METHOD OF DETERMINING THRUST IN FLIGHT OF BYPASS TURBOJET ENGINE WITH MIXING OF FLOWS Russian patent published in 2016 - IPC F02C9/00 

FIELD: engines.

SUBSTANCE: invention relates to control of turbojet bypass engine with mixing of flows TCTRE_cm and TCTRE_cm with afterburner TURBOFANS_cm and enables to determine thrust in flight with high accuracy with account of real gas flow from jet nozzle.

EFFECT: as per measurements of flight information parameters are measured gas at jet nozzle exit, at which the output impulse of the nozzle and actual engine thrust is determined as function of R =ƒ(P_h, t^* _{vinyl chloride}, V_n, n_in, p^* _in, p^* _t, F_c, F_CD).

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