发明名称 Gas turbine engine fuel control system
摘要 A fuel control system having a combustive energy value evaluator determining a combustive energy value of the fuel, and a controller calculating a desired flow rate based at least on the combustive energy value and controlling a fuel metering device such that the fuel flow rate corresponds to the desired fuel flow rate.
申请公布号 US9127596(B2) 申请公布日期 2015.09.08
申请号 US201113091301 申请日期 2011.04.21
申请人 PRATT & WHITNEY CANADA CORP. 发明人 Dooley Kevin A.;Brand Joseph
分类号 F02C9/28;F02C3/20;F02C9/40 主分类号 F02C9/28
代理机构 Norton Rose Fulbright Canada LLP 代理人 Norton Rose Fulbright Canada LLP
主权项 1. A system for monitoring a flow of a liquid fuel mixture of different types of fuel in a gas turbine engine, the system comprising: a sensor sensing a proportion of each of the different types of fuel in the liquid fuel mixture; a unit determining a combustive energy value of the liquid fuel mixture in the engine from the proportions; a controller determining at least one equivalent characteristic of a reference fuel corresponding to the combustive energy value of the liquid fuel mixture; and a display unit displaying the at least one equivalent characteristic.
地址 Longueuil CA