Engineering Transactions, 39, 3-4, pp. 351-367, 1991

Simulation Analysis of the Influence of Variation in Some Selected Design and Control Parameters on the Acceleration Time of a Turbojet Engine

M. Orkisz
Air Force Academy, Dęblin

The equation governing the acceleration time of a turbojet engine is presented in an implicit form; expansion into power series contains first order partial derivatives. The derivatives represent the "sensitivity measure" of the acceleration time to the variation of a) -the design parameters of the compressor (stability margin, moment of inertial, efficiency, compression ratio), b) -technical conditions (deformation of blade profiles, due to erosion, turbine blade clearance), c) -service conditions due to flight speed and altitude. The relations derived enable the wide range simulation analysis of the problem.

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G.W.DOBRANSKI and T.S.MARTIANOWA, Dynamics of aircraft turbine engines [in Russian], Mashinostroenie, Moskva 1989.

P.DZIERŻANOWSKI et. al., Turbojet engines [in Polish], WKL, Warszawa 1983.

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

T.GAJEWSKI, Aircraft turbine propulsion. Foundations of the theory of operation for a pilot [in Polish], DWLot, Poznań 1984.

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

R.GLOWACKI, Washing operations of a duet [in Polish], WPT, 3, 1990.

P.K.KAZANDŻAN, N.D.TICHONOW and AL.JANKU, Theory of aircraft engines [in Russian], Mashinostroenie, Moskva 1983.

A.LESIKIEWICZ, Exoenergic analysis of jet power plants [in Polish], Supplement for Biuletyn WAT, 4, 212, 1970.

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

Y.N.NECAJEW, W.N.KOBIELKOW and A.S.POLJEW, Turbojet engines with variable working cycle for multi-regime aeroplanes [in Russian], Mashinostroenie, Moskva 1988.

M.ORKISZ, Estimation of influence compressor stability reserve on acceleration time of engine rotor groops, Biuletyn WAT, [to be published].

M.ORKISZ, By-pass duet compressor regulation effect on for its stability reserve, Engineering Reports, 3, 1990.

W.A.SOSUNOW and F.A.LITWINOW, Non-steady operation regimes of aircraft tur­bine engines [in Russian], Mashinostroenie, Moskva 1975.

E.WĘGRZYN, Some problems of erosion wear of elements of turbojet engines [in Polish], TLiA, 7, 1989.

B.R.WILIAMS, F/A-18A/F404 propulsion system integration, AIAA Pap., 1330, 1984.

Theory of jet engines, [Ed.] B.S.STECHKIN [in Polish], MON, Warszawa 1961.

M.ORKISZ, Sensitivity of the acceleration time of a turbojet engine on its design and operation parameters [in Polish], WOSL, 1990.