Abstract: Systems, methods and computer readable media are provided for measuring fluid level in a tank. A system may include: a transmitter gauge installed on or in the tank, the transmitter gauge comprising a probe arranged to be at least partially immersed in the fluid and adapted to conduct energy pulses generated by an energy source within the transmitter gauge; a refractometer module operatively coupled to the transmitter gauge, the refractometer module comprising a processor configured to measure travel times of the energy pulses conducted along the probe and to determine the fluid level in the tank based on the measured travel times: if the fluid level in the tank is below a threshold level, according to a first mode of operation, by determining the fluid level in the tank based on the measured travel time of an energy pulse reflected from a terminal end of the probe, a length of the probe, a speed of the reflected energy pulse in air, and a speed of the reflected energy pulse in the liquid.

Abstract: A system and method is provided for measuring and metering deicing fluid as it is dispensed from a tank onto an aircraft to remove ice and to prevent subsequent icing. The system can include a guided wave radar gauge mounted on the tank to measure the volume of fluid in the tank in real-time. As fluid is dispensed from the tank, the gauge measures the change in the volume of fluid in the tank and transmits the volume of fluid in the tank and the volume of fluid dispensed from the tank to a display/controller. The system can also include a refractometer module to enable the measurement of the concentration of a first constituent fluid relative to a second constituent fluid in a mixture thereof. The system can further measure the concentration of one deicing fluid constituent (e.g. glycol) mixed with another fluid constituent (e.g. water) to determine the freeze point of the deicing fluid.