PRE-SWIRL SECTION FOR A GAS TURBINE ENGINE

A gas turbine engine locates the rotating flange joint (25) in the pre-swirl section (20). The rotating flange joint (25) joins the compressor section (4) and the turbine section (6). The fluid flow typically used for the pre-swirl section (20) is used to also cool the rotating flange joint (25). Th...

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1. Verfasser:	THAM, Kok-Mun
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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creator	THAM, Kok-Mun
description	A gas turbine engine locates the rotating flange joint (25) in the pre-swirl section (20). The rotating flange joint (25) joins the compressor section (4) and the turbine section (6). The fluid flow typically used for the pre-swirl section (20) is used to also cool the rotating flange joint (25). The rotating flange joint (25) further assists in swirling the fluid flow in the pre-swirl cavity (27). Le moteur à turbine à gaz de la présente invention localise l'articulation à bride rotative (25) dans la section de pré-tourbillonnement (20). L'articulation à bride rotative (25) relie la section de compresseur (4) et la section de turbine (6). L'écoulement de fluide généralement utilisé pour la section de pré-tourbillonnement (20) est utilisé pour refroidir également l'articulation à bride rotative (25). L'articulation à bride rotative (25) aide en outre à faire tourbillonner l'écoulement de fluide dans la cavité de pré-tourbillonnement (27).
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The fluid flow typically used for the pre-swirl section (20) is used to also cool the rotating flange joint (25). The rotating flange joint (25) further assists in swirling the fluid flow in the pre-swirl cavity (27). Le moteur à turbine à gaz de la présente invention localise l'articulation à bride rotative (25) dans la section de pré-tourbillonnement (20). L'articulation à bride rotative (25) relie la section de compresseur (4) et la section de turbine (6). L'écoulement de fluide généralement utilisé pour la section de pré-tourbillonnement (20) est utilisé pour refroidir également l'articulation à bride rotative (25). L'articulation à bride rotative (25) aide en outre à faire tourbillonner l'écoulement de fluide dans la cavité de pré-tourbillonnement (27).</description><language>eng ; fre</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; 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=20180621&DB=EPODOC&CC=WO&NR=2018111276A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180621&DB=EPODOC&CC=WO&NR=2018111276A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>THAM, Kok-Mun</creatorcontrib><title>PRE-SWIRL SECTION FOR A GAS TURBINE ENGINE</title><description>A gas turbine engine locates the rotating flange joint (25) in the pre-swirl section (20). The rotating flange joint (25) joins the compressor section (4) and the turbine section (6). The fluid flow typically used for the pre-swirl section (20) is used to also cool the rotating flange joint (25). The rotating flange joint (25) further assists in swirling the fluid flow in the pre-swirl cavity (27). Le moteur à turbine à gaz de la présente invention localise l'articulation à bride rotative (25) dans la section de pré-tourbillonnement (20). L'articulation à bride rotative (25) relie la section de compresseur (4) et la section de turbine (6). L'écoulement de fluide généralement utilisé pour la section de pré-tourbillonnement (20) est utilisé pour refroidir également l'articulation à bride rotative (25). L'articulation à bride rotative (25) aide en outre à faire tourbillonner l'écoulement de fluide dans la cavité de pré-tourbillonnement (27).</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAKCHLVDQ73DPJRCHZ1DvH091Nw8w9ScFRwdwxWCAkNcvL0c1Vw9XMHUjwMrGmJOcWpvFCam0HZzTXE2UM3tSA_PrW4IDE5NS-1JD7c38jA0MLQ0NDI3MzR0Jg4VQDHKiVH</recordid><startdate>20180621</startdate><enddate>20180621</enddate><creator>THAM, Kok-Mun</creator><scope>EVB</scope></search><sort><creationdate>20180621</creationdate><title>PRE-SWIRL SECTION FOR A GAS TURBINE ENGINE</title><author>THAM, Kok-Mun</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2018111276A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2018</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>THAM, Kok-Mun</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>THAM, Kok-Mun</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PRE-SWIRL SECTION FOR A GAS TURBINE ENGINE</title><date>2018-06-21</date><risdate>2018</risdate><abstract>A gas turbine engine locates the rotating flange joint (25) in the pre-swirl section (20). The rotating flange joint (25) joins the compressor section (4) and the turbine section (6). The fluid flow typically used for the pre-swirl section (20) is used to also cool the rotating flange joint (25). The rotating flange joint (25) further assists in swirling the fluid flow in the pre-swirl cavity (27). Le moteur à turbine à gaz de la présente invention localise l'articulation à bride rotative (25) dans la section de pré-tourbillonnement (20). L'articulation à bride rotative (25) relie la section de compresseur (4) et la section de turbine (6). L'écoulement de fluide généralement utilisé pour la section de pré-tourbillonnement (20) est utilisé pour refroidir également l'articulation à bride rotative (25). L'articulation à bride rotative (25) aide en outre à faire tourbillonner l'écoulement de fluide dans la cavité de pré-tourbillonnement (27).</abstract><oa>free_for_read</oa></addata></record>
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language	eng ; fre
recordid	cdi_epo_espacenet_WO2018111276A1
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subjects	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
title	PRE-SWIRL SECTION FOR A GAS TURBINE ENGINE
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