Fluid-gauging system and methods
AssigneeSmiths Group PLC
InventorHarry Atkinson
Life of this patent
Estimating the term…
Abstract
An aircraft ultrasonic fuel-gauging system has a number of gauging probes in a tank arranged so as to include at least one set of three colinear probes. The outputs of the probes are supplied to a unit, which checks the operation of the probes in colinear sets by extrapolating height at one of the probes from the outputs of the other probes. Where there are two sets of colinear probes having a common probe it is possible uniquely to identify if the common probe is faulty. The system rejects any faulty probe and uses only the outputs of other probes in computations of fuel quantity.
Claims12
A fluid-gauging system comprising:
- a set of at least three substantially colinear probes arranged to provide respective outputs indicative of the height of fluid at three different locations;
- and a unit connected to receive the outputs of said probes, said unit being arranged to extrapolate the height of fluid at a first of said locations from the outputs of probes at the other two locations, and wherein said unit is arranged to compare the extrapolated height with the output of the probe at the first location to determine if said probes are performing correctly.
A fluid-gauging system comprising:
- a number of probes arranged to provide respective outputs indicative of the height of fluid at different locations, said probes being arranged to include a first set of three substantially colinear probes and a second set of three non-colinear probes;
- and a unit connected to receive the outputs of said probes, said unit being arranged to extrapolate the height of fluid at a first of said locations corresponding to one of said probes in said colinear set from the outputs of other probes of said colinear set, wherein said unit is arranged to compare the extrapolated height with the output of the probe at the first location to determine if said probes are performing, correctly, and wherein said unit is arranged to compute fluid quantity excluding outputs from probes identified as not performing correctly.
An aircraft fuel-gauging system comprising:
- a set of at least three substantially colinear acoustic probes arranged to provide respective outputs indicative of the height of fuel at three different locations in a fuel tank;
- and a unit connected to receive the outputs of said probes, said unit being arranged to extrapolate the height of fuel at a first of said locations from the outputs of probes at the other two locations, and wherein said unit is arranged to compare the extrapolated height with the output of the probe at the first location to determine if said probes are performing correctly.
A method of fluid-gauging, comprising the steps of:
- receiving outputs from a set of at least three substantially colinear probes;
- extrapolating the height of fluid at one of the probes from outputs of the other probes;
- comparing the extrapolated output of the one probe with its actual output;
- and determining whether the probes in the set are functioning correctly.
A method of fluid-gauging comprising the steps of:
- receiving outputs from a plurality of fluid-gauging probes;
- identifying those outputs from a set of probes arranged substantially colinearly of one another;
- extrapolating the height of fluid at one of the probes of said set from Outputs of other probes of said set;
- comparing the extrapolated output of said one probe with its actual output to determine whether all probes in said set are functioning correctly;
- and providing an output indicative of fluid quantity derived only from those probes functioning correctly.
Dependencies are inferred from the claim text.