GB2033394A - Method of bonding epoxy resin - Google Patents
Method of bonding epoxy resin Download PDFInfo
- Publication number
- GB2033394A GB2033394A GB7844068A GB7844068A GB2033394A GB 2033394 A GB2033394 A GB 2033394A GB 7844068 A GB7844068 A GB 7844068A GB 7844068 A GB7844068 A GB 7844068A GB 2033394 A GB2033394 A GB 2033394A
- Authority
- GB
- United Kingdom
- Prior art keywords
- objects
- epoxide resin
- glass transition
- cured
- transition temperature
- 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.)
- Granted
Links
- 229920000647 polyepoxide Polymers 0.000 title claims abstract description 48
- 239000003822 epoxy resin Substances 0.000 title claims abstract description 40
- 238000000034 method Methods 0.000 title claims abstract description 26
- 230000009477 glass transition Effects 0.000 claims abstract description 17
- 230000013011 mating Effects 0.000 claims abstract description 13
- 230000003068 static effect Effects 0.000 claims abstract description 7
- WSFSSNUMVMOOMR-UHFFFAOYSA-N Formaldehyde Chemical compound O=C WSFSSNUMVMOOMR-UHFFFAOYSA-N 0.000 claims description 6
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 claims description 4
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N Phenol Chemical group OC1=CC=CC=C1 ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 claims description 4
- PXKLMJQFEQBVLD-UHFFFAOYSA-N bisphenol F Chemical compound C1=CC(O)=CC=C1CC1=CC=C(O)C=C1 PXKLMJQFEQBVLD-UHFFFAOYSA-N 0.000 claims description 4
- 238000004040 coloring Methods 0.000 claims description 4
- 239000000945 filler Substances 0.000 claims description 4
- 239000012779 reinforcing material Substances 0.000 claims description 4
- 125000000217 alkyl group Chemical group 0.000 claims description 2
- 125000004432 carbon atom Chemical group C* 0.000 claims description 2
- 229910052801 chlorine Inorganic materials 0.000 claims description 2
- 125000001309 chloro group Chemical group Cl* 0.000 claims description 2
- 125000001183 hydrocarbyl group Chemical group 0.000 claims description 2
- 238000005304 joining Methods 0.000 claims description 2
- 229920003986 novolac Polymers 0.000 claims description 2
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 claims 2
- 239000001294 propane Substances 0.000 claims 1
- 239000000853 adhesive Substances 0.000 abstract description 7
- 230000001070 adhesive effect Effects 0.000 abstract description 7
- 239000000203 mixture Substances 0.000 abstract description 6
- 238000007796 conventional method Methods 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 239000004848 polyfunctional curative Substances 0.000 description 13
- 229920005989 resin Polymers 0.000 description 7
- 239000011347 resin Substances 0.000 description 7
- IISBACLAFKSPIT-UHFFFAOYSA-N bisphenol A Chemical compound C=1C=C(O)C=CC=1C(C)(C)C1=CC=C(O)C=C1 IISBACLAFKSPIT-UHFFFAOYSA-N 0.000 description 6
- 239000000654 additive Substances 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 3
- 125000004435 hydrogen atom Chemical group [H]* 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- VILCJCGEZXAXTO-UHFFFAOYSA-N 2,2,2-tetramine Chemical compound NCCNCCNCCN VILCJCGEZXAXTO-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 239000002253 acid Substances 0.000 description 2
- 150000007513 acids Chemical class 0.000 description 2
- WTEOIRVLGSZEPR-UHFFFAOYSA-N boron trifluoride Chemical compound FB(F)F WTEOIRVLGSZEPR-UHFFFAOYSA-N 0.000 description 2
- KRKNYBCHXYNGOX-UHFFFAOYSA-N citric acid Chemical compound OC(=O)CC(O)(C(O)=O)CC(O)=O KRKNYBCHXYNGOX-UHFFFAOYSA-N 0.000 description 2
- -1 cycloaliphatic Chemical group 0.000 description 2
- 238000000113 differential scanning calorimetry Methods 0.000 description 2
- 150000002118 epoxides Chemical class 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229920000768 polyamine Polymers 0.000 description 2
- YBRVSVVVWCFQMG-UHFFFAOYSA-N 4,4'-diaminodiphenylmethane Chemical compound C1=CC(N)=CC=C1CC1=CC=C(N)C=C1 YBRVSVVVWCFQMG-UHFFFAOYSA-N 0.000 description 1
- 229910015900 BF3 Inorganic materials 0.000 description 1
- BRLQWZUYTZBJKN-UHFFFAOYSA-N Epichlorohydrin Chemical compound ClCC1CO1 BRLQWZUYTZBJKN-UHFFFAOYSA-N 0.000 description 1
- 238000005727 Friedel-Crafts reaction Methods 0.000 description 1
- LGRFSURHDFAFJT-UHFFFAOYSA-N Phthalic anhydride Natural products C1=CC=C2C(=O)OC(=O)C2=C1 LGRFSURHDFAFJT-UHFFFAOYSA-N 0.000 description 1
- GOOHAUXETOMSMM-UHFFFAOYSA-N Propylene oxide Chemical compound CC1CO1 GOOHAUXETOMSMM-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 239000005864 Sulphur Substances 0.000 description 1
- 125000001931 aliphatic group Chemical group 0.000 description 1
- 229910052783 alkali metal Inorganic materials 0.000 description 1
- 229910000147 aluminium phosphate Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 150000008064 anhydrides Chemical class 0.000 description 1
- 125000003118 aryl group Chemical group 0.000 description 1
- 125000004429 atom Chemical group 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- JHIWVOJDXOSYLW-UHFFFAOYSA-N butyl 2,2-difluorocyclopropane-1-carboxylate Chemical compound CCCCOC(=O)C1CC1(F)F JHIWVOJDXOSYLW-UHFFFAOYSA-N 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- QGBSISYHAICWAH-UHFFFAOYSA-N dicyandiamide Chemical compound NC(N)=NC#N QGBSISYHAICWAH-UHFFFAOYSA-N 0.000 description 1
- GYZLOYUZLJXAJU-UHFFFAOYSA-N diglycidyl ether Chemical compound C1OC1COCC1CO1 GYZLOYUZLJXAJU-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010292 electrical insulation Methods 0.000 description 1
- 239000013525 flexibilising agent Substances 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 125000000623 heterocyclic group Chemical group 0.000 description 1
- 239000012948 isocyanate Substances 0.000 description 1
- 150000002513 isocyanates Chemical class 0.000 description 1
- 150000002540 isothiocyanates Chemical class 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 125000002496 methyl group Chemical group [H]C([H])([H])* 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 150000002989 phenols Chemical class 0.000 description 1
- 229920006295 polythiol Polymers 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 150000003512 tertiary amines Chemical class 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004634 thermosetting polymer Substances 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- 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
- B29C65/06—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding
- B29C65/0609—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding characterised by the movement of the parts to be joined
- B29C65/0627—Angular, i.e. torsional
-
- 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
- B29C65/06—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding
- B29C65/0672—Spin welding
-
- 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
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
-
- 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
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/114—Single butt joints
- B29C66/1142—Single butt to butt joints
-
- 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
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/116—Single bevelled joints, i.e. one of the parts to be joined being bevelled in the joint area
-
- 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
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/522—Joining tubular articles
- B29C66/5221—Joining tubular articles for forming coaxial connections, i.e. the tubular articles to be joined forming a zero angle relative to each other
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- 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
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/522—Joining tubular articles
- B29C66/5229—Joining tubular articles involving the use of a socket
- B29C66/52291—Joining tubular articles involving the use of a socket said socket comprising a stop
- B29C66/52292—Joining tubular articles involving the use of a socket said socket comprising a stop said stop being internal
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- 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
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/526—Joining bars
- B29C66/5261—Joining bars for forming coaxial connections, i.e. the bars to be joined forming a zero angle relative to each other
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- 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
- B29C66/71—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 composition of the plastics material of the parts to be joined
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- 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
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- 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
- B29C66/731—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 intensive physical properties of the material of the parts to be joined
- B29C66/7311—Thermal properties
- B29C66/73117—Tg, i.e. glass transition temperature
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- 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
- B29C66/7375—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 uncured, partially cured or fully cured
- B29C66/73755—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 uncured, partially cured or fully cured the to-be-joined area of at least one of the parts to be joined being fully cured, i.e. fully cross-linked, fully vulcanized
- B29C66/73756—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 uncured, partially cured or fully cured the to-be-joined area of at least one of the parts to be joined being fully cured, i.e. fully cross-linked, fully vulcanized the to-be-joined areas of both parts to be joined being fully cured
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- 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
- B29C66/7394—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 characterised by the material of at least one of the parts being a thermoset
- B29C66/73941—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 characterised by the material of at least one of the parts being a thermoset characterised by the materials of both parts being thermosets
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- 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
- B29C65/82—Testing the joint
- B29C65/8207—Testing the joint by mechanical methods
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- 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
- B29C65/82—Testing the joint
- B29C65/8207—Testing the joint by mechanical methods
- B29C65/8215—Tensile tests
-
- 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
- B29C66/7392—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 characterised by the material of at least one of the parts being a thermoplastic
- B29C66/73921—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 characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
-
- 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
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
- B29C66/832—Reciprocating joining or pressing tools
- B29C66/8322—Joining or pressing tools reciprocating along one axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Manufacture Of Macromolecular Shaped Articles (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
Objects made of cured epoxide resin are bonded together by a. placing the two objects in contact with each other at substantially planar mating surfaces, b. applying a static force to the objects to urge them into intimate contact with one another at the mating surfaces c. subjecting these surfaces to motion, relative to one another, by rotation or vibration, for a sufficient period for the frictional energy between these surfaces to heat them above the glass transition temperature(s) of the objects, and d. stopping the relative motion whilst maintaining the static force until the mating surfaces have cooled to below the glass transition temperature(s) of the objects. The method may be used with objects having a glass transition temperature of from about 40 DEG C to 200 DEG C, and provides a satisfactory bond within seconds, i.e., more rapidly than does the conventional method of applying a liquid curable adhesive composition and allowing this to cure.
Description
SPECIFICATION
Method of bonding
This invention relates to a method of bonding together two or more objects of cured epoxide resin and to articles made by this method.
Epoxide resins, by which is meant compounds containing more than one 1 2-epoxide group per average molecule, are well known materials, used for a wide variety of purposes, such as in castings and mouldings, as impregnants, and as adhesives. When two objects made of cured epoxide resin are to be bonded together, this is usually effected by applying an epoxide resin adhesive formulation to the surfaces to be joined and maintaining the objects in the requisite position whilst the adhesive cures. By using an epoxide resin adhesive the known advantages of an all epoxide resin system, such as good electrical insulation and chemical resistance, are retained and the bond has a high strength.The curing process for the adhesive is, however, often inconveniently slow, and whilst it may be accelerated by heating, this is not always convenient, due to the size or location of the objects being bonded.
There is therefore a need for a rapid method of bonding together objects made from cured epoxide resins without introducing other, epoxide-free materials. We have now found that this can be achieved by means of friction bonding under certain conditions, whereby frictional heat caused by moving one object relative to the other whilst they are held in close contact causes the epoxide resin composition in the area of contact to attain a soft, rubber-like state, this movement is then stopped, and the contacting surfaces, on cooling, form a strong bond between themselves. Full bond strength is reached in a matter of seconds, rather than of hours as is usual with a conventional epoxide resin adhesive.
This bonding technique bears a superficial similarity to friction welding, which is well known for bonding metal or thermoplastics articles. However, such materials have definite melting points and fusion occurs between the contacting surfaces. Thermoset resins, such as cured epoxide resins, on the other hand, do not melt but only soften when heated and, if heated further, they finally decompose without melting. It was therefore not to be expected that bonding of objects of cured epoxide resins could take place through the generation of frictional heat.We have further found that, provided the cured epoxide resins have a glass transition temperature within the range 400 to about 2000 C, successful friction bonding can take place; cured resins having a glass transition temperature below this range can be friction-bonded, but the resultant joints are usually too weak for practical use, while resins having a glass transition temperature above this range tend to undergo, at the requisite bonding temperature, decomposition at the interface to an extent such that the joint strength is below acceptable levels.
Accordingly, this invention provides a method of joining two objects made of cured epoxide resin, the cured epoxide resin of each object having a glass transition temperature within the range 400 to 2000C, and preferably for at least one such object within the range 800 to 1 C, comprising::
a. placing the two objects in contact with each other at substantially planar mating surfaces,
b. applying a static force to the said objects to urge them into intimate contact with one another at said surfaces,
c. subjecting said surfaces to motion, relative to one another, for a sufficient period for the frictional energy between the said surfaces to heat the said surfaces to above the glass transition temperature or temperatures of the objects, and
d. stopping, or allowing to stop, the said relative motion whilst maintaining the said static force until the mating surfaces have cooled to below the glass transition temperature or temperatures of the objects.
This invention further provides articles made by this method.
By the term 'glass transition temperature, as used in this specification and claims, is meant the approximate midpoint of the temperature range over which the cured epoxide resin changes reversibly from a hard and brittle condition to a rubbery condition, as measured by differential scanning calorimetry, torsion pendulum, thermomechanical analysis, or other acceptable means.
The relative motion between the objects may be reciprocative, with one or more objects being vibrated back and forth with respect to another in the plane of the mating surfaces, or, preferably, the motion is rotational, with one or more objects being rotated against another.
When a rotational method is employed with objects held in contact end to end, the relative speeds of the surfaces in contact, and hence the frictional heating effect, reduce to zero on the axis. We have found that better results are achieved if a small area around the axis is removed from one or both mating surfaces. The area of surface removed usually represents 25% or less of the total mating surface.
The objects to be bonded will usually be rods or tubes.
The bonding of two coaxial rods end-to-end, the relative movement between them being rotational, is illustrated in Figure 1 of the accompanying drawings.
Overlap joints may be produced by rotation of a closely-fitting sleeve or ring of cured epoxide resin around cylindrical objects, also of cured epoxide resin, both of which may be stationary or one of which may be rotating relative to the other. The two rods may abut one another, or they may almost meet, and advantageously the rods are tapered towards the contiguous or adjacent faces while the sleeve or ring tapers outwards. This arrangement is illustrated in Figure 2 of the accompanying drawings.
Alternatively more than two surfaces can be bonded simultaneously by arranging co-axially three objects of cured epoxide resin, each face of the central object contacting the planar mating surface on a face of the adjacent object, and causing the central object to rotate, such as by means of a rotating belt, or vibrate, relative to the other two objects while applying a static force to the three objects to urge them into intimate contact with one another at the said surfaces. Such an arrangement is illustrated in
Figure 3 of the accompanying drawings.
During the bonding process the cured epoxide resin tends slightly to bulge outwards in the immediate area of the bond, due to the heated resin yielding to the force applied to hold the mating surfaces together. Examination under polarised light of the loints so produced shows that the bulging "flash" of the epoxide resin is more highly stressed than the remainder of the joint, and so it is sometimes found advantageous to machine away this flash, particularly if the joint is liable to be heated in service to a temperature exceeding the glass transition temperature of either object.
Any conventional epoxide resin may be employed to make the objects which are bonded by the method of this invention. Preferably they contain at least one group of formula
directly attached to an atom of oxygen, nitrogen, or sulphur, where either R and R2 each represent a hydrogen atom, in which case R' denotes a hydrogen atom or a methyl group, or R and R2 together represent -CH2CH2-, in which case R1 denotes a hydrogen atom.
Particularly preferred is an epoxide resin which is a polyglycidyl ether of 2,2-bis(4hydroxyphenyl)propane, of bis(4-hydroxyphenyl)methane, or of a novolak formed from formaldehyde and either phenol or phenol substituted in the ring by one chlorine atom or one alkyl hydrocarbon group containing one to nine carbon atoms, and which has a 1 2-epoxide group content of at least 0.5 equivalent per kilogram.
The epoxide resins employed to form the objects may be cured by any conventional curing agent for epoxide resins, such as aliphatic, cycloaliphatic, aromatic, or heterocyclic polyamines, polyaminoamides, adducts of polyamines with stoichiometric deficits of polyepoxides, isocyanates, isothiocyanates, polyhydric phenols, phosphoric acid, polythiols, and polycarboxylic acids and their anhydrides. There may also be used catalytic curing agents such as tertiary amines, alkali metal alkoxides, stannous salts of alkanoic acids, dicyandiamide, Friedel-Crafts catalysts, and chelates formed by reaction of boron trifluoride with, e.g., 1 ,3-diketones.
An object made of an epoxide resin composition may be bonded to one made of a different epoxide resin composition, i.e., one containing a different epoxide resin, or a different curing agent, or a significant amount of a flexibiliser, for example. However, if the best results are to be achieved, the glass transition temperatures of the two objects to be bonded together should not differ by more than about 50 C.
The compositions forming the objects may contain inert fillers, reinforcing materials, and colouring matter, if desired. It is, however, preferred that the total volume of such additives constitute at most 35 parts by volume per 100 parts by volume of the cured epoxide resin, although larger proportions may be used. A total of at most 20 parts by volume of such additives per 100 parts by volume of the cured resin is further preferred. Bonding of objecis in which at least one of them is substantially free from such additives is particularly preferred.
The invention will now be illustrated by the following Examples, in which all parts are by weight and temperatures are in degrees Celsius. The resins and hardeners used in the Examples were as follows:
EPOXIDE RESIN I
this term denotes a diglycidyl ether of 2,2-bis(4-hydroxyphenyl)propane, having an epoxide content of 5.0-5.2 equivalents/kg.
EPOXIDE RESIN II
this denotes a solid resin prepared from 2,2-bis(4-hydroxyphenyl)propane and epichlorohydrin and having an epoxide content of 2.2-2.5 equivalents/kg.
HARDENER I
this denotes an adduct of an equimolar amount of triethylenetetramine and propylene oxide.
HARDENER II this denotes triethylenetetramine.
HARDENER Ill
this denotes 4,4'-diaminodiphenylmethane.
HARDENER IV
this denotes phthalic anhydride.
EXAMPLE 1
Rods of circular cross section 1 5.7 mm in diameter were cast from Epoxide resin I and various hardeners. The nature of the hardeners, the amounts added, the curing conditions, and the glass transition temperatures (Tg) of the cured samples (measured by differential scanning calorimetry), are given in Table 1.
TABLE 1
Hardener Parts per 100 parts Sample Designation of Epoxide resin I Curing conditions Tg A I 25 24 hours at 20" 93" B 11 12 24 hours at 20" and 3 hours at 70" 95" C 11 12 24 hours at 20" and 3 hours at 95" 116" D i i 12 3 hours at 60" and 119" 3 hours at 95" E Ill 27 16 hours at 60" and 3 hours at 95" 137" F Ill 27 16 hours at 60" and 3 3 hours at 95" and 3 hours at 120" 142" G lil 27 16 hours at 60" and 3 hours at 95" and 3 hours at 120" and 3 hours at 150" 168" H Ill 27 16 hours at 60 and 3 hours at 95" and 3 hours at 120" and 3 hours at 150" and 3 hours at 180" 171" The rod specimens were prepared by first lightly machining a flat face on one end of each rod, then counterboring these surfaces to a depth of 2 mm and a diameter of 7.5 mm. One rod was then mounted in the three-jaw self-centering chuck of a lathe and rotated at 1280 rpm. A second, similar rod was held in a chuck mounted in the tailstock of the lathe so that it could not turn but could be moved axially. This second rod was then forced against the rotating rod, pressure being applied by means of the tailstock handwheel via a calibrated compression spring device, so arranged that the axial thrust force between the two resin rods was known and reproducible.After a short period of rubbing contact between the rods as recorded in Table 2, the lathe drive was disengaged and a brake applied to bring the chuck to rest as quickly as possible, axial pressure being maintained for a further half-minute whilst the specimen cooled. The bonded specimen was then removed in one piece.
The shear strength of the bond was found by twisting one end of the article and measuring the torque on the other end at break. The results are given in Table 2, each result being the average of three replicates.
TABLE 2
Bonding conditions Time of rubbing Shear strength Sample Force (N) contact (secs) (MN/m2) A 300 7 48.1 B 300 8 49.9 C 300 9 50.9 D 330 9 46.4 D 360 9 46.5 E 330 9 40.9 E 360 9 54.6 F 360 9 54.3 F 360 10 48.1 G 360 10 62.5 G 360 11 55.8 H 360 11 61.3 H 360 12 62.3 EXAMPLE 2
Example 1 was repeated, the rods being made of 100 parts of Epoxide resin I and 27 parts of
Hardener Ill, curing at 1000 for 3 days. The rods were then bonded together as described in Example 1, using an axial force of 360 N for 9 seconds, the 'flash' around the bond area was removed by machining the article to an external diameter of 12 mm. The article was post-cured at 1800 for 20 minutes. The shear strength at room temperature, determined as in Example 1, was found to average (8 replicates) 56.8 MN/m2.
EXAMPLE 3
Example 1 was repeated, rods being made either from 1 00 parts of Epoxide resin I and 27 parts of
Hardener Ill, curing at 650 for 16 hours plus 2 hours at 1800, or from 100 parts of Epoxide resin II and 30 parts of Hardener IV, curing for 16 hours at 1 350 The bonds were formed as described in Example 1, using an axial force of 360 N for 9 seconds. The tensile strengths were measured by pulling the bonded rods in an Instron testing machine and recording the force required to separate the joint. The average tensile strengths of the bonds (4 replicates) were 8.8 MN/m2 for the rods made from Epoxide resin I and 7.5 MN/m2 for those made from Epoxide resin II.
EXAMPLE 4
Example 1 was repeated, bonding rods made from 100 parts of Epoxide resin I and 27 parts of
Hardener Ill and cured at 1400 for 1 hour to rods made from 100 parts of Epoxide resin it, 30 parts of
Hardener IV and 200 parts of silica four, cured at 1350 for 16 hours.
Bonding was effected as described in Example 1, using an axial force of 360 N for 7 seconds.The shear strength of the bond, measured as described in Example 1. was 13.7 MN/m2.
Claims (10)
1. A method of joining two objects made of cured epoxide resin, the cured epoxide resin of each object having a glass transition temperature within the range 400 C to 2000 C, comprisinq a. placing the two objects in contact with each other at substantially planar mating surfaces.
b. applying a static force to the said objects to urge them into intimate contact with one another at said surfaces,
c. subjecting said surfaces to motion, relative to one another, for a sufficient period for the frictional energy between the said surfaces to heat the said surfaces to above the glass transition temperature or temperatures of the objects, and
d. stopping, or allowing to stop, the said relative motion whilst maintaining the said static force until the mating surfaces have cooled to below the glass transition temperature or temperatures of the objects.
2. A method according to claim 1, in which at least one cured epoxide resin has a glass transition temperature within the range 800C to 1800 C.
3. A method according to claim 1 or 2, in which the epoxide resin which is cured is a polyglycidyl ether of 2,2-bis(4#hydrnxyphenyl)propane, of bis(4-hydroxyphenyl)methane, or of a novolak formed from formaldehyde and either phenol or phenol substituted in the ring by one chlorine atom or one alkyl hydrocarbon group containing from one to nine carbon atoms, and has a 1 ,2-epoxide content of at least 0.5 equivalent per kilogram.
4. A method according to any of claims 1 to 3, in which at least one article contains in total at most 35 parts by volume of inert filler, reinforcing material, and colouring matter per 100 parts by volume of cured epoxide resin.
5. A method according to claim 4, in which at least one article contains in total at most 20 parts by volume of inert filler, reinforcing material, and colouring matter per 1 00 parts by volume of cured epoxide resin.
6. A method according to claim 5, in which at least one of the articles is substantially free from inert filler, reinforcing material, and colouring matter.
7. A method according to any of claims 1 to 6, in which the motion of one object, relative to the other, is reciprocative.
8. A method according to any of claims 1 to 6, in which the motion of one object, relative to the other, is rotational.
9. A method according to claim 8, in which up to 25% of the total mating surface is removed from the area around the axis of rotation before the two objects are placed in contact with each other.
10. A method according to any of claims 1 to 9, in which bulging 'flash' in the area of the bond is removed.
1 A method according to claim 1, substantially as described herein.
1 2. A method according to claim 1, substantially as described herein in any of the Examples.
1 3. Articles made by the method of any preceding claim.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB7844068A GB2033394B (en) | 1978-11-10 | 1978-11-10 | Method of binding epoxy resin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB7844068A GB2033394B (en) | 1978-11-10 | 1978-11-10 | Method of binding epoxy resin |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB2033394A true GB2033394A (en) | 1980-05-21 |
| GB2033394B GB2033394B (en) | 1982-11-03 |
Family
ID=10500955
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB7844068A Expired GB2033394B (en) | 1978-11-10 | 1978-11-10 | Method of binding epoxy resin |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2033394B (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1992017328A1 (en) * | 1991-03-28 | 1992-10-15 | Fusion Group Plc | Pipe couplings |
| WO1996022875A1 (en) * | 1995-01-27 | 1996-08-01 | Andersen Corporation | Vibratory welded window and door joints, method and apparatus for manufacturing the same |
| WO2001012421A1 (en) * | 1999-08-12 | 2001-02-22 | Exama Maschinen Gmbh | Multiple-head friction welding method and device for carrying out said method |
| WO2002098635A1 (en) * | 2001-06-07 | 2002-12-12 | Bowmead Holdings Inc. | Method and apparatus for vibration welding of thermoplastic components |
| US7950192B2 (en) | 2003-11-04 | 2011-05-31 | Bystronic Maschinen Ag | Framed panel and related method of manufacture |
| US10179359B2 (en) | 2010-01-12 | 2019-01-15 | Vestas Wind Systems A/S | Joining method of composite parts having a thermoset matrix, and wind turbine blade manufactured using this said method |
| CN112839796A (en) * | 2018-06-04 | 2021-05-25 | 赛世铁克 | Improvements to back height |
| US20220016851A1 (en) * | 2020-07-20 | 2022-01-20 | Saudi Arabian Oil Company | Apparatus and method for threaded-welded reinforced thermosetting resin pipe joints |
| WO2022020323A1 (en) * | 2020-07-20 | 2022-01-27 | Saudi Arabian Oil Company | Apparatus and method for friction welding of reinforced thermosetting resin pipe joints |
| US11761571B2 (en) | 2020-07-20 | 2023-09-19 | Saudi Arabian Oil Company | Apparatus and method for electrofusion welding of reinforced thermosetting resin pipe joints |
| US12055253B2 (en) | 2020-12-17 | 2024-08-06 | Saudi Arabian Oil Company | Apparatus and method for bonding tie layers on reinforced thermosetting resin laminates for use in welding thermoset composite pipe joints |
| US12259075B2 (en) | 2023-01-26 | 2025-03-25 | Saudi Arabian Oil Company | Method and system for automated installation of welded reinforced thermosetting resin pipe joints |
| US12276358B2 (en) | 2023-02-03 | 2025-04-15 | Saudi Arabian Oil Company | Corrosion-free welded connection for reinforced thermoplastic pipes (RTP) |
-
1978
- 1978-11-10 GB GB7844068A patent/GB2033394B/en not_active Expired
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1992017328A1 (en) * | 1991-03-28 | 1992-10-15 | Fusion Group Plc | Pipe couplings |
| WO1996022875A1 (en) * | 1995-01-27 | 1996-08-01 | Andersen Corporation | Vibratory welded window and door joints, method and apparatus for manufacturing the same |
| US5902657A (en) * | 1995-01-27 | 1999-05-11 | Andersen Corporation | Vibratory welded window and door joints, method and apparatus for manufacturing the same |
| US6103035A (en) * | 1995-01-27 | 2000-08-15 | Andersen Corporation | Vibratory welded window and door joints, method and apparatus for manufacturing the same |
| WO2001012421A1 (en) * | 1999-08-12 | 2001-02-22 | Exama Maschinen Gmbh | Multiple-head friction welding method and device for carrying out said method |
| WO2002098635A1 (en) * | 2001-06-07 | 2002-12-12 | Bowmead Holdings Inc. | Method and apparatus for vibration welding of thermoplastic components |
| US7122088B2 (en) | 2001-06-07 | 2006-10-17 | Bystronic Solution Centre Inc. | Method and apparatus for vibration welding of thermoplastic components |
| US7343950B2 (en) | 2001-06-07 | 2008-03-18 | Bystronic Solution Centre Inc | Method and apparatus for vibration welding of thermoplastic components |
| US7950192B2 (en) | 2003-11-04 | 2011-05-31 | Bystronic Maschinen Ag | Framed panel and related method of manufacture |
| US10179359B2 (en) | 2010-01-12 | 2019-01-15 | Vestas Wind Systems A/S | Joining method of composite parts having a thermoset matrix, and wind turbine blade manufactured using this said method |
| CN112839796A (en) * | 2018-06-04 | 2021-05-25 | 赛世铁克 | Improvements to back height |
| CN112839796B (en) * | 2018-06-04 | 2023-03-21 | 赛世铁克 | Adhesion testing device and method of use thereof |
| US20220016851A1 (en) * | 2020-07-20 | 2022-01-20 | Saudi Arabian Oil Company | Apparatus and method for threaded-welded reinforced thermosetting resin pipe joints |
| WO2022020323A1 (en) * | 2020-07-20 | 2022-01-27 | Saudi Arabian Oil Company | Apparatus and method for friction welding of reinforced thermosetting resin pipe joints |
| US11754215B2 (en) | 2020-07-20 | 2023-09-12 | Saudi Arabian Oil Company | Apparatus and method for friction welding of reinforced thermosetting resin pipe joints |
| US11761571B2 (en) | 2020-07-20 | 2023-09-19 | Saudi Arabian Oil Company | Apparatus and method for electrofusion welding of reinforced thermosetting resin pipe joints |
| US11794418B2 (en) * | 2020-07-20 | 2023-10-24 | Saudi Arabian Oil Company | Apparatus and method for threaded-welded reinforced thermosetting resin pipe joints |
| US12055253B2 (en) | 2020-12-17 | 2024-08-06 | Saudi Arabian Oil Company | Apparatus and method for bonding tie layers on reinforced thermosetting resin laminates for use in welding thermoset composite pipe joints |
| US12259075B2 (en) | 2023-01-26 | 2025-03-25 | Saudi Arabian Oil Company | Method and system for automated installation of welded reinforced thermosetting resin pipe joints |
| US12276358B2 (en) | 2023-02-03 | 2025-04-15 | Saudi Arabian Oil Company | Corrosion-free welded connection for reinforced thermoplastic pipes (RTP) |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2033394B (en) | 1982-11-03 |
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