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특허 상세정보

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Automated tuning of gas turbine combustion systems

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/00    F02C-009/26    F02C-009/28    F02C-009/48    F02C-009/20   
출원번호 US-0855220 (2013-04-02)
등록번호 US-9328670 (2016-05-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    DLA Piper LLP (US)
인용정보 피인용 횟수 : 5  인용 특허 : 371
초록
▼

A system for tuning the operation of a gas turbine is provided based on measuring operational parameters of the turbine and directing adjustment of operational controls for various operational elements of the turbine. A controller is provided for communicating with sensors and controls within the system. The controller receiving operational data from the sensors and comparing the data to stored operational standards to determining if turbine operation conforms to the standards. The controller then communicates selected adjustment in an operational parame...

대표
청구항
▼

1. A controller system for tuning the operation of a gas turbine, the turbine having sensor means for measuring operational parameters of the turbine, the operational parameters including stack emissions and combustion dynamics from the turbine, operational element control means for controlling various operational control elements of the turbine, the operational control elements comprising one or more of fuel distribution splits, fuel-air ratio and inlet fuel temperature, and a communication link for the sensor means and the operational element control m...

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