TWO-AXIS GAS TURBINE
PROBLEM TO BE SOLVED: To provide a two-axis gas turbine having high operability.SOLUTION: The gas turbine comprises: a compressor 1; a combustor 20; a gas generator 15 having a high-pressure turbine 2; a power turbine 16 having a low-pressure turbine 3; a load 5 connected to the power turbine 16; a...
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| creator | TAKAHASHI KAZUO ITO TOMOMICHI MORISAKI TETSURO HINO TOKUAKI KUSUMI HISAHIRO |
| description | PROBLEM TO BE SOLVED: To provide a two-axis gas turbine having high operability.SOLUTION: The gas turbine comprises: a compressor 1; a combustor 20; a gas generator 15 having a high-pressure turbine 2; a power turbine 16 having a low-pressure turbine 3; a load 5 connected to the power turbine 16; a motor generator 6 capable of rotary-driving the gas generator 15 and extracting power from the gas generator 15; an electric apparatus 10 for controlling the rotary driving and the power extraction by delivering power to the motor generator 6; and a control device 7 for controlling the electric apparatus 10. The combustor 20 has plural combustion regions to which fuel is supplied via independent fuel adjustment means, and the control device 7 controls an amount of power delivered by the electric apparatus 10 according to the number of the combustion regions to which the fuel is supplied. |
| format | Patent |
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The combustor 20 has plural combustion regions to which fuel is supplied via independent fuel adjustment means, and the control device 7 controls an amount of power delivered by the electric apparatus 10 according to the number of the combustion regions to which the fuel is supplied.</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>2014</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=20140821&DB=EPODOC&CC=JP&NR=2014148933A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140821&DB=EPODOC&CC=JP&NR=2014148933A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TAKAHASHI KAZUO</creatorcontrib><creatorcontrib>ITO TOMOMICHI</creatorcontrib><creatorcontrib>MORISAKI TETSURO</creatorcontrib><creatorcontrib>HINO TOKUAKI</creatorcontrib><creatorcontrib>KUSUMI HISAHIRO</creatorcontrib><title>TWO-AXIS GAS TURBINE</title><description>PROBLEM TO BE SOLVED: To provide a two-axis gas turbine having high operability.SOLUTION: The gas turbine comprises: a compressor 1; a combustor 20; a gas generator 15 having a high-pressure turbine 2; a power turbine 16 having a low-pressure turbine 3; a load 5 connected to the power turbine 16; a motor generator 6 capable of rotary-driving the gas generator 15 and extracting power from the gas generator 15; an electric apparatus 10 for controlling the rotary driving and the power extraction by delivering power to the motor generator 6; and a control device 7 for controlling the electric apparatus 10. 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| language | 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 | TWO-AXIS GAS TURBINE |
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