This is true of aircraft, boats and heavy equipment.
By it's very nature, liquid fuel refuses to stay still.
So to address these issues with fuel level sending technology, we have turned to fuel flow instruments and fuel totalizers.
These instruments measure the fuel flow to the engine and remove that fuel volume from an owner/operator entered starting fuel value. They can give you a knots per gallon indication.
This can be done by several methods - we can count injection pulses and duration or we can get a sensor to measure fuel on the way to the engine, and in injected engines fuel on the way back to the tank. There are several sensor types that will perform this function
Some of our cars do the same thing - only they reset when we fill the tank or in other words when the fuel level reaches full.
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Many owners will swear by the fuel totalizer and it's uncanny accuracy.
I filled the tank and then burned 35 gallons of fuel. When I refilled - I put 35 gallons back into the tank.
Sounds good - and a justification for the expense of having this equipment installed - However an aircraft tank filled in the same manner and in the same location - the fuel totalizer is a self - fuel filling device.
- I will never run out of fuel with this equipment installed.
- I don't need fuel gauges
So what does the FAA say about fuel totalizers
Digital fuel flow computer systems have a fuel flow transducer that directly measures the fuel being fed to the engine.
The fuel flow transducer may be a small paddle wheel, an impeller, or spring-loaded movable vanes.
Digital displays with a fuel computer also allow these instruments to display total fuel consumed, total fuel remaining, and time remaining at the present fuel
flow rate for fuel management. Overall accuracy for fuel remaining and time
remaining readings depends on the transducer processing unit and display.
The largest possible error is the initial fuel supply, which is entered by the pilot at the start of each flight. Errors in the initial fuel supply may be caused
by an uneven ramp, unusual loading, volume changes of the fuel because of
temperature variations, malfunctions in the fuel system such as leaks,
siphoning actions, collapsed bladders, and other factors.
flow rate for fuel management. Overall accuracy for fuel remaining and time
remaining readings depends on the transducer processing unit and display.
The largest possible error is the initial fuel supply, which is entered by the pilot at the start of each flight. Errors in the initial fuel supply may be caused
by an uneven ramp, unusual loading, volume changes of the fuel because of
temperature variations, malfunctions in the fuel system such as leaks,
siphoning actions, collapsed bladders, and other factors.
So, total fuel remaining should be verified with the fuel quantity indicator. According to § 23.1337(b)(1), fuel quantity indicators are required to be calibrated to read "zero" during level flight when the quantity of fuel remaining in the tank is equal to the unusable fuel supply. Therefore, fuel quantity indicators should be used as the primary fuel-remaining instruments.
Fuel quantity indicators that are inaccurate should be periodically calibrated, repaired, or replaced, as necessary, to ensure reliable readings.
Taken from FAA AC 23-17C
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