Resumen
System for measuring the fuel level in ultralights and paramotors, which aims to inform the pilot of the maximum remaining flight time, which basically comprises an optical emitter element (1), a serpentine configuration fiber optic transducer (2) located inside the fuel tank (3), a receiver (4) that converts the optical signal back to the electronic domain and an interface (5) to inform the user, wherein at least one serpentine section of the transducer (2) of the optical fiber is located at half the height of the fuel tank (3) and/or at the bottom of the fuel tank (3) and where the curved areas of the optical fiber of the transducer (2) is capable of being eliminated. External coating to achieve greater sensitivity of the measurements (3 '', 3 '' '', 3 '' '' ''). (Machine-translation by Google Translate, not legally binding)