IGNITER ASSEMBLY FOR A GAS TURBINE COMBUSTOR
An igniter assembly for a gas turbine combustor includes a first electrode, a second electrode, and an insulator. The first electrode, the second electrode, and the insulator form a cavity, the second electrode forms an outlet passage extending from the cavity, a maximum cross-sectional area of the...
Gespeichert in:
| Hauptverfasser: | , , , , , , |
|---|---|
| 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 | Meshkov, Andrey Rahmane, Mohamed Younsi, Karim Selezneva, Svetlana McWaters, Mark Wayne Alberti, Philip Nose Ramamurthi, Badri Narayan |
| description | An igniter assembly for a gas turbine combustor includes a first electrode, a second electrode, and an insulator. The first electrode, the second electrode, and the insulator form a cavity, the second electrode forms an outlet passage extending from the cavity, a maximum cross-sectional area of the cavity is greater than a cross-sectional area of the outlet passage, and the cross-sectional area of the outlet passage is substantially constant along a longitudinal extent of the outlet passage. In addition, the first electrode and the second electrode are configured to ionize gas within the cavity in response to an electrical current applied to the first electrode or to the second electrode. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2019063329A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2019063329A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2019063329A13</originalsourceid><addsrcrecordid>eNrjZNDxdPfzDHENUnAMDnb1dfKJVHDzB3IU3B2DFUJCg5w8_VwVnP19nUKDQ_yDeBhY0xJzilN5oTQ3g7Kba4izh25qQX58anFBYnJqXmpJfGiwkYGhpYGZsbGRpaOhMXGqACagJhk</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>IGNITER ASSEMBLY FOR A GAS TURBINE COMBUSTOR</title><source>esp@cenet</source><creator>Meshkov, Andrey ; Rahmane, Mohamed ; Younsi, Karim ; Selezneva, Svetlana ; McWaters, Mark Wayne ; Alberti, Philip Nose ; Ramamurthi, Badri Narayan</creator><creatorcontrib>Meshkov, Andrey ; Rahmane, Mohamed ; Younsi, Karim ; Selezneva, Svetlana ; McWaters, Mark Wayne ; Alberti, Philip Nose ; Ramamurthi, Badri Narayan</creatorcontrib><description>An igniter assembly for a gas turbine combustor includes a first electrode, a second electrode, and an insulator. The first electrode, the second electrode, and the insulator form a cavity, the second electrode forms an outlet passage extending from the cavity, a maximum cross-sectional area of the cavity is greater than a cross-sectional area of the outlet passage, and the cross-sectional area of the outlet passage is substantially constant along a longitudinal extent of the outlet passage. In addition, the first electrode and the second electrode are configured to ionize gas within the cavity in response to an electrical current applied to the first electrode or to the second electrode.</description><language>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>2019</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=20190228&DB=EPODOC&CC=US&NR=2019063329A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190228&DB=EPODOC&CC=US&NR=2019063329A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Meshkov, Andrey</creatorcontrib><creatorcontrib>Rahmane, Mohamed</creatorcontrib><creatorcontrib>Younsi, Karim</creatorcontrib><creatorcontrib>Selezneva, Svetlana</creatorcontrib><creatorcontrib>McWaters, Mark Wayne</creatorcontrib><creatorcontrib>Alberti, Philip Nose</creatorcontrib><creatorcontrib>Ramamurthi, Badri Narayan</creatorcontrib><title>IGNITER ASSEMBLY FOR A GAS TURBINE COMBUSTOR</title><description>An igniter assembly for a gas turbine combustor includes a first electrode, a second electrode, and an insulator. The first electrode, the second electrode, and the insulator form a cavity, the second electrode forms an outlet passage extending from the cavity, a maximum cross-sectional area of the cavity is greater than a cross-sectional area of the outlet passage, and the cross-sectional area of the outlet passage is substantially constant along a longitudinal extent of the outlet passage. In addition, the first electrode and the second electrode are configured to ionize gas within the cavity in response to an electrical current applied to the first electrode or to the second electrode.</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNDxdPfzDHENUnAMDnb1dfKJVHDzB3IU3B2DFUJCg5w8_VwVnP19nUKDQ_yDeBhY0xJzilN5oTQ3g7Kba4izh25qQX58anFBYnJqXmpJfGiwkYGhpYGZsbGRpaOhMXGqACagJhk</recordid><startdate>20190228</startdate><enddate>20190228</enddate><creator>Meshkov, Andrey</creator><creator>Rahmane, Mohamed</creator><creator>Younsi, Karim</creator><creator>Selezneva, Svetlana</creator><creator>McWaters, Mark Wayne</creator><creator>Alberti, Philip Nose</creator><creator>Ramamurthi, Badri Narayan</creator><scope>EVB</scope></search><sort><creationdate>20190228</creationdate><title>IGNITER ASSEMBLY FOR A GAS TURBINE COMBUSTOR</title><author>Meshkov, Andrey ; Rahmane, Mohamed ; Younsi, Karim ; Selezneva, Svetlana ; McWaters, Mark Wayne ; Alberti, Philip Nose ; Ramamurthi, Badri Narayan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2019063329A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2019</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>Meshkov, Andrey</creatorcontrib><creatorcontrib>Rahmane, Mohamed</creatorcontrib><creatorcontrib>Younsi, Karim</creatorcontrib><creatorcontrib>Selezneva, Svetlana</creatorcontrib><creatorcontrib>McWaters, Mark Wayne</creatorcontrib><creatorcontrib>Alberti, Philip Nose</creatorcontrib><creatorcontrib>Ramamurthi, Badri Narayan</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Meshkov, Andrey</au><au>Rahmane, Mohamed</au><au>Younsi, Karim</au><au>Selezneva, Svetlana</au><au>McWaters, Mark Wayne</au><au>Alberti, Philip Nose</au><au>Ramamurthi, Badri Narayan</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>IGNITER ASSEMBLY FOR A GAS TURBINE COMBUSTOR</title><date>2019-02-28</date><risdate>2019</risdate><abstract>An igniter assembly for a gas turbine combustor includes a first electrode, a second electrode, and an insulator. The first electrode, the second electrode, and the insulator form a cavity, the second electrode forms an outlet passage extending from the cavity, a maximum cross-sectional area of the cavity is greater than a cross-sectional area of the outlet passage, and the cross-sectional area of the outlet passage is substantially constant along a longitudinal extent of the outlet passage. In addition, the first electrode and the second electrode are configured to ionize gas within the cavity in response to an electrical current applied to the first electrode or to the second electrode.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_epo_espacenet_US2019063329A1 |
| 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 | IGNITER ASSEMBLY FOR A GAS TURBINE COMBUSTOR |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-31T14%3A19%3A30IST&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=Meshkov,%20Andrey&rft.date=2019-02-28&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2019063329A1%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 |