Stall detector and surge prevention feature for a gas turbine engine

作者: Rowland M. Evans

DOI:

关键词:

摘要: A proportional fuel control (11) regulates the flow (Wf) from a hydromechanical unit (36) based upon an error signal (E) representing difference between demanded speed (Nd) and actual (Nh). The is generated by integrator (32) as time integral of least plurality acceleration terms (Aa, Ab, Ac, Ad) selected select low gate (38). term (Aa) junction (26) scheduled (Ngs). Stress (Ac, are junctions (48, 50) scheduling means (42, 44) which form stress limiter circuits. stall (Ab) (46) (40) forms prevention feature.

参考文章(20)
Joseph L Peczkowski, Michael P Fodroci, Charles S Longstreet, Fuel control having proportional plus integral governor with variable proportional and integral gains ,(1965)
Roine Brannstrom, Goran Nilsson, Regulating means for gas turbine plant ,(1976)
D. A. Caine, S. Janik, Digital Control for Helicopter Powerplants Journal of The American Helicopter Society. ,vol. 25, pp. 28- 35 ,(1980) , 10.4050/JAHS.25.28
Fred L. Elsaesser, Joseph H. Hall, Stall detector for gas turbine engine ,(1975)
Paul Manwaring Maker, Michael John Joby, Electronic fuel control for a gas turbine engine ,(1975)
Maurice Edward Lloyd, Roderick Stewart Janes, Fuel control for a multi-engine gas turbine installation ,(1976)
Nobuhito Hobo, Sumihiro Kaga, Fuel control system ,(1975)