Fuel supply system of combustion test stand of gas turbine
The invention provides a fuel supply system of a gas turbine combustion test bed, which comprises a fuel main path, a plurality of fuel branches, a replacement gas loop, a purging loop, a diffusing loop and the gas turbine combustion test bed, and is characterized in that the fuel main path is conne...
Gespeichert in:
| Hauptverfasser: | , , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; 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 | MO JINGFEI ZOU PENGFEI HU LONGBING WANG YIMIN SHU CHANG |
| description | The invention provides a fuel supply system of a gas turbine combustion test bed, which comprises a fuel main path, a plurality of fuel branches, a replacement gas loop, a purging loop, a diffusing loop and the gas turbine combustion test bed, and is characterized in that the fuel main path is connected with the plurality of fuel branches; the plurality of fuel branches are respectively connected with respective corresponding gas turbine combustion test beds, the replacement gas loop is respectively connected with the fuel main path, the plurality of fuel branches and the gas turbine combustion test beds, the purging loop is connected with the gas turbine combustion test beds, and the diffusing loop is respectively connected with the fuel main path and the plurality of fuel branches. Based on a plurality of functional branches in the fuel supply system of the gas turbine combustion test bed, stable operation of the gas turbine combustion test bed under working condition parameters of different gas turbines is |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN115163309A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN115163309A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN115163309A3</originalsourceid><addsrcrecordid>eNrjZLByK03NUSguLSjIqVQoriwuSc1VyE9TSM7PTSotLsnMz1MoSS0uUSguScxLAUmkJxYrlJQWJWXmpfIwsKYl5hSn8kJpbgZFN9cQZw_d1IL8-NTigsTk1LzUknhnP0NDU0MzY2MDS0djYtQAAIKDLxQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Fuel supply system of combustion test stand of gas turbine</title><source>esp@cenet</source><creator>MO JINGFEI ; ZOU PENGFEI ; HU LONGBING ; WANG YIMIN ; SHU CHANG</creator><creatorcontrib>MO JINGFEI ; ZOU PENGFEI ; HU LONGBING ; WANG YIMIN ; SHU CHANG</creatorcontrib><description>The invention provides a fuel supply system of a gas turbine combustion test bed, which comprises a fuel main path, a plurality of fuel branches, a replacement gas loop, a purging loop, a diffusing loop and the gas turbine combustion test bed, and is characterized in that the fuel main path is connected with the plurality of fuel branches; the plurality of fuel branches are respectively connected with respective corresponding gas turbine combustion test beds, the replacement gas loop is respectively connected with the fuel main path, the plurality of fuel branches and the gas turbine combustion test beds, the purging loop is connected with the gas turbine combustion test beds, and the diffusing loop is respectively connected with the fuel main path and the plurality of fuel branches. Based on a plurality of functional branches in the fuel supply system of the gas turbine combustion test bed, stable operation of the gas turbine combustion test bed under working condition parameters of different gas turbines is</description><language>chi ; eng</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>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&date=20221011&DB=EPODOC&CC=CN&NR=115163309A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221011&DB=EPODOC&CC=CN&NR=115163309A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MO JINGFEI</creatorcontrib><creatorcontrib>ZOU PENGFEI</creatorcontrib><creatorcontrib>HU LONGBING</creatorcontrib><creatorcontrib>WANG YIMIN</creatorcontrib><creatorcontrib>SHU CHANG</creatorcontrib><title>Fuel supply system of combustion test stand of gas turbine</title><description>The invention provides a fuel supply system of a gas turbine combustion test bed, which comprises a fuel main path, a plurality of fuel branches, a replacement gas loop, a purging loop, a diffusing loop and the gas turbine combustion test bed, and is characterized in that the fuel main path is connected with the plurality of fuel branches; the plurality of fuel branches are respectively connected with respective corresponding gas turbine combustion test beds, the replacement gas loop is respectively connected with the fuel main path, the plurality of fuel branches and the gas turbine combustion test beds, the purging loop is connected with the gas turbine combustion test beds, and the diffusing loop is respectively connected with the fuel main path and the plurality of fuel branches. Based on a plurality of functional branches in the fuel supply system of the gas turbine combustion test bed, stable operation of the gas turbine combustion test bed under working condition parameters of different gas turbines is</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLByK03NUSguLSjIqVQoriwuSc1VyE9TSM7PTSotLsnMz1MoSS0uUSguScxLAUmkJxYrlJQWJWXmpfIwsKYl5hSn8kJpbgZFN9cQZw_d1IL8-NTigsTk1LzUknhnP0NDU0MzY2MDS0djYtQAAIKDLxQ</recordid><startdate>20221011</startdate><enddate>20221011</enddate><creator>MO JINGFEI</creator><creator>ZOU PENGFEI</creator><creator>HU LONGBING</creator><creator>WANG YIMIN</creator><creator>SHU CHANG</creator><scope>EVB</scope></search><sort><creationdate>20221011</creationdate><title>Fuel supply system of combustion test stand of gas turbine</title><author>MO JINGFEI ; ZOU PENGFEI ; HU LONGBING ; WANG YIMIN ; SHU CHANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN115163309A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</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>MO JINGFEI</creatorcontrib><creatorcontrib>ZOU PENGFEI</creatorcontrib><creatorcontrib>HU LONGBING</creatorcontrib><creatorcontrib>WANG YIMIN</creatorcontrib><creatorcontrib>SHU CHANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MO JINGFEI</au><au>ZOU PENGFEI</au><au>HU LONGBING</au><au>WANG YIMIN</au><au>SHU CHANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Fuel supply system of combustion test stand of gas turbine</title><date>2022-10-11</date><risdate>2022</risdate><abstract>The invention provides a fuel supply system of a gas turbine combustion test bed, which comprises a fuel main path, a plurality of fuel branches, a replacement gas loop, a purging loop, a diffusing loop and the gas turbine combustion test bed, and is characterized in that the fuel main path is connected with the plurality of fuel branches; the plurality of fuel branches are respectively connected with respective corresponding gas turbine combustion test beds, the replacement gas loop is respectively connected with the fuel main path, the plurality of fuel branches and the gas turbine combustion test beds, the purging loop is connected with the gas turbine combustion test beds, and the diffusing loop is respectively connected with the fuel main path and the plurality of fuel branches. Based on a plurality of functional branches in the fuel supply system of the gas turbine combustion test bed, stable operation of the gas turbine combustion test bed under working condition parameters of different gas turbines is</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN115163309A |
| 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 | Fuel supply system of combustion test stand of gas turbine |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T16%3A51%3A54IST&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=MO%20JINGFEI&rft.date=2022-10-11&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN115163309A%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 |