Systems and methods for detecting landing gear ground loads
There is provided a system for predicting loading of a landing gear including, a plurality sensors positioned proximate to the landing gear. The plurality of sensors measure strain applied to the landing gear, and each sensor yielding strain data. The system further includes a processor that receives the strain data from the plurality of sensors and predicts at least one ground load based on strain data. There is further provided a method for predicting loading of a landing gear. The method includes powering a plurality of sensors located proximate to a landing gear structure, interrogating the plurality of sensors via data acquisition circuitry to yield strain data, instructing the data acquisition circuitry as to a sampling rate and data resolution to be used for the interrogating, and, finally, processing the strain data to predict a ground load.
1. A method for predicting a ground load applied to a landing gear structure of an aircraft, comprising:
interrogating a plurality of sensors via a data acquisition circuitry to yield a strain data experienced by the landing gear structure,
wherein the plurality of sensors comprises at least five sensors and the plurality of sensors is configured to measure at least five loads, comprising a drag load, a side load, a vertical load, a moment drag load and a moment side load, whereby the strain data may be determined;
receiving via a processor the strain data from the plurality of sensors and predicting via the processor at least one ground load applied to the landing gear based on the strain data and a weight and a balance of the aircraft based only on the strain data;
instructing the data acquisition circuitry via the processor as to a sampling rate and a data resolution comprising a bit resolution to be used during the interrogating the plurality of sensors and to increase the sampling rate and the data resolution in response to a detected increasing strain experienced by the landing gear structure; and
processing the strain data to predict the ground load applied to the landing gear structure.
2. The method of claim 1 , further comprising powering the plurality of sensors.
3. The method of claim 1 further comprising storing the strain data in non-volatile memory of a data concentrator unit, the data concentrator unit being in communication with the data acquisition circuitry.
4. The method of claim 1 , wherein the plurality of sensors is located proximate to the landing gear structure at least at one location selected from a group of locations consisting of: an axle, a piston, a torque linkage, an attachment pin, a trailing arm, and a shock strut.
5. The method of claim 1 , wherein the plurality of sensors is located proximate to the landing gear structure at a piston and a torque linkage.
6. The method of claim 1 , wherein the landing gear structure comprises a piston and a bogie beam that connects to the piston at a piston base, the bogie beam comprising at least two axles and a pivot point, wherein the plurality of sensors is located proximate to the landing gear structure on either side of the pivot point and wherein at least one of the plurality of sensors is positioned on the piston base.
7. The method of claim 1 , wherein the strain data is associated with a sensor location, the method further comprising:
processing the ground load to predict an occurrence of an overload condition based on a model that relates a magnitude of the ground load to a design limit of the landing gear structure at the sensor location.
8. The method of claim 7 , wherein the model comprises information that is generated from a finite element analysis or a static load testing of the landing gear structure.
9. The method of claim 7 , further comprising: generating an alarm following prediction of the occurrence of the overload condition.