ARTICLE, COMPONENT, AND METHOD OF MAKING A COMPONENT OF A GAS TURBINE ENGINE

ARTICLE, COMPONENT, AND METHOD OF MAKING A COMPONENT OF A GAS TURBINE ENGINE

An article 201, a component 100, and a method of making a component 100 are provided. The article 201 includes a contoured proximal face 202 and a contoured distal face 203. The contoured proximal face 202 is arranged and disposed to substantially mirror a contour of an end wall of a component 100....

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: WEBER, Joseph Anthony, KOTTILINGAM, Srikanth Chandrudu, TOLLISON, Brian Lee
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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 WEBER, Joseph Anthony
KOTTILINGAM, Srikanth Chandrudu
TOLLISON, Brian Lee
description An article 201, a component 100, and a method of making a component 100 are provided. The article 201 includes a contoured proximal face 202 and a contoured distal face 203. The contoured proximal face 202 is arranged and disposed to substantially mirror a contour of an end wall of a component 100. The component 100 includes a first end wall 105, a second end wall 107, and an article 201 including a contoured proximal face 202 secured to at least one of the first end wall 105 and the second end wall 107. The method of making a component 100 includes forming an article 201 having a proximal face 202 and a distal face 203, contouring the proximal face 202 of the article 201 to form a contoured proximal face 202 that substantially mirrors a contour of a first end wall 105 or a second end wall 107 of the component 100, and securing the contoured proximal face 202 of the article 201 to one of the first end wall 105 and the second end wall 107.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3236013B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3236013B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3236013B13</originalsourceid><addsrcrecordid>eNrjZPBxDArxdPZx1VFw9vcN8Pdz9QvRUXD0c1HwdQ3x8HdR8HdT8HX09vRzV3BEqACJOiq4OwYrhIQGOXn6uSq4-rkDKR4G1rTEnOJUXijNzaDg5hri7KGbWpAfn1pckJicmpdaEu8aYGxkbGZgaOxkaEyEEgD4LCyk</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>ARTICLE, COMPONENT, AND METHOD OF MAKING A COMPONENT OF A GAS TURBINE ENGINE</title><source>esp@cenet</source><creator>WEBER, Joseph Anthony ; KOTTILINGAM, Srikanth Chandrudu ; TOLLISON, Brian Lee</creator><creatorcontrib>WEBER, Joseph Anthony ; KOTTILINGAM, Srikanth Chandrudu ; TOLLISON, Brian Lee</creatorcontrib><description>An article 201, a component 100, and a method of making a component 100 are provided. The article 201 includes a contoured proximal face 202 and a contoured distal face 203. The contoured proximal face 202 is arranged and disposed to substantially mirror a contour of an end wall of a component 100. The component 100 includes a first end wall 105, a second end wall 107, and an article 201 including a contoured proximal face 202 secured to at least one of the first end wall 105 and the second end wall 107. The method of making a component 100 includes forming an article 201 having a proximal face 202 and a distal face 203, contouring the proximal face 202 of the article 201 to form a contoured proximal face 202 that substantially mirrors a contour of a first end wall 105 or a second end wall 107 of the component 100, and securing the contoured proximal face 202 of the article 201 to one of the first end wall 105 and the second end wall 107.</description><language>eng ; fre ; ger</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2024</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=20240403&amp;DB=EPODOC&amp;CC=EP&amp;NR=3236013B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240403&amp;DB=EPODOC&amp;CC=EP&amp;NR=3236013B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WEBER, Joseph Anthony</creatorcontrib><creatorcontrib>KOTTILINGAM, Srikanth Chandrudu</creatorcontrib><creatorcontrib>TOLLISON, Brian Lee</creatorcontrib><title>ARTICLE, COMPONENT, AND METHOD OF MAKING A COMPONENT OF A GAS TURBINE ENGINE</title><description>An article 201, a component 100, and a method of making a component 100 are provided. The article 201 includes a contoured proximal face 202 and a contoured distal face 203. The contoured proximal face 202 is arranged and disposed to substantially mirror a contour of an end wall of a component 100. The component 100 includes a first end wall 105, a second end wall 107, and an article 201 including a contoured proximal face 202 secured to at least one of the first end wall 105 and the second end wall 107. The method of making a component 100 includes forming an article 201 having a proximal face 202 and a distal face 203, contouring the proximal face 202 of the article 201 to form a contoured proximal face 202 that substantially mirrors a contour of a first end wall 105 or a second end wall 107 of the component 100, and securing the contoured proximal face 202 of the article 201 to one of the first end wall 105 and the second end wall 107.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPBxDArxdPZx1VFw9vcN8Pdz9QvRUXD0c1HwdQ3x8HdR8HdT8HX09vRzV3BEqACJOiq4OwYrhIQGOXn6uSq4-rkDKR4G1rTEnOJUXijNzaDg5hri7KGbWpAfn1pckJicmpdaEu8aYGxkbGZgaOxkaEyEEgD4LCyk</recordid><startdate>20240403</startdate><enddate>20240403</enddate><creator>WEBER, Joseph Anthony</creator><creator>KOTTILINGAM, Srikanth Chandrudu</creator><creator>TOLLISON, Brian Lee</creator><scope>EVB</scope></search><sort><creationdate>20240403</creationdate><title>ARTICLE, COMPONENT, AND METHOD OF MAKING A COMPONENT OF A GAS TURBINE ENGINE</title><author>WEBER, Joseph Anthony ; KOTTILINGAM, Srikanth Chandrudu ; TOLLISON, Brian Lee</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3236013B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>WEBER, Joseph Anthony</creatorcontrib><creatorcontrib>KOTTILINGAM, Srikanth Chandrudu</creatorcontrib><creatorcontrib>TOLLISON, Brian Lee</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WEBER, Joseph Anthony</au><au>KOTTILINGAM, Srikanth Chandrudu</au><au>TOLLISON, Brian Lee</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ARTICLE, COMPONENT, AND METHOD OF MAKING A COMPONENT OF A GAS TURBINE ENGINE</title><date>2024-04-03</date><risdate>2024</risdate><abstract>An article 201, a component 100, and a method of making a component 100 are provided. The article 201 includes a contoured proximal face 202 and a contoured distal face 203. The contoured proximal face 202 is arranged and disposed to substantially mirror a contour of an end wall of a component 100. The component 100 includes a first end wall 105, a second end wall 107, and an article 201 including a contoured proximal face 202 secured to at least one of the first end wall 105 and the second end wall 107. The method of making a component 100 includes forming an article 201 having a proximal face 202 and a distal face 203, contouring the proximal face 202 of the article 201 to form a contoured proximal face 202 that substantially mirrors a contour of a first end wall 105 or a second end wall 107 of the component 100, and securing the contoured proximal face 202 of the article 201 to one of the first end wall 105 and the second end wall 107.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3236013B1
source esp@cenet
subjects BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
title ARTICLE, COMPONENT, AND METHOD OF MAKING A COMPONENT OF A GAS TURBINE ENGINE
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-01T17%3A26%3A35IST&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=WEBER,%20Joseph%20Anthony&rft.date=2024-04-03&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3236013B1%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