COOLING ASSEMBLY FOR BUCKET OF TURBINE SYSTEM AND COOLING METHOD
PROBLEM TO BE SOLVED: To provide a cooling assembly for a bucket of a turbine system and a cooling method.SOLUTION: A cooling assembly for a bucket of a turbine system includes a shroud assembly operably coupled to an outer casing of a turbine section. The cooling assembly also includes an airfoil h...
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creator | WASSYNGER STEPHEN PAUL |
description | PROBLEM TO BE SOLVED: To provide a cooling assembly for a bucket of a turbine system and a cooling method.SOLUTION: A cooling assembly for a bucket of a turbine system includes a shroud assembly operably coupled to an outer casing of a turbine section. The cooling assembly also includes an airfoil having at least one cavity, wherein the at least one cavity is configured to receive a cooling flow from a cooling source through at least one channel disposed within the shroud assembly. |
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The cooling assembly also includes an airfoil having at least one cavity, wherein the at least one cavity is configured to receive a cooling flow from a cooling source through at least one channel disposed within the shroud assembly.</description><language>eng</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>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=20131212&DB=EPODOC&CC=JP&NR=2013249835A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20131212&DB=EPODOC&CC=JP&NR=2013249835A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WASSYNGER STEPHEN PAUL</creatorcontrib><title>COOLING ASSEMBLY FOR BUCKET OF TURBINE SYSTEM AND COOLING METHOD</title><description>PROBLEM TO BE SOLVED: To provide a cooling assembly for a bucket of a turbine system and a cooling method.SOLUTION: A cooling assembly for a bucket of a turbine system includes a shroud assembly operably coupled to an outer casing of a turbine section. 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The cooling assembly also includes an airfoil having at least one cavity, wherein the at least one cavity is configured to receive a cooling flow from a cooling source through at least one channel disposed within the shroud assembly.</abstract><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 | COOLING ASSEMBLY FOR BUCKET OF TURBINE SYSTEM AND COOLING METHOD |
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