Lightweight cast inner diameter vane shroud for variable stator vanes

An inner diameter vane shroud (14) for use in a gas turbine engine is comprised of lightweight cast forward and aft shroud components (20; 22). The forward and aft shroud components (20; 22) are made with an investment casting technique that creates a hollow cavity (30; 32) that runs in a circumfere...

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Hauptverfasser: GIAIMO, JOHN A, TIRONE III, JOHN P
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creator GIAIMO, JOHN A
TIRONE III, JOHN P
description An inner diameter vane shroud (14) for use in a gas turbine engine is comprised of lightweight cast forward and aft shroud components (20; 22). The forward and aft shroud components (20; 22) are made with an investment casting technique that creates a hollow cavity (30; 32) that runs in a circumferential direction through each component. The forward and aft shroud components (20; 22) are matable to form sockets (24A) that receive inner diameter ends of variable stator vanes (28A).
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The forward and aft shroud components (20; 22) are matable to form sockets (24A) that receive inner diameter ends of variable stator vanes (28A).</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>2016</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=20160831&amp;DB=EPODOC&amp;CC=EP&amp;NR=1757776B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20160831&amp;DB=EPODOC&amp;CC=EP&amp;NR=1757776B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GIAIMO, JOHN A</creatorcontrib><creatorcontrib>TIRONE III, JOHN P</creatorcontrib><title>Lightweight cast inner diameter vane shroud for variable stator vanes</title><description>An inner diameter vane shroud (14) for use in a gas turbine engine is comprised of lightweight cast forward and aft shroud components (20; 22). 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The forward and aft shroud components (20; 22) are made with an investment casting technique that creates a hollow cavity (30; 32) that runs in a circumferential direction through each component. The forward and aft shroud components (20; 22) are matable to form sockets (24A) that receive inner diameter ends of variable stator vanes (28A).</abstract><oa>free_for_read</oa></addata></record>
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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 Lightweight cast inner diameter vane shroud for variable stator vanes
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