GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND CONTROLLED BOOST COMPRESSOR

GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND CONTROLLED BOOST COMPRESSOR

A gas turbine engine (100) comprises a compressor section having a downstream most end (113) and a cooling air tap (120) at a location spaced upstream from the downstream most end (113). The cooling air tap (120) is passed through at least one boost compressor (118) and at least one heat exchanger (...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: SNAPE, Nathan, STAUBACH, Joseph Brent
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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 SNAPE, Nathan
STAUBACH, Joseph Brent
description A gas turbine engine (100) comprises a compressor section having a downstream most end (113) and a cooling air tap (120) at a location spaced upstream from the downstream most end (113). The cooling air tap (120) is passed through at least one boost compressor (118) and at least one heat exchanger (124, 130), and then passed to a turbine section to cool the turbine section, the boost compressor (118) being controlled to provide a desired pressure to the turbine section.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3543508B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3543508B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3543508B13</originalsourceid><addsrcrecordid>eNrjZPB3dwxWCAkNcvL0c1Vw9XMHUeGeIR4Knn4hrkHO_v4-ri4KIMrTz13B0TNIwdEPxPcLCfL3AUk5-fsHhwAFfAOCXIOD_YN4GFjTEnOKU3mhNDeDgptriLOHbmpBfnxqcUFicmpeakm8a4CxqYmxqYGFk6ExEUoA7BUueg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND CONTROLLED BOOST COMPRESSOR</title><source>esp@cenet</source><creator>SNAPE, Nathan ; STAUBACH, Joseph Brent</creator><creatorcontrib>SNAPE, Nathan ; STAUBACH, Joseph Brent</creatorcontrib><description>A gas turbine engine (100) comprises a compressor section having a downstream most end (113) and a cooling air tap (120) at a location spaced upstream from the downstream most end (113). The cooling air tap (120) is passed through at least one boost compressor (118) and at least one heat exchanger (124, 130), and then passed to a turbine section to cool the turbine section, the boost compressor (118) being controlled to provide a desired pressure to the turbine section.</description><language>eng ; fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2024</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=20240918&amp;DB=EPODOC&amp;CC=EP&amp;NR=3543508B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20240918&amp;DB=EPODOC&amp;CC=EP&amp;NR=3543508B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SNAPE, Nathan</creatorcontrib><creatorcontrib>STAUBACH, Joseph Brent</creatorcontrib><title>GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND CONTROLLED BOOST COMPRESSOR</title><description>A gas turbine engine (100) comprises a compressor section having a downstream most end (113) and a cooling air tap (120) at a location spaced upstream from the downstream most end (113). The cooling air tap (120) is passed through at least one boost compressor (118) and at least one heat exchanger (124, 130), and then passed to a turbine section to cool the turbine section, the boost compressor (118) being controlled to provide a desired pressure to the turbine section.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPB3dwxWCAkNcvL0c1Vw9XMHUeGeIR4Knn4hrkHO_v4-ri4KIMrTz13B0TNIwdEPxPcLCfL3AUk5-fsHhwAFfAOCXIOD_YN4GFjTEnOKU3mhNDeDgptriLOHbmpBfnxqcUFicmpeakm8a4CxqYmxqYGFk6ExEUoA7BUueg</recordid><startdate>20240918</startdate><enddate>20240918</enddate><creator>SNAPE, Nathan</creator><creator>STAUBACH, Joseph Brent</creator><scope>EVB</scope></search><sort><creationdate>20240918</creationdate><title>GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND CONTROLLED BOOST COMPRESSOR</title><author>SNAPE, Nathan ; STAUBACH, Joseph Brent</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3543508B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>SNAPE, Nathan</creatorcontrib><creatorcontrib>STAUBACH, Joseph Brent</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SNAPE, Nathan</au><au>STAUBACH, Joseph Brent</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND CONTROLLED BOOST COMPRESSOR</title><date>2024-09-18</date><risdate>2024</risdate><abstract>A gas turbine engine (100) comprises a compressor section having a downstream most end (113) and a cooling air tap (120) at a location spaced upstream from the downstream most end (113). The cooling air tap (120) is passed through at least one boost compressor (118) and at least one heat exchanger (124, 130), and then passed to a turbine section to cool the turbine section, the boost compressor (118) being controlled to provide a desired pressure to the turbine section.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP3543508B1
source esp@cenet
subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND CONTROLLED BOOST COMPRESSOR
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-27T12%3A39%3A26IST&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=SNAPE,%20Nathan&rft.date=2024-09-18&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3543508B1%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