An experimental/analytical comparison of strains in encapsulated assemblies
A combined experimental and analytical study of strains developed in encapsulated assemblies during casting, curing and thermal excursions is described. The experimental setup, designed to measure in situ strains, consisted of thin, closed-end, Kovar tubes that were instrumented with strain gages an...
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ftosti:oai:osti.gov:6187028 2023-07-30T04:02:56+02:00 An experimental/analytical comparison of strains in encapsulated assemblies Guess, T.R. Burchett, S.N. 2008-02-07 application/pdf http://www.osti.gov/servlets/purl/6187028 https://www.osti.gov/biblio/6187028 https://doi.org/10.2172/6187028 unknown http://www.osti.gov/servlets/purl/6187028 https://www.osti.gov/biblio/6187028 https://doi.org/10.2172/6187028 doi:10.2172/6187028 36 MATERIALS SCIENCE 45 MILITARY TECHNOLOGY WEAPONRY AND NATIONAL DEFENSE 42 ENGINEERING EPOXIDES ENCAPSULATION STRAINS URETHANE CASTING CURING FINITE ELEMENT METHOD KOVAR MATERIALS TESTING TEMPERATURE DEPENDENCE TUBES ALLOYS CARBAMATES CARBONIC ACID DERIVATIVES CARBOXYLIC ACID SALTS COBALT ALLOYS FABRICATION IRON ALLOYS IRON BASE ALLOYS MANGANESE ADDITIONS MANGANESE ALLOYS NICKEL ALLOYS NUMERICAL SOLUTION ORGANIC COMPOUNDS ORGANIC NITROGEN COMPOUNDS ORGANIC OXYGEN COMPOUNDS TESTING 2008 ftosti https://doi.org/10.2172/6187028 2023-07-11T10:45:51Z A combined experimental and analytical study of strains developed in encapsulated assemblies during casting, curing and thermal excursions is described. The experimental setup, designed to measure in situ strains, consisted of thin, closed-end, Kovar tubes that were instrumented with strain gages and thermocouples before being over-cast with a polymeric encapsulant. Four bisphenol A (three diethanolamine cured and one anhydride cured) epoxy-based materials and one urethane elastomeric material were studied. After cure of the encapsulant, tube strains were measured over the temperature range of {minus}55{degrees}C to 90{degrees}C. The thermal excursion experiments were then numerically modeled using finite element analyses and the computed strains were compared to the experimental strains. The predicted strains were over estimated (conservative) when a linear, elastic, temperature-dependent material model was assumed for the encapsulant and the stress free temperature T{sub i} was assumed to correspond to the cure temperature {Tc} of the encapsulant. Very good agreement was obtained with linear elastic calculations provided that the stress free temperature corresponded to the onset of the glassy-to-rubbery transition range of the encapsulant. Finally, excellent agreement was obtained in one of the materials (828/DEA) when a viscoelastic material model was utilized and a stress free temperature corresponding to the cure temperature was assumed. 13 refs., 20 figs., 3 tabs. Other/Unknown Material Carbonic acid SciTec Connect (Office of Scientific and Technical Information - OSTI, U.S. Department of Energy) |
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Open Polar |
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SciTec Connect (Office of Scientific and Technical Information - OSTI, U.S. Department of Energy) |
op_collection_id |
ftosti |
language |
unknown |
topic |
36 MATERIALS SCIENCE 45 MILITARY TECHNOLOGY WEAPONRY AND NATIONAL DEFENSE 42 ENGINEERING EPOXIDES ENCAPSULATION STRAINS URETHANE CASTING CURING FINITE ELEMENT METHOD KOVAR MATERIALS TESTING TEMPERATURE DEPENDENCE TUBES ALLOYS CARBAMATES CARBONIC ACID DERIVATIVES CARBOXYLIC ACID SALTS COBALT ALLOYS FABRICATION IRON ALLOYS IRON BASE ALLOYS MANGANESE ADDITIONS MANGANESE ALLOYS NICKEL ALLOYS NUMERICAL SOLUTION ORGANIC COMPOUNDS ORGANIC NITROGEN COMPOUNDS ORGANIC OXYGEN COMPOUNDS TESTING |
spellingShingle |
36 MATERIALS SCIENCE 45 MILITARY TECHNOLOGY WEAPONRY AND NATIONAL DEFENSE 42 ENGINEERING EPOXIDES ENCAPSULATION STRAINS URETHANE CASTING CURING FINITE ELEMENT METHOD KOVAR MATERIALS TESTING TEMPERATURE DEPENDENCE TUBES ALLOYS CARBAMATES CARBONIC ACID DERIVATIVES CARBOXYLIC ACID SALTS COBALT ALLOYS FABRICATION IRON ALLOYS IRON BASE ALLOYS MANGANESE ADDITIONS MANGANESE ALLOYS NICKEL ALLOYS NUMERICAL SOLUTION ORGANIC COMPOUNDS ORGANIC NITROGEN COMPOUNDS ORGANIC OXYGEN COMPOUNDS TESTING Guess, T.R. Burchett, S.N. An experimental/analytical comparison of strains in encapsulated assemblies |
topic_facet |
36 MATERIALS SCIENCE 45 MILITARY TECHNOLOGY WEAPONRY AND NATIONAL DEFENSE 42 ENGINEERING EPOXIDES ENCAPSULATION STRAINS URETHANE CASTING CURING FINITE ELEMENT METHOD KOVAR MATERIALS TESTING TEMPERATURE DEPENDENCE TUBES ALLOYS CARBAMATES CARBONIC ACID DERIVATIVES CARBOXYLIC ACID SALTS COBALT ALLOYS FABRICATION IRON ALLOYS IRON BASE ALLOYS MANGANESE ADDITIONS MANGANESE ALLOYS NICKEL ALLOYS NUMERICAL SOLUTION ORGANIC COMPOUNDS ORGANIC NITROGEN COMPOUNDS ORGANIC OXYGEN COMPOUNDS TESTING |
description |
A combined experimental and analytical study of strains developed in encapsulated assemblies during casting, curing and thermal excursions is described. The experimental setup, designed to measure in situ strains, consisted of thin, closed-end, Kovar tubes that were instrumented with strain gages and thermocouples before being over-cast with a polymeric encapsulant. Four bisphenol A (three diethanolamine cured and one anhydride cured) epoxy-based materials and one urethane elastomeric material were studied. After cure of the encapsulant, tube strains were measured over the temperature range of {minus}55{degrees}C to 90{degrees}C. The thermal excursion experiments were then numerically modeled using finite element analyses and the computed strains were compared to the experimental strains. The predicted strains were over estimated (conservative) when a linear, elastic, temperature-dependent material model was assumed for the encapsulant and the stress free temperature T{sub i} was assumed to correspond to the cure temperature {Tc} of the encapsulant. Very good agreement was obtained with linear elastic calculations provided that the stress free temperature corresponded to the onset of the glassy-to-rubbery transition range of the encapsulant. Finally, excellent agreement was obtained in one of the materials (828/DEA) when a viscoelastic material model was utilized and a stress free temperature corresponding to the cure temperature was assumed. 13 refs., 20 figs., 3 tabs. |
author |
Guess, T.R. Burchett, S.N. |
author_facet |
Guess, T.R. Burchett, S.N. |
author_sort |
Guess, T.R. |
title |
An experimental/analytical comparison of strains in encapsulated assemblies |
title_short |
An experimental/analytical comparison of strains in encapsulated assemblies |
title_full |
An experimental/analytical comparison of strains in encapsulated assemblies |
title_fullStr |
An experimental/analytical comparison of strains in encapsulated assemblies |
title_full_unstemmed |
An experimental/analytical comparison of strains in encapsulated assemblies |
title_sort |
experimental/analytical comparison of strains in encapsulated assemblies |
publishDate |
2008 |
url |
http://www.osti.gov/servlets/purl/6187028 https://www.osti.gov/biblio/6187028 https://doi.org/10.2172/6187028 |
genre |
Carbonic acid |
genre_facet |
Carbonic acid |
op_relation |
http://www.osti.gov/servlets/purl/6187028 https://www.osti.gov/biblio/6187028 https://doi.org/10.2172/6187028 doi:10.2172/6187028 |
op_doi |
https://doi.org/10.2172/6187028 |
_version_ |
1772813828860411904 |