZrOCl solution for four hours. It was next centrifuged of unimbibed solution from between the fibers and dried in air.
- the saltloaded rayon tow weighed 12.5 grams and contained 0.84 gram zirconium salt per gram rayon.
- the tow was placed in a tube furnace and heated under a vacuum of 110 microns Hg pressure at a rate of 50 C./hr. to 400 C. then 100 C./Hr. to 1000 C.
- the pyrolyzed fibers were black, had a high luster and weighed 6.0 gms.
- the fiber relics contained 33.7% carbon and 43.0% zirconium by weight.
- the fiber relics were placed in a graphite crucible and heated at 1900 C. for two hours in a hydrogen atmosphere employing a high frequency induction furnace.
- the resulting fibers weighed 4.2 gms., had a black-gray color, showed no evidence of sintering together and had a diameter of 4-5 microns. They were very flexible and had a tensile strength between 100,000 and 150,000 p.s.i.
- the fibers were electrically conductive and X-ray powder dilfraction patterns showed the fibers to be composed of polycrystalline face-centeredcubic zirconium carbide (ZrC). No graphite lines were evident in the X-ray patterns.
- the fibres were over 1 foot long with crystal grain size of less than 0.2 micron.
- Example 4TiC fibers A one-foot length of 9.0 denier viscose rayon tow (22,000 continuous filaments in the tow) was immersed in a 1.6 molar TiC1 aqueous solution for four hours. The tow was blotted of unimbibed solution and dried. The rayon tow containing the TiCl salt was pyrolyzed and carburized in the same manner as described in Example 3. The product fibers were grayish-black, flexible, and had a diameter of 12-15 microns. The only crystalline phase present in the fibers as indicated by X-ray diffraction powder analysis was the face-centered-cubic titanium carbide (TiC). The crystal grain size was less than 0.5 micron and thus, less than 0.2 of the fiber diameter. Fibers of TiC having lengths of 50 feet have been prepared by the same method.
- Example 5 Example 5.-B C fibers A one-foot length of 20 denier viscose rayon two (10,000 continuous filaments in the tow) was immersed in an aqueous solution containing 25% by weight boric acid for one hour. The solution was kept at C. during the imbibment to keep the boric acid in solution. The two was then centrifuged while still hot to remove unimbibed boric acid from between the fibers. After drying the two in air it was subjected to the same pyrolysis and carburization treatment as described in Example 3.
- the reacted fibers were black, free from each other, had appreciable flexibility and strength.
- X-ray diffraction analysis showed the fibers to be composed of crystalline boron carbide (B C).
- the fiber diameter was about 20 microns and the crystal grain size was less than 0.2 of such diameter.
- Example 6 SiC fibers A length of 20 denier viscose rayon tow (10,000 continuous filaments in the tow) 23-inches long and weighing 13.3 grams was immersed in silicon tetrachloride liquid for 30 minutes. Prior to immersion, the two contained 1.4 gms. of absorbed water. After 30 minutes immersion reaction between the silicon tetrachloride and the water in the rayon was complete as indicated by the subsiding of HCl gas evolution from the fibers. The tow was freed of excess silicon tetrachloride by evaporation. The tow then weighed 15 gms. and contained 3.1 grams of silica. The silicon-loaded rayon two was pyrolized and carburized in the same manner as described in Example 3.
- the product fibers had a metallic luster, weighed 3.9 gms., and were characterized by appreciable flexibility and strength.
- X-ray diffraction pattern'analysis indicated a mixture of crysalline SiC and graphite.
- the fiber diameter was about 20 microns and the crystal grain size less than 0.5 micron.
- a process for producing crystalline metal carbide fibers, textiles, and shaped articles which comprises:
- step (e) further heating the relic from first heating step (d) to a temperature in the range of about 1000"- 2000 C. in a non-oxidizing atmosphere to react said metal with said carbonaceous relic to form a metal carbide article.
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Description
PROCESS FOR PRODUCING METAL CARBIDE FIBERS, TEXTILES AND SHAPES Bernard H. Hamling, Warwick, N.Y., assignor to Union Carbide Corporation, a corporation of New York No Drawing. Continuation-impart of applications Ser. N 0. 451,326, Apr. 27, 1965, Ser. No. 522,380, Jan. 24, 1966, Ser. No. 523,549, Jan. 28, 1966, and Ser. No. 576,840, Sept. 2, 1966. This application Dec. 19, 1966, Ser. No.
8 Claims. (Cl. 23-344) ABSTRACT OF THE DISCLOSURE This application is a continuation-in-part of Ser. No. 451,326 filed Apr. 27, 1965, Ser. No. 522,380, filed Jan. 24, 1966, Ser. No. 523,549, filed Jan. 28, 1966, and Ser. No. 576,840, filed Sept. 2, 1966, all by B. H. Hamling. The foregoing applications were all continuationsin-part of Ser. No. 320,843. Ser. Nos. 320,843; 451,326; 522,380 and 523,549 are now abandoned.
This invention relates to fibers, textiles, and shaped articles composed of metal carbides and to a process for producing such fibers, textiles, and shaped articles.
The prior art has prepared certain metal carbide fibers by a number of methods, but each is characterized by important limitations. For example, silicon carbide has been crystallized in a liquid system, but this procedure requires high pressures and/or high temperatures. In the whisker method, fibers are formed from the vapor phase or by electrolysis of molten salt. This method produces fibers which are often irregularly matted, kinked and very closely spaced. Moreover, metal carbide fibers made by the whisker method are characterized by distortions, and relatively short (below 0.25 inch). It has heretofore been impossible to reproduceably prepare flexible metal carbide fibers having a length-to-diameter ratio over 400, characterized by high strength at high temperatures.
On the other hand, it is widely recognized that such fibers would represent an approach to the upper limit for strength-to-weight ratio for a given material, due to the cohesive forces of adjacent atoms. It has been estimated that the weight of pressure vessels reinforced with high strength metal carbide fibers could be on the order of one-seventh that of conventional pressure vessels for high temperature uses.
Heretofore, also, there has been no completely satisfactory method for producing metal carbide articles of predetermined irregular or complicated shapes. Previous methods have involved machining or other shaping techniques, or in the case of foams, the use of various blowing agents. The methods were either difficult and complicated or were unable to provide close control over the final shape of the article.
It is an object of this invention to provide shaped metal carbide articles. Another object of the invention nited States Patent O is to provide a method for producing such articles from non-fibrous organic material. Still another object is to provide a variety of films, tubes, cups and other shapes which are composed of microcrystallinemetal carbides.
It is also an object of this invention to provide an improved method for producing metalcarbide fibers of small diameters of less than about 30 microns, which is re produceable.
Another object is to provide'such a method in'which the metal carbide fibers are of uniform diameter, straight, smooth surfaced and free of distortions.
A further obpect is to provide metal carbide fibers of less than about 30 microns diameter having a length-todiameter ratio over 400, which are flexible and charac terized by high strength at high temperatures.
A still further object is to provide a variety of textile forms, including staple fibers, continuous tow and yarns, woven fabrics, batting and felts, composed of metal carbide fibers.
These and other objects and advantages of the present invention will be apparent from the following description and appended claims.
One aspect of the novel process comprises first providing a compound of a metal dissolved in a solvent, and immersing a preformed organic polymeric material in the resulting solution thereby swelling and opening the organic material interstices such that the metal compound is imbibed or absorbed in the interstices. The unimbibed metal compound is then removed from the organic material outer surfaces and the metal compoundim-bibed material is dried. Next, the latter is first heated to temperature of at least 250 C. at a rate sufliciently low to evolve volatile decomposition products of the organic material without destroying the intergrity of this polymeric material. This pyrolysis step is continued for a sufficient duration to decompose the organic structure of the polymeric material and form a carbonaceous relic containing the metal in finely dispersed form. In the final carburization step, the relic is further heated from the pyrolysis step to temperature of about 1000-2000 C. in a non-oxidizing atmosphere to react the imbibed metal with the carbonaceous organic polymer relic to form a metal carbide shape, fiber, or textile. The non-oxidizing atmosphere of the carburization step may for example be that of an inert gas, hydrogen, or hydrocarbon reducing gas, vacuum or a combination of any of these atmospheres, There results a metal carbide shaped article which has essentially the same physical shape as the original preformed organic polymeric material, although the dimensions may be reduced by as much as about 40 to 6 percent.
Although I do not wish to be bound by same, the theory and mechanism of this process appears to be as follows: Microscopically, organic polymers such as rayon fiber are composed of extremely small crystallites of cellulosic chains (micelles or microfibrils) held together in a matrix of amorphous cellulose. The crystallites, approximately 40 Angstrom units (A.) in diameter and 250 A. long in high tenacity rayon yarns, are parallel to the axis of the rayon fiber and are spaced approximately 20 A. apart in the dry state. A one-denier fiber (1 gram weight per 9000 meters of length) has several million crystallites in its cross-section. When the fiber is immersed in a solvent such as water or aqueous solutions, it swells laterally opening the interstices, the amorphous regions enlarge and the crystallite spacing becomes approximately 50 A. (in the case of rayon). The dissolved selected metal compound such as a salt enters the swollen amorphous regions, which is about of the volume of the swollen rayon, and becomes trapped in the amorphous regions between the crystallites when the solvent is evaporated from the fibers.
The metal compounds do not crystallize upon drying of theorganic polymer, as would normally occur upon drying a solution, since they are effectively suspended and separated as islands about 50 A. in size between the crystallites.
The organic polymers may be imbibed with two or more metal compounds from the same solvent solution, so that carbides of more than one metal may be prepared, e.g. tungsten carbide and zirconium carbide. In the first approximation, most metal compounds enter the polymer interstices in direct, proportion to their solution concentration, allowing ready control of the relative loadings of metal compounds in the preformed organic polymer. Due to the blocking action of the organic crystallites, the metal compounds cannot segregate from each other nor crystallize during the drying and heat conversion steps. Since they are finely dispersed, the metal compounds and later the oxides and carbides are extremely reactive and can be made to undergo the necessary chemical reactions to form the desired metal carbide alloy product at lower temperatures than normally required by conventional coprecipitation or powder blending methods for preparing such mixtures.
Any organic polymeric material can be employed as a starting material in the process of this invention providing it is characterized by the above-described sequence of extremely small crystallites held together in a matrix of amorphous regions which enlarge and admit the metal compounds on immersion in the solvent. Any class of materials which are composed of long-chain molecules held together by chemical cross-links may also be used. Any cellulosic material can be employed including rayon, cellophane, saponified cellulose acetate, cotton, wood and ramie. Other suitable organic materials include the protein fibers (wool and silk) and the man-made acrylics, polyesters, vinyls and polyurethanes. Certain organic materials such as polyethylene and polypropylene are not suitable for practicing the instant process because they cannot be swollen for imbibition of the metal compounds and/or the materials melt and lose their structure during pyrolysis. A preferred cellulosic material is rayon due to its structural uniformity, good imbibition characteristics and low impurity content.
The physical form of the elemental metal carbide composition is essentially the same as and is determined by the physical form of the organic polymer starting material. During conversion of the metal compound-imbibed organic fiber, for example, to the metal carbide fiber, the length of the fiber shrinks to approximately 40 to 60 percent and the diameter to 25 to 35 percent of the original dimensions. Similar shrinkage in all dimensions also occurs with the non-fibrous shapes. Where a yarn composed of a multiplicity of continuous-length metal carbide fibers is desired, a continuous-filament organic yarn is employed as the starting material in the process of this invention. Similarly, where a woven fabric or felt composed of metal carbide fibers is desired, a woven organic fiber cloth or felt can be used as the starting material. Of course, metal carbide woven textiles can be made using conventional textile equipment and techniques starting with metal carbide staple fibers or yarns made by the process of this invention.
In order to obtain adequate tensile strength in the final metal carbide fiber product, cellulosic materials are imbibed with the metal compounds to the extent of at least one-quarter mole and preferably 1.0-2.0 moles of the metal compound(s) in each base mole of cellulose. The term base mole, as used herein refers to the molecular weight of a glycosidic unit of the cellulose chain (molecular weight of 162). With non-cellulosic materials, the degree of imbibition should be at least 0.1 and preferably 0.5-1.0 gram-equivalent metal ion in the metal compound imbibing solution per gram organic polymer. With lower concentrations of metal compound(s), insufficient metal salt is available in the relic to form a strong article and the process becomes less efficient in terms of metal carbide yield per unit weight of preformed organic polymer starting material. Another disadvantage of low metal compound concentrations is that more drastic oxidation conditions are necessary to achieve pyrolysis.
Imbibition or impregnation of the organic material can be carried out by several methods. Where the metal element which will appear in the final metal carbide fiber has salts which are highly soluble in water, the imbibition step can be carried out by immersing the organic material in a concentrated aqueous solution of such salt. For example, where a ZrC fiber is desired, the organic fiber can be imbibed by immersion in an aqueous solution of zirconyl chloride or zirconyl nitrate having concentrations in the range of 2.5 to 3.0 moles per liter. For salts which hydrolyze extensively (acid reaction) when dissolved in water, the acidity of the impregnating solution is preferably not greater than 1.0 molar (in hydrogen ion) in order to prevent degradation of the organic fiber during immersion. The acid may be neutralized with ammonia, if desired.
Pre-swelling the cellulosic organic polymers in water prior to immersion in concentrated imbibing solutions is preferably employed to increase both the rate and extent of salt imbibition. Water is also suitable for swelling protein materials. For acrylic and polyester polymers, aromatic alcohols are suitable swelling agents, and the ketones are useful in swelling vinyl and polyurethane polymers for the same purpose.
Water is the preferred solvent for metal compoundimbibing of cellulosic and protein materials such as wool and silk. Other solvents such as alcohols do not afford as efficient swelling of the polymers nor solubility of the selected metal compound for a high degree of imbibing. For vinyl and polyurethane polymers, esters and ketones are appropriate solvents, as for example normal butyl acetate or methyl ethyl ketone. For acrylic and polyester polymers, suitable solvents for the metal compound imbibition include aromatic alcohols and amines such as aniline, nitro-phenol, meta-cresol and paraphenylphenol.
Immersion times at normal temperatures (2l23 C.) required to give adequate imbibition vary from 30 minutes to several days depending on the salt(s) employed and the type of organic polymer employed. Immersion times greater than about 3 days in concentrated salt solutions are undesirable for fibers since the organic fiber may degrade, resulting in a decrease in amount of metal compound absorbed and causing the polymers to bond to each other. When it is desired to increase the rate of imbibition of the metal compound in the organic polymer to shorten the immersion time, the metal compound solution may be heated to as high as C.
One method of impregnating rayon fibers and other cellulosic fibers and films with certain important metals is to absorb water into rayon and then contact the rayon with a compound of the metal so that it penetrates the fiber and hydrolyzes or reacts with the absorbed water to form insoluble metal oxide products. The metal oxide product remains in the fiber matrix without greatly disturbing the fibrous character of the rayon. The extent or amount of metal deposited within the fiber is directly a function of the amount of water absorbed in the rayon.
Typical hydrolsis reactions are described by the following reactions:
The amount of water absorbed in the rayon fibers is readily controlled by exposing the fibers to air containing the desired amount of moisture. For maximum water absorption the rayon fibers may be immersed directly in liquid water. The amount of water absorbed in textilegrade viscose rayon in equilibrium with moisture in air and liquid water at 75 F. is shown below:
Relative humidity Moisture content, percent at 75 F.: of dry fiber weight 4 100 (immersed in water) 80110 Some hydrolyzable metal compounds are liquid at nor mal conditions and the H O-laden rayon may be immersed directly in the metal compound to cause the hydrolysis product to be formed in the fiber. Examples of liquids are SiC1 TiC1 VOCl VC1 However, many of the hydrolysis reactions proceed very rapidly with the evolution of heat. The resulting severe conditions may degrade or break up the fibers; in this event the metal compound is preferably diluted with a non-reactive, miscible liquid to avoid such conditions. Many non-polar organic liquids, such as benzene, toluene, hexane, carbon tetrachloride, chloroform, are suitable non-reactive liquids. These organic liquids, when used as diluents for the metal compounds, slow the rates of hydrolysis and help to dissipate the heat of reaction. Unreacted metal compound liquid (as well as any diluent) may be removed from between the fibers by evaporation, since they have high vapor pressures.
Other metal compounds which can be incorporated in fibers, films, and the like, by hydrolysis reaction but are not normally liquids are best utilized When dissolved in a non-reactive liquid, which is immiscible with water. Such metal compounds, for example, include TaC1 NbCl ZrC1 UC1 Suitable solvents are bromoform, carbon tetrachloride, diethyl ether, and nitrobenzene.
Following imbibition with metal compound(s) from a solvent solution, it is necessary to remove excess solution from between the organic fibers before they dry in order to avoid bonding together of fibers by caked salt. Allowing excess unimbibed metal or hydrolysis product to remain on the fibers results in reduced strength and increased brittleness in the final metal carbide fiber product. For most cases, blotting thoroughly with absorbent paper or cloth using moderate pressure is sufficient for removing excess solution from the fibers. In addition, vacuum filtration and centrifugation have proven to be effective methods for removing excess solution from between the fibers. Raising the temperature of the wet fibers to 50-60 C. aids in removing excess solution from the fibers during blotting, vacuum filtration or centrifugation.
The metal compound-imbibed organic polymer is then thoroughly dried by any convenient means, such as air drying or heating in a stream of warm gas at a temperature not exceeding 70 C. It is desirable to dry the ploymer rapidly (in about one hour or less) to prevent expulsion of the metal compound from the interior of the organic polymer to its surface.
When a product containing two or more metal carbides is desired, the organic polymer is imbibed with compounds containing all of thedesired metals. For example, if two or more water-soluble salts are employed, the imbibition can be carried out by a single immersion in an aqueous solution containing both salts. When two metals are de-. sired, one of which is imbibed in organic polymers from aqueous solution and the second imbibed by hydrolysis of the metal halide or oxylhalide from organic solution, a preferred method is to imbibe first with the hydrolysis product and then with the water soluble salt.
In the next step of the process of this invention (decomposition of the organic polymer structure), the metal compound-imbibed organic polymer is heated under controlled conditions, namely: (1) to a temperature of at least 250 C., (2) at a rate sutficiently low to evolve volatile decomposition products of the polymer without destroying the polymer integrity, (3) for a sutficient duration to decompose the organic structure of said polymer and form a carbonaceous relic containing the metal compound in finely dispersed form.
It is necessary to heat the metal compound-imbibed polymer at a rate sutficiently low to avoid ignition of the polymer. If the organic polymer burns instead of carbonizes, the metal compound temperature rises execessively, due to its contiguous relation to the organic structure. Under such circumstances it is impossible to control the temperature, and the melting point of intermediate metal compounds formed may be exceeded or excessive crystallization and grain growth occurs. Also, the metal compound may be suspended in the organic compound vapors, and thus lost from the environment and unavailable to form the desired relic. Also, when ignition is avoided the product shaped articles, fibers, and textiles have smoother surfaces, are more free to bend, and are stronger. That is, very rapid heating and expulsion of the decomposition gases causes polymer continuity to be broken and results in excessive crystallization of the metal salt or oxide within the polymer relic which in the final analysis do not yield as smooth, flexible and strong metal carbide products as the unignited amorphous or poorly-crystalline, more dense intermediate metal oxide.
The first heating step is normally performed in a nonoxidizing inert atmosphere, as for example that provided by nitrogen, helium, argon, neon and the like, or a vacuum. However, if it is desirable to reduce the quantity of carbon remaining from the polymer pyrolysis step, a portion or all of this first heating step may be performed in an oxygen-containing atmosphere, perferably with between about 5 and about 25 volume percent oxidizinggas. The balance of the gaseous atmosphere comprises gasses which are chemically non-reactive with the environment, as for example the previously mentioned inert gases. In the event that an oxygen-containing gas is used, a portion of the carbon is removed as a carbon-containing gas through reaction with the oxidizing gas (volatilized). Oxidation provides a method for reducing the carbon content of the polymer relic, and controlling the molar ratio of carbon-to-metal for the ensuing carburization reaction. In general, pyrolysis of cellulose yields about four moles of carbon per mole cellulose as a residue, and the molar ratio of carbon to metal needed for a stoichimetric carburization reaction is between about 3/1 and 7/4.
The heating rate is affected by the environment whether inert or oxidizing, the latter being more diflicult to control. In an oxidizing atmosphere the heating rate may be at least C. per hour or higher, as long as polymer ignition is avoided. It is preferred to heat the polymer at a rate between 10 C. per hour and 100 C. per hour in an atmosphere containing from 5 to 25 volume percent oxygen, although higher heating rates may be satisfactory with effective means for venting the carboncontaining gas. Higher oxygen concentrations may be suitable, particularly during the later portion of the first heating step. The preferred oxidizing gas is oxygen, although other oxidizing gases such as nitrogen dioxide and sulphur trioXide can be used if desired.
When heating of the imbibed polymer is first begun (even in an oxidizing atmosphere), pyrolysis of the polymer to carbon is the predominant chemical reaction. The carbonized organic polymer comprises predominantly carbon but also can include small amounts of residual oxygen and hydrogen. If the heating continues and in an oxidizing atmosphere, oxidation of the carbon becomes the predominant reaction.
In the final process step of this invention, the relic from the first heating-pyrolysis step is further heated to a temperature between about 1000 C. and 2000 C. in a non-oxidizing atmosphere to react the metal with the carbonaceous relic to form a metal carbide fiber, textile, or shaped article. the non-oxidizing atmosphere may be a vacuum, an inert gas as for example nitrogen, helium, or argon, or alternatively a reducing gas such as hydrogen or a hydrocarbon.
A carburization temperature of at least about 1000. C. is necessary to form a crystalline structure, which in turn provides a high-strength product. That is, the tensile strength of the metal carbide products of this invention is greater than 100,000 lbs. per square inch. It is desirable to limit the carburization temperature and time duration to achieve minimum grain size wihin the article. When producing fibers, crystal grain sizes of less than 0.2 of the fiber diameter are preferred. Larger crystal grain sizes reduce the fiber strength and flexibility. The rate of heating in the carburization step is not critical; rates of between about 200 C. per hour and 1000 C. per hour have been found suitable, although higher rates canbe em ployed. Similarly the overall duration of the carburization step is not critical, and periods of between about 1 and 4 hours may be employed for a batch process, while much shorter times can be employed in a continuous process.
As previously indicated, any metal forming a stable carbide may be used to practice the invention. The preferred carburization conditions in terms of reaction temperature and molar ratios will of course very somewhat depending on the selected metal. It has been pointed out that in general the molar ratio of carbon to metal for a stoichiometric reaction is between about 3/1 and 7/4.
ous uses. For example they may be employed for reinforcing plastics for use at relatively low temperatures, and reinforcing metals and ceramics bodies at high temperatures, particularly where high strength, high Youngs modulus, and low weight characteristics are desired. To reinforce plastics, the fibers should be either on and/or continuous within the geometrical shape of the structure because the loading to the embedded fibers is accomplished via a shear transfer process at the matrix-fiber interface. Since the shear strength of polymers is low, a greater transfer length (i.e., on fibers) is necessary if the fibers are to carry the major portion of the load. Short fiber-reinforced plastics generally show tensile strengths of about 50,000 p.s.i., whereas thesame polymers reinforced with continuous fibers may exhibit strengths of 250,000 p.s.i. or greater. Boron carbide (B C) and silicon carbide (SiC) continuous filament yarns prepared by the present invention are particularly suitable for composite reinforcement.
Since these metal carbide fibers may be prepared in the form of cloth and continuous .yarn, they may be used in filament winding of composite structures.
The metal carbide fibers, textiles, and shaped articles of the invention are generally useful in high temperature insulation, corrosion-resistant articles, and the like.
The process of the invention employs a preformed? organic polymeric material. The term preformed means that the organic polymeric material has been fabricated into a fibrous or non-fibrous shape prior to impregnation with the metal compound.
TABLE L-PREPARATION OF MEIEAL CARBIDE FIBERS BY CARBURIZATION OF IMPRE G- ATED RAYON FIBERS carburiza- Metal Melting Preferred impregnation method carburization reactions tion reaction carbide point, FJ temperatures, C.
5, 685= =160 T1013 aqueous soln TiO2+3C-TiC+2CO 1, TOO-2,1C 5, 750 ZIOC]: aqueous soln ZrO +3C-ZrC+2CO.. 1,8G(%2,2(0 7, 030 H 0012 aqueous soln HfOQ+3C HlC+2CO 1, 900-2, 300 5, 160 VCflRagFeous soln. or hydrolysis V;O;+5C 2VC+3CO 1, 100-1, 200
0 I 4. 6, 330*230 Hydraglysis of NbCls from ether Nb2O +5C 2NbC+3CO 1, 300 1, 460
so n 1011. 7, 015 Hydrtalysis of TaCl from ether TazOs+7C- 2TaC+5CO 1, 300-1, 500 so u ion. 7 1 3, 320 3, 435 CrCl; aqueous soln 3Cr2O3+13C 2CfsC2-i-QCO 1, 400-1, 500 4, 650 (N H4)2M0O4 aqueous soln 2MoO2+5C- M0;C+4CO 1, CCU-1,400 4,875 9o M0O2+3C-*M0C+2C0. 1, CCU-1,400 5,180 90 2WOz+5C W-.C+4CO 1, 000-1, 400
5, 200=+=90 o WOz+3C-WC+2CO 1, 000-1,460 4, 130-4, 350 UO CIZ aqueous soln- UO2+3C UC+2CO 1, 200-2, 000 4 350 o UOZ+4C UCZ+2CO 1, 200-2, 000 ThCli aqueous soln. ThOz+3CThC+2CO 1, 300-2, 400 o Th0z+4C ThC2+3C0. 1 0002,400 P110012 aqueous soln PuO2-l-3C- PuC+3CO 1 200-2, (:00 o PuOz+4C PuC2+3CO 1,2002,000 H3BO aqueous soln. 2B2O3+7C- B4C+6CO. 1 200-2, 000 A101; aqueous soln-.. 2AlzO3+9C Al4C3l-6CO 1 4001 00 1 From various literaturelsourees.
include those from Group IV-B (titanium, zirconium,
hafnium), Group V-B (vanadium, niobium, and tantalum), and Group VI-B (chromium, molybdenum, and tungsten) of the Periodic Table, as well as boron, aluminum, silicon, thorium, uranium, and plutonium. Table 1, below, lists preferred impregnation methods and carburization temperatures for the preparation of these metal carbides using rayon fibers.
The metal carbide fibers of this invention have numer- I-Iydrolysis of 81014 SiOz+3C- S1C+2CO The metal carbide shapes of this invention have a wide variety of uses. Metal carbide shapes prepared from,organic foams or sponges are also useful as filters.
For use as filters itis preferred that the metal carbide shapes of this invention be prepared from cellulosic foams or sponges characterized by open porosity, uniform pore size and low density.
The metal carbide films of this invention are sheets which are highly uniform in thickness and which can be as 10 microns. 1
The following Examples 1-6 illustrate the process for preparing crystalline metal carbide products according to this invention.'
Example L+UC fibers 100ml. of 4.2 molar'UO Cl solution. After ten minutes immersion in the solution, the fibers were removed and centrifuged toremove excess solution. The fibers contained 3.3 grams of solution per gram of rayon. They were dried in a warm air stream and after drying weighed 22.2 grams, including 1.57 grams imbided uranium per gram rayon. These fibers were next placed in a tube-type furnace and heated in a vacuum of about 1 micron Hg at a rate of C./hour to 900 C. The furnace was then allowed to cool to room temperature under the vacuum. The resulting carbonaceous fiber relic weighed 14.9 grams and contained finely dispersed uranium with a carbon-to-uranium atom ratio of 3.7. The fibers were black lustrous and strong; there was no fiber breakage.
These carbonaceous fiber relics had approximately the correct carbon-to-uranium ratio for producing monouranium carbide fibers by heating to temperatures of about 1500-2000 C. in a nonoxidizing atmosphere. For example, UC fibers by the reaction UO +3C UC+2CO can be prepared by heating uranium impregnated rayon fibers to about 1700 C. and maintaining this temperature level for a period of 1 hour in an argon atmosphere.
Example 2.WC fiber cloth The solution used for imbibing was made by dissolving 400 grams ofammonium paratungstate in 400 ml. of 30% hydrogen peroxide solution. The solution was heated to 6070 C. at which temperature the ammonium paratungstate reacted with the hydrogen peroxide and dissolved in 510 minutes. The clear solution was then rapidly cooled to room temperature and contained 655 grams of tungsten per liter, with a specific gravity of 1.82 gms./cc. and a pH of 1.1. The rayon cloth was of 5 harness satin weave in both fill and warp directions using a textile grade viscose rayon yarn (1650 denier/ 720 filament), the cloth weight being ounces per square yard. A 6 inch x 18 inch piece of cloth weighing 35.6 grams was immersed in the tungsten salt solution for 17 hours. The cloth was next centrifuged of excess solution and dried in warm air. The dried cloth contained 1.02 grams of tungsten salt/ gram of rayon.
The cloth was converted to the tungsten carbide form by first heating in air at a rate of C./hour to 300 C. and maintaining this temperature for four hours. The cloth was then further heated at a rate of 50 C./ hour until 350 C. was reached and this temperature was maintained for four hours, thereby forming the carbonaceous fiber relic containing finely divided tungstein in dispersed form. The air in the tube furnace was then purged with nitrogen before the carburization reaction commenced. Dry hydrogen gas was passed through the furnace at a rate of 4 liters/minute (SPT) as the cloth was heated to 600 C. within 30 minutes and held at 600 C. for one hour, then heated to 1000 C. and held there for an hour. During the pyrolysis and carburization steps the cloth shrank from 6 inches x 18 inches to 3 inches x 10 inches. The weight of the tungsten carbide cloth was 73% of the weight of the starting rayon cloth.
The carburized cloth had the following physical and chemical characteristics:
(1) Appearance: Lustrous and metallic gray.
(2) Flexibility: Could be folded upon itself without creasing or breaking.
(3) Tear strength: 8 to 14 lbs/inch of width.
(4) Composition: By X-ray powder diffraction analysis, the cloth was composed chiefly of highly crystalline tungsten carbide (WC), (i.e. at least 80 wt. percent) and a trace of tungsten metal.
(5) Carbon content: 4.98 wt. percent.
(6) Specific gravity: 14.7 gms./cc. by the bromoform pycnometer method.
(7) Electrical resistance: 1.1 ohm per 1 inch width by 6 inches long (in the long dimension).
(8) Fiber diameter: 5-6 microns.
(9) Crystal grain size: 1 micron.
10 Example 3.- ZrC fibers The starting rayorrfibers were 1.5 denier viscose tow (133,000 continuous filaments in the tow). The tow weighing 6.8 grams was preswol len in water for 15 minutes prior to immersion in 2.84 molar ZrOCl solution for four hours. It was next centrifuged of unimbibed solution from between the fibers and dried in air. The saltloaded rayon tow weighed 12.5 grams and contained 0.84 gram zirconium salt per gram rayon.
The tow was placed in a tube furnace and heated under a vacuum of 110 microns Hg pressure at a rate of 50 C./hr. to 400 C. then 100 C./Hr. to 1000 C. The pyrolyzed fibers were black, had a high luster and weighed 6.0 gms. The fiber relics contained 33.7% carbon and 43.0% zirconium by weight.
In order to carry out the carburization reaction between the carbon and the zirconium the fiber relics were placed in a graphite crucible and heated at 1900 C. for two hours in a hydrogen atmosphere employing a high frequency induction furnace. The resulting fibers weighed 4.2 gms., had a black-gray color, showed no evidence of sintering together and had a diameter of 4-5 microns. They were very flexible and had a tensile strength between 100,000 and 150,000 p.s.i. The fibers were electrically conductive and X-ray powder dilfraction patterns showed the fibers to be composed of polycrystalline face-centeredcubic zirconium carbide (ZrC). No graphite lines were evident in the X-ray patterns. The fibres were over 1 foot long with crystal grain size of less than 0.2 micron.
Example 4.TiC fibers A one-foot length of 9.0 denier viscose rayon tow (22,000 continuous filaments in the tow) was immersed in a 1.6 molar TiC1 aqueous solution for four hours. The tow was blotted of unimbibed solution and dried. The rayon tow containing the TiCl salt was pyrolyzed and carburized in the same manner as described in Example 3. The product fibers were grayish-black, flexible, and had a diameter of 12-15 microns. The only crystalline phase present in the fibers as indicated by X-ray diffraction powder analysis was the face-centered-cubic titanium carbide (TiC). The crystal grain size was less than 0.5 micron and thus, less than 0.2 of the fiber diameter. Fibers of TiC having lengths of 50 feet have been prepared by the same method.
'Example 5.-B C fibers A one-foot length of 20 denier viscose rayon two (10,000 continuous filaments in the tow) Was immersed in an aqueous solution containing 25% by weight boric acid for one hour. The solution was kept at C. during the imbibment to keep the boric acid in solution. The two was then centrifuged while still hot to remove unimbibed boric acid from between the fibers. After drying the two in air it was subjected to the same pyrolysis and carburization treatment as described in Example 3.
The reacted fibers were black, free from each other, had appreciable flexibility and strength. X-ray diffraction analysis showed the fibers to be composed of crystalline boron carbide (B C). The fiber diameter was about 20 microns and the crystal grain size was less than 0.2 of such diameter.
Example 6.-SiC fibers A length of 20 denier viscose rayon tow (10,000 continuous filaments in the tow) 23-inches long and weighing 13.3 grams was immersed in silicon tetrachloride liquid for 30 minutes. Prior to immersion, the two contained 1.4 gms. of absorbed water. After 30 minutes immersion reaction between the silicon tetrachloride and the water in the rayon was complete as indicated by the subsiding of HCl gas evolution from the fibers. The tow was freed of excess silicon tetrachloride by evaporation. The tow then weighed 15 gms. and contained 3.1 grams of silica. The silicon-loaded rayon two was pyrolized and carburized in the same manner as described in Example 3. The product fibers had a metallic luster, weighed 3.9 gms., and were characterized by appreciable flexibility and strength. X-ray diffraction pattern'analysis indicated a mixture of crysalline SiC and graphite. The fiber diameter was about 20 microns and the crystal grain size less than 0.5 micron.
Although preferred embodiments of this invention have been described in detail, it is contemplated that modifications of the process and composition may be made and that some features may be employed without others, all within the scope of the invention.
What is claimed is:
1. A process for producing crystalline metal carbide fibers, textiles, and shaped articles which comprises:
(a) providing a compound of a metal dissolved in a solvent;
(b) immersing a preformed organic polymeric material in the metal compound-containing solvent thereby swelling and opening the polymeric interstices such that the metal compound is imbibed in said interstices;
(c) removing the unimbibed metal compound from the outer surface of said polymeric material and drying the metal compound-imbibed polymer;
(d) first heating the metal compound-imbibed polymer to temperature of at least 250 C. at a rate sufficiently low to evolve volatile decomposition products of the polymer without destroying the polymer integrity, for a sufficient duration to decompose the organic structure of said polymer and form a carbonaceous relic containing the metal in finely dispersed form; and
(e) further heating the relic from first heating step (d) to a temperature in the range of about 1000"- 2000 C. in a non-oxidizing atmosphere to react said metal with said carbonaceous relic to form a metal carbide article.
2. A process according to claim 1 in which said organic polymer is a fiber.
3. A process according to claim 2 in which said fiber is a cellulosic fiber.
4. Process of claim 3 wherein said cellulosic fiber is rayon.
5. A process according to claim 1 in which the first heating step (d) is at least partly performed in an oxygencontaining atmosphere at a rate sufficiently low to avoid polymer ignition and for a duration to evolve only a sufficient portion of the carbon from said organic polymer for adjustment ofthe metal/carbon stoichiometric ratio to that required to form the metal carbide article in further heating step (e).
6. A process according to claim 1 in which said metal is selected from the group consisting of Groups IV-B, V-B, and VI-B of the Periodic Table, boron, aluminum, silicon, thorium, uranium and plutonium.
7. A process according to claim 1 in which said metal compound is a salt which is converted to a metal oxide during the first heating step (d).
8. A process according to claim 1 in which the further heating step (e) is performed in a hydrogen atmosphere.
References Cited UNITED STATES PATENTS 399,174 3/1889 Von Welsbach 17733.4 575,261 1/1897 Moscheles 11733.4 623,723 4/1899 Kohl et al. l17--33.4 2,870,000 1/1959 Ryznar 7520 3,087,233 4/1963 Turnbull 75-200 3,190,723 6/1965 Jacobson 23140 3,175,884 3/1965 Kuhn 23208 3,246,950 4/1966 Gruber 23 20 s 3,161,473 12/1964 Pultz 23208 L. DEWAYNE RUTLEDGE, Primary Examiner.
Priority Applications (28)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US602571A US3403008A (en) | 1966-12-19 | 1966-12-19 | Process for producing metal carbide fibers, textiles and shapes |
| US602572A US3399979A (en) | 1963-11-01 | 1966-12-19 | Process for producing metal nitride fibers, textiles and shapes |
| IL27279A IL27279A (en) | 1963-11-01 | 1967-01-19 | Metal fibers,textiles and shapes and process for producing them |
| GB2871/67A GB1159210A (en) | 1963-11-01 | 1967-01-19 | Metal Nitride Fibers, Textiles and Shapes and Process for Producing them |
| GB2870/67A GB1177782A (en) | 1963-11-01 | 1967-01-19 | Metal Carbide Fibers, Textiles and Shapes and process for producing them |
| IL27280A IL27280A (en) | 1963-11-01 | 1967-01-19 | Metal carbide fibers,textiles and shapes and process for producing them |
| BE692904D BE692904A (en) | 1963-11-01 | 1967-01-19 | |
| IL27278A IL27278A (en) | 1963-11-01 | 1967-01-19 | Metal nitride fibers,textiles and shapes and process for producing them |
| DE19671619183 DE1619183A1 (en) | 1963-11-01 | 1967-01-21 | Process for the production of fibers, textiles and molded articles from metal nitrides |
| DE19671669551 DE1669551C3 (en) | 1966-01-24 | 1967-01-23 | Process for the production of fibers or fiber structures from crystalline metal carbide |
| FR92094A FR1508760A (en) | 1963-11-01 | 1967-01-23 | Fibers, textile materials and manufactured articles of metallic carbide and process for their production |
| SE988/67A SE309745B (en) | 1963-11-01 | 1967-01-23 | |
| JP42004351A JPS5015889B1 (en) | 1963-11-01 | 1967-01-24 | |
| AT68067A AT277442B (en) | 1963-11-01 | 1967-01-24 | Process for the production of crystalline metal carbide fibers and textiles |
| CH99967A CH487287A (en) | 1963-11-01 | 1967-01-24 | Method of preparing a shaped article of crustalline metal carbide |
| NL676701101A NL153164B (en) | 1963-11-01 | 1967-01-24 | METHOD OF MANUFACTURE OF METALLIC COMPOUND ARTICLES AND ARTICLES OBTAINED BY THIS METHOD. |
| BE693178D BE693178A (en) | 1963-11-01 | 1967-01-25 | |
| BE693177D BE693177A (en) | 1963-11-01 | 1967-01-25 | |
| FR92544A FR1510317A (en) | 1963-11-01 | 1967-01-26 | Fibers, textiles and manufactured metal articles, and process for making them |
| FR92545A FR1509452A (en) | 1963-11-01 | 1967-01-26 | Fibers, textiles and manufactured articles of metal nitride and process for making them |
| AT79267A AT280463B (en) | 1963-11-01 | 1967-01-27 | Process for the production of metal nitride fibers and textiles |
| SE00248/67A SE369529B (en) | 1963-11-01 | 1967-01-27 | |
| NL676701371A NL143999B (en) | 1963-11-01 | 1967-01-27 | PROCESS FOR MANUFACTURE OF AN WHOLE OR ALMOST ALL OF A HIGH MELTING, FIREPROOF NITRIDE OBJECT, AS WELL AS THE OBJECTS OBTAINED IN THIS WAY. |
| NL676701372A NL142419B (en) | 1963-11-01 | 1967-01-27 | PROCEDURE FOR MANUFACTURING AN OBJECT OF ELEMENTARY METAL, AS WELL AS OBJECT OBTAINED BY USING THIS PROCESS. |
| AT79767A AT280464B (en) | 1963-11-01 | 1967-01-27 | Process for the production of fibers, textiles and shapes from elemental metals |
| CH122467A CH478660A (en) | 1963-11-01 | 1967-01-27 | Method of preparing a shaped article of metal nitrides |
| DE19671558434D DE1558434B1 (en) | 1963-11-01 | 1967-01-27 | Process for the production of fibers, textiles and molded articles consisting essentially of metals |
| DE19671669553 DE1669553C3 (en) | 1966-09-02 | 1967-04-13 | Process for the production of shaped structures, in particular fibers, from metal oxides and their use |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US602571A US3403008A (en) | 1966-12-19 | 1966-12-19 | Process for producing metal carbide fibers, textiles and shapes |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US52238066A Continuation-In-Part | 1963-11-01 | 1966-01-24 |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US73784268A Continuation-In-Part | 1968-06-18 | 1968-06-18 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3403008A true US3403008A (en) | 1968-09-24 |
Family
ID=24411892
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US602571A Expired - Lifetime US3403008A (en) | 1963-11-01 | 1966-12-19 | Process for producing metal carbide fibers, textiles and shapes |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3403008A (en) |
Cited By (43)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3673101A (en) * | 1969-12-08 | 1972-06-27 | Grace W R & Co | Process for preparing improved carbide microspheres from ion exchange resins |
| US3713865A (en) * | 1968-07-05 | 1973-01-30 | Ducommun Inc | Composite product and method of making same |
| US3764550A (en) * | 1969-06-09 | 1973-10-09 | Grace W R & Co | Process for the formation of metal carbide and metal carbide plus carbon microspheres |
| US3800023A (en) * | 1972-05-16 | 1974-03-26 | Atomic Energy Commission | Loading a cation exchange resin with uranyl ions |
| US3856622A (en) * | 1972-04-18 | 1974-12-24 | Us Atomic Energy Commision | High temperature nuclear reactor fuel |
| US3876444A (en) * | 1970-04-24 | 1975-04-08 | Gen Electric | Method of treating high strength carbon fibers |
| US3880769A (en) * | 1970-05-25 | 1975-04-29 | Atomic Energy Commission | Method of making microspheroidal nuclear fuels having closed porosity |
| US3887486A (en) * | 1970-05-25 | 1975-06-03 | Us Energy | Porous, microspheroidal, nuclear fuels having internal porosity |
| US3917776A (en) * | 1970-12-12 | 1975-11-04 | Mitsubishi Rayon Co | Process for producing carbon fiber |
| US3929427A (en) * | 1972-07-10 | 1975-12-30 | Union Carbide Corp | Wear-resistant surface composite materials and method for producing same |
| US3932594A (en) * | 1973-12-28 | 1976-01-13 | Union Carbide Corporation | Process for the preparation of fine grain metal carbide powders |
| US3937775A (en) * | 1972-10-23 | 1976-02-10 | Sumitomo Chemical Company, Limited | Process for production of carbon products |
| US3971840A (en) * | 1973-03-27 | 1976-07-27 | The Carborundum Company | Production of high strength carbide fibers by heat treatment |
| US3997638A (en) * | 1974-09-18 | 1976-12-14 | Celanese Corporation | Production of metal ion containing carbon fibers useful in electron shielding applications |
| JPS5214687A (en) * | 1975-07-26 | 1977-02-03 | Res Inst Iron Steel Tohoku Univ | Product of silicon carbide |
| US4008090A (en) * | 1971-09-09 | 1977-02-15 | Sumitomo Electric Industries, Ltd. | Process for the production of tungsten carbide or mixed metal carbides |
| US4100233A (en) * | 1975-04-25 | 1978-07-11 | The Research Institute For Iron, Steel And Other Metals Of The Tohoku University | Silicon carbide fibers having a high strength and a method for producing said fibers |
| US4126652A (en) * | 1976-02-26 | 1978-11-21 | Toyo Boseki Kabushiki Kaisha | Process for preparation of a metal carbide-containing molded product |
| US4166841A (en) * | 1978-05-03 | 1979-09-04 | Ford Motor Company | Method for making pure beta silicon carbide |
| US4190439A (en) * | 1973-12-28 | 1980-02-26 | Union Carbide Corporation | Process for the preparation of fine grain metal carbide powders and sintered articles therefrom |
| US4238547A (en) * | 1973-03-27 | 1980-12-09 | The Carborundum Company | High strength yarn consisting of boron carbide fibers |
| US4456519A (en) * | 1979-07-20 | 1984-06-26 | C. Conradty Nurnberg Gmbh & Co. | Regeneratable, non-consumable electrode for high temperature uses |
| US4505888A (en) * | 1983-05-27 | 1985-03-19 | E. I. Du Pont De Nemours & Company | Tracer for circulation determinations |
| US4537818A (en) * | 1984-08-30 | 1985-08-27 | The United States Of America As Represented By The United States Department Of Energy | Method for production of ceramic oxide and carbide bodies by polymer inclusion and decomposition |
| US4652436A (en) * | 1985-03-05 | 1987-03-24 | Osaka Yuki Kagaku Kogyo Kabushiki Kaisha | Preparation of nitride and carbide from inorganic-organic polymer complex |
| US4756791A (en) * | 1986-08-25 | 1988-07-12 | Gte Laboratories Incorporated | Chemical vapor deposition process for producing metal carbide or nitride whiskers |
| US4810530A (en) * | 1986-08-25 | 1989-03-07 | Gte Laboratories Incorporated | Method of coating metal carbide nitride, and carbonitride whiskers with metal carbides, nitrides, carbonitrides, or oxides |
| DE3743357A1 (en) * | 1987-12-21 | 1989-07-06 | Sueddeutsche Kalkstickstoff | METHOD FOR PRODUCING FINE-PART TRANSITION METAL CARBIDES |
| EP0258547A3 (en) * | 1986-09-04 | 1989-11-08 | Asahi Kasei Kogyo Kabushiki Kaisha | Refractory fiber spatial structure and manufacturing method thereof |
| US4900525A (en) * | 1986-08-25 | 1990-02-13 | Gte Laboratories Incorporated | Chemical vapor deposition reactor for producing metal carbide or nitride whiskers |
| US4904424A (en) * | 1987-05-29 | 1990-02-27 | Hoechst Celanese Corporation | Ceramic alloys from colloidal metal alloy suspensions |
| US4931316A (en) * | 1988-09-06 | 1990-06-05 | Hoechst Celanese Corp. | Preparation of interstitial titanium ceramic fibers |
| US4948573A (en) * | 1986-12-02 | 1990-08-14 | Alcan International Limited | Process for producing silicon carbide and metal carbides |
| US4971834A (en) * | 1989-06-29 | 1990-11-20 | Therm Incorporated | Process for preparing precursor for silicon carbide whiskers |
| US4988564A (en) * | 1986-08-25 | 1991-01-29 | Gte Laboratories Incorporated | Metal carbide, nitride, or carbonitride whiskers coated with metal carbides, nitrides, carbonitrides, or oxides |
| US5114695A (en) * | 1987-04-14 | 1992-05-19 | Alcon International Limited | Process of producing aluminum and titanium nitrides |
| US20040009112A1 (en) * | 2002-07-10 | 2004-01-15 | Advanced Composite Materials Corporation | Silicon carbide fibers essentially devoid of whiskers and method for preparation thereof |
| US20040265208A1 (en) * | 2003-04-25 | 2004-12-30 | Zongtao Zhang | Method for the production of metal carbides |
| US20060147368A1 (en) * | 2002-07-10 | 2006-07-06 | Advanced Composite Materials Corporation | Process for producing silicon carbide fibers essentially devoid of whiskers |
| US20070295716A1 (en) * | 2006-03-30 | 2007-12-27 | Advanced Composite Materials, Llc | Composite materials and devices comprising single crystal silicon carbide heated by electromagnetic radiation |
| WO2009155393A1 (en) * | 2008-06-18 | 2009-12-23 | Advanced Cerametrics, Inc. | Boron carbide ceramic fibers |
| US20110097259A1 (en) * | 2008-05-13 | 2011-04-28 | L'air Liquide Societe Anonyme Pour L'exploitation | Ceramic Foam with Gradient of Porosity in Heterogeneous Catalysis |
| US20140080694A1 (en) * | 2011-03-01 | 2014-03-20 | GM Global Technology Operations LLC | Synthesis of nanosized metal carbides on graphitized carbon as supporting materials for electrocatalysts |
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Cited By (59)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3713865A (en) * | 1968-07-05 | 1973-01-30 | Ducommun Inc | Composite product and method of making same |
| US3764550A (en) * | 1969-06-09 | 1973-10-09 | Grace W R & Co | Process for the formation of metal carbide and metal carbide plus carbon microspheres |
| US3673101A (en) * | 1969-12-08 | 1972-06-27 | Grace W R & Co | Process for preparing improved carbide microspheres from ion exchange resins |
| US3876444A (en) * | 1970-04-24 | 1975-04-08 | Gen Electric | Method of treating high strength carbon fibers |
| US3880769A (en) * | 1970-05-25 | 1975-04-29 | Atomic Energy Commission | Method of making microspheroidal nuclear fuels having closed porosity |
| US3887486A (en) * | 1970-05-25 | 1975-06-03 | Us Energy | Porous, microspheroidal, nuclear fuels having internal porosity |
| US3917776A (en) * | 1970-12-12 | 1975-11-04 | Mitsubishi Rayon Co | Process for producing carbon fiber |
| US4008090A (en) * | 1971-09-09 | 1977-02-15 | Sumitomo Electric Industries, Ltd. | Process for the production of tungsten carbide or mixed metal carbides |
| US3856622A (en) * | 1972-04-18 | 1974-12-24 | Us Atomic Energy Commision | High temperature nuclear reactor fuel |
| US3800023A (en) * | 1972-05-16 | 1974-03-26 | Atomic Energy Commission | Loading a cation exchange resin with uranyl ions |
| US3929427A (en) * | 1972-07-10 | 1975-12-30 | Union Carbide Corp | Wear-resistant surface composite materials and method for producing same |
| US3937775A (en) * | 1972-10-23 | 1976-02-10 | Sumitomo Chemical Company, Limited | Process for production of carbon products |
| US4238547A (en) * | 1973-03-27 | 1980-12-09 | The Carborundum Company | High strength yarn consisting of boron carbide fibers |
| US3971840A (en) * | 1973-03-27 | 1976-07-27 | The Carborundum Company | Production of high strength carbide fibers by heat treatment |
| US4190439A (en) * | 1973-12-28 | 1980-02-26 | Union Carbide Corporation | Process for the preparation of fine grain metal carbide powders and sintered articles therefrom |
| US3932594A (en) * | 1973-12-28 | 1976-01-13 | Union Carbide Corporation | Process for the preparation of fine grain metal carbide powders |
| US3997638A (en) * | 1974-09-18 | 1976-12-14 | Celanese Corporation | Production of metal ion containing carbon fibers useful in electron shielding applications |
| US4100233A (en) * | 1975-04-25 | 1978-07-11 | The Research Institute For Iron, Steel And Other Metals Of The Tohoku University | Silicon carbide fibers having a high strength and a method for producing said fibers |
| JPS5214687A (en) * | 1975-07-26 | 1977-02-03 | Res Inst Iron Steel Tohoku Univ | Product of silicon carbide |
| US4126652A (en) * | 1976-02-26 | 1978-11-21 | Toyo Boseki Kabushiki Kaisha | Process for preparation of a metal carbide-containing molded product |
| US4166841A (en) * | 1978-05-03 | 1979-09-04 | Ford Motor Company | Method for making pure beta silicon carbide |
| EP0005359A1 (en) * | 1978-05-03 | 1979-11-14 | Ford Motor Company Limited | Method for making beta silicon carbide |
| US4456519A (en) * | 1979-07-20 | 1984-06-26 | C. Conradty Nurnberg Gmbh & Co. | Regeneratable, non-consumable electrode for high temperature uses |
| US4505888A (en) * | 1983-05-27 | 1985-03-19 | E. I. Du Pont De Nemours & Company | Tracer for circulation determinations |
| US4537818A (en) * | 1984-08-30 | 1985-08-27 | The United States Of America As Represented By The United States Department Of Energy | Method for production of ceramic oxide and carbide bodies by polymer inclusion and decomposition |
| US4652436A (en) * | 1985-03-05 | 1987-03-24 | Osaka Yuki Kagaku Kogyo Kabushiki Kaisha | Preparation of nitride and carbide from inorganic-organic polymer complex |
| US4756791A (en) * | 1986-08-25 | 1988-07-12 | Gte Laboratories Incorporated | Chemical vapor deposition process for producing metal carbide or nitride whiskers |
| US4810530A (en) * | 1986-08-25 | 1989-03-07 | Gte Laboratories Incorporated | Method of coating metal carbide nitride, and carbonitride whiskers with metal carbides, nitrides, carbonitrides, or oxides |
| US4988564A (en) * | 1986-08-25 | 1991-01-29 | Gte Laboratories Incorporated | Metal carbide, nitride, or carbonitride whiskers coated with metal carbides, nitrides, carbonitrides, or oxides |
| US4900525A (en) * | 1986-08-25 | 1990-02-13 | Gte Laboratories Incorporated | Chemical vapor deposition reactor for producing metal carbide or nitride whiskers |
| EP0258547A3 (en) * | 1986-09-04 | 1989-11-08 | Asahi Kasei Kogyo Kabushiki Kaisha | Refractory fiber spatial structure and manufacturing method thereof |
| US5055348A (en) * | 1986-09-04 | 1991-10-08 | Asahi Kasei Kogyo Kabushiki Kaisha | Refractory fiber spacial structure and manufacturing method thereof |
| US4948573A (en) * | 1986-12-02 | 1990-08-14 | Alcan International Limited | Process for producing silicon carbide and metal carbides |
| US5114695A (en) * | 1987-04-14 | 1992-05-19 | Alcon International Limited | Process of producing aluminum and titanium nitrides |
| US4904424A (en) * | 1987-05-29 | 1990-02-27 | Hoechst Celanese Corporation | Ceramic alloys from colloidal metal alloy suspensions |
| DE3743357A1 (en) * | 1987-12-21 | 1989-07-06 | Sueddeutsche Kalkstickstoff | METHOD FOR PRODUCING FINE-PART TRANSITION METAL CARBIDES |
| US4931316A (en) * | 1988-09-06 | 1990-06-05 | Hoechst Celanese Corp. | Preparation of interstitial titanium ceramic fibers |
| US4971834A (en) * | 1989-06-29 | 1990-11-20 | Therm Incorporated | Process for preparing precursor for silicon carbide whiskers |
| US20040009112A1 (en) * | 2002-07-10 | 2004-01-15 | Advanced Composite Materials Corporation | Silicon carbide fibers essentially devoid of whiskers and method for preparation thereof |
| US20050013997A1 (en) * | 2002-07-10 | 2005-01-20 | Advanced Composite Materials Corporation | Silicon carbide fibers essentially devoid of whiskers and method for preparation thereof |
| US7041266B1 (en) | 2002-07-10 | 2006-05-09 | Advanced Composite Materials Corp. | Silicon carbide fibers essentially devoid of whiskers and products made therefrom |
| US20060104882A1 (en) * | 2002-07-10 | 2006-05-18 | Advanced Composite Materials Corporation | Silicon carbide fibers essentially devoid of whiskers and products made therefrom |
| US20060147368A1 (en) * | 2002-07-10 | 2006-07-06 | Advanced Composite Materials Corporation | Process for producing silicon carbide fibers essentially devoid of whiskers |
| US7083771B2 (en) | 2002-07-10 | 2006-08-01 | Advanced Composite Materials Corporation | Process for producing silicon carbide fibers essentially devoid of whiskers |
| US20040265208A1 (en) * | 2003-04-25 | 2004-12-30 | Zongtao Zhang | Method for the production of metal carbides |
| US7625542B2 (en) | 2003-04-25 | 2009-12-01 | Inframat Corporation | Method for the production of metal carbides |
| US20070295716A1 (en) * | 2006-03-30 | 2007-12-27 | Advanced Composite Materials, Llc | Composite materials and devices comprising single crystal silicon carbide heated by electromagnetic radiation |
| US20090302030A1 (en) * | 2006-03-30 | 2009-12-10 | Advanced Composite Materials Corporation | Composite materials and devices comprising single crystal silicon carbide heated by electromagnetic radiation |
| US8648284B2 (en) | 2006-03-30 | 2014-02-11 | Advanced Composite Materials, Llc | Composite materials and devices comprising single crystal silicon carbide heated by electromagnetic radiation |
| US9688583B2 (en) | 2006-03-30 | 2017-06-27 | Advanced Composite Materials, Llc | Composite materials and devices comprising single crystal silicon carbide heated by electromagnetic radiation |
| US20110097259A1 (en) * | 2008-05-13 | 2011-04-28 | L'air Liquide Societe Anonyme Pour L'exploitation | Ceramic Foam with Gradient of Porosity in Heterogeneous Catalysis |
| WO2009155393A1 (en) * | 2008-06-18 | 2009-12-23 | Advanced Cerametrics, Inc. | Boron carbide ceramic fibers |
| US20090318280A1 (en) * | 2008-06-18 | 2009-12-24 | Advanced Cerametrics, Inc. | Boron carbide ceramic fibers |
| CN102066247A (en) * | 2008-06-18 | 2011-05-18 | 高级金属陶瓷有限公司 | Boron carbide ceramic fibers |
| EP2300367A4 (en) * | 2008-06-18 | 2012-08-01 | Advanced Cerametrics Inc | Boron carbide ceramic fibers |
| US8536080B2 (en) * | 2008-06-18 | 2013-09-17 | Advanced Cetametrics, Inc. | Boron carbide ceramic fibers |
| CN102066247B (en) * | 2008-06-18 | 2014-02-12 | 高级金属陶瓷有限公司 | Boron carbide ceramic fiber |
| US20140080694A1 (en) * | 2011-03-01 | 2014-03-20 | GM Global Technology Operations LLC | Synthesis of nanosized metal carbides on graphitized carbon as supporting materials for electrocatalysts |
| US9295979B2 (en) * | 2011-03-01 | 2016-03-29 | GM Global Technology Operations LLC | Synthesis of nanosized metal carbides on graphitized carbon as supporting materials for electrocatalysts |
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