Quantity gauging
AssigneeSmiths Group PLC
InventorHarry Atkinson
Life of this patent
Estimating the term…
Abstract
An aircraft fuel quantity gauging system has a number of probes within a tank to measure the height of fuel at different locations. Each probe includes a still well and an ultrasonic transducer mounted at the top and bottom of the still well. The lower transducer transmits pulses of acoustic energy upwardly through the fuel to its surface and measures the time of travel back of the reflected pulse back to the transducer. This is used to derive a first, bottom-up measure of fuel height. Similarly, the upper transducer transmits pulses down through air to the fuel surface to derive a second, top-down measurement. These are compared to check for correct operation of the probes.
Claims7
A quantity-gauging system comprising:
- a still well;
- a first acoustic transducer mounted towards one end of said still well and arranged to determine a height of an interface between two different fluids;
- capacitive electrodes disposed within said still well and arranged to provide an indication of a position of said interface;
- and a processing unit connected to receive outputs of said first acoustic transducer and said capacitive electrodes to provide an indication of quantity of one of said fluids derived from the outputs of both said first acoustic transducer and said capacitive electrodes.
Dependencies are inferred from the claim text.