Model and simulation based control of turbines

A system includes a gas turbine system model configured to model a turbine system operational behavior of a gas turbine system, and a shaft contribution model (SCM) including a bottoming cycle performance (BCP) model configured to model a bottoming cycle behavior of a bottoming cycle system. The gas...

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Bibliographic Details
Main Authors Wilkes Kevin Wood, Mitchell Paul Jeffrey, Rosson Randy Scott
Format Patent
LanguageEnglish
Published 04.10.2016
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
ANALOGUE COMPUTERS
BLASTING
CALCULATING
COMBUSTION ENGINES
COMPUTING
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COUNTING
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
PHYSICS
STEAM ENGINES
WEAPONS
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Summary:A system includes a gas turbine system model configured to model a turbine system operational behavior of a gas turbine system, and a shaft contribution model (SCM) including a bottoming cycle performance (BCP) model configured to model a bottoming cycle behavior of a bottoming cycle system. The gas turbine system model is configured to receive a SCM output from the SCM and to use the SCM output to control an actuator. The actuator is operatively coupled to the gas turbine system.
Bibliography:Application Number: US201213492736