CORNER FLOW REDUCTION SEALS

A sealing arrangement for sealing between a first stage nozzle and a plurality of aft frames (100) includes a first inner seal (200) and a second inner seal (200) which are circumferentially oriented and circumferentially aligned. Each of the inner seals (200) includes a wing (208) extending radiall...

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Hauptverfasser: DICINTIO, Richard Martin, MONAGHAN, Elizabeth Angelyn, BARTON, Jesse Ellis
Format: Patent
Sprache:eng ; fre ; ger
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creator DICINTIO, Richard Martin
MONAGHAN, Elizabeth Angelyn
BARTON, Jesse Ellis
description A sealing arrangement for sealing between a first stage nozzle and a plurality of aft frames (100) includes a first inner seal (200) and a second inner seal (200) which are circumferentially oriented and circumferentially aligned. Each of the inner seals (200) includes a wing (208) extending radially inward at an oblique angle. A side seal (400) is radially disposed between the first inner seal (200) and the second inner seal (200). The side seal (400) includes a first wing (408) extending radially outward at an oblique angle and a second wing (408) extending radially outward at an oblique angle, the first wing (408) of the side seal (400) sealingly interfaces with the wing (208) of the first inner seal (200) and the second wing (408) of the side seal (400) sealingly interfaces with the wing (208) of the second inner seal (200).
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Each of the inner seals (200) includes a wing (208) extending radially inward at an oblique angle. A side seal (400) is radially disposed between the first inner seal (200) and the second inner seal (200). The side seal (400) includes a first wing (408) extending radially outward at an oblique angle and a second wing (408) extending radially outward at an oblique angle, the first wing (408) of the side seal (400) sealingly interfaces with the wing (208) of the first inner seal (200) and the second wing (408) of the side seal (400) sealingly interfaces with the wing (208) of the second inner seal (200).</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>2018</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=20180307&amp;DB=EPODOC&amp;CC=EP&amp;NR=3290641A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20180307&amp;DB=EPODOC&amp;CC=EP&amp;NR=3290641A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DICINTIO, Richard Martin</creatorcontrib><creatorcontrib>MONAGHAN, Elizabeth Angelyn</creatorcontrib><creatorcontrib>BARTON, Jesse Ellis</creatorcontrib><title>CORNER FLOW REDUCTION SEALS</title><description>A sealing arrangement for sealing between a first stage nozzle and a plurality of aft frames (100) includes a first inner seal (200) and a second inner seal (200) which are circumferentially oriented and circumferentially aligned. 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language eng ; fre ; ger
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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 CORNER FLOW REDUCTION SEALS
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