Steam cooling a turbine rotor
An axial bore tube assembly (48) for a turbine is provided to supply cooling steam to hot gas components of the turbine wheels and return the spent cooling steam. A pair of inner and outer tubes (52, 50) define a steam supply passage (54) concentric about an inner return passage (56). The forward en...
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creator | WILSON, IAN DAVID DESTEFANO, THOMAS DANIEL |
description | An axial bore tube assembly (48) for a turbine is provided to supply cooling steam to hot gas components of the turbine wheels and return the spent cooling steam. A pair of inner and outer tubes (52, 50) define a steam supply passage (54) concentric about an inner return passage (56). The forward ends of the tubes communicate with an end cap assembly (80) having sets of peripheral holes (88) communicating with first and second sets of radial tubes (92) whereby cooling steam from the concentric passage (54) is supplied through the end cap holes (88) to radial tubes (93) for cooling the buckets and return steam from the buckets is provided through the second set of radial tubes (95) through a second set of openings (90) of the end cap (80) into the coaxial return passage (56). A radial-to-axial flow transitioning device, including anti-swirling vanes (112), is provided in the end cap (81). A strut ring adjacent the aft end of the bore tube assembly permits axial and radial thermal expansion of the inner tube (52) relative to the outer tube (50). |
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A pair of inner and outer tubes (52, 50) define a steam supply passage (54) concentric about an inner return passage (56). The forward ends of the tubes communicate with an end cap assembly (80) having sets of peripheral holes (88) communicating with first and second sets of radial tubes (92) whereby cooling steam from the concentric passage (54) is supplied through the end cap holes (88) to radial tubes (93) for cooling the buckets and return steam from the buckets is provided through the second set of radial tubes (95) through a second set of openings (90) of the end cap (80) into the coaxial return passage (56). A radial-to-axial flow transitioning device, including anti-swirling vanes (112), is provided in the end cap (81). A strut ring adjacent the aft end of the bore tube assembly permits axial and radial thermal expansion of the inner tube (52) relative to the outer tube (50).</description><edition>7</edition><language>eng ; fre ; ger</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=20020619&DB=EPODOC&CC=EP&NR=1010858A3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20020619&DB=EPODOC&CC=EP&NR=1010858A3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WILSON, IAN DAVID</creatorcontrib><creatorcontrib>DESTEFANO, THOMAS DANIEL</creatorcontrib><title>Steam cooling a turbine rotor</title><description>An axial bore tube assembly (48) for a turbine is provided to supply cooling steam to hot gas components of the turbine wheels and return the spent cooling steam. A pair of inner and outer tubes (52, 50) define a steam supply passage (54) concentric about an inner return passage (56). The forward ends of the tubes communicate with an end cap assembly (80) having sets of peripheral holes (88) communicating with first and second sets of radial tubes (92) whereby cooling steam from the concentric passage (54) is supplied through the end cap holes (88) to radial tubes (93) for cooling the buckets and return steam from the buckets is provided through the second set of radial tubes (95) through a second set of openings (90) of the end cap (80) into the coaxial return passage (56). A radial-to-axial flow transitioning device, including anti-swirling vanes (112), is provided in the end cap (81). A strut ring adjacent the aft end of the bore tube assembly permits axial and radial thermal expansion of the inner tube (52) relative to the outer tube (50).</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>eNrjZJANLklNzFVIzs_PycxLV0hUKCktSsrMS1Uoyi_JL-JhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAYYGhgYWphaOxsZEKAEAdmUjkw</recordid><startdate>20020619</startdate><enddate>20020619</enddate><creator>WILSON, IAN DAVID</creator><creator>DESTEFANO, THOMAS DANIEL</creator><scope>EVB</scope></search><sort><creationdate>20020619</creationdate><title>Steam cooling a turbine rotor</title><author>WILSON, IAN DAVID ; DESTEFANO, THOMAS DANIEL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP1010858A33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</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>WILSON, IAN DAVID</creatorcontrib><creatorcontrib>DESTEFANO, THOMAS DANIEL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WILSON, IAN DAVID</au><au>DESTEFANO, THOMAS DANIEL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Steam cooling a turbine rotor</title><date>2002-06-19</date><risdate>2002</risdate><abstract>An axial bore tube assembly (48) for a turbine is provided to supply cooling steam to hot gas components of the turbine wheels and return the spent cooling steam. A pair of inner and outer tubes (52, 50) define a steam supply passage (54) concentric about an inner return passage (56). The forward ends of the tubes communicate with an end cap assembly (80) having sets of peripheral holes (88) communicating with first and second sets of radial tubes (92) whereby cooling steam from the concentric passage (54) is supplied through the end cap holes (88) to radial tubes (93) for cooling the buckets and return steam from the buckets is provided through the second set of radial tubes (95) through a second set of openings (90) of the end cap (80) into the coaxial return passage (56). A radial-to-axial flow transitioning device, including anti-swirling vanes (112), is provided in the end cap (81). A strut ring adjacent the aft end of the bore tube assembly permits axial and radial thermal expansion of the inner tube (52) relative to the outer tube (50).</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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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 | Steam cooling a turbine rotor |
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