ROTATING CARBON PISTON RING SEAL

A gas turbine engine assembly includes a compressor (52) including a plurality of rotors (64), where at least one of the plurality of rotors (64) includes a radial inner sealing surface (68). A rotating shaft (50) drives rotation of the plurality of rotors (64), where the rotating shaft (50) include...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: WEBB, Scot A
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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 WEBB, Scot A
description A gas turbine engine assembly includes a compressor (52) including a plurality of rotors (64), where at least one of the plurality of rotors (64) includes a radial inner sealing surface (68). A rotating shaft (50) drives rotation of the plurality of rotors (64), where the rotating shaft (50) includes an annular groove (72) proximate the radial inner sealing surface (68). A seal (74) is disposed within the annular groove (72), and the seal (74) comprises at least two annular sections (88A-F) forming a complete circumference. Each of the at least two annular sections (88A-F) are separate parts and include a radially-facing sealing surface (84) engaged to the radial inner sealing surface (68) of the rotor (64) and an annular slot (82) disposed radially inward of the radially-facing sealing surface (84). A retainer (80) is disposed within the annular slot (82) limiting radial expansion of the at least two annular sections (88A-F).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3719265B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3719265B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3719265B13</originalsourceid><addsrcrecordid>eNrjZFAI8g9xDPH0c1dwdgxy8vdTCPAMDgFSQSChYFdHHx4G1rTEnOJUXijNzaDg5hri7KGbWpAfn1pckJicmpdaEu8aYGxuaGlkZupkaEyEEgCzqyGC</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>ROTATING CARBON PISTON RING SEAL</title><source>esp@cenet</source><creator>WEBB, Scot A</creator><creatorcontrib>WEBB, Scot A</creatorcontrib><description>A gas turbine engine assembly includes a compressor (52) including a plurality of rotors (64), where at least one of the plurality of rotors (64) includes a radial inner sealing surface (68). A rotating shaft (50) drives rotation of the plurality of rotors (64), where the rotating shaft (50) includes an annular groove (72) proximate the radial inner sealing surface (68). A seal (74) is disposed within the annular groove (72), and the seal (74) comprises at least two annular sections (88A-F) forming a complete circumference. Each of the at least two annular sections (88A-F) are separate parts and include a radially-facing sealing surface (84) engaged to the radial inner sealing surface (68) of the rotor (64) and an annular slot (82) disposed radially inward of the radially-facing sealing surface (84). A retainer (80) is disposed within the annular slot (82) limiting radial expansion of the at least two annular sections (88A-F).</description><language>eng ; fre ; ger</language><subject>BLASTING ; CYLINDERS ; ENGINE PLANTS IN GENERAL ; ENGINEERING ELEMENTS AND UNITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; 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>2022</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=20220601&amp;DB=EPODOC&amp;CC=EP&amp;NR=3719265B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20220601&amp;DB=EPODOC&amp;CC=EP&amp;NR=3719265B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WEBB, Scot A</creatorcontrib><title>ROTATING CARBON PISTON RING SEAL</title><description>A gas turbine engine assembly includes a compressor (52) including a plurality of rotors (64), where at least one of the plurality of rotors (64) includes a radial inner sealing surface (68). A rotating shaft (50) drives rotation of the plurality of rotors (64), where the rotating shaft (50) includes an annular groove (72) proximate the radial inner sealing surface (68). A seal (74) is disposed within the annular groove (72), and the seal (74) comprises at least two annular sections (88A-F) forming a complete circumference. Each of the at least two annular sections (88A-F) are separate parts and include a radially-facing sealing surface (84) engaged to the radial inner sealing surface (68) of the rotor (64) and an annular slot (82) disposed radially inward of the radially-facing sealing surface (84). A retainer (80) is disposed within the annular slot (82) limiting radial expansion of the at least two annular sections (88A-F).</description><subject>BLASTING</subject><subject>CYLINDERS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</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>PISTONS</subject><subject>SEALINGS</subject><subject>STEAM ENGINES</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAI8g9xDPH0c1dwdgxy8vdTCPAMDgFSQSChYFdHHx4G1rTEnOJUXijNzaDg5hri7KGbWpAfn1pckJicmpdaEu8aYGxuaGlkZupkaEyEEgCzqyGC</recordid><startdate>20220601</startdate><enddate>20220601</enddate><creator>WEBB, Scot A</creator><scope>EVB</scope></search><sort><creationdate>20220601</creationdate><title>ROTATING CARBON PISTON RING SEAL</title><author>WEBB, Scot A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3719265B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</creationdate><topic>BLASTING</topic><topic>CYLINDERS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</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>PISTONS</topic><topic>SEALINGS</topic><topic>STEAM ENGINES</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>WEBB, Scot A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WEBB, Scot A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ROTATING CARBON PISTON RING SEAL</title><date>2022-06-01</date><risdate>2022</risdate><abstract>A gas turbine engine assembly includes a compressor (52) including a plurality of rotors (64), where at least one of the plurality of rotors (64) includes a radial inner sealing surface (68). A rotating shaft (50) drives rotation of the plurality of rotors (64), where the rotating shaft (50) includes an annular groove (72) proximate the radial inner sealing surface (68). A seal (74) is disposed within the annular groove (72), and the seal (74) comprises at least two annular sections (88A-F) forming a complete circumference. Each of the at least two annular sections (88A-F) are separate parts and include a radially-facing sealing surface (84) engaged to the radial inner sealing surface (68) of the rotor (64) and an annular slot (82) disposed radially inward of the radially-facing sealing surface (84). A retainer (80) is disposed within the annular slot (82) limiting radial expansion of the at least two annular sections (88A-F).</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3719265B1
source esp@cenet
subjects BLASTING
CYLINDERS
ENGINE PLANTS IN GENERAL
ENGINEERING ELEMENTS AND UNITS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
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 ROTATING CARBON PISTON RING SEAL
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-22T16%3A59%3A35IST&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=WEBB,%20Scot%20A&rft.date=2022-06-01&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3719265B1%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