发明名称 Stall detector and surge prevention feature for a gas turbine engine
摘要 A proportional fuel fuel control (11) regulates the fuel flow (Wf) from a hydromechanical unit (36) based upon an error signal (E) representing the difference between a demanded speed signal (Nd) and an actual speed signal (Nh). The demanded speed signal (Nd) is generated by an integrator (32) as the time integral of the least of a plurality of acceleration terms (Aa, Ab, Ac, Ad) selected by a select low gate (38). The demanded acceleration term (Aa) is generated by junction (26) as the difference between the demanded signal (Nd) and a scheduled speed signal (Ngs). Stress acceleration terms (Ac, Ad) are generated by junctions (48, 50) and scheduling means (42, 44) which form stress limiter circuits. A stall acceleration term (Ab) is generated by a junction (46) and a scheduling means (40) which forms a stall prevention feature.
申请公布号 US4449360(A) 申请公布日期 1984.05.22
申请号 US19810259317 申请日期 1981.04.30
申请人 AVIATION ELECTRIC LTD. 发明人 EVANS, ROWLAND M.
分类号 F02C9/28;(IPC1-7):F02C9/28 主分类号 F02C9/28
代理机构 代理人
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