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특허 상세정보

Automated tuning of gas turbine combustion systems

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/48    F02C-009/28    F02C-009/20    F02C-009/16    F02C-009/56    F02C-009/40   
미국특허분류(USC) 701/100; 700/286; 700/287; 700/290; 290/052
출원번호 US-0463060 (2009-05-08)
등록번호 US-8437941 (2013-05-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    DLA Piper LLP (US)
인용정보 피인용 횟수 : 16  인용 특허 : 360
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 method for tuning the operation of a combustion turbine comprising: monitoring a set of operational parameters including stack emissions and combustion dynamics and comparing the operational parameters to standard operational data;using a computer, determining the dominant gas turbine combustion system tuning scenario through the use of Boolean hierarchical logic and multiple levels of control settings; andmaking an adjustment to at least one operational control element of the combustion turbine based on the dominant gas turbine combustion system tu...

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