MOUNTING A CERAMIC COMPONENT TO A NON-CERAMIC COMPONENT IN A GAS TURBINE ENGINE

MOUNTING A CERAMIC COMPONENT TO A NON-CERAMIC COMPONENT IN A GAS TURBINE ENGINE

A combustor with a centerline (38) is provided that includes a support structure (116) and a heat shield (118). The heat shield (118) extends circumferentially about and axially along the centerline (38). The heat shield (118) is configured from or otherwise includes ceramic material. The heat shiel...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: KRAMER, Stephen K
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
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 KRAMER, Stephen K
description A combustor with a centerline (38) is provided that includes a support structure (116) and a heat shield (118). The heat shield (118) extends circumferentially about and axially along the centerline (38). The heat shield (118) is configured from or otherwise includes ceramic material. The heat shield (118) is mounted to the support structure (116) by an interlocking joint connection (36). The interlocking joint connection (36) includes a projection (66) and a groove (50). The projection (66) is configured with the support structure (116) and includes a plurality of fingers (76) arranged along and projecting into the groove (50). The groove (50) is formed in the heat shield (118).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP4060237B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP4060237B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP4060237B13</originalsourceid><addsrcrecordid>eNrjZPD39Q_1C_H0c1dwVHB2DXL09XRWcPb3DfD3c_ULUQjxBwr7-fvpYkp5-gGl3B2DFUJCg5w8_VwVXP3cgRQPA2taYk5xKi-U5mZQcHMNcfbQTS3Ij08tLkhMTs1LLYl3DTAxMDMwMjZ3MjQmQgkAqGctyg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>MOUNTING A CERAMIC COMPONENT TO A NON-CERAMIC COMPONENT IN A GAS TURBINE ENGINE</title><source>esp@cenet</source><creator>KRAMER, Stephen K</creator><creatorcontrib>KRAMER, Stephen K</creatorcontrib><description>A combustor with a centerline (38) is provided that includes a support structure (116) and a heat shield (118). The heat shield (118) extends circumferentially about and axially along the centerline (38). The heat shield (118) is configured from or otherwise includes ceramic material. The heat shield (118) is mounted to the support structure (116) by an interlocking joint connection (36). The interlocking joint connection (36) includes a projection (66) and a groove (50). The projection (66) is configured with the support structure (116) and includes a plurality of fingers (76) arranged along and projecting into the groove (50). The groove (50) is formed in the heat shield (118).</description><language>eng ; fre ; ger</language><subject>BLASTING ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2023</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=20231129&amp;DB=EPODOC&amp;CC=EP&amp;NR=4060237B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20231129&amp;DB=EPODOC&amp;CC=EP&amp;NR=4060237B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KRAMER, Stephen K</creatorcontrib><title>MOUNTING A CERAMIC COMPONENT TO A NON-CERAMIC COMPONENT IN A GAS TURBINE ENGINE</title><description>A combustor with a centerline (38) is provided that includes a support structure (116) and a heat shield (118). The heat shield (118) extends circumferentially about and axially along the centerline (38). The heat shield (118) is configured from or otherwise includes ceramic material. The heat shield (118) is mounted to the support structure (116) by an interlocking joint connection (36). The interlocking joint connection (36) includes a projection (66) and a groove (50). The projection (66) is configured with the support structure (116) and includes a plurality of fingers (76) arranged along and projecting into the groove (50). The groove (50) is formed in the heat shield (118).</description><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION PROCESSES</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPD39Q_1C_H0c1dwVHB2DXL09XRWcPb3DfD3c_ULUQjxBwr7-fvpYkp5-gGl3B2DFUJCg5w8_VwVXP3cgRQPA2taYk5xKi-U5mZQcHMNcfbQTS3Ij08tLkhMTs1LLYl3DTAxMDMwMjZ3MjQmQgkAqGctyg</recordid><startdate>20231129</startdate><enddate>20231129</enddate><creator>KRAMER, Stephen K</creator><scope>EVB</scope></search><sort><creationdate>20231129</creationdate><title>MOUNTING A CERAMIC COMPONENT TO A NON-CERAMIC COMPONENT IN A GAS TURBINE ENGINE</title><author>KRAMER, Stephen K</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4060237B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION PROCESSES</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KRAMER, Stephen K</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KRAMER, Stephen K</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>MOUNTING A CERAMIC COMPONENT TO A NON-CERAMIC COMPONENT IN A GAS TURBINE ENGINE</title><date>2023-11-29</date><risdate>2023</risdate><abstract>A combustor with a centerline (38) is provided that includes a support structure (116) and a heat shield (118). The heat shield (118) extends circumferentially about and axially along the centerline (38). The heat shield (118) is configured from or otherwise includes ceramic material. The heat shield (118) is mounted to the support structure (116) by an interlocking joint connection (36). The interlocking joint connection (36) includes a projection (66) and a groove (50). The projection (66) is configured with the support structure (116) and includes a plurality of fingers (76) arranged along and projecting into the groove (50). The groove (50) is formed in the heat shield (118).</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP4060237B1
source esp@cenet
subjects BLASTING
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title MOUNTING A CERAMIC COMPONENT TO A NON-CERAMIC COMPONENT IN 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=2024-12-30T05%3A38%3A39IST&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=KRAMER,%20Stephen%20K&rft.date=2023-11-29&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP4060237B1%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