Engineering Transactions, 39, 2, pp. 191-206, 1991

An Estimate of the Influence of the Compressor Stability Margin on the Pick-Up Time of a Turbojet Engine

M. Orkisz
Air Force Academy, Dęblin

The relations are derived enabling to estimate the acceleration time of the turbojet engine rotor set. The terms are established allowing for the determination of the effect of individual operational and structural engine parameters upon the time needed for acceleration of the rotor system. Influence of the economic and optimum ranges of operation upon that time is also analyzed.

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Copyright © Polish Academy of Sciences & Institute of Fundamental Technological Research (IPPT PAN).


B.BOLINSKI and Z.STELMASZCZYK, Operation of turbine engines [in Polish], WKL, Warszawa 1981.

G.W. DOBRANSKIJ and T.S.MARTIANOVA, Dynamic1J of turbojet engines [in Russian], Masinostroenie, Moskva 1989.

Z. DŻYGADLO et al., Rotor assemblies of turbojet engines [in Polish], WKL, Warszawa 1982.

R.M. FIEDOROV, The phenomenon of pumping in turboprop engines and pumping prevention [in Russian], Woenno-Wozdusnaja Inżynierskaja Krasnoznamiennaja Akademia imieni Prof.N.E.Żukovskovo, 94, 1969.

T. GAJEWSKI, Turbine power plants in aircraft engineering. Theory and operation [in Polish], DWLot, Poznań 1984.

T. GAJEWSKI, A. LESIKIEWICZ and R. SZYMANIK, Jet engines [in Polish], WNT, Warszawa 1973.

S.A. GAJEVSKIJ et al., Automatics of aviation gas turbine power plants [in Russian], Woennoje lzdatielstwo MO SSSR, Moskwa 1980.

R. KACZMAREK and M. ORKISZ, Operation and stability of axial compressors [in Polish], PWL i WOPK, 3, 1988.

P.K. KAZANDZAN, N.D.TICHONOV and A.K. JANKO, Theory of aircraft engines [in Russian], Maśinostroenie, Moskva 1983.

J. KUHLBERG and W. ZIMERMAN, Flight testing of an all electronic propulsion control system, AIAA Pap., 0147, 1980.

J. LEŚ, Design and operation of aircraft engines [in Polish], Polit. Rzeszowska, Rzeszów 1984.

M. ORKISZ, Unstable operation of an axial compressor [in Polish]; WPT, 10, 1985.

M. ORKISZ, An estimate of the influence of the stability margin of a compressor on the thrust of a turbojet engine [in Polish], Enging. Trans., 39, 2, 1991.

A.J. SOBEY and A.M. SUGGS, Control of aircraft and missile powerplants, John and Sos. Inc., New York and London 1963.

W.A. SOSUNOV and F.A. LITWINOV, Non-stationary regimes of aviation turbojet engines [in Russian], Masinostroenie, Moskva 1975.

S. SZCZECIŃSKI, Double-rotor and bypass turbojet engines[in Polish], WKL, Warszawa 1971.

S. SZCZECIŃSKI, A study of the problem of blade clearance in aircraft turbine engines as a design and operation parameter [in Polish], Dodatek do Biuletynu WAT, 4, 248, 1973.

B.R. WILLIAMS and C.J. WENDEL, F/A-18A/F404 propulsion system integration, AIAA Pap., 1330, 1984.