The Boeing Company

Theboeing Company

Scott C Farner

Brandon M Courter

Nam V Ngo

Joseph M Dray

Terrance L Thomas

James Schimert

Sabyasachi Basu

Joseph Edward Dale Sharp

Randall Wade Dickson

Art Wineland

Systems and methods for aircraft flight control rigging are described. An example system includes a first set of laser rangefinders to measure, for each laser rangefinder of the first set, a distance from the laser rangefinder to a respective target location on a fixed surface of an aircraft, and a second set of laser rangefinders to measure, for each laser rangefinder of the second set, a distance to a respective target location on a control surface of the aircraft. The example system also includes a processor to (i) receive signals indicative of the distance measured by each rangefinder and (ii) generate a first plot line graphic of the measured distances of each of the rangefinders of the first set to its respective target location and a second plot line graphic of the measured distances of each of the laser rangefinders of the second set to its respective target location.

Optical systems and methods for aircraft flight control rigging

A system for testing continuity of a cable assembly includes an optical time domain reflectometry (OTDR) device selectively coupled to an input connector of a cable and a design database storing cable data. The cable data indicates at least a length of the cable. The system includes a processor and memory in communication with the processor. The processor is configured to execute instructions stored on the memory which cause the processor to receive the cable data from the design database, receive OTDR data associated with the cable from the OTDR device, and calculate a distance-to-fault based on the OTDR data. In response to the distance-to-fault being less than the length of the cable, the processor determines that a connectivity failure has occurred with the cable and generates fault data indicating the connectivity failure.

System and method for optical time-domain reflectometry and design data wire testing

A method for wire connectivity testing includes receiving wiring data indicating at least a length of a wire segment of a vehicle from a design database. The method further includes receiving spread-spectrum time-domain reflectometry (SSTDR) data associated with the wire segment from an SSTDR device coupled to an endpoint of the wire segment. The method also includes calculating a distance-to-fault based on the SSTDR data. The method includes comparing the distance-to-fault to the length of the wire segment. The method further includes, in response to the distance-to-fault being less than the length of the wire segment, generating fault data indicating a failure within the wire segment. The method also includes sending the fault data to a user output device.

System and method for spread-spectrum time-domain reflectometry and design data wire testing

There is provided an automated data driven method for predicting one or more operational states, such as wear or degradation, of a mechanical system over time. The method has the steps of collecting data on the mechanical system from a data recording device, preprocessing the collected data, selecting a training data set that represents a base condition for statistical comparison, fitting a statistical model to the training data set to relate a predicted response to nuisance variables at the base condition, and using an output model to predict what an observed response would have been at the base condition and calculating the difference between the observed response and the predicted response to predict the one or more operational states of the mechanical system.

Data driven method and system for predicting operational states of mechanical systems

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Daniel Island, SC, United States of America

Scott C Farner