FIELD: engines and pumps.
SUBSTANCE: proposed method consists in determining the parametre that defines current weight to be derived from said parametre, calculating reduced thrust proportional to aforesaid current weight and generating instruction to be sent to aircraft healthy engines. The latter generate reduced thrust complying with calculated one. The invention covers also the device to this end.
EFFECT: improved flight performances with no reduction in payload.
7 cl, 2 dwg
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