PAROI ANNULAIRE DE CHAMBRE DE COMBUSTION EN AVAL D'UN COMPRESSEUR CENTRIFUGE
The internal wall (30) or external wall has a set of cooling holes (44), each being inclined at an inclination angle with respect to a normal to the wall. The holes are distributed according to a set of axially spaced lines from/to each other to allow air to circulate from a cold side of the wall to...
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creator | LEGLAYE, FRANCOIS COMMARET, PATRICE, ANDRE CABRE, JEAN-FRANCOIS |
description | The internal wall (30) or external wall has a set of cooling holes (44), each being inclined at an inclination angle with respect to a normal to the wall. The holes are distributed according to a set of axially spaced lines from/to each other to allow air to circulate from a cold side of the wall to penetrate on a hot side, in order to form a film of cooling air along the wall. Geometric drilling axes of each of the holes are directed according to a direction of air flow (F2) circulating around the wall in order to maintain supply of air axially across the holes along the wall. An independent claim is also included for a combustion chamber. |
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The holes are distributed according to a set of axially spaced lines from/to each other to allow air to circulate from a cold side of the wall to penetrate on a hot side, in order to form a film of cooling air along the wall. Geometric drilling axes of each of the holes are directed according to a direction of air flow (F2) circulating around the wall in order to maintain supply of air axially across the holes along the wall. An independent claim is also included for a combustion chamber.</description><language>fre</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>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=20180817&DB=EPODOC&CC=FR&NR=2999277B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180817&DB=EPODOC&CC=FR&NR=2999277B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LEGLAYE, FRANCOIS</creatorcontrib><creatorcontrib>COMMARET, PATRICE, ANDRE</creatorcontrib><creatorcontrib>CABRE, JEAN-FRANCOIS</creatorcontrib><title>PAROI ANNULAIRE DE CHAMBRE DE COMBUSTION EN AVAL D'UN COMPRESSEUR CENTRIFUGE</title><description>The internal wall (30) or external wall has a set of cooling holes (44), each being inclined at an inclination angle with respect to a normal to the wall. 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An independent claim is also included for a combustion chamber.</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPAJcAzy91Rw9PML9XH0DHJVcHFVcPZw9HWCMv19nUKDQzz9_RRc_RQcwxx9FFzUQ_1A4gFBrsHBrqFBCs6ufiFBnm6h7q48DKxpiTnFqbxQmptBwc01xNlDN7UgPz61uCAxOTUvtSTeLcjI0tLSyNzcydCYCCUANOQtZw</recordid><startdate>20180817</startdate><enddate>20180817</enddate><creator>LEGLAYE, FRANCOIS</creator><creator>COMMARET, PATRICE, ANDRE</creator><creator>CABRE, JEAN-FRANCOIS</creator><scope>EVB</scope></search><sort><creationdate>20180817</creationdate><title>PAROI ANNULAIRE DE CHAMBRE DE COMBUSTION EN AVAL D'UN COMPRESSEUR CENTRIFUGE</title><author>LEGLAYE, FRANCOIS ; COMMARET, PATRICE, ANDRE ; CABRE, JEAN-FRANCOIS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR2999277B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</language><creationdate>2018</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>LEGLAYE, FRANCOIS</creatorcontrib><creatorcontrib>COMMARET, PATRICE, ANDRE</creatorcontrib><creatorcontrib>CABRE, JEAN-FRANCOIS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LEGLAYE, FRANCOIS</au><au>COMMARET, PATRICE, ANDRE</au><au>CABRE, JEAN-FRANCOIS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PAROI ANNULAIRE DE CHAMBRE DE COMBUSTION EN AVAL D'UN COMPRESSEUR CENTRIFUGE</title><date>2018-08-17</date><risdate>2018</risdate><abstract>The internal wall (30) or external wall has a set of cooling holes (44), each being inclined at an inclination angle with respect to a normal to the wall. 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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 | PAROI ANNULAIRE DE CHAMBRE DE COMBUSTION EN AVAL D'UN COMPRESSEUR CENTRIFUGE |
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