Gasturbogruppe mit sequentieller Verbrennung

Gasturbogruppe mit sequentieller Verbrennung

In a gas-turbine group which is operated with sequential combustion, preferably via two combustion chambers (4, 9) having in each case turbines arranged downstream, the temperature of the exhaust gases (8) from the first turbine (5) is recorded directly in front of the self-ignition point in the sec...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: ALTHAUS, ROLF
Format: Patent
Sprache: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 ALTHAUS, ROLF
description In a gas-turbine group which is operated with sequential combustion, preferably via two combustion chambers (4, 9) having in each case turbines arranged downstream, the temperature of the exhaust gases (8) from the first turbine (5) is recorded directly in front of the self-ignition point in the second combustion chamber (9) for the dosing of the fuel quantity for the first combustion chamber (4). The temperature is recorded by means of thermocouples (17) which are integrated in fuel lances (16) of the second combustion chamber (9), as a result of which influence is at the same time exerted on the fuel quantity (10) of this combustion chamber (9).
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_DE4422701B4</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>DE4422701B4</sourcerecordid><originalsourceid>FETCH-epo_espacenet_DE4422701B43</originalsourceid><addsrcrecordid>eNrjZNBxTywuKS1Kyk8vKi0oSFXIzSxRKE4tLE3NK8lMzclJLVIISy1KKkrNyyvNS-dhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfEuriYmRkbmBoZOJsZEKAEAn-0qJQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Gasturbogruppe mit sequentieller Verbrennung</title><source>esp@cenet</source><creator>ALTHAUS, ROLF</creator><creatorcontrib>ALTHAUS, ROLF</creatorcontrib><description>In a gas-turbine group which is operated with sequential combustion, preferably via two combustion chambers (4, 9) having in each case turbines arranged downstream, the temperature of the exhaust gases (8) from the first turbine (5) is recorded directly in front of the self-ignition point in the second combustion chamber (9) for the dosing of the fuel quantity for the first combustion chamber (4). The temperature is recorded by means of thermocouples (17) which are integrated in fuel lances (16) of the second combustion chamber (9), as a result of which influence is at the same time exerted on the fuel quantity (10) of this combustion chamber (9).</description><language>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>2010</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=20100512&amp;DB=EPODOC&amp;CC=DE&amp;NR=4422701B4$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20100512&amp;DB=EPODOC&amp;CC=DE&amp;NR=4422701B4$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ALTHAUS, ROLF</creatorcontrib><title>Gasturbogruppe mit sequentieller Verbrennung</title><description>In a gas-turbine group which is operated with sequential combustion, preferably via two combustion chambers (4, 9) having in each case turbines arranged downstream, the temperature of the exhaust gases (8) from the first turbine (5) is recorded directly in front of the self-ignition point in the second combustion chamber (9) for the dosing of the fuel quantity for the first combustion chamber (4). The temperature is recorded by means of thermocouples (17) which are integrated in fuel lances (16) of the second combustion chamber (9), as a result of which influence is at the same time exerted on the fuel quantity (10) of this combustion chamber (9).</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>2010</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNBxTywuKS1Kyk8vKi0oSFXIzSxRKE4tLE3NK8lMzclJLVIISy1KKkrNyyvNS-dhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfEuriYmRkbmBoZOJsZEKAEAn-0qJQ</recordid><startdate>20100512</startdate><enddate>20100512</enddate><creator>ALTHAUS, ROLF</creator><scope>EVB</scope></search><sort><creationdate>20100512</creationdate><title>Gasturbogruppe mit sequentieller Verbrennung</title><author>ALTHAUS, ROLF</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE4422701B43</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ger</language><creationdate>2010</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>ALTHAUS, ROLF</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ALTHAUS, ROLF</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Gasturbogruppe mit sequentieller Verbrennung</title><date>2010-05-12</date><risdate>2010</risdate><abstract>In a gas-turbine group which is operated with sequential combustion, preferably via two combustion chambers (4, 9) having in each case turbines arranged downstream, the temperature of the exhaust gases (8) from the first turbine (5) is recorded directly in front of the self-ignition point in the second combustion chamber (9) for the dosing of the fuel quantity for the first combustion chamber (4). The temperature is recorded by means of thermocouples (17) which are integrated in fuel lances (16) of the second combustion chamber (9), as a result of which influence is at the same time exerted on the fuel quantity (10) of this combustion chamber (9).</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language ger
recordid cdi_epo_espacenet_DE4422701B4
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 Gasturbogruppe mit sequentieller Verbrennung
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-22T19%3A48%3A15IST&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=ALTHAUS,%20ROLF&rft.date=2010-05-12&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EDE4422701B4%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