Blade for a low pressure section of a steam turbine engine

Blade for a low pressure section of a steam turbine engine

A steam turbine rotating blade (20) for a low pressure section of a steam turbine engine (10) is disclosed. The steam turbine rotating blade (20) includes an airfoil portion (42). A root section (44) is attached to one end of the airfoil portion (42). A dovetail section (40) projects from the root s...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: RIAZ, MUHAMMAD SAQIB, STATHOPOULOS, DIMITRIOS
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator RIAZ, MUHAMMAD SAQIB
STATHOPOULOS, DIMITRIOS
description A steam turbine rotating blade (20) for a low pressure section of a steam turbine engine (10) is disclosed. The steam turbine rotating blade (20) includes an airfoil portion (42). A root section (44) is attached to one end of the airfoil portion (42). A dovetail section (40) projects from the root section (44), wherein the dovetail section (40) includes a skewed axial entry dovetail (40). A tip section (46) is attached to the airfoil portion (46) at an end opposite from the root section (44). A cover (48) is integrally formed as part of the tip section (46). A part span shroud (50) is attached at an intermediate section of the airfoil portion (42) between the ends thereof. The blade (20) includes an exit annulus area of about 47.7 ft 2 (4.43m 2 ) or greater.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2177714A2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2177714A2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2177714A23</originalsourceid><addsrcrecordid>eNrjZLByyklMSVVIyy9SSFTIyS9XKChKLS4uLUpVKE5NLsnMz1PITwPKFJekJuYqlJQWJWXmpSqk5qUDKR4G1rTEnOJUXijNzaDg5hri7KGbWpAfn1pckJicmpdaEu8aYGRobm5uaOJoZEyEEgDIWC4E</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Blade for a low pressure section of a steam turbine engine</title><source>esp@cenet</source><creator>RIAZ, MUHAMMAD SAQIB ; STATHOPOULOS, DIMITRIOS</creator><creatorcontrib>RIAZ, MUHAMMAD SAQIB ; STATHOPOULOS, DIMITRIOS</creatorcontrib><description>A steam turbine rotating blade (20) for a low pressure section of a steam turbine engine (10) is disclosed. The steam turbine rotating blade (20) includes an airfoil portion (42). A root section (44) is attached to one end of the airfoil portion (42). A dovetail section (40) projects from the root section (44), wherein the dovetail section (40) includes a skewed axial entry dovetail (40). A tip section (46) is attached to the airfoil portion (46) at an end opposite from the root section (44). A cover (48) is integrally formed as part of the tip section (46). A part span shroud (50) is attached at an intermediate section of the airfoil portion (42) between the ends thereof. The blade (20) includes an exit annulus area of about 47.7 ft 2 (4.43m 2 ) or greater.</description><language>eng ; fre ; ger</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2010</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&amp;date=20100421&amp;DB=EPODOC&amp;CC=EP&amp;NR=2177714A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20100421&amp;DB=EPODOC&amp;CC=EP&amp;NR=2177714A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>RIAZ, MUHAMMAD SAQIB</creatorcontrib><creatorcontrib>STATHOPOULOS, DIMITRIOS</creatorcontrib><title>Blade for a low pressure section of a steam turbine engine</title><description>A steam turbine rotating blade (20) for a low pressure section of a steam turbine engine (10) is disclosed. The steam turbine rotating blade (20) includes an airfoil portion (42). A root section (44) is attached to one end of the airfoil portion (42). A dovetail section (40) projects from the root section (44), wherein the dovetail section (40) includes a skewed axial entry dovetail (40). A tip section (46) is attached to the airfoil portion (46) at an end opposite from the root section (44). A cover (48) is integrally formed as part of the tip section (46). A part span shroud (50) is attached at an intermediate section of the airfoil portion (42) between the ends thereof. The blade (20) includes an exit annulus area of about 47.7 ft 2 (4.43m 2 ) or greater.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</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>2010</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLByyklMSVVIyy9SSFTIyS9XKChKLS4uLUpVKE5NLsnMz1PITwPKFJekJuYqlJQWJWXmpSqk5qUDKR4G1rTEnOJUXijNzaDg5hri7KGbWpAfn1pckJicmpdaEu8aYGRobm5uaOJoZEyEEgDIWC4E</recordid><startdate>20100421</startdate><enddate>20100421</enddate><creator>RIAZ, MUHAMMAD SAQIB</creator><creator>STATHOPOULOS, DIMITRIOS</creator><scope>EVB</scope></search><sort><creationdate>20100421</creationdate><title>Blade for a low pressure section of a steam turbine engine</title><author>RIAZ, MUHAMMAD SAQIB ; STATHOPOULOS, DIMITRIOS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2177714A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2010</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</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>RIAZ, MUHAMMAD SAQIB</creatorcontrib><creatorcontrib>STATHOPOULOS, DIMITRIOS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>RIAZ, MUHAMMAD SAQIB</au><au>STATHOPOULOS, DIMITRIOS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Blade for a low pressure section of a steam turbine engine</title><date>2010-04-21</date><risdate>2010</risdate><abstract>A steam turbine rotating blade (20) for a low pressure section of a steam turbine engine (10) is disclosed. The steam turbine rotating blade (20) includes an airfoil portion (42). A root section (44) is attached to one end of the airfoil portion (42). A dovetail section (40) projects from the root section (44), wherein the dovetail section (40) includes a skewed axial entry dovetail (40). A tip section (46) is attached to the airfoil portion (46) at an end opposite from the root section (44). A cover (48) is integrally formed as part of the tip section (46). A part span shroud (50) is attached at an intermediate section of the airfoil portion (42) between the ends thereof. The blade (20) includes an exit annulus area of about 47.7 ft 2 (4.43m 2 ) or greater.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP2177714A2
source esp@cenet
subjects BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
title Blade for a low pressure section of a steam turbine engine
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-06T05%3A51%3A08IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=RIAZ,%20MUHAMMAD%20SAQIB&rft.date=2010-04-21&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2177714A2%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true