A control system for controlling a shut-off valve of an aircraft. The shut-off valve is configured to open a bypass circuit that is initially closed. This circuit makes it possible to feed air to an aircraft engine without going via an air filter associated with an air intake. The control system comprises: a manual control member for controlling the shut-off valve, this member being actuatable manually so as to cause the bypass circuit to open; and a computer configured to compute a current value of a level of clogging TC of an air filter. The control system further comprises a comparator for comparing the current value of the level of clogging TC with a first threshold value TC1 and with a second threshold value TC2, and an alerter for generating a first sensory signal and a second sensory signal.
SYSTEME DE COMMANDE D'UN CLAPET D'OBTURATION D'UN AERONEF, AERONEF EQUIPE D'UN TEL SYSTEME DE COMMANDE ET PROCEDE DE COMMANDE ASSOCIE
SYSTEM FOR CONTROLLING A CHECK VALVE OF AN AIRCRAFT, AIRCRAFT PROVIDED WITH SUCH A CONTROL SYSTEM AND ASSOCIATED CONTROL METHOD
SYSTEM ZUM STEUERN EINER VENTILKLAPPE EINES LUFTFAHRZEUGS, MIT DIESEM STEUERUNGSSYSTEMS AUSGESTATTETES LUFTFAHRZEUG UND ENTSPRECHENDES STEUERUNGSVERFAHREN
2022-04-06
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02M Zuführen von Brennstoff-Luft-Gemischen oder deren Bestandteilen bei Brennkraftmaschinen allgemein , SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF |
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