A leaf seal for gas turbine stator shrouds and a nozzle band

A leaf seal assembly (80) is secured to the trailing edge of a shroud segment (68) for sealing between the shroud segment and the leading edge side wall of a nozzle outer band (90). The leaf seal includes a circumferentially elongated seal plate biased by a pair of spring clips (86) disposed in a gr...

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Hauptverfasser: BURDGICK, STEVEN SEBASTIAN, SEXTON, BRENDAN FRANCIS
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Sprache:eng ; fre ; ger
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creator BURDGICK, STEVEN SEBASTIAN
SEXTON, BRENDAN FRANCIS
description A leaf seal assembly (80) is secured to the trailing edge of a shroud segment (68) for sealing between the shroud segment and the leading edge side wall of a nozzle outer band (90). The leaf seal includes a circumferentially elongated seal plate biased by a pair of spring clips (86) disposed in a groove (82) along the trailing edge of the shroud segment to maintain the seal plate in engagement with the flange (88) on the leading edge side wall of the nozzle outer band. The leaf seal plate and spring clips receive pins (89) tack-welded to the shroud segment to secure the leaf seal assembly in place.
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The leaf seal includes a circumferentially elongated seal plate biased by a pair of spring clips (86) disposed in a groove (82) along the trailing edge of the shroud segment to maintain the seal plate in engagement with the flange (88) on the leading edge side wall of the nozzle outer band. The leaf seal plate and spring clips receive pins (89) tack-welded to the shroud segment to secure the leaf seal assembly in place.</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 ; CYLINDERS ; ENGINE PLANTS IN GENERAL ; ENGINEERING ELEMENTS AND UNITS ; GAS-TURBINE PLANTS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; 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 ; PISTONS ; SEALINGS ; STEAM ENGINES ; THERMAL INSULATION IN GENERAL ; WEAPONS</subject><creationdate>2003</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=20030924&amp;DB=EPODOC&amp;CC=EP&amp;NR=1156188A3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20030924&amp;DB=EPODOC&amp;CC=EP&amp;NR=1156188A3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BURDGICK, STEVEN SEBASTIAN</creatorcontrib><creatorcontrib>SEXTON, BRENDAN FRANCIS</creatorcontrib><title>A leaf seal for gas turbine stator shrouds and a nozzle band</title><description>A leaf seal assembly (80) is secured to the trailing edge of a shroud segment (68) for sealing between the shroud segment and the leading edge side wall of a nozzle outer band (90). 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language eng ; fre ; ger
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source esp@cenet
subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
CYLINDERS
ENGINE PLANTS IN GENERAL
ENGINEERING ELEMENTS AND UNITS
GAS-TURBINE PLANTS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
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
PISTONS
SEALINGS
STEAM ENGINES
THERMAL INSULATION IN GENERAL
WEAPONS
title A leaf seal for gas turbine stator shrouds and a nozzle band
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