Mixer for cooling and sealing air system for turbomachinery
A system for mixing flows from a compressor is provided. The system comprises an ejector (150) that combines a first flow (122) and a second flow (132), from the compressor, into a third flow (158). A bypass flow (142) is connected between the first flow (122) and the third flow (158). A mixer (300)...
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| creator | BALL, DAVID W. JR WHALING, KENNETH N ELURIPATI, RAVI PRAVEEN S DAVIS, JAMES L SARAVANAN, NATTAMAI V SENGAR, AJIT S |
| description | A system for mixing flows from a compressor is provided. The system comprises an ejector (150) that combines a first flow (122) and a second flow (132), from the compressor, into a third flow (158). A bypass flow (142) is connected between the first flow (122) and the third flow (158). A mixer (300) combines the bypass flow (142) and the third flow (158) into a fourth flow (165). The fourth flow has a pressure and temperature intermediate the respective pressures and temperatures of the bypass flow and the third flow. |
| format | Patent |
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JR ; WHALING, KENNETH N ; ELURIPATI, RAVI PRAVEEN S ; DAVIS, JAMES L ; SARAVANAN, NATTAMAI V ; SENGAR, AJIT S</creatorcontrib><description>A system for mixing flows from a compressor is provided. The system comprises an ejector (150) that combines a first flow (122) and a second flow (132), from the compressor, into a third flow (158). A bypass flow (142) is connected between the first flow (122) and the third flow (158). A mixer (300) combines the bypass flow (142) and the third flow (158) into a fourth flow (165). The fourth flow has a pressure and temperature intermediate the respective pressures and temperatures of the bypass flow and the third flow.</description><language>eng ; fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; MIXING, e.g. DISSOLVING, EMULSIFYING, DISPERSING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</subject><creationdate>2008</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=20081015&DB=EPODOC&CC=EP&NR=1980717A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20081015&DB=EPODOC&CC=EP&NR=1980717A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BALL, DAVID W. 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The fourth flow has a pressure and temperature intermediate the respective pressures and temperatures of the bypass flow and the third flow.</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>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>MIXING, e.g. DISSOLVING, EMULSIFYING, DISPERSING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2008</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLD2zaxILVJIyy9SSM7Pz8nMS1dIzEtRKE5NhLAzixSKK4tLUnPBSkpKi5LycxOTMzLzUosqeRhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJvGuAoaWFgbmhuaORMRFKAFOHLy8</recordid><startdate>20081015</startdate><enddate>20081015</enddate><creator>BALL, DAVID W. 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JR</creatorcontrib><creatorcontrib>WHALING, KENNETH N</creatorcontrib><creatorcontrib>ELURIPATI, RAVI PRAVEEN S</creatorcontrib><creatorcontrib>DAVIS, JAMES L</creatorcontrib><creatorcontrib>SARAVANAN, NATTAMAI V</creatorcontrib><creatorcontrib>SENGAR, AJIT S</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BALL, DAVID W. JR</au><au>WHALING, KENNETH N</au><au>ELURIPATI, RAVI PRAVEEN S</au><au>DAVIS, JAMES L</au><au>SARAVANAN, NATTAMAI V</au><au>SENGAR, AJIT S</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Mixer for cooling and sealing air system for turbomachinery</title><date>2008-10-15</date><risdate>2008</risdate><abstract>A system for mixing flows from a compressor is provided. The system comprises an ejector (150) that combines a first flow (122) and a second flow (132), from the compressor, into a third flow (158). A bypass flow (142) is connected between the first flow (122) and the third flow (158). A mixer (300) combines the bypass flow (142) and the third flow (158) into a fourth flow (165). The fourth flow has a pressure and temperature intermediate the respective pressures and temperatures of the bypass flow and the third flow.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP1980717A2 |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING MIXING, e.g. DISSOLVING, EMULSIFYING, DISPERSING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL STEAM ENGINES TRANSPORTING WEAPONS |
| title | Mixer for cooling and sealing air system for turbomachinery |
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