| 摘要 |
According to the invention, during level automatic flight of the aircraft (A) at steady altitude, the preset value EPRt, common to all the turbojets (M1 to M4) and corresponding to a particular value of the ratio EPR of the gas pressures at the outlet and at the inlet of the turbojets, is converted into a preset value N1t related to the speed of rotation N1 of the fan of said turbojets and the fuel supply to all said turbojets is slaved to said preset value N1t.
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