REPAIR STRIP AND PROCESS FOR WIND TURBINE LEADING EDGE PROTECTION TAPE
A method is described for repairing the surface of rotor blades or aircraft wings, comprising (a) a composite substrate; and (b) a protection layer having at least one area of at least partial damage, the method comprising (i) removing at least part of the damaged part of the protection tape; (ii) o...
Gespeichert in:
1. Verfasser: | |
---|---|
Format: | Patent |
Sprache: | eng ; fre ; ger |
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 | Schoeppel, Wolfgang |
description | A method is described for repairing the surface of rotor blades or aircraft wings, comprising
(a) a composite substrate; and
(b) a protection layer having at least one area of at least partial damage,
the method comprising
(i) removing at least part of the damaged part of the protection tape;
(ii) optionally, reconstruct the surface of damaged composite substrate;
(iii) optionally, apply primer solution to the surface of the composite substrate;
(iv) optionally, apply a polymer solution, preferably in at least one organic solvent;
(v) applying a repair patch of a polymer tape comprising at least one thermoplastic elastomer onto at least of a part of the composite surface;
(vi) applying heat so that the repair patch melts and covers the damaged area, thereby forming a protection layer. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3345752A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3345752A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3345752A13</originalsourceid><addsrcrecordid>eNrjZHALcg1w9AxSCA4J8gxQcPRzUQgI8nd2DQ5WcPMPUgj3BAqEhAY5efq5Kvi4Orp4-rkruLq4u4JUhbg6h3j6-ymEOAa48jCwpiXmFKfyQmluBgU31xBnD93Ugvz41OKCxOTUvNSSeNcAY2MTU3NTI0dDYyKUAABGwCvC</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>REPAIR STRIP AND PROCESS FOR WIND TURBINE LEADING EDGE PROTECTION TAPE</title><source>esp@cenet</source><creator>Schoeppel, Wolfgang</creator><creatorcontrib>Schoeppel, Wolfgang</creatorcontrib><description>A method is described for repairing the surface of rotor blades or aircraft wings, comprising
(a) a composite substrate; and
(b) a protection layer having at least one area of at least partial damage,
the method comprising
(i) removing at least part of the damaged part of the protection tape;
(ii) optionally, reconstruct the surface of damaged composite substrate;
(iii) optionally, apply primer solution to the surface of the composite substrate;
(iv) optionally, apply a polymer solution, preferably in at least one organic solvent;
(v) applying a repair patch of a polymer tape comprising at least one thermoplastic elastomer onto at least of a part of the composite surface;
(vi) applying heat so that the repair patch melts and covers the damaged area, thereby forming a protection layer.</description><language>eng ; fre ; ger</language><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES ; INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS ; 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>2018</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=20180711&DB=EPODOC&CC=EP&NR=3345752A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180711&DB=EPODOC&CC=EP&NR=3345752A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Schoeppel, Wolfgang</creatorcontrib><title>REPAIR STRIP AND PROCESS FOR WIND TURBINE LEADING EDGE PROTECTION TAPE</title><description>A method is described for repairing the surface of rotor blades or aircraft wings, comprising
(a) a composite substrate; and
(b) a protection layer having at least one area of at least partial damage,
the method comprising
(i) removing at least part of the damaged part of the protection tape;
(ii) optionally, reconstruct the surface of damaged composite substrate;
(iii) optionally, apply primer solution to the surface of the composite substrate;
(iv) optionally, apply a polymer solution, preferably in at least one organic solvent;
(v) applying a repair patch of a polymer tape comprising at least one thermoplastic elastomer onto at least of a part of the composite surface;
(vi) applying heat so that the repair patch melts and covers the damaged area, thereby forming a protection layer.</description><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES</subject><subject>INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHALcg1w9AxSCA4J8gxQcPRzUQgI8nd2DQ5WcPMPUgj3BAqEhAY5efq5Kvi4Orp4-rkruLq4u4JUhbg6h3j6-ymEOAa48jCwpiXmFKfyQmluBgU31xBnD93Ugvz41OKCxOTUvNSSeNcAY2MTU3NTI0dDYyKUAABGwCvC</recordid><startdate>20180711</startdate><enddate>20180711</enddate><creator>Schoeppel, Wolfgang</creator><scope>EVB</scope></search><sort><creationdate>20180711</creationdate><title>REPAIR STRIP AND PROCESS FOR WIND TURBINE LEADING EDGE PROTECTION TAPE</title><author>Schoeppel, Wolfgang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3345752A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</creationdate><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES</topic><topic>INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS</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>Schoeppel, Wolfgang</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Schoeppel, Wolfgang</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>REPAIR STRIP AND PROCESS FOR WIND TURBINE LEADING EDGE PROTECTION TAPE</title><date>2018-07-11</date><risdate>2018</risdate><abstract>A method is described for repairing the surface of rotor blades or aircraft wings, comprising
(a) a composite substrate; and
(b) a protection layer having at least one area of at least partial damage,
the method comprising
(i) removing at least part of the damaged part of the protection tape;
(ii) optionally, reconstruct the surface of damaged composite substrate;
(iii) optionally, apply primer solution to the surface of the composite substrate;
(iv) optionally, apply a polymer solution, preferably in at least one organic solvent;
(v) applying a repair patch of a polymer tape comprising at least one thermoplastic elastomer onto at least of a part of the composite surface;
(vi) applying heat so that the repair patch melts and covers the damaged area, thereby forming a protection layer.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng ; fre ; ger |
recordid | cdi_epo_espacenet_EP3345752A1 |
source | esp@cenet |
subjects | AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS 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 | REPAIR STRIP AND PROCESS FOR WIND TURBINE LEADING EDGE PROTECTION TAPE |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-12T06%3A39%3A10IST&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=Schoeppel,%20Wolfgang&rft.date=2018-07-11&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3345752A1%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 |