LEAN FUEL SUCTION GAS TURBINE
PROBLEM TO BE SOLVED: To provide a lean fuel suction gas turbine capable of slipping-out of mixed gas, by performing efficient operation, while simplifying the whole constitution. SOLUTION: This lean fuel suction gas turbine has a compressor 1 for generating compressed gas G2 by compressing mixed ga...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Patent |
| Sprache: | eng |
| 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 | KAJITA SHINICHI |
| description | PROBLEM TO BE SOLVED: To provide a lean fuel suction gas turbine capable of slipping-out of mixed gas, by performing efficient operation, while simplifying the whole constitution. SOLUTION: This lean fuel suction gas turbine has a compressor 1 for generating compressed gas G2 by compressing mixed gas G1 of the combustible limit concentration or less of mixing fuel and air, a first catalytic combustor 2 for burning the compressed gas G2 by catalytic reaction, a turbine 3 driven by combustion gas G3 from the first catalytic combustor 2, and a regenerator 6 for heating the compressed gas G2 introduced to the first catalytic combustor 2 by exhaust gas G4 from the turbine 3. A duct burner 7 for burning the exhaust gas G4 by a flame by first auxiliary fuel F1 is arranged between the turbine 3 and the regenerator 6. COPYRIGHT: (C)2010,JPO&INPIT |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_JP2010019247A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>JP2010019247A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_JP2010019247A3</originalsourceid><addsrcrecordid>eNrjZJD1cXX0U3ALdfVRCA51DvH091NwdwxWCAkNcvL0c-VhYE1LzClO5YXS3AxKbq4hzh66qQX58anFBYnJqXmpJfFeAUYGhgYGhpZGJuaOxkQpAgDAtiFR</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>LEAN FUEL SUCTION GAS TURBINE</title><source>esp@cenet</source><creator>KAJITA SHINICHI</creator><creatorcontrib>KAJITA SHINICHI</creatorcontrib><description>PROBLEM TO BE SOLVED: To provide a lean fuel suction gas turbine capable of slipping-out of mixed gas, by performing efficient operation, while simplifying the whole constitution. SOLUTION: This lean fuel suction gas turbine has a compressor 1 for generating compressed gas G2 by compressing mixed gas G1 of the combustible limit concentration or less of mixing fuel and air, a first catalytic combustor 2 for burning the compressed gas G2 by catalytic reaction, a turbine 3 driven by combustion gas G3 from the first catalytic combustor 2, and a regenerator 6 for heating the compressed gas G2 introduced to the first catalytic combustor 2 by exhaust gas G4 from the turbine 3. A duct burner 7 for burning the exhaust gas G4 by a flame by first auxiliary fuel F1 is arranged between the turbine 3 and the regenerator 6. COPYRIGHT: (C)2010,JPO&INPIT</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION APPARATUS ; COMBUSTION ENGINES ; COMBUSTION PROCESSES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; 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&date=20100128&DB=EPODOC&CC=JP&NR=2010019247A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20100128&DB=EPODOC&CC=JP&NR=2010019247A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KAJITA SHINICHI</creatorcontrib><title>LEAN FUEL SUCTION GAS TURBINE</title><description>PROBLEM TO BE SOLVED: To provide a lean fuel suction gas turbine capable of slipping-out of mixed gas, by performing efficient operation, while simplifying the whole constitution. SOLUTION: This lean fuel suction gas turbine has a compressor 1 for generating compressed gas G2 by compressing mixed gas G1 of the combustible limit concentration or less of mixing fuel and air, a first catalytic combustor 2 for burning the compressed gas G2 by catalytic reaction, a turbine 3 driven by combustion gas G3 from the first catalytic combustor 2, and a regenerator 6 for heating the compressed gas G2 introduced to the first catalytic combustor 2 by exhaust gas G4 from the turbine 3. A duct burner 7 for burning the exhaust gas G4 by a flame by first auxiliary fuel F1 is arranged between the turbine 3 and the regenerator 6. COPYRIGHT: (C)2010,JPO&INPIT</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION PROCESSES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</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>eNrjZJD1cXX0U3ALdfVRCA51DvH091NwdwxWCAkNcvL0c-VhYE1LzClO5YXS3AxKbq4hzh66qQX58anFBYnJqXmpJfFeAUYGhgYGhpZGJuaOxkQpAgDAtiFR</recordid><startdate>20100128</startdate><enddate>20100128</enddate><creator>KAJITA SHINICHI</creator><scope>EVB</scope></search><sort><creationdate>20100128</creationdate><title>LEAN FUEL SUCTION GAS TURBINE</title><author>KAJITA SHINICHI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2010019247A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2010</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION PROCESSES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</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>KAJITA SHINICHI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KAJITA SHINICHI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>LEAN FUEL SUCTION GAS TURBINE</title><date>2010-01-28</date><risdate>2010</risdate><abstract>PROBLEM TO BE SOLVED: To provide a lean fuel suction gas turbine capable of slipping-out of mixed gas, by performing efficient operation, while simplifying the whole constitution. SOLUTION: This lean fuel suction gas turbine has a compressor 1 for generating compressed gas G2 by compressing mixed gas G1 of the combustible limit concentration or less of mixing fuel and air, a first catalytic combustor 2 for burning the compressed gas G2 by catalytic reaction, a turbine 3 driven by combustion gas G3 from the first catalytic combustor 2, and a regenerator 6 for heating the compressed gas G2 introduced to the first catalytic combustor 2 by exhaust gas G4 from the turbine 3. A duct burner 7 for burning the exhaust gas G4 by a flame by first auxiliary fuel F1 is arranged between the turbine 3 and the regenerator 6. COPYRIGHT: (C)2010,JPO&INPIT</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_epo_espacenet_JP2010019247A |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | LEAN FUEL SUCTION GAS TURBINE |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-27T21%3A05%3A22IST&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=KAJITA%20SHINICHI&rft.date=2010-01-28&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EJP2010019247A%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 |