AIR INJECTION SYSTEM FOR COOLING A ROTOR IN A GAS TURBINE ENGINE AND METHOD OF COOLING SUCH ROTOR

An air injection system for use in a gas turbine engine includes at least one outlet port through which air is extracted from the engine only during less than full load operation, at least one rotor cooling pipe, which is used to inject the air extracted from the outlet port(s) into a rotor chamber,...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: LEE, CHING-PANG, SIMKO, DUSTAN M, TERPOS, BRIAN H, THAM, KOK-MUN
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 LEE, CHING-PANG
SIMKO, DUSTAN M
TERPOS, BRIAN H
THAM, KOK-MUN
description An air injection system for use in a gas turbine engine includes at least one outlet port through which air is extracted from the engine only during less than full load operation, at least one rotor cooling pipe, which is used to inject the air extracted from the outlet port(s) into a rotor chamber, a piping system that provides fluid communication between the one outlet port(s) and the rotor cooling pipe(s), a blower system for extracting air from the engine through the outlet port(s) and for conveying the extracted air through the piping system and the rotor cooling pipe(s) into the rotor chamber, and a valve system. The valve system is closed during full load engine operation to prevent air from passing through the piping system, and open during less than full load engine operation to allow air to pass through the piping system.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2917490A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2917490A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2917490A13</originalsourceid><addsrcrecordid>eNqNi7sKwkAQANNYiPoP-wOCUUFSnpe9h5hdudsUVuGQsxINxP9Hg2JtNVPMTIukfABPB9TimSCeo2ADhgNo5qMnCwoCC4_RW62KIG3Ye0JAsiMU1dCgOK6Bze-KrXafcV5Mruk25MWXswIMinbL3D-6PPTpku_52eFpXZW7bbVS5eaP5AX_mTK8</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AIR INJECTION SYSTEM FOR COOLING A ROTOR IN A GAS TURBINE ENGINE AND METHOD OF COOLING SUCH ROTOR</title><source>esp@cenet</source><creator>LEE, CHING-PANG ; SIMKO, DUSTAN M ; TERPOS, BRIAN H ; THAM, KOK-MUN</creator><creatorcontrib>LEE, CHING-PANG ; SIMKO, DUSTAN M ; TERPOS, BRIAN H ; THAM, KOK-MUN</creatorcontrib><description>An air injection system for use in a gas turbine engine includes at least one outlet port through which air is extracted from the engine only during less than full load operation, at least one rotor cooling pipe, which is used to inject the air extracted from the outlet port(s) into a rotor chamber, a piping system that provides fluid communication between the one outlet port(s) and the rotor cooling pipe(s), a blower system for extracting air from the engine through the outlet port(s) and for conveying the extracted air through the piping system and the rotor cooling pipe(s) into the rotor chamber, and a valve system. The valve system is closed during full load engine operation to prevent air from passing through the piping system, and open during less than full load engine operation to allow air to pass through the piping system.</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>2015</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=20150916&amp;DB=EPODOC&amp;CC=EP&amp;NR=2917490A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20150916&amp;DB=EPODOC&amp;CC=EP&amp;NR=2917490A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LEE, CHING-PANG</creatorcontrib><creatorcontrib>SIMKO, DUSTAN M</creatorcontrib><creatorcontrib>TERPOS, BRIAN H</creatorcontrib><creatorcontrib>THAM, KOK-MUN</creatorcontrib><title>AIR INJECTION SYSTEM FOR COOLING A ROTOR IN A GAS TURBINE ENGINE AND METHOD OF COOLING SUCH ROTOR</title><description>An air injection system for use in a gas turbine engine includes at least one outlet port through which air is extracted from the engine only during less than full load operation, at least one rotor cooling pipe, which is used to inject the air extracted from the outlet port(s) into a rotor chamber, a piping system that provides fluid communication between the one outlet port(s) and the rotor cooling pipe(s), a blower system for extracting air from the engine through the outlet port(s) and for conveying the extracted air through the piping system and the rotor cooling pipe(s) into the rotor chamber, and a valve system. The valve system is closed during full load engine operation to prevent air from passing through the piping system, and open during less than full load engine operation to allow air to pass through the piping system.</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNi7sKwkAQANNYiPoP-wOCUUFSnpe9h5hdudsUVuGQsxINxP9Hg2JtNVPMTIukfABPB9TimSCeo2ADhgNo5qMnCwoCC4_RW62KIG3Ye0JAsiMU1dCgOK6Bze-KrXafcV5Mruk25MWXswIMinbL3D-6PPTpku_52eFpXZW7bbVS5eaP5AX_mTK8</recordid><startdate>20150916</startdate><enddate>20150916</enddate><creator>LEE, CHING-PANG</creator><creator>SIMKO, DUSTAN M</creator><creator>TERPOS, BRIAN H</creator><creator>THAM, KOK-MUN</creator><scope>EVB</scope></search><sort><creationdate>20150916</creationdate><title>AIR INJECTION SYSTEM FOR COOLING A ROTOR IN A GAS TURBINE ENGINE AND METHOD OF COOLING SUCH ROTOR</title><author>LEE, CHING-PANG ; SIMKO, DUSTAN M ; TERPOS, BRIAN H ; THAM, KOK-MUN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2917490A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2015</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>LEE, CHING-PANG</creatorcontrib><creatorcontrib>SIMKO, DUSTAN M</creatorcontrib><creatorcontrib>TERPOS, BRIAN H</creatorcontrib><creatorcontrib>THAM, KOK-MUN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LEE, CHING-PANG</au><au>SIMKO, DUSTAN M</au><au>TERPOS, BRIAN H</au><au>THAM, KOK-MUN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIR INJECTION SYSTEM FOR COOLING A ROTOR IN A GAS TURBINE ENGINE AND METHOD OF COOLING SUCH ROTOR</title><date>2015-09-16</date><risdate>2015</risdate><abstract>An air injection system for use in a gas turbine engine includes at least one outlet port through which air is extracted from the engine only during less than full load operation, at least one rotor cooling pipe, which is used to inject the air extracted from the outlet port(s) into a rotor chamber, a piping system that provides fluid communication between the one outlet port(s) and the rotor cooling pipe(s), a blower system for extracting air from the engine through the outlet port(s) and for conveying the extracted air through the piping system and the rotor cooling pipe(s) into the rotor chamber, and a valve system. The valve system is closed during full load engine operation to prevent air from passing through the piping system, and open during less than full load engine operation to allow air to pass through the piping system.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP2917490A1
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 AIR INJECTION SYSTEM FOR COOLING A ROTOR IN A GAS TURBINE ENGINE AND METHOD OF COOLING SUCH ROTOR
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-11T10%3A31%3A00IST&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=LEE,%20CHING-PANG&rft.date=2015-09-16&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2917490A1%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