GAS TURBINE WITH A VALVE COOLING SYSTEM
The present application provides a gas turbine engine 100. The gas turbine engine 100 may include a compressor air extraction system 110 with a number of valves 365, an exhaust frame cooling system 310 with an exhaust frame blower 330, and a turbine valve cooling system 350 with one or more valve pr...
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| creator | AMPILI KISHORE KUMAR SRINIVAS AVISHETTI LAXMIKANT MERCHANT ANIL KUMAR DASOJI |
| description | The present application provides a gas turbine engine 100. The gas turbine engine 100 may include a compressor air extraction system 110 with a number of valves 365, an exhaust frame cooling system 310 with an exhaust frame blower 330, and a turbine valve cooling system 350 with one or more valve protection boxes 360 surrounding one or more of the valves 365. The valve protection boxes 360 may be in communication with a flow of air from the exhaust frame blower 330.
本申请提供种燃气涡轮发动机(100)。该燃气涡轮发动机(100)可包括：压缩机空气提取系统(110)，其具有多个阀(365)；排气框架冷却系统(310)，其具有排气框架送风机(330)；和涡轮阀冷却系统(350)，其具有个或更多个阀保护盒(360)，所述阀保护盒(360)包围阀(365)中的个或更多个。阀保护盒(360)可与来自排气框架送风机(330)的空气流连通。 |
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本申请提供种燃气涡轮发动机(100)。该燃气涡轮发动机(100)可包括：压缩机空气提取系统(110)，其具有多个阀(365)；排气框架冷却系统(310)，其具有排气框架送风机(330)；和涡轮阀冷却系统(350)，其具有个或更多个阀保护盒(360)，所述阀保护盒(360)包围阀(365)中的个或更多个。阀保护盒(360)可与来自排气框架送风机(330)的空气流连通。</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>2017</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=20170804&DB=EPODOC&CC=CN&NR=107013337A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170804&DB=EPODOC&CC=CN&NR=107013337A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>AMPILI KISHORE KUMAR</creatorcontrib><creatorcontrib>SRINIVAS AVISHETTI</creatorcontrib><creatorcontrib>LAXMIKANT MERCHANT</creatorcontrib><creatorcontrib>ANIL KUMAR DASOJI</creatorcontrib><title>GAS TURBINE WITH A VALVE COOLING SYSTEM</title><description>The present application provides a gas turbine engine 100. The gas turbine engine 100 may include a compressor air extraction system 110 with a number of valves 365, an exhaust frame cooling system 310 with an exhaust frame blower 330, and a turbine valve cooling system 350 with one or more valve protection boxes 360 surrounding one or more of the valves 365. The valve protection boxes 360 may be in communication with a flow of air from the exhaust frame blower 330.
本申请提供种燃气涡轮发动机(100)。该燃气涡轮发动机(100)可包括：压缩机空气提取系统(110)，其具有多个阀(365)；排气框架冷却系统(310)，其具有排气框架送风机(330)；和涡轮阀冷却系统(350)，其具有个或更多个阀保护盒(360)，所述阀保护盒(360)包围阀(365)中的个或更多个。阀保护盒(360)可与来自排气框架送风机(330)的空气流连通。</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>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB3dwxWCAkNcvL0c1UI9wzxUHBUCHP0CXNVcPb39_H0c1cIjgwOcfXlYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GBuYGhsbGxuaOxsSoAQDSeyOf</recordid><startdate>20170804</startdate><enddate>20170804</enddate><creator>AMPILI KISHORE KUMAR</creator><creator>SRINIVAS AVISHETTI</creator><creator>LAXMIKANT MERCHANT</creator><creator>ANIL KUMAR DASOJI</creator><scope>EVB</scope></search><sort><creationdate>20170804</creationdate><title>GAS TURBINE WITH A VALVE COOLING SYSTEM</title><author>AMPILI KISHORE KUMAR ; SRINIVAS AVISHETTI ; LAXMIKANT MERCHANT ; ANIL KUMAR DASOJI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN107013337A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2017</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>AMPILI KISHORE KUMAR</creatorcontrib><creatorcontrib>SRINIVAS AVISHETTI</creatorcontrib><creatorcontrib>LAXMIKANT MERCHANT</creatorcontrib><creatorcontrib>ANIL KUMAR DASOJI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>AMPILI KISHORE KUMAR</au><au>SRINIVAS AVISHETTI</au><au>LAXMIKANT MERCHANT</au><au>ANIL KUMAR DASOJI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE WITH A VALVE COOLING SYSTEM</title><date>2017-08-04</date><risdate>2017</risdate><abstract>The present application provides a gas turbine engine 100. The gas turbine engine 100 may include a compressor air extraction system 110 with a number of valves 365, an exhaust frame cooling system 310 with an exhaust frame blower 330, and a turbine valve cooling system 350 with one or more valve protection boxes 360 surrounding one or more of the valves 365. The valve protection boxes 360 may be in communication with a flow of air from the exhaust frame blower 330.
本申请提供种燃气涡轮发动机(100)。该燃气涡轮发动机(100)可包括：压缩机空气提取系统(110)，其具有多个阀(365)；排气框架冷却系统(310)，其具有排气框架送风机(330)；和涡轮阀冷却系统(350)，其具有个或更多个阀保护盒(360)，所述阀保护盒(360)包围阀(365)中的个或更多个。阀保护盒(360)可与来自排气框架送风机(330)的空气流连通。</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 | GAS TURBINE WITH A VALVE COOLING SYSTEM |
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