METHOD OF SHUTTING-DOWN A TURBINE ENGINE AND SYSTEM FOR CARRYING OUT SAID METHOD
Upon shutdown of a liquid fuel turbine engine, the liquide fuel supply is turned off and compressed air is passed through the fuel lines and fuel injectors to purge all remaining liquid fuel into the combustion chamber to be combusted therein. A l'arrêt d'un moteur à turbine à carburant li...
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creator | WILLIS, JEFFREY, W PONT, GUILLERMO EDELMAN, EDWARD, C LINZNER, GUNTHER |
description | Upon shutdown of a liquid fuel turbine engine, the liquide fuel supply is turned off and compressed air is passed through the fuel lines and fuel injectors to purge all remaining liquid fuel into the combustion chamber to be combusted therein.
A l'arrêt d'un moteur à turbine à carburant liquide, l'alimentation en carburant liquide est coupée, et de l'air comprimé est envoyé à travers les conduites de carburant et les injecteurs de carburant, de manière à purger tout le carburant liquide restant dans la chambre de combustion pour être brûlé dans celle-ci. |
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A l'arrêt d'un moteur à turbine à carburant liquide, l'alimentation en carburant liquide est coupée, et de l'air comprimé est envoyé à travers les conduites de carburant et les injecteurs de carburant, de manière à purger tout le carburant liquide restant dans la chambre de combustion pour être brûlé dans celle-ci.</description><edition>7</edition><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>2002</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=20020411&DB=EPODOC&CC=WO&NR=0229225A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20020411&DB=EPODOC&CC=WO&NR=0229225A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WILLIS, JEFFREY, W</creatorcontrib><creatorcontrib>PONT, GUILLERMO</creatorcontrib><creatorcontrib>EDELMAN, EDWARD, C</creatorcontrib><creatorcontrib>LINZNER, GUNTHER</creatorcontrib><title>METHOD OF SHUTTING-DOWN A TURBINE ENGINE AND SYSTEM FOR CARRYING OUT SAID METHOD</title><description>Upon shutdown of a liquid fuel turbine engine, the liquide fuel supply is turned off and compressed air is passed through the fuel lines and fuel injectors to purge all remaining liquid fuel into the combustion chamber to be combusted therein.
A l'arrêt d'un moteur à turbine à carburant liquide, l'alimentation en carburant liquide est coupée, et de l'air comprimé est envoyé à travers les conduites de carburant et les injecteurs de carburant, de manière à purger tout le carburant liquide restant dans la chambre de combustion pour être brûlé dans celle-ci.</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>2002</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAjwdQ3x8HdR8HdTCPYIDQnx9HPXdfEP91NwVAgJDXLy9HNVcPVzB1GOfi4KwZHBIa6-Cm7-QQrOjkFBkUDVCv6hIQrBjp4uChCTeBhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJfLi_gZGRpZGRqaOhMRFKAAFmLoY</recordid><startdate>20020411</startdate><enddate>20020411</enddate><creator>WILLIS, JEFFREY, W</creator><creator>PONT, GUILLERMO</creator><creator>EDELMAN, EDWARD, C</creator><creator>LINZNER, GUNTHER</creator><scope>EVB</scope></search><sort><creationdate>20020411</creationdate><title>METHOD OF SHUTTING-DOWN A TURBINE ENGINE AND SYSTEM FOR CARRYING OUT SAID METHOD</title><author>WILLIS, JEFFREY, W ; PONT, GUILLERMO ; EDELMAN, EDWARD, C ; LINZNER, GUNTHER</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO0229225A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2002</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>WILLIS, JEFFREY, W</creatorcontrib><creatorcontrib>PONT, GUILLERMO</creatorcontrib><creatorcontrib>EDELMAN, EDWARD, C</creatorcontrib><creatorcontrib>LINZNER, GUNTHER</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WILLIS, JEFFREY, W</au><au>PONT, GUILLERMO</au><au>EDELMAN, EDWARD, C</au><au>LINZNER, GUNTHER</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD OF SHUTTING-DOWN A TURBINE ENGINE AND SYSTEM FOR CARRYING OUT SAID METHOD</title><date>2002-04-11</date><risdate>2002</risdate><abstract>Upon shutdown of a liquid fuel turbine engine, the liquide fuel supply is turned off and compressed air is passed through the fuel lines and fuel injectors to purge all remaining liquid fuel into the combustion chamber to be combusted therein.
A l'arrêt d'un moteur à turbine à carburant liquide, l'alimentation en carburant liquide est coupée, et de l'air comprimé est envoyé à travers les conduites de carburant et les injecteurs de carburant, de manière à purger tout le carburant liquide restant dans la chambre de combustion pour être brûlé dans celle-ci.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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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 | METHOD OF SHUTTING-DOWN A TURBINE ENGINE AND SYSTEM FOR CARRYING OUT SAID METHOD |
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