发明名称 Gas turbine fuel control system
摘要 An electronic fuel control system for varying the fuel flow to a gas turbine engine during the engine's acceleration. The reference speed set point of the engine's fuel controlling governor is increased as a function of the elapsed time from engine start-up and the engine characteristics so that the engine accelerates substantially along its "required to run line.
申请公布号 US4337615(A) 申请公布日期 1982.07.06
申请号 US19790022532 申请日期 1979.03.21
申请人 THE GARRETT CORPORATION 发明人 LACROIX, STEPHEN R.
分类号 F02C9/28;(IPC1-7):F02C9/32 主分类号 F02C9/28
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