INTEGRATED HEALTH MANAGEMENT APPROACH TO PROPULSION CONTROL SYSTEM PROTECTION LIMITING
摘要
<p>A real-time gas turbine management system includes a controller system coupled to a gas turbine engine. The controller system is configured to control demand on a first and second component of a gas turbine engine. The controller system is configured to identify a set point reference of the first component, identify a set point reference of the second component, and identify a data set indicative of a level of deterioration of the gas turbine engine. The controller system is also configured to change the set point reference of the first component to extend a lifespan of the gas turbine engine and/or change the set point reference of the second component to extend the lifespan of the gas turbine engine.</p>
申请公布号
EP2972620(A1)
申请公布日期
2016.01.20
申请号
EP20140717562
申请日期
2014.03.11
申请人
ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.;ROLLS-ROYCE CORPORATION
发明人
MYER, JOSEPH, D.;SKERTIC, RICHARD, J.;CALHOUN, KEITH A.