CA1185772A - ULTRASONIC END-CAPPING OF .beta. ALUMINA TUBES - Google Patents
ULTRASONIC END-CAPPING OF .beta. ALUMINA TUBESInfo
- Publication number
- CA1185772A CA1185772A CA000405267A CA405267A CA1185772A CA 1185772 A CA1185772 A CA 1185772A CA 000405267 A CA000405267 A CA 000405267A CA 405267 A CA405267 A CA 405267A CA 1185772 A CA1185772 A CA 1185772A
- Authority
- CA
- Canada
- Prior art keywords
- accordance
- ultrasonic
- cap
- polymer
- mandrel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 title claims abstract description 29
- 238000000034 method Methods 0.000 claims abstract description 69
- 239000000203 mixture Substances 0.000 claims abstract description 59
- 239000011230 binding agent Substances 0.000 claims abstract description 58
- 229920000642 polymer Polymers 0.000 claims abstract description 33
- 239000002243 precursor Substances 0.000 claims abstract description 23
- 229920001169 thermoplastic Polymers 0.000 claims abstract description 19
- 238000001125 extrusion Methods 0.000 claims abstract description 15
- 239000004416 thermosoftening plastic Substances 0.000 claims abstract description 12
- 239000006057 Non-nutritive feed additive Substances 0.000 claims abstract description 7
- 238000005304 joining Methods 0.000 claims abstract description 7
- 239000000155 melt Substances 0.000 claims abstract description 7
- 229920001400 block copolymer Polymers 0.000 claims description 28
- 125000003118 aryl group Chemical group 0.000 claims description 12
- 238000005245 sintering Methods 0.000 claims description 12
- 230000005484 gravity Effects 0.000 claims description 11
- 239000004793 Polystyrene Substances 0.000 claims description 10
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 claims description 10
- 229920002223 polystyrene Polymers 0.000 claims description 10
- PAYRUJLWNCNPSJ-UHFFFAOYSA-N Aniline Chemical compound NC1=CC=CC=C1 PAYRUJLWNCNPSJ-UHFFFAOYSA-N 0.000 claims description 8
- 239000002245 particle Substances 0.000 claims description 8
- 239000007787 solid Substances 0.000 claims description 7
- KAKZBPTYRLMSJV-UHFFFAOYSA-N Butadiene Chemical compound C=CC=C KAKZBPTYRLMSJV-UHFFFAOYSA-N 0.000 claims description 6
- 229920001971 elastomer Polymers 0.000 claims description 6
- FUJCRWPEOMXPAD-UHFFFAOYSA-N Li2O Inorganic materials [Li+].[Li+].[O-2] FUJCRWPEOMXPAD-UHFFFAOYSA-N 0.000 claims description 5
- KKCBUQHMOMHUOY-UHFFFAOYSA-N Na2O Inorganic materials [O-2].[Na+].[Na+] KKCBUQHMOMHUOY-UHFFFAOYSA-N 0.000 claims description 5
- 239000000806 elastomer Substances 0.000 claims description 5
- 150000002148 esters Chemical class 0.000 claims description 5
- 229910052799 carbon Inorganic materials 0.000 claims description 4
- 238000009826 distribution Methods 0.000 claims description 4
- 238000003825 pressing Methods 0.000 claims description 4
- 125000001931 aliphatic group Chemical group 0.000 claims description 3
- BEWFIPLBFJGWSR-UHFFFAOYSA-N butyl 12-acetyloxyoctadec-9-enoate Chemical compound CCCCCCC(OC(C)=O)CC=CCCCCCCCC(=O)OCCCC BEWFIPLBFJGWSR-UHFFFAOYSA-N 0.000 claims description 2
- 235000014113 dietary fatty acids Nutrition 0.000 claims description 2
- 239000000194 fatty acid Substances 0.000 claims description 2
- 229930195729 fatty acid Natural products 0.000 claims description 2
- 150000004665 fatty acids Chemical class 0.000 claims description 2
- BPJZKLBPJBMLQG-KWRJMZDGSA-N propanoyl (z,12r)-12-hydroxyoctadec-9-enoate Chemical compound CCCCCC[C@@H](O)C\C=C/CCCCCCCC(=O)OC(=O)CC BPJZKLBPJBMLQG-KWRJMZDGSA-N 0.000 claims description 2
- 125000000218 acetic acid group Chemical group C(C)(=O)* 0.000 claims 1
- 229920001577 copolymer Polymers 0.000 claims 1
- 229910052593 corundum Inorganic materials 0.000 claims 1
- XUCJHNOBJLKZNU-UHFFFAOYSA-M dilithium;hydroxide Chemical compound [Li+].[Li+].[OH-] XUCJHNOBJLKZNU-UHFFFAOYSA-M 0.000 claims 1
- 229910001845 yogo sapphire Inorganic materials 0.000 claims 1
- 230000008569 process Effects 0.000 abstract description 10
- 239000004014 plasticizer Substances 0.000 abstract description 7
- 229920002725 thermoplastic elastomer Polymers 0.000 abstract description 7
- 239000001993 wax Substances 0.000 description 26
- 239000003921 oil Substances 0.000 description 15
- 239000000463 material Substances 0.000 description 13
- 238000002156 mixing Methods 0.000 description 10
- ZNRLMGFXSPUZNR-UHFFFAOYSA-N 2,2,4-trimethyl-1h-quinoline Chemical compound C1=CC=C2C(C)=CC(C)(C)NC2=C1 ZNRLMGFXSPUZNR-UHFFFAOYSA-N 0.000 description 8
- -1 poly(alpha-methyl styrene) Polymers 0.000 description 8
- 239000011347 resin Substances 0.000 description 8
- 229920005989 resin Polymers 0.000 description 8
- 229920013623 Solprene Polymers 0.000 description 7
- 239000004615 ingredient Substances 0.000 description 7
- YMWUJEATGCHHMB-UHFFFAOYSA-N Dichloromethane Chemical compound ClCCl YMWUJEATGCHHMB-UHFFFAOYSA-N 0.000 description 6
- 239000000919 ceramic Substances 0.000 description 6
- MMMNTDFSPSQXJP-UHFFFAOYSA-N orphenadrine citrate Chemical compound OC(=O)CC(O)(C(O)=O)CC(O)=O.C=1C=CC=C(C)C=1C(OCCN(C)C)C1=CC=CC=C1 MMMNTDFSPSQXJP-UHFFFAOYSA-N 0.000 description 6
- 238000012545 processing Methods 0.000 description 6
- 239000004698 Polyethylene Substances 0.000 description 5
- CDBYLPFSWZWCQE-UHFFFAOYSA-L Sodium Carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 description 5
- CMOYPQWMTBSLJK-ACQXMXPUSA-N methyl (z,12r)-12-acetyloxyoctadec-9-enoate Chemical compound CCCCCC[C@@H](OC(C)=O)C\C=C/CCCCCCCC(=O)OC CMOYPQWMTBSLJK-ACQXMXPUSA-N 0.000 description 5
- 229920000573 polyethylene Polymers 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- 239000004614 Process Aid Substances 0.000 description 4
- 150000002500 ions Chemical class 0.000 description 4
- IIPYXGDZVMZOAP-UHFFFAOYSA-N lithium nitrate Chemical compound [Li+].[O-][N+]([O-])=O IIPYXGDZVMZOAP-UHFFFAOYSA-N 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 4
- 238000002360 preparation method Methods 0.000 description 4
- 239000002904 solvent Substances 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- ZWEHNKRNPOVVGH-UHFFFAOYSA-N 2-Butanone Chemical compound CCC(C)=O ZWEHNKRNPOVVGH-UHFFFAOYSA-N 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- 239000003963 antioxidant agent Substances 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 229910052734 helium Inorganic materials 0.000 description 3
- 239000001307 helium Substances 0.000 description 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 3
- 239000003208 petroleum Substances 0.000 description 3
- 150000003097 polyterpenes Chemical class 0.000 description 3
- YBYIRNPNPLQARY-UHFFFAOYSA-N 1H-indene Chemical compound C1=CC=C2CC=CC2=C1 YBYIRNPNPLQARY-UHFFFAOYSA-N 0.000 description 2
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 2
- 239000005062 Polybutadiene Substances 0.000 description 2
- 239000004809 Teflon Substances 0.000 description 2
- 229920006362 Teflon® Polymers 0.000 description 2
- XEOSKTHOPLADLN-QTJNJRLBSA-N acetyl (z,12r)-12-hydroxyoctadec-9-enoate Chemical class CCCCCC[C@@H](O)C\C=C/CCCCCCCC(=O)OC(C)=O XEOSKTHOPLADLN-QTJNJRLBSA-N 0.000 description 2
- 239000010775 animal oil Substances 0.000 description 2
- 230000003078 antioxidant effect Effects 0.000 description 2
- 239000010951 brass Substances 0.000 description 2
- 238000013329 compounding Methods 0.000 description 2
- 238000000748 compression moulding Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 239000000945 filler Substances 0.000 description 2
- 239000008240 homogeneous mixture Substances 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000005504 petroleum refining Methods 0.000 description 2
- 229910052697 platinum Inorganic materials 0.000 description 2
- 229920002857 polybutadiene Polymers 0.000 description 2
- 229920000098 polyolefin Polymers 0.000 description 2
- 229910000029 sodium carbonate Inorganic materials 0.000 description 2
- 235000017550 sodium carbonate Nutrition 0.000 description 2
- 229920001059 synthetic polymer Polymers 0.000 description 2
- 239000008158 vegetable oil Substances 0.000 description 2
- 235000013311 vegetables Nutrition 0.000 description 2
- YHMYGUUIMTVXNW-UHFFFAOYSA-N 1,3-dihydrobenzimidazole-2-thione Chemical compound C1=CC=C2NC(S)=NC2=C1 YHMYGUUIMTVXNW-UHFFFAOYSA-N 0.000 description 1
- DKCPKDPYUFEZCP-UHFFFAOYSA-N 2,6-di-tert-butylphenol Chemical compound CC(C)(C)C1=CC=CC(C(C)(C)C)=C1O DKCPKDPYUFEZCP-UHFFFAOYSA-N 0.000 description 1
- NJIDLJRHMJCJIV-UHFFFAOYSA-N C.C(CC)(=O)O Chemical compound C.C(CC)(=O)O NJIDLJRHMJCJIV-UHFFFAOYSA-N 0.000 description 1
- 244000025254 Cannabis sativa Species 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 102100024133 Coiled-coil domain-containing protein 50 Human genes 0.000 description 1
- 229920008712 Copo Polymers 0.000 description 1
- 102100022662 Guanylyl cyclase C Human genes 0.000 description 1
- 101710198293 Guanylyl cyclase C Proteins 0.000 description 1
- 101000910772 Homo sapiens Coiled-coil domain-containing protein 50 Proteins 0.000 description 1
- 229920002633 Kraton (polymer) Polymers 0.000 description 1
- KFUJMHHNLGCTIJ-UHFFFAOYSA-N Propiverine hydrochloride Chemical compound [Cl-].C=1C=CC=CC=1C(C=1C=CC=CC=1)(OCCC)C(=O)OC1CC[NH+](C)CC1 KFUJMHHNLGCTIJ-UHFFFAOYSA-N 0.000 description 1
- 235000021355 Stearic acid Nutrition 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- MCRWZBYTLVCCJJ-DKALBXGISA-N [(1s,3r)-3-[[(3s,4s)-3-methoxyoxan-4-yl]amino]-1-propan-2-ylcyclopentyl]-[(1s,4s)-5-[6-(trifluoromethyl)pyrimidin-4-yl]-2,5-diazabicyclo[2.2.1]heptan-2-yl]methanone Chemical compound C([C@]1(N(C[C@]2([H])C1)C(=O)[C@@]1(C[C@@H](CC1)N[C@@H]1[C@@H](COCC1)OC)C(C)C)[H])N2C1=CC(C(F)(F)F)=NC=N1 MCRWZBYTLVCCJJ-DKALBXGISA-N 0.000 description 1
- BNOODXBBXFZASF-UHFFFAOYSA-N [Na].[S] Chemical compound [Na].[S] BNOODXBBXFZASF-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 230000005587 bubbling Effects 0.000 description 1
- BEWFIPLBFJGWSR-AONZOJHOSA-N butyl (z,12r)-12-acetyloxyoctadec-9-enoate Chemical compound CCCCCC[C@@H](OC(C)=O)C\C=C/CCCCCCCC(=O)OCCCC BEWFIPLBFJGWSR-AONZOJHOSA-N 0.000 description 1
- 238000001354 calcination Methods 0.000 description 1
- 238000003490 calendering Methods 0.000 description 1
- 239000012700 ceramic precursor Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003153 chemical reaction reagent Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- NBVXSUQYWXRMNV-UHFFFAOYSA-N fluoromethane Chemical compound FC NBVXSUQYWXRMNV-UHFFFAOYSA-N 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 125000005647 linker group Chemical group 0.000 description 1
- 229910001947 lithium oxide Inorganic materials 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- 238000005297 material degradation process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000006082 mold release agent Substances 0.000 description 1
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 1
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 description 1
- 238000010525 oxidative degradation reaction Methods 0.000 description 1
- 239000012188 paraffin wax Substances 0.000 description 1
- RPMPQTVHEJVLCR-UHFFFAOYSA-N pentaaluminum;sodium;oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[O-2].[O-2].[O-2].[O-2].[O-2].[Na+].[Al+3].[Al+3].[Al+3].[Al+3].[Al+3] RPMPQTVHEJVLCR-UHFFFAOYSA-N 0.000 description 1
- 229920003251 poly(α-methylstyrene) Polymers 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000008117 stearic acid Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000010301 surface-oxidation reaction Methods 0.000 description 1
- 235000019871 vegetable fat Nutrition 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/534—Joining single elements to open ends of tubular or hollow articles or to the ends of bars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C57/00—Shaping of tube ends, e.g. flanging, belling or closing; Apparatus therefor, e.g. collapsible mandrels
- B29C57/10—Closing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/08—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7377—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline
- B29C66/73771—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being amorphous
- B29C66/73772—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being amorphous the to-be-joined areas of both parts to be joined being amorphous
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7377—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline
- B29C66/73775—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being crystalline
- B29C66/73776—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being crystalline the to-be-joined areas of both parts to be joined being crystalline
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
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Abstract
ABSTRACT OF THE DISCLOSURE
This invention comprises a method of ultra-sonically end-capping a tubular green body which comprises a mixture of 40-60 volume percent sinterable beta"-alumina precursor particulate and 60-40 volume percent organic sacrificial binder wherein said sacri-ficial binder comprises a thermoplastic elastomer, a plasticizer which may be oil, wax or oil and wax, stiffening polymers, a processing aid and optional components. The tube is preferably formed by extrusion molding. The green body tube may be end-capped by ultrasonic forming or by ultrasonic bonding of an end-cap to the tube. During this process, ultrasonic vibration energy is dissipated as heat energy which melts the thermoplastic binder composition and welds the joining surfaces.
This invention comprises a method of ultra-sonically end-capping a tubular green body which comprises a mixture of 40-60 volume percent sinterable beta"-alumina precursor particulate and 60-40 volume percent organic sacrificial binder wherein said sacri-ficial binder comprises a thermoplastic elastomer, a plasticizer which may be oil, wax or oil and wax, stiffening polymers, a processing aid and optional components. The tube is preferably formed by extrusion molding. The green body tube may be end-capped by ultrasonic forming or by ultrasonic bonding of an end-cap to the tube. During this process, ultrasonic vibration energy is dissipated as heat energy which melts the thermoplastic binder composition and welds the joining surfaces.
Description
3577~
ULTRASONIC END-CAPPING OF BETA" ALUMINA TUBES
. .
T~is invention relates to preparation of end-capped tubular betal' alumina ceramic bodies~ In ~ particular, this invention relates to ultrasonic end-capp.ing of extruded beta~-alumina tubular ceramic precursors~ also known as green bodies, such that after binder remcval and sintering the bond is hermetic and the integri~y of the bonded area is comparable to the body of ~he tube~
10Beta~-alumina tubes need to be end-capped at one end in order to be used in construction of sodium- sulfur batteries or similar energy conversion devices.
~ltrasonic end-capping as taught in khis inven~ion, can proceed. by either of two rou~es, ultrasonic forming or ultrasonic bonding, with the latter being preferred.
During the end-capping process, the ultrasonic vibrations from the ultrasonic horn are transmitted to the part and travel to the joint area of interface. Here the vibratory energy i5 dissipated in the form of fri.ctional heat which 20 melts the binder and welds the joining surfaces.
While ultrasonic bonding technique is known, it has only been used to bond materials of thermoplastic compositions. In contrast, the composition of the tllbular ~odies of the subject invention comprise a thermoplastic elastomer binder in combination with ceramic particulate.
In view of the different characteristics of thermoplastic elastomers, it was not expected that such technique cculd be used to bond compositions containing these elastomers.
Further, using betan-alumina par~iculate precursor in the composition of the tubes, in vîew of its hydroscopic n~ture, was expected to result in an unsatisfactory bond due to the ~o ming conditions that were expected to deveIop at the joint interface of such materials during bondin~.
Still further, the composition of the tubular bodies ~ which includes waxes and oils as plasticizers, was not felt suitable for ultrasonic technique in view of the fact that these included materials usually interfere with the resins abili.ty to transmit vibratory energy. Also, the inclusion of hi~h levels of precursor ceramic, as in the s~bject com~sition~ was thought to preclude the presence of a suf~icient amount of binder material deemed necessary for successful bondingO Tubes which have been extruded using the composition o this invention had previously been end-capped using solvent bonding. However, that technique is l~ss reliable due to such problems as bubbling of the solvent and misalignment of the cap to the tube.
This invention permits improvements in the end-capping of green body tubes comprised of a mixture of sacri~icial binder, densely packed with powdered beta"
alumina precursor particulate such that after binder removal and sintering~ the bond is hermetic and the integrity of ~he bonded area is comparable to the body of the tube. U.SO patents 4,158,688 and 4,158,689 ~o P~t~ et al which are assigned to Ford Motor Company, disclose preparation of green bodies of unusual dimensional precision using sacrificial binders similar to that of this invention. In these patents, the green bodies formed incluae compression molded cordieri~e ribbed sheets and extrusion molded betan-alumina precursor particulate tubes.
The extrusion composition used to make ~he tubes would not be optimal for use as the composition of the tubes which are ultrasonically end-capped by the process o the subject invention.
This invention relates to a method of ultrasonically end-capping a tubular green body so that aft~r binder removal and sintering, the bond is hermetic and the integrity of the bonded area i5 comparable to the 30 body of the tube. The method comprises providing a tubular green body comprised of a mixture of about 40 to 60 vDlume percent sinterable particulate solids and 60 to 40 volume percent organic sacrif icial binder, wherein the binder consists essentially of (a~ a thermoplastic block copolymer component selected from the group consisting of linear, radial, arld linear and radial block copolymers, having a first aromatic block which is glassy or crystalline at 20 to 25C has a softening po~t between about 80 and 250C and a 7;~
second aliphatic block which is differerlt from the first block and behaves as an elastomer at temperatures between about 15C below and about 100C above said softening point of the first block, (b) oil at least about 75 percent 5 by weight of which boils in a range between about 285 to 560C, and which has a viscosi~y of between about 30 and 220 Saybolt Universal Seconds (SUS) at 100C, and has an Aniline Point in a range between about 75 and 125C; (c) wax which melts at a temperature in a range between about 55 and 80C, a~ least 75 percent by weight of which boils at temperatures in a range between about 315C and 490C; (d) first stiffening thermoplastic polymer which is glassy or crystalline at 20 to 25C, has a softening point between about: 80 and 253C and comprises 15 aromatic ~onomeric units associable with block (a); (~) second stifening thermop~astic polymer, different from the first polymer, and which is glas~y or crystalline at 20 to 25C, has a softening point between about 80 and 250C and comprises aromatic monomeric units associable 20 with block copolymer (a) and (f) processing aid comprising esters of fatt~ acids, ~erein ~he sinterable particulate solids consists essentially of a particle size distribution of betan-alumina particulate precursor solids, and the weight of (a) being greater than ~b) and (c) combined, greater 25 than (d~ and (e) combined and greater than about two times (b)5 (c), (d) (e) or (f) alone; forming an end-cap of desired configuration having a composition comprising said mixture, applying pressure and ultrasonic vibrations by means of an ultrasonic horn to the tubular ~reen body and 30 end-cap between a tubular mandrel and the ultrasonic horn maintaining the pressure and ultrasollic vibrations for a time necessary for the ultrasonic vibrations to travel to ~he tubular body end-cap interface wherein they are dissipated in the ~orm of frictional heat and melt the 35 thermoplastic elastomer binder so as to weld the joining surfaces. The mandrel has a shaped end of desired configuration and the ultrasonic horn has a female mold shape adapted to receive the mandrel with the tubular body disposed thereon.
~ s~
More particularly in ultrasonic bonding, the end-cap is first formed by molding or stamping from the same ceramic binder composition as i5 used to form the tube, This end-cap is then placed on the top of the mandrel 5 having the ~ubular green body ~hereon or up into th~ horn.
Most preferably, the tubular mandrel has a hemispherically shaped end as does the face of the horn. In ultrasonic forming, the end-cap is formed by forcin~ the tubular green body between the mandrel and the ultrasonic horn both of which preferably have a hemispherical end shape while ultrasonic vibrations are applied through the horn.
The improved method of ~he invention will be more fully understood from the following detailed description of the invention when read in conjunction with the drawings.
In the detailed description of the invention which follows, reference is made to the accompanying dxawings~ in which:
Figure 1 illustrates ultrasonic welding ~quipment suitable to perform the end-capping of the subject invention; and Figure 2 is a fragmentary cross section view of the horn and mandrel-tube taken along the central axis of the mandrel.
As described above, the improved method of the invention relates to the ultrasonic end-capping Of tubular green bodies comprising a mixture of betan-alumina precursor particulate and sacrificial binder. Each of the components of the mixture within the scope of the invention as well a~ the processing steps are described hereinafter in greater detail.
~ he tubular ~reen bodies which can be end-capped by ~he method of this invention may be formed by either compre sion or extrusion molding. However, they are pxeferably prepared by extrusion molding. The extru~aon molded green bodies can be end-capped by the ultxasonic method of the subject ~nvention. End-ca~ping should , be done as soon after extrusion of the tubing as is 7~
practicalp preferable within two weeks. End-capping by ultrasonic bonding or ultrasonic forming can be performed by means of the ultrasonic welder, sranso~ Model 400C
shown in ~igure 1. Figure 2 illustrates in detail the horn and mandrel of Figure 1 as well as the tube placement. In end-capping by ei~her bonding or forming, a ~ube 1 which has be n carefully cut to give a smooth surface whose face 2 is perpendicular to the length of the tube is placed over the mandrel 3. Th~ mandrel as well as ~he ultrasonic horn 4 preferably have hemispherically shaped ends 5 and 6 respectively. In ultrasonic bonding, an end-cap may be formed by stamping or cutting a disc from a shee~ of ma~erial having the same composition and ~pproximate thickness as that of the tube walls. This end-cap also preferably has a h~mispherical shape. This end cap is then placed centrally up into the ultrasonic horn or pr~ferably on top of the mandrel. The horn is then brought down over the mandrel and pressure and ultrasonic vibrations are applied to weld the joining surfaces. In ultrasonic forming, a tube like that above is placed over the mandrel. The ultrasonic horn is then brought down over the ~Ub? to contact the tube while ultrasonic vibrations are applied, thus forming the tube into an end cap. Ultrasonic vibrations and pressure are applied to weld the joining surfaces. In both the bonding and forming end-capping process, it i5 preferable to rotate the tube during the process.
In the subject invention, circular high gain horns are preferably used. The crown section of the horn is of 30 size of the tubular green body used~ Ultrasonic end capping as taught in this application is generally performed on green body tubes which have a wall thickness of 3 mm or less~ however, tubes having a w211 thickness greater than 3 mm may also be Pnd capped by the process of 35 this invention~ Ultrasonic welding of binder ceramic compositions as carried out in this invention is fast, clean and produces excellent joint int~grity. This process causes minimum distortion and mate-rial degradation.
* - Trademark ~135~7~
After burn out and sintering, tube and end cap have densities 98% of ~heoretical and the line of demarcation between the end cap and the tube no longer exists. The in~erface between the tu~e and end cap now appears to have the same properties as the ~ube.
The following lists the preferred ranges of binder components~ including optional components .
~ he sacrificial binders of this invention comprise a major amount by weight of a block copolymer thermoplastic elastomer, plasticizer therefor and ~hermoplastic polymer.
The block copolymer may be a lin ar block copolymer such as is disclosed in U.S~ Patent 4rl58g689t a radial block copo?ymer such as is disclosed in U.S; Patent 4J158,688, or a combination of these block copolymers.
Suitable radial block polymers for use in this invention are those having the structural formula X-[B-(AB)~-A]~' wherein ~X" is a linking group, A or B, ~ n is O or a positive integer, ~ is a positive integer greater than 2, "A" is a linear or branehed polymer that is glassy or crystalline at room temperature 20 to 25C- and has its soEtening point in the range of about 80C~ to abou~ 250C, and "B" is a polymer different from ''A" that behaves as an elastomer at processing temperatures, i.eO, between about 15C below and about 100C above the softening point of Itp,l~
Suitable linear block polymers for use in this invention are those having the structural formula AB-(AB)a ~ ~
wherein *~ is 0 or a positive integer, "Al' is a linear or branched polymer that is glassy or crystalline at room temperature and has a softening point in the range of about 80C. ~o abou~ 250~C. and "B" is a polymer different from ~A" that behaves as an elastomer at processing temperatures.
Linear and radial block copolymers are widely known. Commercially available linear and radial block copolymers are Rratons*and Solprene~, respectively. Kraton is a tradename of Shell Oil Company and Solprene is a tra~ename of Phillips Petroleum Company. Other examples of these polymers appear in ubb~- ~recl~c~ke~ Thermoplastic Ela~tomers," Hendricks et al, 2nd Edition, pp. 515-533, VAN
NOST ~ND, N.Y. ~1973) and Rubber World, "Compounding Radial Block Copolymers."
The binders of this invention preferably comprise a block copolymer consisting essentially of thermoplastic radial block copolymer. Of the radial block copolym~rs, those with aforedescribed "A" and "B" blocks are preferred 9 with aromatic "A" blocl~ and aliphatic "B" block being preferred. Other nA" and "B" blocks appear in Col. 2, line
ULTRASONIC END-CAPPING OF BETA" ALUMINA TUBES
. .
T~is invention relates to preparation of end-capped tubular betal' alumina ceramic bodies~ In ~ particular, this invention relates to ultrasonic end-capp.ing of extruded beta~-alumina tubular ceramic precursors~ also known as green bodies, such that after binder remcval and sintering the bond is hermetic and the integri~y of the bonded area is comparable to the body of ~he tube~
10Beta~-alumina tubes need to be end-capped at one end in order to be used in construction of sodium- sulfur batteries or similar energy conversion devices.
~ltrasonic end-capping as taught in khis inven~ion, can proceed. by either of two rou~es, ultrasonic forming or ultrasonic bonding, with the latter being preferred.
During the end-capping process, the ultrasonic vibrations from the ultrasonic horn are transmitted to the part and travel to the joint area of interface. Here the vibratory energy i5 dissipated in the form of fri.ctional heat which 20 melts the binder and welds the joining surfaces.
While ultrasonic bonding technique is known, it has only been used to bond materials of thermoplastic compositions. In contrast, the composition of the tllbular ~odies of the subject invention comprise a thermoplastic elastomer binder in combination with ceramic particulate.
In view of the different characteristics of thermoplastic elastomers, it was not expected that such technique cculd be used to bond compositions containing these elastomers.
Further, using betan-alumina par~iculate precursor in the composition of the tubes, in vîew of its hydroscopic n~ture, was expected to result in an unsatisfactory bond due to the ~o ming conditions that were expected to deveIop at the joint interface of such materials during bondin~.
Still further, the composition of the tubular bodies ~ which includes waxes and oils as plasticizers, was not felt suitable for ultrasonic technique in view of the fact that these included materials usually interfere with the resins abili.ty to transmit vibratory energy. Also, the inclusion of hi~h levels of precursor ceramic, as in the s~bject com~sition~ was thought to preclude the presence of a suf~icient amount of binder material deemed necessary for successful bondingO Tubes which have been extruded using the composition o this invention had previously been end-capped using solvent bonding. However, that technique is l~ss reliable due to such problems as bubbling of the solvent and misalignment of the cap to the tube.
This invention permits improvements in the end-capping of green body tubes comprised of a mixture of sacri~icial binder, densely packed with powdered beta"
alumina precursor particulate such that after binder removal and sintering~ the bond is hermetic and the integrity of ~he bonded area is comparable to the body of the tube. U.SO patents 4,158,688 and 4,158,689 ~o P~t~ et al which are assigned to Ford Motor Company, disclose preparation of green bodies of unusual dimensional precision using sacrificial binders similar to that of this invention. In these patents, the green bodies formed incluae compression molded cordieri~e ribbed sheets and extrusion molded betan-alumina precursor particulate tubes.
The extrusion composition used to make ~he tubes would not be optimal for use as the composition of the tubes which are ultrasonically end-capped by the process o the subject invention.
This invention relates to a method of ultrasonically end-capping a tubular green body so that aft~r binder removal and sintering, the bond is hermetic and the integrity of the bonded area i5 comparable to the 30 body of the tube. The method comprises providing a tubular green body comprised of a mixture of about 40 to 60 vDlume percent sinterable particulate solids and 60 to 40 volume percent organic sacrif icial binder, wherein the binder consists essentially of (a~ a thermoplastic block copolymer component selected from the group consisting of linear, radial, arld linear and radial block copolymers, having a first aromatic block which is glassy or crystalline at 20 to 25C has a softening po~t between about 80 and 250C and a 7;~
second aliphatic block which is differerlt from the first block and behaves as an elastomer at temperatures between about 15C below and about 100C above said softening point of the first block, (b) oil at least about 75 percent 5 by weight of which boils in a range between about 285 to 560C, and which has a viscosi~y of between about 30 and 220 Saybolt Universal Seconds (SUS) at 100C, and has an Aniline Point in a range between about 75 and 125C; (c) wax which melts at a temperature in a range between about 55 and 80C, a~ least 75 percent by weight of which boils at temperatures in a range between about 315C and 490C; (d) first stiffening thermoplastic polymer which is glassy or crystalline at 20 to 25C, has a softening point between about: 80 and 253C and comprises 15 aromatic ~onomeric units associable with block (a); (~) second stifening thermop~astic polymer, different from the first polymer, and which is glas~y or crystalline at 20 to 25C, has a softening point between about 80 and 250C and comprises aromatic monomeric units associable 20 with block copolymer (a) and (f) processing aid comprising esters of fatt~ acids, ~erein ~he sinterable particulate solids consists essentially of a particle size distribution of betan-alumina particulate precursor solids, and the weight of (a) being greater than ~b) and (c) combined, greater 25 than (d~ and (e) combined and greater than about two times (b)5 (c), (d) (e) or (f) alone; forming an end-cap of desired configuration having a composition comprising said mixture, applying pressure and ultrasonic vibrations by means of an ultrasonic horn to the tubular ~reen body and 30 end-cap between a tubular mandrel and the ultrasonic horn maintaining the pressure and ultrasollic vibrations for a time necessary for the ultrasonic vibrations to travel to ~he tubular body end-cap interface wherein they are dissipated in the ~orm of frictional heat and melt the 35 thermoplastic elastomer binder so as to weld the joining surfaces. The mandrel has a shaped end of desired configuration and the ultrasonic horn has a female mold shape adapted to receive the mandrel with the tubular body disposed thereon.
~ s~
More particularly in ultrasonic bonding, the end-cap is first formed by molding or stamping from the same ceramic binder composition as i5 used to form the tube, This end-cap is then placed on the top of the mandrel 5 having the ~ubular green body ~hereon or up into th~ horn.
Most preferably, the tubular mandrel has a hemispherically shaped end as does the face of the horn. In ultrasonic forming, the end-cap is formed by forcin~ the tubular green body between the mandrel and the ultrasonic horn both of which preferably have a hemispherical end shape while ultrasonic vibrations are applied through the horn.
The improved method of ~he invention will be more fully understood from the following detailed description of the invention when read in conjunction with the drawings.
In the detailed description of the invention which follows, reference is made to the accompanying dxawings~ in which:
Figure 1 illustrates ultrasonic welding ~quipment suitable to perform the end-capping of the subject invention; and Figure 2 is a fragmentary cross section view of the horn and mandrel-tube taken along the central axis of the mandrel.
As described above, the improved method of the invention relates to the ultrasonic end-capping Of tubular green bodies comprising a mixture of betan-alumina precursor particulate and sacrificial binder. Each of the components of the mixture within the scope of the invention as well a~ the processing steps are described hereinafter in greater detail.
~ he tubular ~reen bodies which can be end-capped by ~he method of this invention may be formed by either compre sion or extrusion molding. However, they are pxeferably prepared by extrusion molding. The extru~aon molded green bodies can be end-capped by the ultxasonic method of the subject ~nvention. End-ca~ping should , be done as soon after extrusion of the tubing as is 7~
practicalp preferable within two weeks. End-capping by ultrasonic bonding or ultrasonic forming can be performed by means of the ultrasonic welder, sranso~ Model 400C
shown in ~igure 1. Figure 2 illustrates in detail the horn and mandrel of Figure 1 as well as the tube placement. In end-capping by ei~her bonding or forming, a ~ube 1 which has be n carefully cut to give a smooth surface whose face 2 is perpendicular to the length of the tube is placed over the mandrel 3. Th~ mandrel as well as ~he ultrasonic horn 4 preferably have hemispherically shaped ends 5 and 6 respectively. In ultrasonic bonding, an end-cap may be formed by stamping or cutting a disc from a shee~ of ma~erial having the same composition and ~pproximate thickness as that of the tube walls. This end-cap also preferably has a h~mispherical shape. This end cap is then placed centrally up into the ultrasonic horn or pr~ferably on top of the mandrel. The horn is then brought down over the mandrel and pressure and ultrasonic vibrations are applied to weld the joining surfaces. In ultrasonic forming, a tube like that above is placed over the mandrel. The ultrasonic horn is then brought down over the ~Ub? to contact the tube while ultrasonic vibrations are applied, thus forming the tube into an end cap. Ultrasonic vibrations and pressure are applied to weld the joining surfaces. In both the bonding and forming end-capping process, it i5 preferable to rotate the tube during the process.
In the subject invention, circular high gain horns are preferably used. The crown section of the horn is of 30 size of the tubular green body used~ Ultrasonic end capping as taught in this application is generally performed on green body tubes which have a wall thickness of 3 mm or less~ however, tubes having a w211 thickness greater than 3 mm may also be Pnd capped by the process of 35 this invention~ Ultrasonic welding of binder ceramic compositions as carried out in this invention is fast, clean and produces excellent joint int~grity. This process causes minimum distortion and mate-rial degradation.
* - Trademark ~135~7~
After burn out and sintering, tube and end cap have densities 98% of ~heoretical and the line of demarcation between the end cap and the tube no longer exists. The in~erface between the tu~e and end cap now appears to have the same properties as the ~ube.
The following lists the preferred ranges of binder components~ including optional components .
~ he sacrificial binders of this invention comprise a major amount by weight of a block copolymer thermoplastic elastomer, plasticizer therefor and ~hermoplastic polymer.
The block copolymer may be a lin ar block copolymer such as is disclosed in U.S~ Patent 4rl58g689t a radial block copo?ymer such as is disclosed in U.S; Patent 4J158,688, or a combination of these block copolymers.
Suitable radial block polymers for use in this invention are those having the structural formula X-[B-(AB)~-A]~' wherein ~X" is a linking group, A or B, ~ n is O or a positive integer, ~ is a positive integer greater than 2, "A" is a linear or branehed polymer that is glassy or crystalline at room temperature 20 to 25C- and has its soEtening point in the range of about 80C~ to abou~ 250C, and "B" is a polymer different from ''A" that behaves as an elastomer at processing temperatures, i.eO, between about 15C below and about 100C above the softening point of Itp,l~
Suitable linear block polymers for use in this invention are those having the structural formula AB-(AB)a ~ ~
wherein *~ is 0 or a positive integer, "Al' is a linear or branched polymer that is glassy or crystalline at room temperature and has a softening point in the range of about 80C. ~o abou~ 250~C. and "B" is a polymer different from ~A" that behaves as an elastomer at processing temperatures.
Linear and radial block copolymers are widely known. Commercially available linear and radial block copolymers are Rratons*and Solprene~, respectively. Kraton is a tradename of Shell Oil Company and Solprene is a tra~ename of Phillips Petroleum Company. Other examples of these polymers appear in ubb~- ~recl~c~ke~ Thermoplastic Ela~tomers," Hendricks et al, 2nd Edition, pp. 515-533, VAN
NOST ~ND, N.Y. ~1973) and Rubber World, "Compounding Radial Block Copolymers."
The binders of this invention preferably comprise a block copolymer consisting essentially of thermoplastic radial block copolymer. Of the radial block copolym~rs, those with aforedescribed "A" and "B" blocks are preferred 9 with aromatic "A" blocl~ and aliphatic "B" block being preferred. Other nA" and "B" blocks appear in Col. 2, line
2~ 56 through Col. 3, line 3 of U.S. Patent 4,158,688~ The * - Trademarks 77~
preferred radical block copolymers, suitable for use in this invention have molecular weights ( ~) of about 100,000-200,000, a specific gravity between 0.9-1.; and an apparent viscosity of between about 40-50 thousand poise at 10 seconds~l at about 20-25C.
The molecular weights of the ilAI1 segments and the "Bl' segments of the block copolymers suitable for use in the method of this invention will vary wi~h the polymer segment involved as will be obvious to one skilled in the art in ~hat physical characteristics must be met as hereinbefore recited. For instance~ where the block copolymer has polystyrene "A" blocks and polybutadiene "B"
blocks, preferrably unsaturated polylbutadienet the polystyrene segments advantageously have number average molecular weights (Mn) below about 20,000 and at least two of such segments have molecular weights (Mn) above about 10,000~ While the polybutadiene segments advantageously have molecular weights (Mn) below about 80rO00 and at least one such segment has a molecular weight Mn) above about 15,000. The lower limit of molecular weight (Mn~ for the two "A" blocks is governed by the mir.imum "A" block chain lenyth required to insure the formation of a heterogeneous phase while the upper limit of "A" blocks is set by the viscosity of both "A" and "B" blocks when such viscosity begins to hamper domain formation or processing.
The sacrifical binder employed in the method of this invention includes a plasticizer comprising oil and a wax in combination. The oils and waxes used for this purpose are naphthenic, paraffinic or a mixture of paraffinic and naphthenic constituents. They are sufficien~ly volatile to be removed easily and rapidly in the burn-out process but insufficiently volatile to be substantially removed during mixing and/or molding. The loss due to volatilization during mixing and/or molding is advantageously below 20 and preferably below 10 weight ~8~
percent. The selection is such that their evolution during burn out takes place over a broad temperature range, thus avoiding stress points and defects in parts.
Functionally, the oils and waxes must be compatible with the rubbery phase of the principal binder resin when it becomes rubbery on plasticization at a temperature somewhat below the softening point of the "A" segments of the principal resin. This gives the binder a capability of accepting higher filler loadings while remaining strong and flexible.
At least 75% by weight of the oils used as plasticizers boil ln the range of about 285C~ to about 560C., preferably in the range of about 285C to about 465C. They have viscosities at 100C. in the range of about 30 to about 220 Saybolt Universal Seconds, hereinafter referred to as S.U.S~, advantageously in the range of about 35 to about 155 S.U.S., and preferably in the range of about 35 to about 80 S.U.S. These oils have an Aniline Point in the ranse of about 75F. to about 125E'. The oils may be a product of petroleum refining operations or vegetable or animal oils and -they may include or ~e low molecular weight synthetic polymers such as polystyrene, poly(alpha-methyl styrene), or a polyolefin. Examples of suitable ` commercially available oils include Flexon* 580, 680, 765 and 845 marketed by Exxon and Shellflex* 131, 371 and 790 marketed by Shell Chemical Co.
The waxes used have melting points in the range of about 55C. to about 80C. At least about 75% by weight of such wax boils at temperatures in the range of about 315C. to about 490C. These may be a product of petroleum refining operations, vegetable or animal oils or synthetic polymers such as low molecular weight polyolefins. Examples of suitable commercially available waxes are Sunoco* Wax 3420, 4412 and 4418 marketed by Sun Chemical as well as paraffin wax (M.P.
54C.~ marketed by International Wax Re~ining.
* Trademarks `~:
. ~ ....
~57~7~
The binder of this invention further includes a first and a second stiffening thermoplastic polymer which are glassy or crystalline at 20-25C, have a softening point between about 80-250C and comprise aromatic monomeric units associable with the block copolymer. The stiffening polymer preferably has a molecular weight in the range between ahout 50,000 and 400,000, more preferably 100,000 and 300~000, wherein such molecular weight refers to a weight average molecular weight (Flory). The second stiffening polym~r is different from the first stiffening polylmer and also functions as a tackifying thermoplastic polymer Preferred second stiffening polymers have a melt viscosity of about 10 poises a~ 157-205C.
For example, if the "A" block of the block copolymer is a polystyrene, then the first stiffening thermoplastic polymer preferably is a polystyrene or other thermoplastic aromatic polymer. In addition to stiffening, such a thermoplastic polymer should also aid in mixing the sacrificial binder composition ingredientsO
thermoplastic polystyrene polymer such as Styron 495, marketed by Dow Chernical Company, does this because it has a lower viscosity than the thermoplastic block copolymer at processing conditions; on the other hand it is sufficiently crystalline at room temperature to advantageously stiffen the formed green body. E`urthermore, according to this example, if the first stiffening polymer is polystyrene as mentioned, the second stifening polymer is aromatic but has a different aromatic moiety, e.g., indene. A preferred second polymer is polyindene. Low molecular weight polyidenes have the further advantage of low viscosity at processing conditions. The low viscosity aids flow of the sacrificial binder compositions.
Using two different polymers also advantageously permits the sequential expulsion of the stiffening polymers during firing of the green bodies.
* ~r ~ a ~ ~
The process aid comprising esters of fatty acids are preferably selected from acetyl ricinoleate esters, which are single and double esters of ricinoleic acidO Their presence serves as an effective processing aid, acting as an anti--stick agent during calendering and extruding. The acetyl ricinoleate esters are also useful in wetting and dispersing the ceramic particulate so as to form a homogeneous mixture. The most useful type of this plasticizer processing aid for the subject invention is the Flexricin~plasticizer, such as Flexrincin P-4, methyl acetyl ricinoleate, and Flexricin P-6, butyl acetyl ricinoleate.
In this particular binder mixture, the weight of the thermoplastic block copolymer is greater than the weight of the oil and wax combined, and greater than the weight of the stiffening polymers combined. The weight of the block copolymer is also greater than two times the weight of the oil, the wax, the first stiffening polymer, the second stiffening polymer or the process aid alone.
Additional process aids which are conventional to molding and forming operations with polymeric materials are likewise useful in the practice of this invention to improve the flow characteristics of the binder-filler mixture to during such operations. Process aids which may be of assistance include fluorocarbon mold release agents, stearic acid, polyethylene, polyethylene wax, mixtures of natural waxes and wax derivatives, vegetable fats, partially oxidized polyethylene, polyterpenes resins, etc.
Others will be apparent to those skilled in the art Other ingredients may be employed in the binders of this invention~ For example/ antioxidants are useful to retard oxidative degradation of the block polymer during mixing r thus minimizing loss of strength in the green body. The antioxidant also allows more rapid removal of binder during burn off by minimizing surface oxidation which may tend to seal off the surface. Suitable antioxidan~s e /~ k . ~ 13 ~
include, but not by way of limitatior,, 2,6-ditert-butyl-phenol, a polymerized 1,2-dihydro-2,2,4-trimethyl quinoline, 2-mercaptobenzimidazole~
tetra-bis-methylene-3-(3,5-ditert-butyl-4-hydroxy ph~nyl) 5 propionate methane, etc.
Sacrificial Binders with O~tiona~ onents_(VolumeL
Percent (Binder 40-60 volume % of total) Solprene 414C 30-80 Agerit~*Resin D 0~6 5unoco Wax 3420~ 5 20 Sunoco '~ax 4412~
Styron 495 2-10 lS Picco*6140-3 2-10 Flexon 845 4-30 Shellflex 371 5~25 Flexricin P~4 2-10 Sinterable Particulate The powdered beta"-alumina precursor partic~late useful in the practice of the method of this application has a particle size (diameter) distribution of between about 0.1-850 microns, with a preferred average particle size of greater than 3.5 microns, most preferably between about 3.5 and about 20 microns. The preferred beta"-a:lumina precursor particulate is prepared by combining sodium carbonate, lithium nitrate and alpha-alumina (Linde C) in such amounts as to form a beta 1l -alumina precursor particulate composition which comprises 8.85% soda/0.75%
lithia/90.40% alumina by weight.
* Trademarks ~357~
The following examples are presented by way of description of the process of the invention and to set forth the best mode contemplated by the inventors, but are not to be construed as limiting.
Example 1 Tubes having 12 mm outside diameter were prepared by extrusion of a typical binder mixture containing the following ingredients. Their length was from 3-20 cm.
Binder Component ~ ~ Wt. ~ Volume ~
.
Solprene 414C 4.80 7.7540% of Binder Agerite Resin D 0.53 0.85 4%
Sunoco Wax 3420 1.15 1.86 10%
Sunoco Wax 4412 0.90 1~45 8%
Styron 495 0.70 1O13 5% "
Picco 6140-3 0.70 1.13 5~ n Flexon 845 0u54 0.87 5~ "
Shellflex 371 1.70 2.74 15% "
Flexricin P-4 0.94 1.52 8% "
beta'l-alumina precursor 50.0080.70 55~ of total mix ( 8.85% Na20, 0.75% Li20 and 90.40% A1203) a) The Preparation of a__Powdered Bn-alumina Precursor: Dried samples of Na2CO3 and LiNO3 were mixed with Linde C A1203 and milled for one hour in a polyethylene container using high-purity A1203 balls~
The ra~io of reagents was chosen so that the final products would have compositions of 8.85% Na20 - 0.75% Li20 -90.40% A1203 by weight. The powders were calcined for two hours at 1260C in platinum crucibles~ On cooling the powders were crushed and milled for one hour in
preferred radical block copolymers, suitable for use in this invention have molecular weights ( ~) of about 100,000-200,000, a specific gravity between 0.9-1.; and an apparent viscosity of between about 40-50 thousand poise at 10 seconds~l at about 20-25C.
The molecular weights of the ilAI1 segments and the "Bl' segments of the block copolymers suitable for use in the method of this invention will vary wi~h the polymer segment involved as will be obvious to one skilled in the art in ~hat physical characteristics must be met as hereinbefore recited. For instance~ where the block copolymer has polystyrene "A" blocks and polybutadiene "B"
blocks, preferrably unsaturated polylbutadienet the polystyrene segments advantageously have number average molecular weights (Mn) below about 20,000 and at least two of such segments have molecular weights (Mn) above about 10,000~ While the polybutadiene segments advantageously have molecular weights (Mn) below about 80rO00 and at least one such segment has a molecular weight Mn) above about 15,000. The lower limit of molecular weight (Mn~ for the two "A" blocks is governed by the mir.imum "A" block chain lenyth required to insure the formation of a heterogeneous phase while the upper limit of "A" blocks is set by the viscosity of both "A" and "B" blocks when such viscosity begins to hamper domain formation or processing.
The sacrifical binder employed in the method of this invention includes a plasticizer comprising oil and a wax in combination. The oils and waxes used for this purpose are naphthenic, paraffinic or a mixture of paraffinic and naphthenic constituents. They are sufficien~ly volatile to be removed easily and rapidly in the burn-out process but insufficiently volatile to be substantially removed during mixing and/or molding. The loss due to volatilization during mixing and/or molding is advantageously below 20 and preferably below 10 weight ~8~
percent. The selection is such that their evolution during burn out takes place over a broad temperature range, thus avoiding stress points and defects in parts.
Functionally, the oils and waxes must be compatible with the rubbery phase of the principal binder resin when it becomes rubbery on plasticization at a temperature somewhat below the softening point of the "A" segments of the principal resin. This gives the binder a capability of accepting higher filler loadings while remaining strong and flexible.
At least 75% by weight of the oils used as plasticizers boil ln the range of about 285C~ to about 560C., preferably in the range of about 285C to about 465C. They have viscosities at 100C. in the range of about 30 to about 220 Saybolt Universal Seconds, hereinafter referred to as S.U.S~, advantageously in the range of about 35 to about 155 S.U.S., and preferably in the range of about 35 to about 80 S.U.S. These oils have an Aniline Point in the ranse of about 75F. to about 125E'. The oils may be a product of petroleum refining operations or vegetable or animal oils and -they may include or ~e low molecular weight synthetic polymers such as polystyrene, poly(alpha-methyl styrene), or a polyolefin. Examples of suitable ` commercially available oils include Flexon* 580, 680, 765 and 845 marketed by Exxon and Shellflex* 131, 371 and 790 marketed by Shell Chemical Co.
The waxes used have melting points in the range of about 55C. to about 80C. At least about 75% by weight of such wax boils at temperatures in the range of about 315C. to about 490C. These may be a product of petroleum refining operations, vegetable or animal oils or synthetic polymers such as low molecular weight polyolefins. Examples of suitable commercially available waxes are Sunoco* Wax 3420, 4412 and 4418 marketed by Sun Chemical as well as paraffin wax (M.P.
54C.~ marketed by International Wax Re~ining.
* Trademarks `~:
. ~ ....
~57~7~
The binder of this invention further includes a first and a second stiffening thermoplastic polymer which are glassy or crystalline at 20-25C, have a softening point between about 80-250C and comprise aromatic monomeric units associable with the block copolymer. The stiffening polymer preferably has a molecular weight in the range between ahout 50,000 and 400,000, more preferably 100,000 and 300~000, wherein such molecular weight refers to a weight average molecular weight (Flory). The second stiffening polym~r is different from the first stiffening polylmer and also functions as a tackifying thermoplastic polymer Preferred second stiffening polymers have a melt viscosity of about 10 poises a~ 157-205C.
For example, if the "A" block of the block copolymer is a polystyrene, then the first stiffening thermoplastic polymer preferably is a polystyrene or other thermoplastic aromatic polymer. In addition to stiffening, such a thermoplastic polymer should also aid in mixing the sacrificial binder composition ingredientsO
thermoplastic polystyrene polymer such as Styron 495, marketed by Dow Chernical Company, does this because it has a lower viscosity than the thermoplastic block copolymer at processing conditions; on the other hand it is sufficiently crystalline at room temperature to advantageously stiffen the formed green body. E`urthermore, according to this example, if the first stiffening polymer is polystyrene as mentioned, the second stifening polymer is aromatic but has a different aromatic moiety, e.g., indene. A preferred second polymer is polyindene. Low molecular weight polyidenes have the further advantage of low viscosity at processing conditions. The low viscosity aids flow of the sacrificial binder compositions.
Using two different polymers also advantageously permits the sequential expulsion of the stiffening polymers during firing of the green bodies.
* ~r ~ a ~ ~
The process aid comprising esters of fatty acids are preferably selected from acetyl ricinoleate esters, which are single and double esters of ricinoleic acidO Their presence serves as an effective processing aid, acting as an anti--stick agent during calendering and extruding. The acetyl ricinoleate esters are also useful in wetting and dispersing the ceramic particulate so as to form a homogeneous mixture. The most useful type of this plasticizer processing aid for the subject invention is the Flexricin~plasticizer, such as Flexrincin P-4, methyl acetyl ricinoleate, and Flexricin P-6, butyl acetyl ricinoleate.
In this particular binder mixture, the weight of the thermoplastic block copolymer is greater than the weight of the oil and wax combined, and greater than the weight of the stiffening polymers combined. The weight of the block copolymer is also greater than two times the weight of the oil, the wax, the first stiffening polymer, the second stiffening polymer or the process aid alone.
Additional process aids which are conventional to molding and forming operations with polymeric materials are likewise useful in the practice of this invention to improve the flow characteristics of the binder-filler mixture to during such operations. Process aids which may be of assistance include fluorocarbon mold release agents, stearic acid, polyethylene, polyethylene wax, mixtures of natural waxes and wax derivatives, vegetable fats, partially oxidized polyethylene, polyterpenes resins, etc.
Others will be apparent to those skilled in the art Other ingredients may be employed in the binders of this invention~ For example/ antioxidants are useful to retard oxidative degradation of the block polymer during mixing r thus minimizing loss of strength in the green body. The antioxidant also allows more rapid removal of binder during burn off by minimizing surface oxidation which may tend to seal off the surface. Suitable antioxidan~s e /~ k . ~ 13 ~
include, but not by way of limitatior,, 2,6-ditert-butyl-phenol, a polymerized 1,2-dihydro-2,2,4-trimethyl quinoline, 2-mercaptobenzimidazole~
tetra-bis-methylene-3-(3,5-ditert-butyl-4-hydroxy ph~nyl) 5 propionate methane, etc.
Sacrificial Binders with O~tiona~ onents_(VolumeL
Percent (Binder 40-60 volume % of total) Solprene 414C 30-80 Agerit~*Resin D 0~6 5unoco Wax 3420~ 5 20 Sunoco '~ax 4412~
Styron 495 2-10 lS Picco*6140-3 2-10 Flexon 845 4-30 Shellflex 371 5~25 Flexricin P~4 2-10 Sinterable Particulate The powdered beta"-alumina precursor partic~late useful in the practice of the method of this application has a particle size (diameter) distribution of between about 0.1-850 microns, with a preferred average particle size of greater than 3.5 microns, most preferably between about 3.5 and about 20 microns. The preferred beta"-a:lumina precursor particulate is prepared by combining sodium carbonate, lithium nitrate and alpha-alumina (Linde C) in such amounts as to form a beta 1l -alumina precursor particulate composition which comprises 8.85% soda/0.75%
lithia/90.40% alumina by weight.
* Trademarks ~357~
The following examples are presented by way of description of the process of the invention and to set forth the best mode contemplated by the inventors, but are not to be construed as limiting.
Example 1 Tubes having 12 mm outside diameter were prepared by extrusion of a typical binder mixture containing the following ingredients. Their length was from 3-20 cm.
Binder Component ~ ~ Wt. ~ Volume ~
.
Solprene 414C 4.80 7.7540% of Binder Agerite Resin D 0.53 0.85 4%
Sunoco Wax 3420 1.15 1.86 10%
Sunoco Wax 4412 0.90 1~45 8%
Styron 495 0.70 1O13 5% "
Picco 6140-3 0.70 1.13 5~ n Flexon 845 0u54 0.87 5~ "
Shellflex 371 1.70 2.74 15% "
Flexricin P-4 0.94 1.52 8% "
beta'l-alumina precursor 50.0080.70 55~ of total mix ( 8.85% Na20, 0.75% Li20 and 90.40% A1203) a) The Preparation of a__Powdered Bn-alumina Precursor: Dried samples of Na2CO3 and LiNO3 were mixed with Linde C A1203 and milled for one hour in a polyethylene container using high-purity A1203 balls~
The ra~io of reagents was chosen so that the final products would have compositions of 8.85% Na20 - 0.75% Li20 -90.40% A1203 by weight. The powders were calcined for two hours at 1260C in platinum crucibles~ On cooling the powders were crushed and milled for one hour in
3~ polyethylene vessels using A1203 balls. X-Ray defraction indica~ed the composition of the milling operation effectively broke down the loosely bonded agglomerates formed during calcination~
I
~85~
(b) Mlxing of beta''-alumina precursor with binder ingredients:
_ Mixing of the binder composition is carried out on a x 180 mm two-roll, vented research mill. The mill rolls were elec~rically heated with individual heat controls and chrome coated, The mill speed was 3.2 m per minutP and had a friction ratio of 1.4 to 1~ The gap between the rolls varied from 0.17 to 0076 mm during mixins 9 The temperature of both rolls was se~ at 155C
and allowed tG stabilize.
The order of addition of binder ingredients and specific conditions used in the mixing steps are listed belo~:
1~ Set roll gap a~ 0.17 mm and add thermoplastic elastomer (Solprene 414)~ As soon as a Solprene 414 melt is formed on the rolls, add 5% by wt. of betal'-alumina precursor and the Agerite resin D.
2. Subsequently keep opening the mill rolls and adding the rest of the beta"-alumina precursor. The gap between the two rolls should be 0.70 - 0.7~ mm at the co~pletion of addition of beta"-alumina precursor.
3. Add petxoleum waxes slowly (Sonoco wax 3420 and 4412). The powdery material f~lling off the mill rolls is placed on mill rolls continuously. The banded material at edges of rolls is cut with sharp knife and placed on center of rolls repeatedly. The temperature of rolls is raised to 160~C for the next step.
I
~85~
(b) Mlxing of beta''-alumina precursor with binder ingredients:
_ Mixing of the binder composition is carried out on a x 180 mm two-roll, vented research mill. The mill rolls were elec~rically heated with individual heat controls and chrome coated, The mill speed was 3.2 m per minutP and had a friction ratio of 1.4 to 1~ The gap between the rolls varied from 0.17 to 0076 mm during mixins 9 The temperature of both rolls was se~ at 155C
and allowed tG stabilize.
The order of addition of binder ingredients and specific conditions used in the mixing steps are listed belo~:
1~ Set roll gap a~ 0.17 mm and add thermoplastic elastomer (Solprene 414)~ As soon as a Solprene 414 melt is formed on the rolls, add 5% by wt. of betal'-alumina precursor and the Agerite resin D.
2. Subsequently keep opening the mill rolls and adding the rest of the beta"-alumina precursor. The gap between the two rolls should be 0.70 - 0.7~ mm at the co~pletion of addition of beta"-alumina precursor.
3. Add petxoleum waxes slowly (Sonoco wax 3420 and 4412). The powdery material f~lling off the mill rolls is placed on mill rolls continuously. The banded material at edges of rolls is cut with sharp knife and placed on center of rolls repeatedly. The temperature of rolls is raised to 160~C for the next step.
4. Then polystyrene (Styron 495) and polyindene resin (Picco-6140-3) are added to the mix in that order.
The mix is still crumbling at this stage. The banded material at edges of rolls is cut continuously and placed in center of rolls until completion of mixing.
7;~
- 16 ~
5c The addi~ion of Flexon 845 and Shellflex 371 follows with cutting of material at edges of rolls and returning the cut and crumbled material to the middle of rolls~
6. Flexricin P-4 is incorporated to the mix slightly slower ~han the o~her two oils. The temperature of rolls is brought to 138C before initiation of addition of Flexricin P-4.
7. Upon completion of addition of all the ingredien~s, the mix is cut at edges of rolls and sliced in middle of rolls for 5 minutes. The cut ma~erial is returned to the center of rolls.
8. Mixing is completed within 40 45 minutes.
9~ The mill is set at a speed of 1.5 m/~e~ and the mix is sliced off the mill and transferred to the extrusion set-up.
lOo Total weight of mixed material is 62~0 gms.
At the completion of mixing cycle, the binder composition is homogeneous. This is indicated by brPaking a small piece of tape and examining its consistency.
c) Extrusion _ ; .
G~5 e G~ ' A ram type extrusion apparatus was'to extrude the green body tubes. The techniques for extruding different sizes of tubes (diameter and wall thickness) differed primarily in the die set used for the extrusion.
7'7~
To perform the extrusion, mixed binder and ceramic composition is broken or cut into a size convenient for insertion into the barrel of the extruder. After insertion into the preheated extruder barrel, the ram is inserted and a force of approximately 250 kg to 500 kg is applied to pack the composition. At this point the ram is stopped and the force allowed to decay as the composition is preheated for about 15 minutes prior to extrusion. After the preheat, the ram is once again forced against the composition until tube extrudes from the die orifice. The rate at which tube is extruded and the temperatures of the barrel and die are adjusted until a smooth tube is obtained. Typical extrusion rates are 600 mm/min for the 12 mm tube and 100 mm/min for the 7 mm tube. The tube is extruded over a mandrel of 10.5 mm diameter for the 12 mm tubing and 6.5 mm diameter for the 7 mm tubing. This is done to maintain straight tubing while the green body is still hot enough to deform easily. After a sufficient length of tubing has been extruded, it is cut fxom the die and placed on another mandrel for cooling to room temperature. After reaching ambient temperature, the tubing can be easily handled, cut and stored without use o~ a mandrel.
d) End-Cappi~L~ tubes The shaped caps were ob-tained by placing the same binder mixture (as mixture used to extrude tubes) on an 80 x 180 mm two-roll mill. After the material was banded~ the rolls were adjusted for obtaining binder sheets with a thickness of 1 mm. Cixcular disks were cut from the binder sheets with a disk diameter equal tc the outside diameter of tube (12 mm). Hemispherically shaped caps were obtained by taking disks cut from the milled sheet and pressing these disks into a hemispherical teflon cavity (heated to 150C), by using a brass or steel mandrel whose end has been shaped to give the device the hemispherical shape of the interior of the end cap.
:-, The apparatus used for ultrasonic end-capping was a Branson, Model 400C, Ultrasonic Welder. Using this ultrasonic welder, molded caps of a variety of shapes have been successfully bonded. A tube which has been carefully cut to give a smooth surface whose ace is perpendicular to the length of the tube is placed over a mandrel. The horn of the ultrasonic welder (Branson, Model 400C, ultrasonic welder~ has a tube shape with a hemispherical end cut into the base of the horn. The end-cap is then centrally placed on top of the mandrel. Alternately but less desirably, thP end-cap is placed up into the horn and positioned with a solid rod having a flat end cut perpendicular to the length of the rod. The horn of the ultrasonic welder is then carefully brought down to give initial contact between the end-cap and the tube. Ultrasonic power is applied while the horn is lowered to its final position to produce the bond. The various horns used for end-capping different diameter (O.D.) and thickess tubes were tuned to between 19,950 and 20,000 Hz. Although not mandatory, a better success rate in producing helium leak tight end-capped tubes was achieved if the tubes were rotated during the ultrasonic bonding. Generally, a total time of 15 seconds from power on to power off was adequate. It has been found advantageous to apply ultrasonics for 3 to 5 seconds prior to applying pressure with the ultrasonic horn, after which the ultrasonics are applied for 5 to 15 seconds with this pressure. Pressure may be retained for 5 to 10 seconds after the ultrasonics are turned off, in order to allow the end-capped tube to cool, and then the horn is raised to allow removal of the tube from the mandrel. For better ultrasonic end-capping~ it was found necessary, in order to obtain better sealing, to use high amplitude vibrations.
As a result, a black booster horn was attached between the converter and aluminum horn. This change resulted in increasing the amount of amplitude by 2.5 times at the face of horn. This increased amplitude was most suitable for cnd-capping.
~85~7~
(e)Binder removal . . _ Binder removal is accomplished by heating the tubes in a circulating oven (Temperite~ Type MU 182424A) using filtered air as the atmosphere. It has been found to be advantageous to support the tubes in a vertical position by slipping them over an alumina mandrel whose diameter is small enough to allow for shrinka~e of the tube during binder removal. The tubes were removed from the burn-out oven and placed immedia-tely in a desiccator which has been preheated to 65~C. Tubes and desiccator are allowed to cool to room tem~erature and the tubes are held in the desiccator until needed for sintering. A typical burn-out schedule is found in the following table~
Temperature Range Rate GC C/Hour 150 - 600 9.7 600 hold for 4 hours 150 hold for 7.3 hours lS0 65 Allow oven to cool at its own , rate f) Sintering After binder burn out tubes were encapsulated in platinum cylinders and arranged in vertical positions in a cold furnaceO The furnace was slowly heated to 1585C, held for fifteen minutes, cooled to 1~00C, held for one ~,he~) :
hour, t~ allowed to cool to room temperaturec After burn out and sintering of end~capped tubes, it was found that they were hermetically sealed.
Hermeticity was checked with a Veeco Model 12 helium leak detectorr The resistivity and modulus of rupture of the sintered 10 mm O.D~ tube were 4.6 ohm-cm at 300C and 500 ~85~7~72 - 2~ -MN/CM2 respectively. The efficiency of sound end-capped tubes was good. During burn out and sintering, tubes shrink by approximately 20%.
Example 2 The procedure of Example 1 was repeated with the exception that the hemispherically shaped cap was grinded with a brass screen so that complete contact betwe~n tube and cap was obtained before the application of ultrasonic vibrations. The efficiency of leak tight end-capped tubes lQ was slightly increased. No flash was generated by the end-capping proFess.
Example 3 Example 1 was repeated with the excep~ion that flat disks with a 12 mm diameter were used for the end-capping. Leak tight end-capped tubes were obtained.
The efficiency of sound end-capped tubes was slightly lower because of misalignment of cap and tube.
Example 4 The procedure of Example 1 was repeated with the e~ception that the end-cap had a piston-like shape. It was prepared by compression molding of binder composition at 150C. Half of this cap had a diameter equal to the inside diameter of tube and half had a diameter equal to the outside diameter of tube. Upon application of ultrasonics9 end-capped tubes with good hermeticity and properties were obtained.
Example 5 Example 1 was repeated with the exception that a hemispherically shaped end-cap was prepared by compression molding. For higher efficiency of ultrasonically end-capped tubes, the joining oE tube to cap should take place close to the end of hemispherical section. The ultrasonic intensity of horn is not as high in straight section as in hemispherical.
~577~
Example 6 Example 1 is repeated with the exception that a higher pressure is exerted on the part by the horn. Upon application of over 100 lbs pressure on green tube, crack formation increases and efficiency at leak tight tubes decrease.
Exam~le 7 The procedure of Example 1 is repeated with the exception that the area of cap to be attached to the tube is exposed to methylene chloride before application of ultrasonic vibrations. At the completion of welding the tube-cap interface is not visible. Thus the appearance of end-capped tubes was improved. These tubes were leak tight.
Exam~le 8 Example 1 is repeated again with the exception that a larger diameter disk was used (15-17 mm). This size disk was chosen to avoid misalignment problems in end-capping but we run across the flash problem arising ~0 from larger diameter disks. Bo'ch of these problems were eliminated by heating the disk at 150C, placing it over the tube, and lowering the horn for the application of ultrasonic vibrations. On lowering the horn, the hot disk was shaven off by horn to optimum diameter. The end-capped tubes were leak tight and had good appearance.
Example 9 Upon repeating Example 8, the larger diameter disk and tube were heated at 150C before the application of ultrasonic vibrations. Upon welding the cap to the tube there was buckling of tube close to the interface~
-~2-Example 10 An 18 mm tube (outside diameter) was pxecision cut to a length of 10 cm as the 12 mm tube of Example 1.
A disk with a diameter of 22 mm was stamped out from a milled sheet of binder material. After heating the disk at 150C, it was placed on top of tube and horn was brought down to make contact with the parts. On lowerillg the horn, the cap was shaven off to suitable size for end-capping. Leak tigh~ -tubes were obtained after burn out and sintering.
Example 11 The procedure of Example 10 was repeated with the exception that the length of the 18 mm tube is 20 centimeters. A longer mandrel for supporting the tube was constructed for use in end-capping these longer tubes. Upon application of ultrasonic vibration the cap was attached to the tube. The hermeticity of tubes determined with the helium leak detector was good.
Example 12 The procedure of Example 11 was repeated with the exception that the thickness of disk was changed from 1.4 mm to 2 mm. Upon application of ultrasonic vibrations, sealed tubes were obtained with good hermeticity. The joint area was not as smooth as in tubes o~ Example 11.
Example_13 The procedure of Example 10 was repeated with the exception that the ultrasonic horn was coated with a Teflon* coating. The end-capped tubes had no aluminum film originating from aluminum horn. They were hermetically sealed.
Example 14 The procedure of Example 1 was repeated with the exception that Flexricin P-4 was increased from 0.94 gms to * Trademarks 1~17~ On compounding this mixture, it was softer and was used for preparation of disks. The tubes were prepared by using the amounts of binder components of Example 1. Tubes with good hermeticity were obtained.
The joint area was smootn. A softer cap and a stiffer tube were preferred~
The volume fraction of beta"-alumina precursor powder in Example 1 was increased to 56% and the volume fraction of organic ingredients was reduced to 44% of total mix.
The procedure of example 1 was repeated and good end-capped tubes were obtained.
Example 15 The volume fraction of beta"-alumina precursor powder in Example 1 was reduced to 54~ and the volume fraction of organic ingredients was increased to 46% of total mix.
Upon repeating the procedure of Example 1, end-capped tubes with good hermeticity were obtained.
Example 17 Another binder mixture is prepared with the exception of reducing the amount of wax 3420 by 0.35 grams and incoroporating 0.35 grams of Wingtack 95. Tubes (18 mm O.D.) and disks made from this mixture were used for end-capping as in example 1. The strength of bond in these end-capped tubes was higher. Good end-capped tubes were obtained.
.
Example 18 Another binder mixture is prepared with the -exception of reducing the amount of wax 3420 by 0.50 grams and incorporating 0O50 grams of Wingtack Plus. A
homogeneous mixture was obtained after mixing ingredients.
Good end-capped tubes were obtained from this mixture after it was aged for a monthO The Wingtack resins is d e ~ .
, .
~' , _ ,. .. .. .
~8~7~
particularly useful in situations involving delayed end-capping of the tubes.
Example 19 Tubes with an outside diameter of 7mm and disks with 0.5 mm thickness were prepared from binder compound described in Example 1. Upon ultrasonic end-capping the closed tubes bulged close to the joint areaO This is due to the fact that thin wall tubes cannot take pressure as well as thicker tubes.
Example 20 The tubes and disks described in Example 19 were used again for end capping. The tube was supported by placing a grass sleeve around the tube. Upon application of ultrasonic vibrations, the buldging on closed tubes was reduced.
Example 21 The procedure of Example 1 was repeated with the exception that the powder beta"-alumina precursor had the composition ~.7% Na20/0.7% Li20/90.6% A12O3. The ef~iciency of the tubes was not as high as when using the composition of Example 1.
Example 22 The procedure of Example 1 was repeated with the exception that the powdered beta"-alumina precursor had the composition 9.0% Na20/0.8% Li20/ 90.2% A1203. The efficiency of the tubes was not as high as when using the composition of Example 1.
Example 23 The procedure of Example 8 is repeated with the exception that the larger disk is not heated before the applica~ion of ultrasonics. The closed tubes are rubbed with methylene chloride at interface to remove excessive flash. Efficiency is not as high as in Example B.
~8~7~;~
~ 25 -Example 24 The procedure of Example 23 is repeated with the exception that methyl ethyl ketone is used for removal of ~ e ~5, v~
-e~-ec~ibc- flashO The solvent is removed from tube interface very slowly. The efficiency of sound tubes is not as high as in cases where no solvent is used.
Example 25 Example 1 was repeated with the exception that ultrasonic forming was used for closing one end of the ~ irCC,~
circul~ 12 mm outside diameter tube. A tube which has been carefully cut to give a smooth surface whose face is perpendicular to the length of the tube is placed over a mandrel. The horn of ultrasonic welder (Branson Model 400 C) which has a hemispherical cavity cut into the face of the horn is then carefully brought down to make contact with the end of tube. Ultrasonic power is applied while the black booster horn (high amplitude vibrations) is lowered to its final position for closing the tube.
Ultrasonic forming uses no end caps. Upon burn out of binder and sintering, the tube were formed to be hermetically sealed. As with ultrasonic bonding it was found advantageous to rotate the tubes during this process to form an even smooth shape.
Example 26 Example 25 was repeated with the exception that the outside diameter of tube is 25 mm. These tubes were ultrasonically formed. Af~er burn out of binder and sintering, the tubes had good properties.
Example 27 Example 25 was repeated with the exception that the outside diameter of tube was 18 mm~ The tubes were rotated during ultrasonic forming. The formed tubes had improved appearance.
~8~7~7~
In the above Examples 1 - 27, Solprene 414C is a thermoplastic elastomer manufactured by Phillips Petroleum.
It is a radial block copolymer of styrene and butadiene with a molecular weight (Mw) of about 160,000. The 414C
has a specific gravity of 0.95, melt flow of 72 (grams/10 min. at 190C and apparent viscosity of 46,000 poise at 10 sec~~l at room temperature. Agerite Resin D is an antioxidant available from Vanderbilt Company; it is a polymerized 1,2-dihydro-2,2,4-trimethyl quinoline. Typical properties of Agerite Resin D are specific gravity - 1.06;
softening point ~ 74C; and very soluble in acetone Sunoco Wax 3420 is a paraffinic wax that melts at 58Co Specific gravity at 150C is 1.2 g/cc and kinematic viscosity is 3.6 centistokes at 99C. Sunoco Wax 4412 is a paraffinic wax that melts at 63C. Specific gravity is 0~925 at 60C and kinematic viscosity at 99C is 4.2 centistokes. Styron 495 is a polystyrene available from Dow Chemical Company; it has a vicat softening point of 97C, melt flow rate of 3.5 grams/10 min. and specific gravity of 1.05 at 150C.
Styron 495 has a molecular weight (Mw) of about 200,000.
Picco 6140-3 is a polyindene available from Hercules; its melt viscosity is 10 poises at 205C~ The softening point is 140C and density 1.07 at 25C. Flexon 845 is a paraffinic petroleum oil from Exxon Chemical Company.
Flexon 845 has a viscosity of 230 SUS at 99C and ASniline Point is 117C. Shellflex 371 is a paraffinic-napthenic oil available from Shell Oil Company. Shellflex has a specific gravity of 0.897 at 150C; it has 49% paraffinic carbon, 50% naphthenic carbon and 1~ aromatic carbon. The molecular weight is 400, viscosity at 38C is 427 SUS., and Aniline Point is 100C. Flexricin P-4 is methyl acetyl ricinoleateO Its specific gravity is 0.936 and boiling point at 2 mm is 185C. Its molecular weight is 346 ~ingtack Plus are resins available from Goodyear Chemical Company. Winqtack 95, considered a synthetic polyterpene, has a softening point of 100Co Specific gravity at
The mix is still crumbling at this stage. The banded material at edges of rolls is cut continuously and placed in center of rolls until completion of mixing.
7;~
- 16 ~
5c The addi~ion of Flexon 845 and Shellflex 371 follows with cutting of material at edges of rolls and returning the cut and crumbled material to the middle of rolls~
6. Flexricin P-4 is incorporated to the mix slightly slower ~han the o~her two oils. The temperature of rolls is brought to 138C before initiation of addition of Flexricin P-4.
7. Upon completion of addition of all the ingredien~s, the mix is cut at edges of rolls and sliced in middle of rolls for 5 minutes. The cut ma~erial is returned to the center of rolls.
8. Mixing is completed within 40 45 minutes.
9~ The mill is set at a speed of 1.5 m/~e~ and the mix is sliced off the mill and transferred to the extrusion set-up.
lOo Total weight of mixed material is 62~0 gms.
At the completion of mixing cycle, the binder composition is homogeneous. This is indicated by brPaking a small piece of tape and examining its consistency.
c) Extrusion _ ; .
G~5 e G~ ' A ram type extrusion apparatus was'to extrude the green body tubes. The techniques for extruding different sizes of tubes (diameter and wall thickness) differed primarily in the die set used for the extrusion.
7'7~
To perform the extrusion, mixed binder and ceramic composition is broken or cut into a size convenient for insertion into the barrel of the extruder. After insertion into the preheated extruder barrel, the ram is inserted and a force of approximately 250 kg to 500 kg is applied to pack the composition. At this point the ram is stopped and the force allowed to decay as the composition is preheated for about 15 minutes prior to extrusion. After the preheat, the ram is once again forced against the composition until tube extrudes from the die orifice. The rate at which tube is extruded and the temperatures of the barrel and die are adjusted until a smooth tube is obtained. Typical extrusion rates are 600 mm/min for the 12 mm tube and 100 mm/min for the 7 mm tube. The tube is extruded over a mandrel of 10.5 mm diameter for the 12 mm tubing and 6.5 mm diameter for the 7 mm tubing. This is done to maintain straight tubing while the green body is still hot enough to deform easily. After a sufficient length of tubing has been extruded, it is cut fxom the die and placed on another mandrel for cooling to room temperature. After reaching ambient temperature, the tubing can be easily handled, cut and stored without use o~ a mandrel.
d) End-Cappi~L~ tubes The shaped caps were ob-tained by placing the same binder mixture (as mixture used to extrude tubes) on an 80 x 180 mm two-roll mill. After the material was banded~ the rolls were adjusted for obtaining binder sheets with a thickness of 1 mm. Cixcular disks were cut from the binder sheets with a disk diameter equal tc the outside diameter of tube (12 mm). Hemispherically shaped caps were obtained by taking disks cut from the milled sheet and pressing these disks into a hemispherical teflon cavity (heated to 150C), by using a brass or steel mandrel whose end has been shaped to give the device the hemispherical shape of the interior of the end cap.
:-, The apparatus used for ultrasonic end-capping was a Branson, Model 400C, Ultrasonic Welder. Using this ultrasonic welder, molded caps of a variety of shapes have been successfully bonded. A tube which has been carefully cut to give a smooth surface whose ace is perpendicular to the length of the tube is placed over a mandrel. The horn of the ultrasonic welder (Branson, Model 400C, ultrasonic welder~ has a tube shape with a hemispherical end cut into the base of the horn. The end-cap is then centrally placed on top of the mandrel. Alternately but less desirably, thP end-cap is placed up into the horn and positioned with a solid rod having a flat end cut perpendicular to the length of the rod. The horn of the ultrasonic welder is then carefully brought down to give initial contact between the end-cap and the tube. Ultrasonic power is applied while the horn is lowered to its final position to produce the bond. The various horns used for end-capping different diameter (O.D.) and thickess tubes were tuned to between 19,950 and 20,000 Hz. Although not mandatory, a better success rate in producing helium leak tight end-capped tubes was achieved if the tubes were rotated during the ultrasonic bonding. Generally, a total time of 15 seconds from power on to power off was adequate. It has been found advantageous to apply ultrasonics for 3 to 5 seconds prior to applying pressure with the ultrasonic horn, after which the ultrasonics are applied for 5 to 15 seconds with this pressure. Pressure may be retained for 5 to 10 seconds after the ultrasonics are turned off, in order to allow the end-capped tube to cool, and then the horn is raised to allow removal of the tube from the mandrel. For better ultrasonic end-capping~ it was found necessary, in order to obtain better sealing, to use high amplitude vibrations.
As a result, a black booster horn was attached between the converter and aluminum horn. This change resulted in increasing the amount of amplitude by 2.5 times at the face of horn. This increased amplitude was most suitable for cnd-capping.
~85~7~
(e)Binder removal . . _ Binder removal is accomplished by heating the tubes in a circulating oven (Temperite~ Type MU 182424A) using filtered air as the atmosphere. It has been found to be advantageous to support the tubes in a vertical position by slipping them over an alumina mandrel whose diameter is small enough to allow for shrinka~e of the tube during binder removal. The tubes were removed from the burn-out oven and placed immedia-tely in a desiccator which has been preheated to 65~C. Tubes and desiccator are allowed to cool to room tem~erature and the tubes are held in the desiccator until needed for sintering. A typical burn-out schedule is found in the following table~
Temperature Range Rate GC C/Hour 150 - 600 9.7 600 hold for 4 hours 150 hold for 7.3 hours lS0 65 Allow oven to cool at its own , rate f) Sintering After binder burn out tubes were encapsulated in platinum cylinders and arranged in vertical positions in a cold furnaceO The furnace was slowly heated to 1585C, held for fifteen minutes, cooled to 1~00C, held for one ~,he~) :
hour, t~ allowed to cool to room temperaturec After burn out and sintering of end~capped tubes, it was found that they were hermetically sealed.
Hermeticity was checked with a Veeco Model 12 helium leak detectorr The resistivity and modulus of rupture of the sintered 10 mm O.D~ tube were 4.6 ohm-cm at 300C and 500 ~85~7~72 - 2~ -MN/CM2 respectively. The efficiency of sound end-capped tubes was good. During burn out and sintering, tubes shrink by approximately 20%.
Example 2 The procedure of Example 1 was repeated with the exception that the hemispherically shaped cap was grinded with a brass screen so that complete contact betwe~n tube and cap was obtained before the application of ultrasonic vibrations. The efficiency of leak tight end-capped tubes lQ was slightly increased. No flash was generated by the end-capping proFess.
Example 3 Example 1 was repeated with the excep~ion that flat disks with a 12 mm diameter were used for the end-capping. Leak tight end-capped tubes were obtained.
The efficiency of sound end-capped tubes was slightly lower because of misalignment of cap and tube.
Example 4 The procedure of Example 1 was repeated with the e~ception that the end-cap had a piston-like shape. It was prepared by compression molding of binder composition at 150C. Half of this cap had a diameter equal to the inside diameter of tube and half had a diameter equal to the outside diameter of tube. Upon application of ultrasonics9 end-capped tubes with good hermeticity and properties were obtained.
Example 5 Example 1 was repeated with the exception that a hemispherically shaped end-cap was prepared by compression molding. For higher efficiency of ultrasonically end-capped tubes, the joining oE tube to cap should take place close to the end of hemispherical section. The ultrasonic intensity of horn is not as high in straight section as in hemispherical.
~577~
Example 6 Example 1 is repeated with the exception that a higher pressure is exerted on the part by the horn. Upon application of over 100 lbs pressure on green tube, crack formation increases and efficiency at leak tight tubes decrease.
Exam~le 7 The procedure of Example 1 is repeated with the exception that the area of cap to be attached to the tube is exposed to methylene chloride before application of ultrasonic vibrations. At the completion of welding the tube-cap interface is not visible. Thus the appearance of end-capped tubes was improved. These tubes were leak tight.
Exam~le 8 Example 1 is repeated again with the exception that a larger diameter disk was used (15-17 mm). This size disk was chosen to avoid misalignment problems in end-capping but we run across the flash problem arising ~0 from larger diameter disks. Bo'ch of these problems were eliminated by heating the disk at 150C, placing it over the tube, and lowering the horn for the application of ultrasonic vibrations. On lowering the horn, the hot disk was shaven off by horn to optimum diameter. The end-capped tubes were leak tight and had good appearance.
Example 9 Upon repeating Example 8, the larger diameter disk and tube were heated at 150C before the application of ultrasonic vibrations. Upon welding the cap to the tube there was buckling of tube close to the interface~
-~2-Example 10 An 18 mm tube (outside diameter) was pxecision cut to a length of 10 cm as the 12 mm tube of Example 1.
A disk with a diameter of 22 mm was stamped out from a milled sheet of binder material. After heating the disk at 150C, it was placed on top of tube and horn was brought down to make contact with the parts. On lowerillg the horn, the cap was shaven off to suitable size for end-capping. Leak tigh~ -tubes were obtained after burn out and sintering.
Example 11 The procedure of Example 10 was repeated with the exception that the length of the 18 mm tube is 20 centimeters. A longer mandrel for supporting the tube was constructed for use in end-capping these longer tubes. Upon application of ultrasonic vibration the cap was attached to the tube. The hermeticity of tubes determined with the helium leak detector was good.
Example 12 The procedure of Example 11 was repeated with the exception that the thickness of disk was changed from 1.4 mm to 2 mm. Upon application of ultrasonic vibrations, sealed tubes were obtained with good hermeticity. The joint area was not as smooth as in tubes o~ Example 11.
Example_13 The procedure of Example 10 was repeated with the exception that the ultrasonic horn was coated with a Teflon* coating. The end-capped tubes had no aluminum film originating from aluminum horn. They were hermetically sealed.
Example 14 The procedure of Example 1 was repeated with the exception that Flexricin P-4 was increased from 0.94 gms to * Trademarks 1~17~ On compounding this mixture, it was softer and was used for preparation of disks. The tubes were prepared by using the amounts of binder components of Example 1. Tubes with good hermeticity were obtained.
The joint area was smootn. A softer cap and a stiffer tube were preferred~
The volume fraction of beta"-alumina precursor powder in Example 1 was increased to 56% and the volume fraction of organic ingredients was reduced to 44% of total mix.
The procedure of example 1 was repeated and good end-capped tubes were obtained.
Example 15 The volume fraction of beta"-alumina precursor powder in Example 1 was reduced to 54~ and the volume fraction of organic ingredients was increased to 46% of total mix.
Upon repeating the procedure of Example 1, end-capped tubes with good hermeticity were obtained.
Example 17 Another binder mixture is prepared with the exception of reducing the amount of wax 3420 by 0.35 grams and incoroporating 0.35 grams of Wingtack 95. Tubes (18 mm O.D.) and disks made from this mixture were used for end-capping as in example 1. The strength of bond in these end-capped tubes was higher. Good end-capped tubes were obtained.
.
Example 18 Another binder mixture is prepared with the -exception of reducing the amount of wax 3420 by 0.50 grams and incorporating 0O50 grams of Wingtack Plus. A
homogeneous mixture was obtained after mixing ingredients.
Good end-capped tubes were obtained from this mixture after it was aged for a monthO The Wingtack resins is d e ~ .
, .
~' , _ ,. .. .. .
~8~7~
particularly useful in situations involving delayed end-capping of the tubes.
Example 19 Tubes with an outside diameter of 7mm and disks with 0.5 mm thickness were prepared from binder compound described in Example 1. Upon ultrasonic end-capping the closed tubes bulged close to the joint areaO This is due to the fact that thin wall tubes cannot take pressure as well as thicker tubes.
Example 20 The tubes and disks described in Example 19 were used again for end capping. The tube was supported by placing a grass sleeve around the tube. Upon application of ultrasonic vibrations, the buldging on closed tubes was reduced.
Example 21 The procedure of Example 1 was repeated with the exception that the powder beta"-alumina precursor had the composition ~.7% Na20/0.7% Li20/90.6% A12O3. The ef~iciency of the tubes was not as high as when using the composition of Example 1.
Example 22 The procedure of Example 1 was repeated with the exception that the powdered beta"-alumina precursor had the composition 9.0% Na20/0.8% Li20/ 90.2% A1203. The efficiency of the tubes was not as high as when using the composition of Example 1.
Example 23 The procedure of Example 8 is repeated with the exception that the larger disk is not heated before the applica~ion of ultrasonics. The closed tubes are rubbed with methylene chloride at interface to remove excessive flash. Efficiency is not as high as in Example B.
~8~7~;~
~ 25 -Example 24 The procedure of Example 23 is repeated with the exception that methyl ethyl ketone is used for removal of ~ e ~5, v~
-e~-ec~ibc- flashO The solvent is removed from tube interface very slowly. The efficiency of sound tubes is not as high as in cases where no solvent is used.
Example 25 Example 1 was repeated with the exception that ultrasonic forming was used for closing one end of the ~ irCC,~
circul~ 12 mm outside diameter tube. A tube which has been carefully cut to give a smooth surface whose face is perpendicular to the length of the tube is placed over a mandrel. The horn of ultrasonic welder (Branson Model 400 C) which has a hemispherical cavity cut into the face of the horn is then carefully brought down to make contact with the end of tube. Ultrasonic power is applied while the black booster horn (high amplitude vibrations) is lowered to its final position for closing the tube.
Ultrasonic forming uses no end caps. Upon burn out of binder and sintering, the tube were formed to be hermetically sealed. As with ultrasonic bonding it was found advantageous to rotate the tubes during this process to form an even smooth shape.
Example 26 Example 25 was repeated with the exception that the outside diameter of tube is 25 mm. These tubes were ultrasonically formed. Af~er burn out of binder and sintering, the tubes had good properties.
Example 27 Example 25 was repeated with the exception that the outside diameter of tube was 18 mm~ The tubes were rotated during ultrasonic forming. The formed tubes had improved appearance.
~8~7~7~
In the above Examples 1 - 27, Solprene 414C is a thermoplastic elastomer manufactured by Phillips Petroleum.
It is a radial block copolymer of styrene and butadiene with a molecular weight (Mw) of about 160,000. The 414C
has a specific gravity of 0.95, melt flow of 72 (grams/10 min. at 190C and apparent viscosity of 46,000 poise at 10 sec~~l at room temperature. Agerite Resin D is an antioxidant available from Vanderbilt Company; it is a polymerized 1,2-dihydro-2,2,4-trimethyl quinoline. Typical properties of Agerite Resin D are specific gravity - 1.06;
softening point ~ 74C; and very soluble in acetone Sunoco Wax 3420 is a paraffinic wax that melts at 58Co Specific gravity at 150C is 1.2 g/cc and kinematic viscosity is 3.6 centistokes at 99C. Sunoco Wax 4412 is a paraffinic wax that melts at 63C. Specific gravity is 0~925 at 60C and kinematic viscosity at 99C is 4.2 centistokes. Styron 495 is a polystyrene available from Dow Chemical Company; it has a vicat softening point of 97C, melt flow rate of 3.5 grams/10 min. and specific gravity of 1.05 at 150C.
Styron 495 has a molecular weight (Mw) of about 200,000.
Picco 6140-3 is a polyindene available from Hercules; its melt viscosity is 10 poises at 205C~ The softening point is 140C and density 1.07 at 25C. Flexon 845 is a paraffinic petroleum oil from Exxon Chemical Company.
Flexon 845 has a viscosity of 230 SUS at 99C and ASniline Point is 117C. Shellflex 371 is a paraffinic-napthenic oil available from Shell Oil Company. Shellflex has a specific gravity of 0.897 at 150C; it has 49% paraffinic carbon, 50% naphthenic carbon and 1~ aromatic carbon. The molecular weight is 400, viscosity at 38C is 427 SUS., and Aniline Point is 100C. Flexricin P-4 is methyl acetyl ricinoleateO Its specific gravity is 0.936 and boiling point at 2 mm is 185C. Its molecular weight is 346 ~ingtack Plus are resins available from Goodyear Chemical Company. Winqtack 95, considered a synthetic polyterpene, has a softening point of 100Co Specific gravity at
5'77~2 . - 27 25C is 0.93 and molecular weight of 1200. Wingtack Plus,a polyterpene resin has a softening point of 94C, specific gravity of 0.93 and molecular weight of 1100.
In view of this disclosure, many modifications of this invention will be apparent to those skilled in the art. It is intended that all such modifications which fall within the true scope of the invention will be included within the terms of the appended claims.
In view of this disclosure, many modifications of this invention will be apparent to those skilled in the art. It is intended that all such modifications which fall within the true scope of the invention will be included within the terms of the appended claims.
Claims (31)
1. A method of ultrasonically end-capping a tubular green body, which comprises:
(A) providing a tubular green body comprised of a mixture of about 40 to 60 volume percent sinterable particulate solids and 60 to 40 volume percent organic sacrificial binder, wherein said binder consists essentially of:
a) a thermoplastic block copolymer component selected from the group consisting of linear, radial and linear and radial block copolymers, having a first aromatic block which is glassy or crystalline at 20°
to 25°C, and which has a softening point between about 80° and 250°C and a second aliphatic block which is different from said first block and behaves as an elastomer at temperatures between about 15°C below and about 100°C
above said softening point of said first block;
b) oil at least about 75 percent by weight of which boils in a range between about 285° to 560°C, has a viscosity of between about 30 and 220 Saybolt Universal Seconds (SUS) at 100°C, and has an Aniline Point in the range between about 75° and 125°C;
c) wax which melts at a temperature in a range between about 55° and 80°C and at least 75 percent by weight of which boils at temperatures in a range between about 315° and 490°C;
d) first stiffening thermoplastic polymer which is glassy or crystalline at 20° to 25°C, has a softening point between about 80° and 250°C and comprises aromatic monomeric units associable with the block copolymer (a);
e) second stiffening thermoplastic polymer, different from said first polymer and which is glassy or crystalline at 20° to 25°C and comprising aromatic monomeric units associable with the first block and has a softening point between about 80° and 250°C;
f) processing aid comprising an ester of fatty acids; and said sinterable particulate solids consisting essentially of a particle size distribution of beta"-alumina precursor particulate solids, the weight of (a) being greater than (b) and (c) combined, greater than (d) and (e) combined and greater than about two times (b), (c), (d), (e) or (f) alone; and (B) forming an end-cap of desired configuration having a composition comprising said mixture;
(C) applying pressure and ultrasonic vibrations by means of an ultrasonic horn to said tubular green body and end-cap between a tubular mandrel and said ultrasonic horn, said mandrel having a shaped end of desired con-figuration and the ultrasonic horn having a female mold shape adapted to receive said mandrel with said tubular body disposed thereon; and (D) maintaining said pressure and ultrasonic vibrations for a time necessary for ultrasonic vibrations to travel to the tubular body end-cap interface, wherein they are dissipated in the form of frictional heat and melt said binder so as to weld the joining surfaces.
(A) providing a tubular green body comprised of a mixture of about 40 to 60 volume percent sinterable particulate solids and 60 to 40 volume percent organic sacrificial binder, wherein said binder consists essentially of:
a) a thermoplastic block copolymer component selected from the group consisting of linear, radial and linear and radial block copolymers, having a first aromatic block which is glassy or crystalline at 20°
to 25°C, and which has a softening point between about 80° and 250°C and a second aliphatic block which is different from said first block and behaves as an elastomer at temperatures between about 15°C below and about 100°C
above said softening point of said first block;
b) oil at least about 75 percent by weight of which boils in a range between about 285° to 560°C, has a viscosity of between about 30 and 220 Saybolt Universal Seconds (SUS) at 100°C, and has an Aniline Point in the range between about 75° and 125°C;
c) wax which melts at a temperature in a range between about 55° and 80°C and at least 75 percent by weight of which boils at temperatures in a range between about 315° and 490°C;
d) first stiffening thermoplastic polymer which is glassy or crystalline at 20° to 25°C, has a softening point between about 80° and 250°C and comprises aromatic monomeric units associable with the block copolymer (a);
e) second stiffening thermoplastic polymer, different from said first polymer and which is glassy or crystalline at 20° to 25°C and comprising aromatic monomeric units associable with the first block and has a softening point between about 80° and 250°C;
f) processing aid comprising an ester of fatty acids; and said sinterable particulate solids consisting essentially of a particle size distribution of beta"-alumina precursor particulate solids, the weight of (a) being greater than (b) and (c) combined, greater than (d) and (e) combined and greater than about two times (b), (c), (d), (e) or (f) alone; and (B) forming an end-cap of desired configuration having a composition comprising said mixture;
(C) applying pressure and ultrasonic vibrations by means of an ultrasonic horn to said tubular green body and end-cap between a tubular mandrel and said ultrasonic horn, said mandrel having a shaped end of desired con-figuration and the ultrasonic horn having a female mold shape adapted to receive said mandrel with said tubular body disposed thereon; and (D) maintaining said pressure and ultrasonic vibrations for a time necessary for ultrasonic vibrations to travel to the tubular body end-cap interface, wherein they are dissipated in the form of frictional heat and melt said binder so as to weld the joining surfaces.
2. A method in accordance with claim 1, wherein said tubular green body disposed on said mandrel has faces perpendicular to length of said body.
3. A method in accordance with claim 2 wherein said end cap comprises a disc shaped end cap.
4. A method in accordance with claim 3 wherein said end-cap comprises hemispherically shaped end-cap.
5. A method in accordance with claims 3 or 4 wherein said end-cap is centrally placed on top of said mandrel prior to applying said pressure and ultrasonic vibrations.
6. A method in accordance with claims 3 or 4 wherein said end-cap is placed up into said ultrasonic horn prior to applying said pressure and ultrasonic vibrations.
7. A method according to claims 1, 3 or 4 wherein said desired configuration of said mandrel and said ultra-sonic horn is hemispherical.
8. A method in accordance with claim 1, wherein said end-capping further comprises applying only said ultrasonic vibrations for a time prior to applying ultra-sonic vibrations and pressure at the same time.
9. A method in accordance with claim 8 wherein said end-capping still further comprises applying only said pressure for a time after applying ultrasonic vibra-tions and pressure at the same time.
10. A method in accordance with claim 1, wherein forming said end-cap comprises forcing said tubular body between said mandrel and said ultrasonic horn until a continuous smooth end-cap has been formed while applying ultrasonic vibrations to said tubular body.
11. A method in accordance with claim 10, wherein said desired configuration of said mandrel and ultrasonic horn is hemispherical.
12. A method in accordance with claim 1, 2 or 3, wherein said tube is rotated during said application of ultrasonic vibrations.
13. A method in accordance with claim 8, 9 or 10, wherein said tube is rotated during said application of ultrasonic vibrations.
14. A method in accordance with claim 1, wherein said block copolymer comprises said radial block copolymer.
15. A method in accordance with claim 14 wherein said first block comprises a copolymer of styrene.
16. A method in accordance with claim 15, wherein said second block comprises a polymer of butadiene.
17. A method in accordance with claim 16, wherein said polymer of butadiene comprises an unsaturated polymer.
18. A method in accordance with claim 17, wherein said first stiffening polymer comprises a polystyrene thermoplastic.
19. A method in accordance with claim 18, wherein said second stiffening polymer comprises a polyindene thermoplastic.
20. A method in accordance with claim 19, wherein said block copolymer has a weight exceeding the combination of weights of (b), (d), (d) (e) and (f).
21. A method in accordance with claim 20, wherein said radial block copolymer has a molecular weight (Mw) of about 100,000-200,000.
22. A method in accordance with claim 21, wherein said radial bock polymer has a specific gravity between about 0.9-1.
23. A method in accordance with claim 22, wherein said block polymer has an apparent viscosity of between abour 40-50 thousand poise at 10-1 sec. and about 20-25°C.
24. A method in accordance with claim 1, wherein said particle size distribution of said beta"-alumina particulate precursor comprises particle sizes of between about .1-850 microns.
25. A method in accordance with claim 24, wherein said average particle size is greater than about 3.5 microns.
26. A method in accordance with claim 25, wherein said average particle size is between about 3.5-20 microns.
27. A method in accordance with claim 21, wherein composition of said beta"-alumina precursor particulate comprises 8.85 weight percent Na2O, 0.75 weight percent Li2O, and 90.40 weight percent Al2O3.
28. A method in accordance with claim 27, wherein said processing aid is acetyl recinoleate ester.
29. A method in accordance with claim 28, wherein said processing aid is selected from methyl acetyl ricin-oleate and butyl acetyl ricinoleate.
30. A method in accordance with claim 29, wherein said tubular green body was formed by extrusion.
31. A method in accordance with claim 30, which further comprises subjecting the end-capped green body to binder burn out and sintering.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/300,404 US4364783A (en) | 1981-09-08 | 1981-09-08 | Ultrasonic end-capping of beta"-alumina tubes |
| US300,404 | 1994-09-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1185772A true CA1185772A (en) | 1985-04-23 |
Family
ID=23158961
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA000405267A Expired CA1185772A (en) | 1981-09-08 | 1982-06-16 | ULTRASONIC END-CAPPING OF .beta. ALUMINA TUBES |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US4364783A (en) |
| JP (1) | JPS5859055A (en) |
| CA (1) | CA1185772A (en) |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3205076A1 (en) * | 1981-02-13 | 1982-11-25 | Kurosaki Refractories Co., Ltd., Kitakyushu, Fukuoka | Process for producing an extrusion moulding and material composition for this |
| JPS593066A (en) * | 1982-06-29 | 1984-01-09 | 日本碍子株式会社 | Manufacture of ceramic thin tube |
| FR2555159B1 (en) * | 1983-11-21 | 1986-06-27 | Ceraver | METHOD FOR WELDING TWO HOLLOW CERAMIC HALF PIECES, AND WELDING MACHINE FOR CARRYING OUT THE METHOD |
| US4767479A (en) * | 1987-09-21 | 1988-08-30 | United Technologies Corporation | Method for bonding ceramic casting cores |
| US4957668A (en) * | 1988-12-07 | 1990-09-18 | General Motors Corporation | Ultrasonic compacting and bonding particles |
| DE3920851A1 (en) * | 1989-06-24 | 1991-01-10 | Asea Brown Boveri | SINTERING DEVICE AND METHOD FOR THE PRODUCTION THEREOF |
| US5275767A (en) * | 1991-06-19 | 1994-01-04 | Micciche Frank S | Manufacture of plastic containers |
| US5397407A (en) * | 1994-01-12 | 1995-03-14 | Innovative Automation Inc. | Apparatus for cooling ultrasonic tube sealers |
| US5511721A (en) * | 1994-11-07 | 1996-04-30 | General Electric Company | Braze blocking insert for liquid phase brazing operations |
| US5993722A (en) * | 1997-06-25 | 1999-11-30 | Le-Mark International Ltd. | Method for making ceramic heater having reduced internal stress |
| US6379485B1 (en) | 1998-04-09 | 2002-04-30 | Siemens Westinghouse Power Corporation | Method of making closed end ceramic fuel cell tubes |
| US6558597B1 (en) * | 1999-08-10 | 2003-05-06 | Praxair Technology, Inc. | Process for making closed-end ceramic tubes |
| US6228508B1 (en) * | 2000-02-07 | 2001-05-08 | Spraying Systems Co. | Process for preparing a metal body having a hermetic seal |
| US7819302B2 (en) * | 2004-09-30 | 2010-10-26 | The Boeing Company | Aluminum end caps ultrasonically welded to end of aluminum tube |
| JP2006248159A (en) * | 2005-03-14 | 2006-09-21 | Seiko Epson Corp | Ink cartridge and manufacturing method thereof |
| US7815575B2 (en) * | 2005-05-09 | 2010-10-19 | Salutron, Inc. | Ultrasonic monitor with a biocompatible oil based transmission medium |
| US8212171B2 (en) * | 2006-12-22 | 2012-07-03 | Sonics & Materials Inc. | System and method for ultrasonic assisted EDM machining |
| DE102012203339A1 (en) | 2012-03-02 | 2013-09-05 | Lechler Gmbh | Method for manufacturing green element for fluid nozzle, involves pressing heated stamper in components, and partially melting and welding components in one of parting line and stamper adjacent area |
| JP6422981B2 (en) * | 2013-09-12 | 2018-11-14 | ビーエーエスエフ ソシエタス・ヨーロピアBasf Se | Β-aluminum oxide ceramics by extrusion of mixtures containing sodium compounds |
| WO2015130316A1 (en) * | 2014-02-28 | 2015-09-03 | General Electric Company | Method and system for manufacturing solid electrolyte tubes |
| US10052713B2 (en) * | 2015-08-20 | 2018-08-21 | Ultex Corporation | Bonding method and bonded structure |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3556884A (en) * | 1966-05-02 | 1971-01-19 | Lusteroid Container Co Inc | Plastic tube construction |
| CA1066830A (en) * | 1976-01-07 | 1979-11-20 | Ford Motor Company Of Canada | Sacrificial binders for molding particulate solids and the molding thereof |
| US4158689A (en) * | 1976-01-07 | 1979-06-19 | Ford Motor Company | Molding particulate solids and sacrificial binders therefor |
| US4289719A (en) * | 1976-12-10 | 1981-09-15 | International Business Machines Corporation | Method of making a multi-layer ceramic substrate |
-
1981
- 1981-09-08 US US06/300,404 patent/US4364783A/en not_active Expired - Fee Related
-
1982
- 1982-06-16 CA CA000405267A patent/CA1185772A/en not_active Expired
- 1982-09-07 JP JP57155776A patent/JPS5859055A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| US4364783A (en) | 1982-12-21 |
| JPS5859055A (en) | 1983-04-07 |
| JPH0233674B2 (en) | 1990-07-30 |
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