Method for determining, predicting and correcting breakout friction errors influencing aircraft telescopic landing gear strut pressures
View Patent ↗Aircraft landing gear strut breakout friction values are used to correct measured strut pressure as related to the amount of weight supported; with the ability to generate and refine the breakout friction value database, and ability to predict a future breakout friction correction value by trending historical measurements, as compared to recent measurements, as further compared to real-time breakout friction values. The system is used in monitoring, measuring, computing and displaying the weight and center of gravity for aircraft utilizing telescopic oleo landing gear struts. Pressure sensors, temperature sensors, humidity sensors, axle deflection sensors, accelerometers, inclinometers are mounted in relation to each of the landing gear struts to monitor, measure and record strut pressure as related to strut telescopic movement, rates of strut telescopic movement, axle deflection, current temperature, current relative humidity, vertical acceleration; experienced by landing gear struts, as the aircraft proceeds through typical ground and flight operations.
1. A method of determining aircraft weight, the aircraft having landing gear struts, each landing gear strut comprising a piston telescoping in a cylinder, the strut comprising fluid and a seal, the piston experiencing breakout friction with the cylinder, comprising the steps of:
a. taxiing the aircraft so as to cause taxi induced telescopic movement of the piston within the cylinder over time;
b. measuring a pressure over time of the fluid during such taxi induced telescopic movement, the measured pressure having high pressure values and low pressure values;
c. identifying an asymmetry of the high and low pressure values about a mean of the measured pressures;
d. applying a correction factor to the measured pressures to determine weight of the aircraft, with the correction factor including the identified asymmetry.