MIXING SYSTEM

This application describes a mixing system 32 for a gas turbine combustor arrangement, the mixing system 32 comprising a lobed mixer 10 and a wall 40, 42 enclosing a fluid flow path 34, wherein the lobed mixer 10 is arranged in the wall 40, 42 between a first part of the wall 40 and a second part of...

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Hauptverfasser:	Wysocki, Stefan, Luebcke, Holger
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
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creator	Wysocki, Stefan Luebcke, Holger
description	This application describes a mixing system 32 for a gas turbine combustor arrangement, the mixing system 32 comprising a lobed mixer 10 and a wall 40, 42 enclosing a fluid flow path 34, wherein the lobed mixer 10 is arranged in the wall 40, 42 between a first part of the wall 40 and a second part of the wall 42, and wherein the first part of the wall 40 and the second part of the wall 42 are spaced apart in the direction of a lobed mixer axis 50. Details of the lobed mixer 10 and a method of mixing two flows in a mixing system are also described.
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Details of the lobed mixer 10 and a method of mixing two flows in a mixing system are also described.</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>2019</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=20190403&DB=EPODOC&CC=EP&NR=3091288B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190403&DB=EPODOC&CC=EP&NR=3091288B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Wysocki, Stefan</creatorcontrib><creatorcontrib>Luebcke, Holger</creatorcontrib><title>MIXING SYSTEM</title><description>This application describes a mixing system 32 for a gas turbine combustor arrangement, the mixing system 32 comprising a lobed mixer 10 and a wall 40, 42 enclosing a fluid flow path 34, wherein the lobed mixer 10 is arranged in the wall 40, 42 between a first part of the wall 40 and a second part of the wall 42, and wherein the first part of the wall 40 and the second part of the wall 42 are spaced apart in the direction of a lobed mixer axis 50. Details of the lobed mixer 10 and a method of mixing two flows in a mixing system are also described.</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZOD19Yzw9HNXCI4MDnH15WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxgaWhkYWFk6GxkQoAQCCJhxt</recordid><startdate>20190403</startdate><enddate>20190403</enddate><creator>Wysocki, Stefan</creator><creator>Luebcke, Holger</creator><scope>EVB</scope></search><sort><creationdate>20190403</creationdate><title>MIXING SYSTEM</title><author>Wysocki, Stefan ; Luebcke, Holger</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3091288B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</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>Wysocki, Stefan</creatorcontrib><creatorcontrib>Luebcke, Holger</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Wysocki, Stefan</au><au>Luebcke, Holger</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>MIXING SYSTEM</title><date>2019-04-03</date><risdate>2019</risdate><abstract>This application describes a mixing system 32 for a gas turbine combustor arrangement, the mixing system 32 comprising a lobed mixer 10 and a wall 40, 42 enclosing a fluid flow path 34, wherein the lobed mixer 10 is arranged in the wall 40, 42 between a first part of the wall 40 and a second part of the wall 42, and wherein the first part of the wall 40 and the second part of the wall 42 are spaced apart in the direction of a lobed mixer axis 50. Details of the lobed mixer 10 and a method of mixing two flows in a mixing system are also described.</abstract><oa>free_for_read</oa></addata></record>
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language	eng ; fre ; ger
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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	MIXING SYSTEM
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