Title:
Gas turbine combustor control system
Document Type and Number:
Japanese Patent JP6343286
Kind Code:
B2
Abstract:
In one embodiment, a gas turbine system includes a controller configured to receive fuel composition information related to a fuel used for combustion in a turbine combustor; receive oxidant composition information related to an oxidant used for combustion in the turbine combustor; receive oxidant flow information related to a flow of the oxidant to the turbine combustor; determine a stoichiometric fuel-to-oxidant ratio based at least on the fuel composition information and the oxidant composition information; and generate a control signal for input to a fuel flow control system configured to control a flow of the fuel to the turbine combustor based on the oxidant flow information, a target equivalence ratio, and the stoichiometric fuel-to-oxidant ratio to enable combustion at the target equivalence ratio in the presence of an exhaust diluent within the turbine combustor.
Inventors:
Mint Carl Dean
Application Number:
JP2015540788A
Publication Date:
June 13, 2018
Filing Date:
October 31, 2013
Export Citation:
Assignee:
Exxon Mobil Upstream Research Company
GENERAL ELECTRIC COMPANY
GENERAL ELECTRIC COMPANY
International Classes:
F02C9/00; F02C3/30; F02C3/34; F02C9/16; F02C9/28; F23R3/00; G01N21/3504
Domestic Patent References:
| JP2010209332A | ||||
| JP2012505987A |
Foreign References:
| WO2012018457A1 |
Attorney, Agent or Firm:
Koichi Tsujii
Sadao Kumakura
Disciple Maru Ken
Mitsuru Matsushita
Ichiro Kurasawa
Sadao Kumakura
Disciple Maru Ken
Mitsuru Matsushita
Ichiro Kurasawa