Method for reinforcing openings of laminated composite material load-carrying structure
The invention relates to a method for reinforcing openings of a laminated composite material load-carrying structure, and aims to provide an opening reinforcement method which ensures easily controlled quality, is simple and is high in work efficiency. The method mainly comprises the following steps...
Gespeichert in:
Hauptverfasser: | , , , , , |
---|---|
Format: | Patent |
Sprache: | chi ; eng |
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 | TIE YING LI CHENG ZHAO HUADONG XU PING HUANG CONGKUI ZHENG YANPING |
description | The invention relates to a method for reinforcing openings of a laminated composite material load-carrying structure, and aims to provide an opening reinforcement method which ensures easily controlled quality, is simple and is high in work efficiency. The method mainly comprises the following steps of: laying fiber prepreg on a mandrel to prepare a patch 1, continuously laying fiber prepreg on the patch 1 to prepare a composite material body, laying a patch 2, integrally sewing hole edges of the composite material body and the symmetrically laid patches, and integrally compacting and curing, wherein the patches are cone-shaped; a thickness variation transition area is formed at the boundary of a reinforcing area; double means of patch reinforcing and sewing reinforcing are adopted; and the reinforcing area and the composite material body can be integrally/independently formed. When reinforcement is implemented by the method, the manufacturing cost of a mold can be reduced, the patches and the composite mater |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN102452175A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN102452175A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN102452175A3</originalsourceid><addsrcrecordid>eNqNyzEKAjEQheE0FqLeYTzAgru6WMui2GglWC5DMlkDSSZMsoW3N4IHsPr44b2let6ovNiAZQEhF6vaxQk4UaxmYAseg4tYyIDmkDi7QhBqi0MPntE0GkXe31suMusyC63VwqLPtPm5UtvL-TFcG0o8Uk6oKVIZh3u76w591x770_6fzQe7azq4</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Method for reinforcing openings of laminated composite material load-carrying structure</title><source>esp@cenet</source><creator>TIE YING ; LI CHENG ; ZHAO HUADONG ; XU PING ; HUANG CONGKUI ; ZHENG YANPING</creator><creatorcontrib>TIE YING ; LI CHENG ; ZHAO HUADONG ; XU PING ; HUANG CONGKUI ; ZHENG YANPING</creatorcontrib><description>The invention relates to a method for reinforcing openings of a laminated composite material load-carrying structure, and aims to provide an opening reinforcement method which ensures easily controlled quality, is simple and is high in work efficiency. The method mainly comprises the following steps of: laying fiber prepreg on a mandrel to prepare a patch 1, continuously laying fiber prepreg on the patch 1 to prepare a composite material body, laying a patch 2, integrally sewing hole edges of the composite material body and the symmetrically laid patches, and integrally compacting and curing, wherein the patches are cone-shaped; a thickness variation transition area is formed at the boundary of a reinforcing area; double means of patch reinforcing and sewing reinforcing are adopted; and the reinforcing area and the composite material body can be integrally/independently formed. When reinforcement is implemented by the method, the manufacturing cost of a mold can be reduced, the patches and the composite mater</description><language>chi ; eng</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>2012</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&date=20120516&DB=EPODOC&CC=CN&NR=102452175A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20120516&DB=EPODOC&CC=CN&NR=102452175A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TIE YING</creatorcontrib><creatorcontrib>LI CHENG</creatorcontrib><creatorcontrib>ZHAO HUADONG</creatorcontrib><creatorcontrib>XU PING</creatorcontrib><creatorcontrib>HUANG CONGKUI</creatorcontrib><creatorcontrib>ZHENG YANPING</creatorcontrib><title>Method for reinforcing openings of laminated composite material load-carrying structure</title><description>The invention relates to a method for reinforcing openings of a laminated composite material load-carrying structure, and aims to provide an opening reinforcement method which ensures easily controlled quality, is simple and is high in work efficiency. The method mainly comprises the following steps of: laying fiber prepreg on a mandrel to prepare a patch 1, continuously laying fiber prepreg on the patch 1 to prepare a composite material body, laying a patch 2, integrally sewing hole edges of the composite material body and the symmetrically laid patches, and integrally compacting and curing, wherein the patches are cone-shaped; a thickness variation transition area is formed at the boundary of a reinforcing area; double means of patch reinforcing and sewing reinforcing are adopted; and the reinforcing area and the composite material body can be integrally/independently formed. When reinforcement is implemented by the method, the manufacturing cost of a mold can be reduced, the patches and the composite mater</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>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyzEKAjEQheE0FqLeYTzAgru6WMui2GglWC5DMlkDSSZMsoW3N4IHsPr44b2let6ovNiAZQEhF6vaxQk4UaxmYAseg4tYyIDmkDi7QhBqi0MPntE0GkXe31suMusyC63VwqLPtPm5UtvL-TFcG0o8Uk6oKVIZh3u76w591x770_6fzQe7azq4</recordid><startdate>20120516</startdate><enddate>20120516</enddate><creator>TIE YING</creator><creator>LI CHENG</creator><creator>ZHAO HUADONG</creator><creator>XU PING</creator><creator>HUANG CONGKUI</creator><creator>ZHENG YANPING</creator><scope>EVB</scope></search><sort><creationdate>20120516</creationdate><title>Method for reinforcing openings of laminated composite material load-carrying structure</title><author>TIE YING ; LI CHENG ; ZHAO HUADONG ; XU PING ; HUANG CONGKUI ; ZHENG YANPING</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN102452175A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2012</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>TIE YING</creatorcontrib><creatorcontrib>LI CHENG</creatorcontrib><creatorcontrib>ZHAO HUADONG</creatorcontrib><creatorcontrib>XU PING</creatorcontrib><creatorcontrib>HUANG CONGKUI</creatorcontrib><creatorcontrib>ZHENG YANPING</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TIE YING</au><au>LI CHENG</au><au>ZHAO HUADONG</au><au>XU PING</au><au>HUANG CONGKUI</au><au>ZHENG YANPING</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method for reinforcing openings of laminated composite material load-carrying structure</title><date>2012-05-16</date><risdate>2012</risdate><abstract>The invention relates to a method for reinforcing openings of a laminated composite material load-carrying structure, and aims to provide an opening reinforcement method which ensures easily controlled quality, is simple and is high in work efficiency. The method mainly comprises the following steps of: laying fiber prepreg on a mandrel to prepare a patch 1, continuously laying fiber prepreg on the patch 1 to prepare a composite material body, laying a patch 2, integrally sewing hole edges of the composite material body and the symmetrically laid patches, and integrally compacting and curing, wherein the patches are cone-shaped; a thickness variation transition area is formed at the boundary of a reinforcing area; double means of patch reinforcing and sewing reinforcing are adopted; and the reinforcing area and the composite material body can be integrally/independently formed. When reinforcement is implemented by the method, the manufacturing cost of a mold can be reduced, the patches and the composite mater</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | chi ; eng |
recordid | cdi_epo_espacenet_CN102452175A |
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 for reinforcing openings of laminated composite material load-carrying structure |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-13T18%3A13%3A03IST&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=TIE%20YING&rft.date=2012-05-16&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN102452175A%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 |