Method for machining the trailing edge of a turbine engine blade
The present invention relates to a method for manufacturing a turbine engine blade, the blade comprising an airfoil and the profile of the airfoil being defined by a theoretical digital model, including the manufacture of a blank having a thickened portion along the trailing edge of the airfoil rela...
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 | LOUESDON YVON MARIE-JOSEPH ALQUIER DAMIEN TAMI JOSEPH QUACH DANIEL MALTAVERNE SABINE CISSE FADOUA LE MERDI FLORIAN |
description | The present invention relates to a method for manufacturing a turbine engine blade, the blade comprising an airfoil and the profile of the airfoil being defined by a theoretical digital model, including the manufacture of a blank having a thickened portion along the trailing edge of the airfoil relative to the theoretical profile, characterized in that said thickened portion is removed by adaptive machining, including the following steps: positioning the blank in a reference frame; acquiring, by probing at a predetermined number of points (Ni) on a first surface of the blank along the trailing edge, the position of said points in the reference frame; determining the differences, in one direction, in the delta position (Ni) from corresponding points of the theoretical model; producing machining grids on said surface of the blank, the peaks of the grids being determined from said points (Ni); determining the amount of material to be removed from the surface of the grids, said amount being based on the position |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN104246635A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN104246635A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN104246635A3</originalsourceid><addsrcrecordid>eNrjZHDwTS3JyE9RSMsvUshNTM7IzMvMS1coyUhVKClKzMwBcVJT0lMV8tMUEhVKSouSMvNSFVLz0kFUUk5iSioPA2taYk5xKi-U5mZQdHMNcfbQTS3Ij08tLkhMTs1LLYl39jM0MDEyMTMzNnU0JkYNAHS0MIg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Method for machining the trailing edge of a turbine engine blade</title><source>esp@cenet</source><creator>LOUESDON YVON MARIE-JOSEPH ; ALQUIER DAMIEN ; TAMI JOSEPH ; QUACH DANIEL ; MALTAVERNE SABINE ; CISSE FADOUA ; LE MERDI FLORIAN</creator><creatorcontrib>LOUESDON YVON MARIE-JOSEPH ; ALQUIER DAMIEN ; TAMI JOSEPH ; QUACH DANIEL ; MALTAVERNE SABINE ; CISSE FADOUA ; LE MERDI FLORIAN</creatorcontrib><description>The present invention relates to a method for manufacturing a turbine engine blade, the blade comprising an airfoil and the profile of the airfoil being defined by a theoretical digital model, including the manufacture of a blank having a thickened portion along the trailing edge of the airfoil relative to the theoretical profile, characterized in that said thickened portion is removed by adaptive machining, including the following steps: positioning the blank in a reference frame; acquiring, by probing at a predetermined number of points (Ni) on a first surface of the blank along the trailing edge, the position of said points in the reference frame; determining the differences, in one direction, in the delta position (Ni) from corresponding points of the theoretical model; producing machining grids on said surface of the blank, the peaks of the grids being determined from said points (Ni); determining the amount of material to be removed from the surface of the grids, said amount being based on the position</description><language>chi ; eng</language><subject>CONTROL OR REGULATING SYSTEMS IN GENERAL ; CONTROLLING ; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS ; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS ; PHYSICS ; REGULATING</subject><creationdate>2014</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=20141224&DB=EPODOC&CC=CN&NR=104246635A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20141224&DB=EPODOC&CC=CN&NR=104246635A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LOUESDON YVON MARIE-JOSEPH</creatorcontrib><creatorcontrib>ALQUIER DAMIEN</creatorcontrib><creatorcontrib>TAMI JOSEPH</creatorcontrib><creatorcontrib>QUACH DANIEL</creatorcontrib><creatorcontrib>MALTAVERNE SABINE</creatorcontrib><creatorcontrib>CISSE FADOUA</creatorcontrib><creatorcontrib>LE MERDI FLORIAN</creatorcontrib><title>Method for machining the trailing edge of a turbine engine blade</title><description>The present invention relates to a method for manufacturing a turbine engine blade, the blade comprising an airfoil and the profile of the airfoil being defined by a theoretical digital model, including the manufacture of a blank having a thickened portion along the trailing edge of the airfoil relative to the theoretical profile, characterized in that said thickened portion is removed by adaptive machining, including the following steps: positioning the blank in a reference frame; acquiring, by probing at a predetermined number of points (Ni) on a first surface of the blank along the trailing edge, the position of said points in the reference frame; determining the differences, in one direction, in the delta position (Ni) from corresponding points of the theoretical model; producing machining grids on said surface of the blank, the peaks of the grids being determined from said points (Ni); determining the amount of material to be removed from the surface of the grids, said amount being based on the position</description><subject>CONTROL OR REGULATING SYSTEMS IN GENERAL</subject><subject>CONTROLLING</subject><subject>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</subject><subject>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHDwTS3JyE9RSMsvUshNTM7IzMvMS1coyUhVKClKzMwBcVJT0lMV8tMUEhVKSouSMvNSFVLz0kFUUk5iSioPA2taYk5xKi-U5mZQdHMNcfbQTS3Ij08tLkhMTs1LLYl39jM0MDEyMTMzNnU0JkYNAHS0MIg</recordid><startdate>20141224</startdate><enddate>20141224</enddate><creator>LOUESDON YVON MARIE-JOSEPH</creator><creator>ALQUIER DAMIEN</creator><creator>TAMI JOSEPH</creator><creator>QUACH DANIEL</creator><creator>MALTAVERNE SABINE</creator><creator>CISSE FADOUA</creator><creator>LE MERDI FLORIAN</creator><scope>EVB</scope></search><sort><creationdate>20141224</creationdate><title>Method for machining the trailing edge of a turbine engine blade</title><author>LOUESDON YVON MARIE-JOSEPH ; ALQUIER DAMIEN ; TAMI JOSEPH ; QUACH DANIEL ; MALTAVERNE SABINE ; CISSE FADOUA ; LE MERDI FLORIAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN104246635A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2014</creationdate><topic>CONTROL OR REGULATING SYSTEMS IN GENERAL</topic><topic>CONTROLLING</topic><topic>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</topic><topic>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><toplevel>online_resources</toplevel><creatorcontrib>LOUESDON YVON MARIE-JOSEPH</creatorcontrib><creatorcontrib>ALQUIER DAMIEN</creatorcontrib><creatorcontrib>TAMI JOSEPH</creatorcontrib><creatorcontrib>QUACH DANIEL</creatorcontrib><creatorcontrib>MALTAVERNE SABINE</creatorcontrib><creatorcontrib>CISSE FADOUA</creatorcontrib><creatorcontrib>LE MERDI FLORIAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LOUESDON YVON MARIE-JOSEPH</au><au>ALQUIER DAMIEN</au><au>TAMI JOSEPH</au><au>QUACH DANIEL</au><au>MALTAVERNE SABINE</au><au>CISSE FADOUA</au><au>LE MERDI FLORIAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method for machining the trailing edge of a turbine engine blade</title><date>2014-12-24</date><risdate>2014</risdate><abstract>The present invention relates to a method for manufacturing a turbine engine blade, the blade comprising an airfoil and the profile of the airfoil being defined by a theoretical digital model, including the manufacture of a blank having a thickened portion along the trailing edge of the airfoil relative to the theoretical profile, characterized in that said thickened portion is removed by adaptive machining, including the following steps: positioning the blank in a reference frame; acquiring, by probing at a predetermined number of points (Ni) on a first surface of the blank along the trailing edge, the position of said points in the reference frame; determining the differences, in one direction, in the delta position (Ni) from corresponding points of the theoretical model; producing machining grids on said surface of the blank, the peaks of the grids being determined from said points (Ni); determining the amount of material to be removed from the surface of the grids, said amount being based on the position</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | chi ; eng |
recordid | cdi_epo_espacenet_CN104246635A |
source | esp@cenet |
subjects | CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING |
title | Method for machining the trailing edge of a turbine engine blade |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-28T00%3A41%3A23IST&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=LOUESDON%20YVON%20MARIE-JOSEPH&rft.date=2014-12-24&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN104246635A%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 |