Process and device for feeding the turbojet engines of an...

B - Operations – Transporting – 64 – D

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B64D 31/08 (2006.01) B64C 15/02 (2006.01) B64D 37/00 (2006.01) F02C 9/28 (2006.01) F02C 9/42 (2006.01)

Patent

CA 2472276

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.

- Selon l'invention, en vol automatique en palier à altitude stabilisée de l'aéronef (A), la valeur de consigne EPRt, commune à tous les turbo-réacteurs (M1 à M4) et correspondant à une valeur particulière du rapport EPR entre les pressions des gaz à la sortie et à l'entrée des turbo-réacteurs, est convertie en une valeur de consigne N1t liée à la vitesse de rotation N1 de la soufflante desdits turboréacteurs et l'alimentation en carburant de tous lesdits turboréacteurs est asservie à ladite valeur de consigne N1t.

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