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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1992, Vol. 13 ›› Issue (1): 101-105.

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STUDY ON TWO VARIABLE CONTROL PLAN FOR TWIN SPOOL TURBOJET ENGINE

Zhang Jia-zhen, Hua Kai, Huang Xian   

  1. Faculty 709 of Northwestern Polytechnical University, Xi' an, 710072
  • Received:1990-05-10 Revised:1991-06-25 Online:1992-01-25 Published:1992-01-25

Abstract:

The two-variable control plan for twin spool turbojet engine under maximum state is discussed in this paper. The performances of the engine adopting two-variable control plan are calculated with the nonlinear simulation programs. The result of the calculation shows that engine performances with two-variable control plan are higher than those with single variable plan. There are various combination schemes of two performance parameters, while every scheme is only suitable for a use of engine. When the control plan including equal low pressure rotating lspeed and equal turbine temperature is adopted, surge margin of high pressure compressor will be reduced. A complex control plan designed in this paper may be a good way out of difficulty. At the end of the paper, some problems met in practice for two-variable control system of engine are analyzed.

Key words: control plan, two variables, performance of turbojet engine