Integrated fire and flight control system with automatic...

Details Integrated fire and flight control system with automatic... Integrated fire and flight control system with automatic...

G - Physics

05

D

G05D 1/08 (2006.01) B64C 27/04 (2006.01)

Patent

CA 2321586

An integrated fire and flight control (IFFC) system (10) senses the actual engine torque (126) of a rotary wing aircraft in successive real time intervals and compares the sensed interval values with one or more reference maximum torque limits (144) for each of one or more prescribed maximum time intervals and, in the presence of an above limit actual torque for an above limit prescribed time interval, the IFFC automatically reduces the collective axis command (54).

L'invention concerne un système (10) intégré de commande de tir et de vol (IFFC: integrated fire and flight control) qui détecte le couple (126) effectif du moteur d'un aéronef à voilure tournante pendant des intervalles de temps réels successifs et compare les valeurs détectées pour ces intervalles avec une ou plusieurs limites (144) de référence de couple maximal pour chaque intervalle de temps maximum prescrit. En présence d'un couple effectif dépassant la valeur limite supérieure pendant un intervalle de temps supérieur à l'intervalle prescrit, le système IFFC réduit automatiquement la commande (54) d'axe collectif.

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