JPS5545739A - Bonding of polyolefin liner to metallic crown cap - Google Patents
Bonding of polyolefin liner to metallic crown capInfo
- Publication number
- JPS5545739A JPS5545739A JP11907578A JP11907578A JPS5545739A JP S5545739 A JPS5545739 A JP S5545739A JP 11907578 A JP11907578 A JP 11907578A JP 11907578 A JP11907578 A JP 11907578A JP S5545739 A JPS5545739 A JP S5545739A
- Authority
- JP
- Japan
- Prior art keywords
- resin
- epoxy
- crown cap
- polyolefin
- bonding
- 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.)
- Pending
Links
Landscapes
- Lining Or Joining Of Plastics Or The Like (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Closures For Containers (AREA)
Abstract
PURPOSE:To bond a polyolefin liner to a metallc crown cap firmly, by using a primer layer, formed from a resin composition comprising a solution of an epoxy resin or vinyl chloride resin in an organic solvent and a dispersed epoxy group- containing polyolefin. CONSTITUTION:A polyolefin liner (L), e.g. ethylene/1-butene copolymer, is bonded to a metallic crown cap (C) with a primer layer, formed from a resin composition comprising a solution of an epoxy resin, e.g. epoxy-phenolic, or epoxy-amino resin, a vinyl chloride resin or vinyl. Chloride-vinyl acetate copolymer in an organic solvent and a dispensed solid epoxy group-containing polyolefin having an average molecular weight >=1,000 and a softening point of 80-180 deg.C, laid between L and C.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11907578A JPS5545739A (en) | 1978-09-29 | 1978-09-29 | Bonding of polyolefin liner to metallic crown cap |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11907578A JPS5545739A (en) | 1978-09-29 | 1978-09-29 | Bonding of polyolefin liner to metallic crown cap |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5545739A true JPS5545739A (en) | 1980-03-31 |
Family
ID=14752252
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11907578A Pending JPS5545739A (en) | 1978-09-29 | 1978-09-29 | Bonding of polyolefin liner to metallic crown cap |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5545739A (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6134322A (en) * | 1984-07-27 | 1986-02-18 | Hitachi Ltd | Low environmental-pollution type gas turbine |
US4766721A (en) * | 1985-10-11 | 1988-08-30 | Hitachi, Ltd. | Combustor for gas turbine |
JPH04294754A (en) * | 1991-03-15 | 1992-10-19 | Asahi Chem Ind Co Ltd | Screw metal cap liner |
US5377483A (en) * | 1993-07-07 | 1995-01-03 | Mowill; R. Jan | Process for single stage premixed constant fuel/air ratio combustion |
US5572862A (en) * | 1993-07-07 | 1996-11-12 | Mowill Rolf Jan | Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules |
US5613357A (en) * | 1993-07-07 | 1997-03-25 | Mowill; R. Jan | Star-shaped single stage low emission combustor system |
US5628182A (en) * | 1993-07-07 | 1997-05-13 | Mowill; R. Jan | Star combustor with dilution ports in can portions |
US5638674A (en) * | 1993-07-07 | 1997-06-17 | Mowill; R. Jan | Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission |
EP0863369A2 (en) | 1997-03-07 | 1998-09-09 | R. Jan Mowill | Single stage combustor with fuel / air premixing |
US5924276A (en) * | 1996-07-17 | 1999-07-20 | Mowill; R. Jan | Premixer with dilution air bypass valve assembly |
WO2001040713A1 (en) | 1999-12-03 | 2001-06-07 | Mowill Rolf Jan | Cooled premixer exit nozzle for gas turbine combustor and method of operation therefor |
EP1319896A2 (en) | 2001-12-14 | 2003-06-18 | R. Jan Mowill | Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities |
-
1978
- 1978-09-29 JP JP11907578A patent/JPS5545739A/en active Pending
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6134322A (en) * | 1984-07-27 | 1986-02-18 | Hitachi Ltd | Low environmental-pollution type gas turbine |
JPH0331899B2 (en) * | 1984-07-27 | 1991-05-09 | Hitachi Ltd | |
US4766721A (en) * | 1985-10-11 | 1988-08-30 | Hitachi, Ltd. | Combustor for gas turbine |
JPH04294754A (en) * | 1991-03-15 | 1992-10-19 | Asahi Chem Ind Co Ltd | Screw metal cap liner |
US5572862A (en) * | 1993-07-07 | 1996-11-12 | Mowill Rolf Jan | Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules |
EP0635681A1 (en) | 1993-07-07 | 1995-01-25 | R. Jan Mowill | Single stage premixed constant fuel/air ratio combustor |
US5477671A (en) * | 1993-07-07 | 1995-12-26 | Mowill; R. Jan | Single stage premixed constant fuel/air ratio combustor |
US5481866A (en) * | 1993-07-07 | 1996-01-09 | Mowill; R. Jan | Single stage premixed constant fuel/air ratio combustor |
US5377483A (en) * | 1993-07-07 | 1995-01-03 | Mowill; R. Jan | Process for single stage premixed constant fuel/air ratio combustion |
US5613357A (en) * | 1993-07-07 | 1997-03-25 | Mowill; R. Jan | Star-shaped single stage low emission combustor system |
US5628182A (en) * | 1993-07-07 | 1997-05-13 | Mowill; R. Jan | Star combustor with dilution ports in can portions |
US5638674A (en) * | 1993-07-07 | 1997-06-17 | Mowill; R. Jan | Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission |
US5765363A (en) * | 1993-07-07 | 1998-06-16 | Mowill; R. Jan | Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission |
US5924276A (en) * | 1996-07-17 | 1999-07-20 | Mowill; R. Jan | Premixer with dilution air bypass valve assembly |
EP0863369A2 (en) | 1997-03-07 | 1998-09-09 | R. Jan Mowill | Single stage combustor with fuel / air premixing |
WO2001040713A1 (en) | 1999-12-03 | 2001-06-07 | Mowill Rolf Jan | Cooled premixer exit nozzle for gas turbine combustor and method of operation therefor |
EP1319896A2 (en) | 2001-12-14 | 2003-06-18 | R. Jan Mowill | Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities |
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