METHOD FOR OPERATING A GAS TURBINE PLANT WITH GASEOUS FUEL
The invention relates to a method for operating a gas turbine plant with gaseous fuel, which is conveyed to the gas turbine plant through a gas line (6), burnt in a combustion chamber (4) and then supplied to a gas turbine. At least one valve (12a, 12b) for controlling the flow of the fuel to the co...
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| creator | NAUBER NIKLAS BECKMANN BJORN OVER MAARTEN |
| description | The invention relates to a method for operating a gas turbine plant with gaseous fuel, which is conveyed to the gas turbine plant through a gas line (6), burnt in a combustion chamber (4) and then supplied to a gas turbine. At least one valve (12a, 12b) for controlling the flow of the fuel to the combustion chamber (4) is installed in the gas line (6), a critical opening position (Skrit) being defined for the valve (12a, 12b). According to the invention, to provide an improved method for operating a gas turbine plant in which the power (P) of the gas turbine plant is kept at a maximum for as long as possible in the event of insufficient pressure in the gas line (6), a temperature (TB) of the fuel in the gas line (6) is reduced when the valve (12a, 12b) is about to exceed the critical opening position (Skrit).
一种用于运行具有气态燃料的燃气轮机设施的方法，所述气态燃料通过气体管路(6)被运输到所述燃气轮机设施、在燃烧室(4)中燃烧并且紧接着被输送给燃气轮机。在所述气体管路(6)中装入有至少一个阀门(12a，12b)，用于进行至燃烧室(4)的燃料的流量调节，其中对于所述阀门(12a，12b)定义临界打开位置(Skrit)。关于用于运行燃气轮机设施的改进方法，其中在气体管路(6)中的压力不足的情况下燃气轮机设施的 |
| format | Patent |
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一种用于运行具有气态燃料的燃气轮机设施的方法，所述气态燃料通过气体管路(6)被运输到所述燃气轮机设施、在燃烧室(4)中燃烧并且紧接着被输送给燃气轮机。在所述气体管路(6)中装入有至少一个阀门(12a，12b)，用于进行至燃烧室(4)的燃料的流量调节，其中对于所述阀门(12a，12b)定义临界打开位置(Skrit)。关于用于运行燃气轮机设施的改进方法，其中在气体管路(6)中的压力不足的情况下燃气轮机设施的</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>2021</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=20210316&DB=EPODOC&CC=CN&NR=112513442A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210316&DB=EPODOC&CC=CN&NR=112513442A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NAUBER NIKLAS</creatorcontrib><creatorcontrib>BECKMANN BJORN</creatorcontrib><creatorcontrib>OVER MAARTEN</creatorcontrib><title>METHOD FOR OPERATING A GAS TURBINE PLANT WITH GASEOUS FUEL</title><description>The invention relates to a method for operating a gas turbine plant with gaseous fuel, which is conveyed to the gas turbine plant through a gas line (6), burnt in a combustion chamber (4) and then supplied to a gas turbine. At least one valve (12a, 12b) for controlling the flow of the fuel to the combustion chamber (4) is installed in the gas line (6), a critical opening position (Skrit) being defined for the valve (12a, 12b). According to the invention, to provide an improved method for operating a gas turbine plant in which the power (P) of the gas turbine plant is kept at a maximum for as long as possible in the event of insufficient pressure in the gas line (6), a temperature (TB) of the fuel in the gas line (6) is reduced when the valve (12a, 12b) is about to exceed the critical opening position (Skrit).
一种用于运行具有气态燃料的燃气轮机设施的方法，所述气态燃料通过气体管路(6)被运输到所述燃气轮机设施、在燃烧室(4)中燃烧并且紧接着被输送给燃气轮机。在所述气体管路(6)中装入有至少一个阀门(12a，12b)，用于进行至燃烧室(4)的燃料的流量调节，其中对于所述阀门(12a，12b)定义临界打开位置(Skrit)。关于用于运行燃气轮机设施的改进方法，其中在气体管路(6)中的压力不足的情况下燃气轮机设施的</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>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLDydQ3x8HdRcPMPUvAPcA1yDPH0c1dwVHB3DFYICQ1y8vRzVQjwcfQLUQj3DPEACbv6hwYruIW6-vAwsKYl5hSn8kJpbgZFN9cQZw_d1IL8-NTigsTk1LzUknhnP0NDI1NDYxMTI0djYtQAAJToKLM</recordid><startdate>20210316</startdate><enddate>20210316</enddate><creator>NAUBER NIKLAS</creator><creator>BECKMANN BJORN</creator><creator>OVER MAARTEN</creator><scope>EVB</scope></search><sort><creationdate>20210316</creationdate><title>METHOD FOR OPERATING A GAS TURBINE PLANT WITH GASEOUS FUEL</title><author>NAUBER NIKLAS ; BECKMANN BJORN ; OVER MAARTEN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112513442A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</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>NAUBER NIKLAS</creatorcontrib><creatorcontrib>BECKMANN BJORN</creatorcontrib><creatorcontrib>OVER MAARTEN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NAUBER NIKLAS</au><au>BECKMANN BJORN</au><au>OVER MAARTEN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD FOR OPERATING A GAS TURBINE PLANT WITH GASEOUS FUEL</title><date>2021-03-16</date><risdate>2021</risdate><abstract>The invention relates to a method for operating a gas turbine plant with gaseous fuel, which is conveyed to the gas turbine plant through a gas line (6), burnt in a combustion chamber (4) and then supplied to a gas turbine. At least one valve (12a, 12b) for controlling the flow of the fuel to the combustion chamber (4) is installed in the gas line (6), a critical opening position (Skrit) being defined for the valve (12a, 12b). According to the invention, to provide an improved method for operating a gas turbine plant in which the power (P) of the gas turbine plant is kept at a maximum for as long as possible in the event of insufficient pressure in the gas line (6), a temperature (TB) of the fuel in the gas line (6) is reduced when the valve (12a, 12b) is about to exceed the critical opening position (Skrit).
一种用于运行具有气态燃料的燃气轮机设施的方法，所述气态燃料通过气体管路(6)被运输到所述燃气轮机设施、在燃烧室(4)中燃烧并且紧接着被输送给燃气轮机。在所述气体管路(6)中装入有至少一个阀门(12a，12b)，用于进行至燃烧室(4)的燃料的流量调节，其中对于所述阀门(12a，12b)定义临界打开位置(Skrit)。关于用于运行燃气轮机设施的改进方法，其中在气体管路(6)中的压力不足的情况下燃气轮机设施的</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| 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 | METHOD FOR OPERATING A GAS TURBINE PLANT WITH GASEOUS FUEL |
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