Aircraft brake and tire condition diagnosis and prognosis
A method of diagnosis and prognosis for various operative systems is provided so that maintenance can be efficiently and effectively scheduled and provided. The invention is applicable to a broad range of systems, but particularly to aircraft brake systems and tires. An aircraft brake may be modeled by attributing brake wear factor values to various parameters associated with the aircraft brake that impact wear. Over the course of time and during braking events, the brake wear factor values are summed and a running total of that sum is kept over the life of the brake. At a point in time when the sum of weighted factors exceeds a preset threshold, an indicia is generated that service is required.
1. A method of diagnosis and prognosis for aircraft brakes, comprising:
establishing a model of an aircraft brake by attributing brake wear factor values to various parameters, derived from both brake performance data and environmental condition data, associated with the aircraft brakes and periodically adjusting said model by comparing estimated wear derived from the summing of magnitudes of said brake wear factor values with actual wear derived by monitoring positions of wear pins;
summing magnitudes of said brake wear factor values over a course of time during which actual in-use braking events occur;
keeping a running total sum of said brake wear factor values;
providing a first indicia of service necessity when said running total sum exceeds a first threshold; and
wherein said brake performance data is taken from a group comprising the parameters of brake pressure, brake temperature, wheel speed, aircraft lateral acceleration, pilot brake pedal position/angle, park status, and thrust reverser status, said environmental condition data is taken from the group comprising the parameters of airport identification codes, date, and time, and weather conditions and the presence or absence of external factors at an airport, including use of oxidizing agents, are derived from said airport identification code, date, and time, and wherein said brake wear factor values are derived from said parameters of said groups being weighted as to their individual impacts on brake wear.
2. The method of diagnosis and prognosis for aircraft brakes as recited in claim 1 , wherein said oxidizing agents include de-icing fluid causing catalytic weight loss in carbon disc heat sinks.
3. The method of diagnosis and prognosis for aircraft brakes as recited in claim 1 , which further includes the step of extrapolating said running total sum of said brake wear factor values to project when brake thickness will be small enough to require brake service.
4. The method of diagnosis and prognosis for aircraft brakes as recited in claim 3 , wherein said first threshold is indicative of a time at which a new or replacement heat stack for the aircraft brake should be ordered or requested.
5. The method of diagnosis and prognosis for aircraft brakes as recited in claim 4 , wherein a second indicia of service necessity is provided when said running total exceeds a second threshold, said second indicia correlating with a need for immediate heat stack replacement.
6. The method of diagnosis and prognosis for aircraft brakes as recited in claim 1 , wherein said parameters of said groups are further weighted as a function of parameters taken from the group of ambient temperature, aircraft mass, and aircraft speed.
7. The method of diagnosis and prognosis for aircraft brakes as recited in claim 6 , wherein at least certain of said parameters are taken from a flight data recorder.