SYSTEM OF INTEGRATING BAFFLE FOR ENHANCED COOLING OF CMC LINER
PROBLEM TO BE SOLVED: To provide a system of integrating baffles for the enhanced cooling of CMC liners.SOLUTION: A system of integrating baffles for the enhanced cooling of CMC liners 300 and 700 is composed of a combustor assembly having a dome mount assembly 200, an outer liner 300 and an inner l...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Patent |
Sprache: | 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 | DERY BRYAN ROBERT BUSH SCOTT MATTHEW CORSMEIER DONALD MICHAEL |
description | PROBLEM TO BE SOLVED: To provide a system of integrating baffles for the enhanced cooling of CMC liners.SOLUTION: A system of integrating baffles for the enhanced cooling of CMC liners 300 and 700 is composed of a combustor assembly having a dome mount assembly 200, an outer liner 300 and an inner liner 700. Liners include those manufactured from and in a process for a CMC (Ceramic Matrix Composite). One or more liner baffles 500 and 800 such as an outer baffle 500 and an inner baffle 800 are provided to reduce the lowering of pressure across the liner, allowing the addition of more cooling holes and thereby reducing cooling hole spaces while not increasing the required amount of cooling air. The CMC liners 300 and 700 are incorporated as desired to take the advantage of shapes and hole alignment which are made possible by using the conventional design of the CMC. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_JP2013127355A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>JP2013127355A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_JP2013127355A3</originalsourceid><addsrcrecordid>eNrjZLALjgwOcfVV8HdT8PQLcXUPcgzx9HNXcHJ0c_NxVXDzD1Jw9fNw9HN2dVFw9vf3AckBlTr7OisA2a5BPAysaYk5xam8UJqbQcnNNcTZQze1ID8-tbggMTk1L7Uk3ivAyMDQ2NDI3NjU1NGYKEUAfEIqEw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>SYSTEM OF INTEGRATING BAFFLE FOR ENHANCED COOLING OF CMC LINER</title><source>esp@cenet</source><creator>DERY BRYAN ROBERT ; BUSH SCOTT MATTHEW ; CORSMEIER DONALD MICHAEL</creator><creatorcontrib>DERY BRYAN ROBERT ; BUSH SCOTT MATTHEW ; CORSMEIER DONALD MICHAEL</creatorcontrib><description>PROBLEM TO BE SOLVED: To provide a system of integrating baffles for the enhanced cooling of CMC liners.SOLUTION: A system of integrating baffles for the enhanced cooling of CMC liners 300 and 700 is composed of a combustor assembly having a dome mount assembly 200, an outer liner 300 and an inner liner 700. Liners include those manufactured from and in a process for a CMC (Ceramic Matrix Composite). One or more liner baffles 500 and 800 such as an outer baffle 500 and an inner baffle 800 are provided to reduce the lowering of pressure across the liner, allowing the addition of more cooling holes and thereby reducing cooling hole spaces while not increasing the required amount of cooling air. The CMC liners 300 and 700 are incorporated as desired to take the advantage of shapes and hole alignment which are made possible by using the conventional design of the CMC.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION APPARATUS ; COMBUSTION ENGINES ; COMBUSTION PROCESSES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2013</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=20130627&DB=EPODOC&CC=JP&NR=2013127355A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20130627&DB=EPODOC&CC=JP&NR=2013127355A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DERY BRYAN ROBERT</creatorcontrib><creatorcontrib>BUSH SCOTT MATTHEW</creatorcontrib><creatorcontrib>CORSMEIER DONALD MICHAEL</creatorcontrib><title>SYSTEM OF INTEGRATING BAFFLE FOR ENHANCED COOLING OF CMC LINER</title><description>PROBLEM TO BE SOLVED: To provide a system of integrating baffles for the enhanced cooling of CMC liners.SOLUTION: A system of integrating baffles for the enhanced cooling of CMC liners 300 and 700 is composed of a combustor assembly having a dome mount assembly 200, an outer liner 300 and an inner liner 700. Liners include those manufactured from and in a process for a CMC (Ceramic Matrix Composite). One or more liner baffles 500 and 800 such as an outer baffle 500 and an inner baffle 800 are provided to reduce the lowering of pressure across the liner, allowing the addition of more cooling holes and thereby reducing cooling hole spaces while not increasing the required amount of cooling air. The CMC liners 300 and 700 are incorporated as desired to take the advantage of shapes and hole alignment which are made possible by using the conventional design of the CMC.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION PROCESSES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLALjgwOcfVV8HdT8PQLcXUPcgzx9HNXcHJ0c_NxVXDzD1Jw9fNw9HN2dVFw9vf3AckBlTr7OisA2a5BPAysaYk5xam8UJqbQcnNNcTZQze1ID8-tbggMTk1L7Uk3ivAyMDQ2NDI3NjU1NGYKEUAfEIqEw</recordid><startdate>20130627</startdate><enddate>20130627</enddate><creator>DERY BRYAN ROBERT</creator><creator>BUSH SCOTT MATTHEW</creator><creator>CORSMEIER DONALD MICHAEL</creator><scope>EVB</scope></search><sort><creationdate>20130627</creationdate><title>SYSTEM OF INTEGRATING BAFFLE FOR ENHANCED COOLING OF CMC LINER</title><author>DERY BRYAN ROBERT ; BUSH SCOTT MATTHEW ; CORSMEIER DONALD MICHAEL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2013127355A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2013</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION PROCESSES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>DERY BRYAN ROBERT</creatorcontrib><creatorcontrib>BUSH SCOTT MATTHEW</creatorcontrib><creatorcontrib>CORSMEIER DONALD MICHAEL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DERY BRYAN ROBERT</au><au>BUSH SCOTT MATTHEW</au><au>CORSMEIER DONALD MICHAEL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEM OF INTEGRATING BAFFLE FOR ENHANCED COOLING OF CMC LINER</title><date>2013-06-27</date><risdate>2013</risdate><abstract>PROBLEM TO BE SOLVED: To provide a system of integrating baffles for the enhanced cooling of CMC liners.SOLUTION: A system of integrating baffles for the enhanced cooling of CMC liners 300 and 700 is composed of a combustor assembly having a dome mount assembly 200, an outer liner 300 and an inner liner 700. Liners include those manufactured from and in a process for a CMC (Ceramic Matrix Composite). One or more liner baffles 500 and 800 such as an outer baffle 500 and an inner baffle 800 are provided to reduce the lowering of pressure across the liner, allowing the addition of more cooling holes and thereby reducing cooling hole spaces while not increasing the required amount of cooling air. The CMC liners 300 and 700 are incorporated as desired to take the advantage of shapes and hole alignment which are made possible by using the conventional design of the CMC.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_JP2013127355A |
source | esp@cenet |
subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | SYSTEM OF INTEGRATING BAFFLE FOR ENHANCED COOLING OF CMC LINER |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-18T18%3A03%3A45IST&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=DERY%20BRYAN%20ROBERT&rft.date=2013-06-27&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EJP2013127355A%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 |