METHOD OF CURING A COMPOSITE ARTICLE USING DIFFERENTIAL VACUUM

A method of curing a composite layup may include applying an inner bag vacuum pressure to an inner bag chamber (166) and an outer vacuum pressure to an outer vacuum chamber (194). The vacuum inner bag chamber may be formed by a vacuum bag (150) covering a composite layup (106) and sealed to a formin...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: MICHAEL R. ANDERSON, GRANT C. ZENKNER
Format: Patent
Sprache:eng ; por
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator MICHAEL R. ANDERSON
GRANT C. ZENKNER
description A method of curing a composite layup may include applying an inner bag vacuum pressure to an inner bag chamber (166) and an outer vacuum pressure to an outer vacuum chamber (194). The vacuum inner bag chamber may be formed by a vacuum bag (150) covering a composite layup (106) and sealed to a forming tool (104) with an inner bag chamber seal (158). The inner bag vacuum pressure may be no less than the outer vacuum pressure. The temperature of the composite layup may be increased to an elevated temperature to initiate a temperature hold period. The method may additionally include venting the outer vacuum chamber to atmosphere to initiate an outer vacuum chamber venting period during the temperature hold period, and applying compaction pressure to the inner bag chamber seal during the outer vacuum chamber venting period. The outer vacuum pressure may be re-applied to the outer vacuum chamber to terminate the outer vacuum chamber venting period.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_PT3153289TT</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>PT3153289TT</sourcerecordid><originalsourceid>FETCH-epo_espacenet_PT3153289TT3</originalsourceid><addsrcrecordid>eNrjZLDzdQ3x8HdR8HdTcA4N8vRzV3BUcPb3DfAP9gxxVXAMCvF09nFVCA0Gybh4urm5Brn6hXg6-iiEOTqHhvryMLCmJeYUp_JCaW4GBTfXEGcP3dSC_PjU4oLE5NS81JL4gBBjQ1NjIwvLkBBjIpQAAAI5Ki8</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>METHOD OF CURING A COMPOSITE ARTICLE USING DIFFERENTIAL VACUUM</title><source>esp@cenet</source><creator>MICHAEL R. ANDERSON ; GRANT C. ZENKNER</creator><creatorcontrib>MICHAEL R. ANDERSON ; GRANT C. ZENKNER</creatorcontrib><description>A method of curing a composite layup may include applying an inner bag vacuum pressure to an inner bag chamber (166) and an outer vacuum pressure to an outer vacuum chamber (194). The vacuum inner bag chamber may be formed by a vacuum bag (150) covering a composite layup (106) and sealed to a forming tool (104) with an inner bag chamber seal (158). The inner bag vacuum pressure may be no less than the outer vacuum pressure. The temperature of the composite layup may be increased to an elevated temperature to initiate a temperature hold period. The method may additionally include venting the outer vacuum chamber to atmosphere to initiate an outer vacuum chamber venting period during the temperature hold period, and applying compaction pressure to the inner bag chamber seal during the outer vacuum chamber venting period. The outer vacuum pressure may be re-applied to the outer vacuum chamber to terminate the outer vacuum chamber venting period.</description><language>eng ; por</language><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; PERFORMING OPERATIONS ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; TRANSPORTING ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>2019</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20190530&amp;DB=EPODOC&amp;CC=PT&amp;NR=3153289T$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20190530&amp;DB=EPODOC&amp;CC=PT&amp;NR=3153289T$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MICHAEL R. ANDERSON</creatorcontrib><creatorcontrib>GRANT C. ZENKNER</creatorcontrib><title>METHOD OF CURING A COMPOSITE ARTICLE USING DIFFERENTIAL VACUUM</title><description>A method of curing a composite layup may include applying an inner bag vacuum pressure to an inner bag chamber (166) and an outer vacuum pressure to an outer vacuum chamber (194). The vacuum inner bag chamber may be formed by a vacuum bag (150) covering a composite layup (106) and sealed to a forming tool (104) with an inner bag chamber seal (158). The inner bag vacuum pressure may be no less than the outer vacuum pressure. The temperature of the composite layup may be increased to an elevated temperature to initiate a temperature hold period. The method may additionally include venting the outer vacuum chamber to atmosphere to initiate an outer vacuum chamber venting period during the temperature hold period, and applying compaction pressure to the inner bag chamber seal during the outer vacuum chamber venting period. The outer vacuum pressure may be re-applied to the outer vacuum chamber to terminate the outer vacuum chamber venting period.</description><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>PERFORMING OPERATIONS</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>TRANSPORTING</subject><subject>WORKING OF PLASTICS</subject><subject>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLDzdQ3x8HdR8HdTcA4N8vRzV3BUcPb3DfAP9gxxVXAMCvF09nFVCA0Gybh4urm5Brn6hXg6-iiEOTqHhvryMLCmJeYUp_JCaW4GBTfXEGcP3dSC_PjU4oLE5NS81JL4gBBjQ1NjIwvLkBBjIpQAAAI5Ki8</recordid><startdate>20190530</startdate><enddate>20190530</enddate><creator>MICHAEL R. ANDERSON</creator><creator>GRANT C. ZENKNER</creator><scope>EVB</scope></search><sort><creationdate>20190530</creationdate><title>METHOD OF CURING A COMPOSITE ARTICLE USING DIFFERENTIAL VACUUM</title><author>MICHAEL R. ANDERSON ; GRANT C. ZENKNER</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_PT3153289TT3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; por</language><creationdate>2019</creationdate><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>PERFORMING OPERATIONS</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>TRANSPORTING</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>MICHAEL R. ANDERSON</creatorcontrib><creatorcontrib>GRANT C. ZENKNER</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MICHAEL R. ANDERSON</au><au>GRANT C. ZENKNER</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD OF CURING A COMPOSITE ARTICLE USING DIFFERENTIAL VACUUM</title><date>2019-05-30</date><risdate>2019</risdate><abstract>A method of curing a composite layup may include applying an inner bag vacuum pressure to an inner bag chamber (166) and an outer vacuum pressure to an outer vacuum chamber (194). The vacuum inner bag chamber may be formed by a vacuum bag (150) covering a composite layup (106) and sealed to a forming tool (104) with an inner bag chamber seal (158). The inner bag vacuum pressure may be no less than the outer vacuum pressure. The temperature of the composite layup may be increased to an elevated temperature to initiate a temperature hold period. The method may additionally include venting the outer vacuum chamber to atmosphere to initiate an outer vacuum chamber venting period during the temperature hold period, and applying compaction pressure to the inner bag chamber seal during the outer vacuum chamber venting period. The outer vacuum pressure may be re-applied to the outer vacuum chamber to terminate the outer vacuum chamber venting period.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; por
recordid cdi_epo_espacenet_PT3153289TT
source esp@cenet
subjects AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
PERFORMING OPERATIONS
SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR
SHAPING OR JOINING OF PLASTICS
TRANSPORTING
WORKING OF PLASTICS
WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
title METHOD OF CURING A COMPOSITE ARTICLE USING DIFFERENTIAL VACUUM
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-26T15%3A07%3A25IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=MICHAEL%20R.%20ANDERSON&rft.date=2019-05-30&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EPT3153289TT%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true