SYSTEMS AND METHODS FOR GENERATING PREDICTABLE LOAD UPON COMPLETION OF START SEQUENCE OF TURBINE
PROBLEM TO BE SOLVED: To provide systems and methods for generating a predictable load upon a completion of a start sequence of a gas turbine.SOLUTION: A system may include a controller to control the gas turbine, and a processor communicatively coupled to the controller. The processor may be config...
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| creator | NATHAN S RACE NOEMIE DION OUELLET |
| description | PROBLEM TO BE SOLVED: To provide systems and methods for generating a predictable load upon a completion of a start sequence of a gas turbine.SOLUTION: A system may include a controller to control the gas turbine, and a processor communicatively coupled to the controller. The processor may be configured to receive a start duration and a desired final load, and to calculate a target load rate to substantially reach the desired final load within the start duration on the basis of the start duration and the desired final load. Measurements of a present load rate may be received from a measuring device and used to periodically recalculate the target load rate. The present load rate may be periodically adjusted by the controller on the basis of the recalculation. |
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The processor may be configured to receive a start duration and a desired final load, and to calculate a target load rate to substantially reach the desired final load within the start duration on the basis of the start duration and the desired final load. Measurements of a present load rate may be received from a measuring device and used to periodically recalculate the target load rate. The present load rate may be periodically adjusted by the controller on the basis of the recalculation.</description><language>eng</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 ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; 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=20140519&DB=EPODOC&CC=JP&NR=2014092154A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140519&DB=EPODOC&CC=JP&NR=2014092154A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NATHAN S RACE</creatorcontrib><creatorcontrib>NOEMIE DION OUELLET</creatorcontrib><title>SYSTEMS AND METHODS FOR GENERATING PREDICTABLE LOAD UPON COMPLETION OF START SEQUENCE OF TURBINE</title><description>PROBLEM TO BE SOLVED: To provide systems and methods for generating a predictable load upon a completion of a start sequence of a gas turbine.SOLUTION: A system may include a controller to control the gas turbine, and a processor communicatively coupled to the controller. 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The processor may be configured to receive a start duration and a desired final load, and to calculate a target load rate to substantially reach the desired final load within the start duration on the basis of the start duration and the desired final load. Measurements of a present load rate may be received from a measuring device and used to periodically recalculate the target load rate. The present load rate may be periodically adjusted by the controller on the basis of the recalculation.</abstract><oa>free_for_read</oa></addata></record> |
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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 NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | SYSTEMS AND METHODS FOR GENERATING PREDICTABLE LOAD UPON COMPLETION OF START SEQUENCE OF TURBINE |
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