PROCESS AND DEVICE FOR FEEDING THE TURBOJET ENGINES OF AN AIRCRAFT IN AUTOMATIC FLIGHT

摘要

according to the invention, the automatic landing flight altitude of the aircraft (a) is stabilized, the set value eprt.common to all turbo engines (m1 to m4) and corresponding to a particular value of the ratio between the pressure p of the gas at the exit and entry of turbo engines.the set value is converted into a rotational speed n1t related to n1 of the turbo blower, and the fuel jet is enslaved to all ladite set value n1t.