Method and device for providing an multi-engine aircraft...

Details Method and device for providing an multi-engine aircraft... Method and device for providing an multi-engine aircraft...

B - Operations, Transporting

64

D

B64D 31/00 (2006.01) F02C 9/28 (2006.01)

Patent

CA 2620186

The invention concerns a device (1) comprising means (6A, 6B, 6n) which determine for each of the engines of the aircraft, an individual minimum flexible temperature and means (8) which determine a global minimum flexible temperature based on said individual minimum temperatures, enabling a maximum available thrust to be calculated.

Le dispositif (1) comporte des moyens (6A, 6B, 6n) qui determinent, pour chacun des moteurs de l'aeronef, line temperature flexible minimale individuelle et des moyens (8) qui determinent une temperature flexible minimale globale a partir desdites temperatures minimales individuelles, permettant de calculer une poussee maximale disponible.

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